ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 15607.67
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 72.7
Monthly MSFC 50% earth geomagnetic index (Kp) : 1.25
ET - UTC (sec) : 66.18
UT1 - UTC (sec) : 0.00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
326/18:30:00.000 0.0 0.0 0.0
N/A 0.0 0.0 187.1
000/00:00:00.000 0.0 0.0 179.1
328/09:45:33.979 -0.5 0.6 0.6
N/A 0.0 -0.0 187.4
000/00:00:07.958 -0.3 -0.0 179.2
328/10:20:30.409 0.8 1.9 1.9
N/A -1.1 0.2 188.5
000/00:27:00.819 1.3 -0.0 179.6
328/10:45:32.231 0.3 0.3 0.3
N/A 0.2 0.0 188.5
000/00:00:04.462 -0.1 -0.0 179.6
Coasting Arc #1 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2009/324/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4724883.78 A = 6724995.08 meter
Y = -4757783.05 meter E = .0017468
Z = 355127.31 I = 51.43765
XDOT = 3644.325720 Wp = 32.67631
YDOT = -3161.015287 meter/sec RA = 222.77891 deg
ZDOT = 6014.998762 TA = 331.20202
MA = 331.29833
Ha = 187.226 n.mi
Hp = 179.658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15501587.19 X = -4673055.42
Y = -15609524.43 feet Y = -4810329.73 meter
Z = 1165115.86 Z = 332298.83
XDOT = 11956.449214 XDOT = 3650.181618
YDOT = -10370.785061 feet/sec YDOT = -3120.230177 meter/sec
ZDOT = 19734.247907 ZDOT = 6032.717091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21379471.16 X = 6516462.81
Y = -5203549.85 feet Y = -1586041.99 meter
Z = 1074818.69 Z = 327604.74
XDOT = 2374.900456 XDOT = 723.869659
YDOT = 13938.198198 feet/sec YDOT = 4248.362811 meter/sec
ZDOT = 19804.048166 ZDOT = 6036.273881
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09324.56276393 .00016717 00000-0 10270-3 0 9006
2 25544 51.6464 223.4136 0006217 357.5893 2.5240 15.76513791 30590
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324.56276393 = yrday.fracday
Element set: 900
Inclination: 51.6464 deg
RA of node: 223.4136 deg
Eccentricity: .0006217
Arg of perigee: 357.5893 deg
Mean anomaly: 2.5240 deg
Mean motion: 15.76513791 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 310
Coasting Arc #2 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2009/325/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3714272.62 A = 6713381.04 meter
Y = 2288371.19 meter E = .0014425
Z = -5113929.81 I = 51.42226
XDOT = -5257.376426 Wp = 75.69642
YDOT = -5445.617016 meter/sec RA = 217.59428 deg
ZDOT = 1388.435655 TA = 207.60851
MA = 207.68519
Ha = 187.207 n.mi
Hp = 179.311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12185933.78 X = -3714742.63
Y = 7507779.50 feet Y = 2246833.87 meter
Z = -16777984.94 Z = -5131974.92
XDOT = -17248.610322 XDOT = -5202.836707
YDOT = -17866.197558 feet/sec YDOT = -5504.103284 meter/sec
ZDOT = 4555.235090 ZDOT = 1363.026917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -420923.19 X = -128297.39
Y = -14223029.44 feet Y = -4335179.37 meter
Z = -16849117.81 Z = -5135611.11
XDOT = 23088.350088 XDOT = 7037.329107
YDOT = -5934.293710 feet/sec YDOT = -1808.772723 meter/sec
ZDOT = 4454.709574 ZDOT = 1357.795478
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09325.51356871 .00016717 00000-0 10270-3 0 9013
2 25544 51.6466 218.5131 0006184 .6471 359.4701 15.76572533 30745
Satellite: ISS
Catalog Number: 25544
Epoch time: 09325.51356871 = yrday.fracday
Element set: 901
Inclination: 51.6466 deg
RA of node: 218.5131 deg
Eccentricity: .0006184
Arg of perigee: .6471 deg
Mean anomaly: 359.4701 deg
Mean motion: 15.76572533 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 302
Coasting Arc #3 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/326/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4344756.01 A = 6723060.20 meter
Y = 4703038.31 meter E = .0004725
Z = -2056242.08 I = 51.47939
XDOT = -4904.788868 Wp = 78.69699
YDOT = 2111.243698 meter/sec RA = 212.45603 deg
ZDOT = -5544.611073 TA = 124.30826
MA = 124.26352
Ha = 187.276 n.mi
Hp = 179.384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14254448.84 X = 4301831.87
Y = 15429915.72 feet Y = 4751384.10 meter
Z = -6746201.04 Z = -2035238.86
XDOT = -16091.826995 XDOT = -4901.097574
YDOT = 6926.652552 feet/sec YDOT = 2056.416552 meter/sec
ZDOT = -18190.981211 ZDOT = -5568.429696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20439068.92 X = -6229828.21
Y = 4962924.34 feet Y = 1512699.34 meter
Z = -6663083.58 Z = -2030907.88
XDOT = 2103.132951 XDOT = 641.034923
YDOT = -15843.544480 feet/sec YDOT = -4829.112357 meter/sec
ZDOT = -18284.919774 ZDOT = -5573.243547
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09326.52773759 .00016717 00000-0 10270-3 0 9024
2 25544 51.6465 213.2853 0006061 3.3113 356.8091 15.76573281 30906
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326.52773759 = yrday.fracday
Element set: 902
Inclination: 51.6465 deg
RA of node: 213.2853 deg
Eccentricity: .0006061
Arg of perigee: 3.3113 deg
Mean anomaly: 356.8091 deg
Mean motion: 15.76573281 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 304
Coasting Arc #4 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2009/326/18:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4821365.76 A = 6715830.17 meter
Y = 1286487.11 meter E = .0010375
Z = -4502309.82 I = 51.45938
XDOT = -4371.334401 Wp = 78.62917
YDOT = -5519.880291 meter/sec RA = 211.00977 deg
ZDOT = 3111.914860 TA = 222.45004
MA = 222.53033
Ha = 187.139 n.mi
Hp = 179.126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15818129.12 X = -4813521.47
Y = 4220758.23 feet Y = 1232615.97 meter
Z = -14771357.67 Z = -4525713.15
XDOT = -14341.648298 XDOT = -4324.402551
YDOT = -18109.843476 feet/sec YDOT = -5568.500965 meter/sec
ZDOT = 10209.694421 ZDOT = 3090.792220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16186953.15 X = -4933783.32
Y = -1809459.88 feet Y = -551523.37 meter
Z = -14863694.66 Z = -4530454.13
XDOT = -6933.963158 XDOT = -2113.471971
YDOT = -20934.839105 feet/sec YDOT = -6380.938959 meter/sec
ZDOT = 10126.066642 ZDOT = 3086.425112
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09326.78127601 .00016717 00000-0 10270-3 0 9032
2 25544 51.6435 211.9733 0005666 6.8395 353.2846 15.76603458 30948
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326.78127601 = yrday.fracday
Element set: 903
Inclination: 51.6435 deg
RA of node: 211.9733 deg
Eccentricity: .0005666
Arg of perigee: 6.8395 deg
Mean anomaly: 353.2846 deg
Mean motion: 15.76603458 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 324
Coasting Arc #5 (Orbit 3109)
---------------------------------------
Vector Time (GMT): 2009/327/18:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3373075.87 A = 6719519.77 meter
Y = 4686177.44 meter E = .0008350
Z = -3448064.64 I = 51.49851
XDOT = -6115.832176 Wp = 46.31009
YDOT = 1054.929038 meter/sec RA = 205.89167 deg
ZDOT = -4550.273089 TA = 174.62094
MA = 174.61197
Ha = 187.218 n.mi
Hp = 179.091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11066521.87 X = 3337173.80
Y = 15374597.92 feet Y = 4723696.65 meter
Z = -11312548.04 Z = -3431764.94
XDOT = -20065.066194 XDOT = -6105.069350
YDOT = 3461.053273 feet/sec YDOT = 986.598661 meter/sec
ZDOT = -14928.717485 ZDOT = -4579.957967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5071909.68 X = 1545918.07
Y = 18291485.54 feet Y = 5575244.79 meter
Z = -11247986.47 Z = -3428386.28
XDOT = -18596.281662 XDOT = -5668.146651
YDOT = -4093.351471 feet/sec YDOT = -1247.653528 meter/sec
ZDOT = -15045.873601 ZDOT = -4585.982274
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09327.79541388 .00016717 00000-0 10270-3 0 9047
2 25544 51.6435 206.7450 0005717 10.3740 349.7541 15.76651705 31106
Satellite: ISS
Catalog Number: 25544
Epoch time: 09327.79541388 = yrday.fracday
Element set: 904
Inclination: 51.6435 deg
RA of node: 206.7450 deg
Eccentricity: .0005717
Arg of perigee: 10.3740 deg
Mean anomaly: 349.7541 deg
Mean motion: 15.76651705 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3110
Checksum: 307
Coasting Arc #6 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2009/328/09:45:37.958
Vector Time (MET): N/A
Weight (LBS) : 731746.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2507445.42 A = 6717338.76 meter
Y = 4639319.97 meter E = .0011950
Z = -4173604.89 I = 51.51024
XDOT = -6753.840519 Wp = 44.68305
YDOT = 347.554696 meter/sec RA = 202.61189 deg
ZDOT = -3669.273869 TA = 187.77013
MA = 187.78866
Ha = 187.350 n.mi
Hp = 179.239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8226526.96 X = 2475656.26
Y = 15220866.05 feet Y = 4667182.19 meter
Z = -13692929.42 Z = -4161500.51
XDOT = -22158.269420 XDOT = -6739.400064
YDOT = 1140.271313 feet/sec YDOT = 272.110208 meter/sec
ZDOT = -12038.300095 ZDOT = -3702.049374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14664213.36 X = -4469652.23
Y = -9253300.86 feet Y = -2820406.10 meter
Z = -13644929.26 Z = -4158974.44
XDOT = 18065.228256 XDOT = 5506.281572
YDOT = -10676.720243 feet/sec YDOT = -3254.264330 meter/sec
ZDOT = -12167.697134 ZDOT = -3708.714087
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09328.42923894 .00016717 00000-0 10270-3 0 9055
2 25544 51.6459 203.4825 0005895 8.4948 351.6316 15.76572109 31200
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328.42923894 = yrday.fracday
Element set: 905
Inclination: 51.6459 deg
RA of node: 203.4825 deg
Eccentricity: .0005895
Arg of perigee: 8.4948 deg
Mean anomaly: 351.6316 deg
Mean motion: 15.76572109 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 329
Coasting Arc #7 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2009/328/10:34:00.819
Vector Time (MET): N/A
Weight (LBS) : 731742.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1366322.84 A = 6716544.39 meter
Y = -4600206.27 meter E = .0008931
Z = 4690709.39 I = 51.50381
XDOT = 7189.211731 Wp = 65.51459
YDOT = 632.721729 meter/sec RA = 202.43394 deg
ZDOT = 2714.221772 TA = 357.75422
MA = 357.75823
Ha = 188.549 n.mi
Hp = 179.578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4482686.49 X = -1337567.91
Y = -15092540.27 feet Y = -4615324.78 meter
Z = 15389466.50 Z = 4684141.30
XDOT = 23586.652660 XDOT = 7168.416827
YDOT = 2075.858692 feet/sec YDOT = 712.999319 meter/sec
ZDOT = 8904.927074 ZDOT = 2749.096959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13389263.50 X = 4081047.52
Y = 8331309.32 feet Y = 2539383.08 meter
Z = 15363327.67 Z = 4682742.27
XDOT = -18454.537916 XDOT = -5624.943157
YDOT = 12980.897115 feet/sec YDOT = 3956.577441 meter/sec
ZDOT = 9042.658694 ZDOT = 2756.202370
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09328.49264297 .00016717 00000-0 10270-3 0 9068
2 25544 51.6455 203.1555 0007492 9.0784 351.0515 15.76126549 31212
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328.49264297 = yrday.fracday
Element set: 906
Inclination: 51.6455 deg
RA of node: 203.1555 deg
Eccentricity: .0007492
Arg of perigee: 9.0784 deg
Mean anomaly: 351.0515 deg
Mean motion: 15.76126549 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 314
Coasting Arc #8 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2009/328/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3520996.94 A = 6715328.07 meter
Y = -2825807.58 meter E = .0012209
Z = 4969145.86 I = 51.49989
XDOT = 6152.133256 Wp = 29.68336
YDOT = 4209.731938 meter/sec RA = 202.35575 deg
ZDOT = -1952.790783 TA = 79.27827
MA = 79.14084
Ha = 188.511 n.mi
Hp = 179.564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11551827.24 X = 3528194.39
Y = -9271022.24 feet Y = -2786393.74 meter
Z = 16302971.98 Z = 4986268.42
XDOT = 20184.164227 XDOT = 6114.088487
YDOT = 13811.456488 feet/sec YDOT = 4278.316108 meter/sec
ZDOT = -6406.793906 ZDOT = -1922.995498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1762477.48 X = -537203.14
Y = 14631656.49 feet Y = 4459728.90 meter
Z = 16370453.96 Z = 4989714.37
XDOT = -23062.244242 XDOT = -7029.372045
YDOT = 4303.978140 feet/sec YDOT = 1311.852537 meter/sec
ZDOT = -6288.960565 ZDOT = -1916.875180
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09328.49264394 .00016717 00000-0 10270-3 0 9077
2 25544 51.6455 203.1557 0007504 9.8343 350.2966 15.76103453 31217
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328.49264394 = yrday.fracday
Element set: 907
Inclination: 51.6455 deg
RA of node: 203.1557 deg
Eccentricity: .0007504
Arg of perigee: 9.8343 deg
Mean anomaly: 350.2966 deg
Mean motion: 15.76103453 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 308
Coasting Arc #9 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2009/329/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5186232.41 A = 6723923.76 meter
Y = -3558027.67 meter E = .0019052
Z = 2345434.95 I = 51.55711
XDOT = 4562.769195 Wp = 53.43160
YDOT = -3075.995233 meter/sec RA = 197.23307 deg
ZDOT = 5403.901894 TA = 333.06336
MA = 333.16213
Ha = 188.798 n.mi
Hp = 179.430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17015198.20 X = -5157454.35
Y = -11673319.12 feet Y = -3615862.37 meter
Z = 7694996.55 Z = 2320309.58
XDOT = 14969.715206 XDOT = 4570.574795
YDOT = -10091.847877 feet/sec YDOT = -3024.928244 meter/sec
ZDOT = 17729.336922 ZDOT = 5426.087010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20308200.33 X = 6189939.46
Y = -3857441.59 feet Y = -1175748.20 meter
Z = 7595621.42 Z = 2315145.41
XDOT = -3615.166477 XDOT = -1101.902742
YDOT = 16174.525515 feet/sec YDOT = 4929.995377 meter/sec
ZDOT = 17816.802730 ZDOT = 5430.561472
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09329.50713650 .00016717 00000-0 10270-3 0 9085
2 25544 51.6458 197.9299 0007577 14.2980 345.8397 15.76082797 31372
Satellite: ISS
Catalog Number: 25544
Epoch time: 09329.50713650 = yrday.fracday
Element set: 908
Inclination: 51.6458 deg
RA of node: 197.9299 deg
Eccentricity: .0007577
Arg of perigee: 14.2980 deg
Mean anomaly: 345.8397 deg
Mean motion: 15.76082797 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 361
Coasting Arc #10 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2009/330/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4425327.77 A = 6717759.23 meter
Y = 2585901.86 meter E = .0011432
Z = -4349514.94 I = 51.56642
XDOT = -5651.827762 Wp = 70.18295
YDOT = -3966.013172 meter/sec RA = 192.03120 deg
ZDOT = 3403.468349 TA = 234.12675
MA = 234.23295
Ha = 188.661 n.mi
Hp = 179.153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14518791.90 X = -4432785.31
Y = 8483929.99 feet Y = 2536373.70 meter
Z = -14270062.13 Z = -4371031.62
XDOT = -18542.742000 XDOT = -5623.592803
YDOT = -13011.854238 feet/sec YDOT = -4029.057501 meter/sec
ZDOT = 11166.234742 ZDOT = 3376.079674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3890131.71 X = 1185712.15
Y = -16285278.70 feet Y = -4963752.95 meter
Z = -14354916.67 Z = -4375378.60
XDOT = 21088.915862 XDOT = 6427.901555
YDOT = -4677.856036 feet/sec YDOT = -1425.810520 meter/sec
ZDOT = 11057.894997 ZDOT = 3370.446395
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09330.45819974 .00016717 00000-0 10270-3 0 9098
2 25544 51.6460 193.0310 0007517 16.5633 343.5776 15.76136865 31529
Satellite: ISS
Catalog Number: 25544
Epoch time: 09330.45819974 = yrday.fracday
Element set: 909
Inclination: 51.6460 deg
RA of node: 193.0310 deg
Eccentricity: .0007517
Arg of perigee: 16.5633 deg
Mean anomaly: 343.5776 deg
Mean motion: 15.76136865 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 321
Coasting Arc #11 (Orbit 3167)
---------------------------------------
Vector Time (GMT): 2009/331/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4588024.97 A = 6720629.56 meter
Y = 3398283.41 meter E = .0010810
Z = -3558945.10 I = 51.60544
XDOT = -5579.198921 Wp = 45.81448
YDOT = 2873.903093 meter/sec RA = 186.92591 deg
ZDOT = -4449.198845 TA = 176.63487
MA = 176.62760
Ha = 188.728 n.mi
Hp = 179.212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15052575.37 X = 4566972.89
Y = 11149223.79 feet Y = 3449471.85 meter
Z = -11676329.06 Z = -3536706.96
XDOT = -18304.458401 XDOT = -5589.306839
YDOT = 9428.815923 feet/sec YDOT = 2811.456856 meter/sec
ZDOT = -14597.109070 ZDOT = -4476.327664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18459527.77 X = -5626464.07
Y = 3489681.18 feet Y = 1063654.83 meter
Z = -11588349.17 Z = -3532128.83
XDOT = 5746.905315 XDOT = 1751.656740
YDOT = -18418.861866 feet/sec YDOT = -5614.069097 meter/sec
ZDOT = -14704.122168 ZDOT = -4481.816437
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09331.47264622 .00016717 00000-0 10270-3 0 9107
2 25544 51.6458 187.8052 0007435 19.4872 340.6575 15.76152102 31680
Satellite: ISS
Catalog Number: 25544
Epoch time: 09331.47264622 = yrday.fracday
Element set: 910
Inclination: 51.6458 deg
RA of node: 187.8052 deg
Eccentricity: .0007435
Arg of perigee: 19.4872 deg
Mean anomaly: 340.6575 deg
Mean motion: 15.76152102 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3168
Checksum: 311
Coasting Arc #12 (Orbit 3183)
---------------------------------------
Vector Time (GMT): 2009/332/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5274583.91 A = 6720888.27 meter
Y = -2484123.72 meter E = .0017118
Z = 3337090.00 I = 51.63730
XDOT = 4777.898227 Wp = 66.38082
YDOT = 3839.994957 meter/sec RA = 181.72097 deg
ZDOT = -4667.882408 TA = 74.30746
MA = 74.11868
Ha = 188.711 n.mi
Hp = 178.779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17305065.32 X = 5285758.38
Y = -8150012.22 feet Y = -2425077.91 meter
Z = 10948457.99 Z = 3362741.63
XDOT = 15675.519119 XDOT = 4757.279961
YDOT = 12598.408652 feet/sec YDOT = 3893.309193 meter/sec
ZDOT = -15314.574831 ZDOT = -4644.720640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5450058.60 X = -1661177.86
Y = 18274531.28 feet Y = 5570077.14 meter
Z = 11049664.47 Z = 3367937.73
XDOT = -18572.921649 XDOT = -5661.026519
YDOT = 3715.684475 feet/sec YDOT = 1132.540628 meter/sec
ZDOT = -15222.922415 ZDOT = -4639.946752
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09332.48706974 .00016717 00000-0 10270-3 0 9111
2 25544 51.6457 182.5791 0007647 23.5390 336.6123 15.76232530 31843
Satellite: ISS
Catalog Number: 25544
Epoch time: 09332.48706974 = yrday.fracday
Element set: 911
Inclination: 51.6457 deg
RA of node: 182.5791 deg
Eccentricity: .0007647
Arg of perigee: 23.5390 deg
Mean anomaly: 336.6123 deg
Mean motion: 15.76232530 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3184
Checksum: 318
Coasting Arc #13 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2009/333/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3686352.20 A = 6717123.50 meter
Y = -3346188.67 meter E = .0012215
Z = 4497504.40 I = 51.65342
XDOT = 6435.430577 Wp = 74.49719
YDOT = -2866.983636 meter/sec RA = 176.61756 deg
ZDOT = 3137.882670 TA = 344.23346
MA = 344.27146
Ha = 188.952 n.mi
Hp = 178.715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12094331.36 X = -3670509.25
Y = -10978309.30 feet Y = -3387323.39 meter
Z = 14755591.85 Z = 4479633.81
XDOT = 21113.617380 XDOT = 6451.767676
YDOT = -9406.114291 feet/sec YDOT = -2794.927741 meter/sec
ZDOT = 10294.890650 ZDOT = 3169.186381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16273495.69 X = 4960161.49
Y = -2012941.00 feet Y = -613544.42 meter
Z = 14684856.95 Z = 4475944.40
XDOT = -6829.681513 XDOT = -2081.686925
YDOT = 20882.302077 feet/sec YDOT = 6364.925673 meter/sec
ZDOT = 10418.418572 ZDOT = 3175.533981
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09333.50147236 .00016717 00000-0 10270-3 0 9126
2 25544 51.6449 177.3525 0007650 27.4713 332.6854 15.76213100 32005
Satellite: ISS
Catalog Number: 25544
Epoch time: 09333.50147236 = yrday.fracday
Element set: 912
Inclination: 51.6449 deg
RA of node: 177.3525 deg
Eccentricity: .0007650
Arg of perigee: 27.4713 deg
Mean anomaly: 332.6854 deg
Mean motion: 15.76213100 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 285
Coasting Arc #14 (Orbit 3214)
---------------------------------------
Vector Time (GMT): 2009/334/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5869829.04 A = 6723824.75 meter
Y = 2534286.01 meter E = .0013944
Z = -2065342.85 I = 51.70565
XDOT = -3631.200141 Wp = 35.06809
YDOT = -3897.788549 meter/sec RA = 171.42534 deg
ZDOT = 5566.955335 TA = 301.87367
MA = 302.00929
Ha = 188.750 n.mi
Hp = 178.563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19257969.29 X = -5887698.25
Y = 8314586.66 feet Y = 2468546.43 meter
Z = -6776059.23 Z = -2093902.47
XDOT = -11913.386290 XDOT = -3614.388569
YDOT = -12788.020173 feet/sec YDOT = -3938.301349 meter/sec
ZDOT = 18264.289157 ZDOT = 5549.354872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5961227.61 X = 1816982.18
Y = -20072997.16 feet Y = -6118249.53 meter
Z = -6888777.96 Z = -2099699.52
XDOT = 16057.306743 XDOT = 4894.267095
YDOT = -1442.628775 feet/sec YDOT = -439.713251 meter/sec
ZDOT = 18194.594759 ZDOT = 5545.712483
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09334.45245187 .00016717 00000-0 10270-3 0 9136
2 25544 51.6438 172.4524 0007572 29.2579 330.9008 15.76259615 32150
Satellite: ISS
Catalog Number: 25544
Epoch time: 09334.45245187 = yrday.fracday
Element set: 913
Inclination: 51.6438 deg
RA of node: 172.4524 deg
Eccentricity: .0007572
Arg of perigee: 29.2579 deg
Mean anomaly: 330.9008 deg
Mean motion: 15.76259615 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3215
Checksum: 320
Coasting Arc #15 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2009/335/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2589555.54 A = 6714327.01 meter
Y = 3524094.47 meter E = .0019874
Z = -5111971.39 I = 51.70203
XDOT = -6953.465677 Wp = 63.03528
YDOT = 2918.278722 meter/sec RA = 166.30815 deg
ZDOT = -1506.233322 TA = 192.48742
MA = 192.53674
Ha = 188.798 n.mi
Hp = 178.454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8495917.13 X = 2574789.75
Y = 11561989.74 feet Y = 3552970.53 meter
Z = -16771559.68 Z = -5099426.38
XDOT = -22813.207603 XDOT = -6978.264368
YDOT = 9574.405257 feet/sec YDOT = 2840.382512 meter/sec
ZDOT = -4941.710374 ZDOT = -1540.074037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14393864.87 X = -4387250.01
Y = -584620.52 feet Y = -178192.33 meter
Z = -16721851.02 Z = -5096820.19
XDOT = 6834.306133 XDOT = 2083.096509
YDOT = -22688.143146 feet/sec YDOT = -6915.346031 meter/sec
ZDOT = -5075.297550 ZDOT = -1546.950693
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09335.46680945 .00016717 00000-0 10270-3 0 9144
2 25544 51.6424 167.2250 0007548 33.1868 326.9769 15.76309410 32317
Satellite: ISS
Catalog Number: 25544
Epoch time: 09335.46680945 = yrday.fracday
Element set: 914
Inclination: 51.6424 deg
RA of node: 167.2250 deg
Eccentricity: .0007548
Arg of perigee: 33.1868 deg
Mean anomaly: 326.9769 deg
Mean motion: 15.76309410 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 325
Coasting Arc #16 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2009/336/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6197229.77 A = 6725375.45 meter
Y = -2552562.31 meter E = .0014992
Z = 523856.58 I = 51.76901
XDOT = 2265.985594 Wp = 99.19107
YDOT = 4236.815415 meter/sec RA = 161.14404 deg
ZDOT = -6019.034709 TA = 75.11591
MA = 74.94993
Ha = 188.822 n.mi
Hp = 178.204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20332118.68 X = 6222767.52
Y = -8374548.26 feet Y = -2483118.53 meter
Z = 1718689.56 Z = 554025.03
XDOT = 7434.335938 XDOT = 2247.680401
YDOT = 13900.313042 feet/sec YDOT = 4262.053586 meter/sec
ZDOT = -19747.489203 ZDOT = -6008.070110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5898838.42 X = -1797965.95
Y = 21173289.45 feet Y = 6453618.62 meter
Z = 1837803.50 Z = 560162.51
XDOT = -14058.951641 XDOT = -4285.168460
YDOT = -2168.404641 feet/sec YDOT = -660.929735 meter/sec
ZDOT = -19703.994535 ZDOT = -6005.777534
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09336.48114501 .00016717 00000-0 10270-3 0 9158
2 25544 51.6427 161.9984 0007584 37.0324 323.1362 15.76344207 32473
Satellite: ISS
Catalog Number: 25544
Epoch time: 09336.48114501 = yrday.fracday
Element set: 915
Inclination: 51.6427 deg
RA of node: 161.9984 deg
Eccentricity: .0007584
Arg of perigee: 37.0324 deg
Mean anomaly: 323.1362 deg
Mean motion: 15.76344207 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 305
Coasting Arc #17 (Orbit 3262)
---------------------------------------
Vector Time (GMT): 2009/337/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1373795.82 A = 6713408.64 meter
Y = -3928150.36 meter E = .0009620
Z = 5262007.58 I = 51.75609
XDOT = 7133.213395 Wp = 49.94380
YDOT = -2912.308951 meter/sec RA = 156.00137 deg
ZDOT = -305.302582 TA = 42.98346
MA = 42.90834
Ha = 188.879 n.mi
Hp = 178.120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4507204.14 X = -1355330.73
Y = -12887632.43 feet Y = -3943410.58 meter
Z = 17263804.39 Z = 5255377.78
XDOT = 23402.931086 XDOT = 7166.732310
YDOT = -9554.819392 feet/sec YDOT = -2832.353688 meter/sec
ZDOT = -1001.648892 ZDOT = -270.567940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13066958.19 X = 3982808.86
Y = 4070601.09 feet Y = 1240719.21 meter
Z = 17237450.83 Z = 5253975.01
XDOT = -6150.680997 XDOT = -1874.727568
YDOT = 23494.581811 feet/sec YDOT = 7161.148536 meter/sec
ZDOT = -864.480332 ZDOT = -263.493605
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09337.49545828 .00016717 00000-0 10270-3 0 9161
2 25544 51.6420 156.7704 0007522 40.9097 319.2631 15.76354098 32632
Satellite: ISS
Catalog Number: 25544
Epoch time: 09337.49545828 = yrday.fracday
Element set: 916
Inclination: 51.6420 deg
RA of node: 156.7704 deg
Eccentricity: .0007522
Arg of perigee: 40.9097 deg
Mean anomaly: 319.2631 deg
Mean motion: 15.76354098 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3263
Checksum: 327
Coasting Arc #18 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2009/338/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6150331.02 A = 6724896.67 meter
Y = 2477758.19 meter E = .0021179
Z = 1055005.64 I = 51.82151
XDOT = -917.235981 Wp = 52.20546
YDOT = -4833.796236 meter/sec RA = 150.87005 deg
ZDOT = 5937.711909 TA = 319.32521
MA = 319.48320
Ha = 188.828 n.mi
Hp = 177.972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20178251.37 X = -6182705.71
Y = 8129127.90 feet Y = 2408800.38 meter
Z = 3461304.58 Z = 1025048.80
XDOT = -3009.304401 XDOT = -891.960042
YDOT = -15858.911537 feet/sec YDOT = -4843.912916 meter/sec
ZDOT = 19480.682116 ZDOT = 5933.316573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5292890.76 X = 1613273.10
Y = -21119539.68 feet Y = -6437235.70 meter
Z = 3342982.07 Z = 1018940.94
XDOT = 13126.322766 XDOT = 4000.903179
YDOT = 6406.821203 feet/sec YDOT = 1952.799103 meter/sec
ZDOT = 19463.124621 ZDOT = 5932.360384
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09338.50974837 .00016717 00000-0 10270-3 0 9171
2 25544 51.6412 151.5423 0007510 44.4532 315.7234 15.76405795 32792
Satellite: ISS
Catalog Number: 25544
Epoch time: 09338.50974837 = yrday.fracday
Element set: 917
Inclination: 51.6412 deg
RA of node: 151.5423 deg
Eccentricity: .0007510
Arg of perigee: 44.4532 deg
Mean anomaly: 315.7234 deg
Mean motion: 15.76405795 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 317
Coasting Arc #19 (Orbit 3293)
---------------------------------------
Vector Time (GMT): 2009/339/10:45:34.462
Vector Time (MET): N/A
Weight (LBS) : 731713.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 246422.62 A = 6714575.43 meter
Y = 4545646.96 meter E = .0018085
Z = -4950711.44 I = 51.81268
XDOT = -6890.966080 Wp = 85.35105
YDOT = 2678.144737 meter/sec RA = 145.70086 deg
ZDOT = 2124.072713 TA = 205.17279
MA = 205.26104
Ha = 188.824 n.mi
Hp = 177.765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 808473.18 X = 219623.85
Y = 14913539.88 feet Y = 4548253.44 meter
Z = -16242491.59 Z = -4949578.78
XDOT = -22608.156429 XDOT = -6930.719810
YDOT = 8786.564099 feet/sec YDOT = 2600.863324 meter/sec
ZDOT = 6968.742497 ZDOT = 2090.500064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12733372.91 X = -3881132.06
Y = -7815338.94 feet Y = -2382115.31 meter
Z = -16237842.38 Z = -4949294.36
XDOT = 5226.099649 XDOT = 1592.915173
YDOT = -22663.197365 feet/sec YDOT = -6907.742557 meter/sec
ZDOT = 6836.114431 ZDOT = 2083.647679
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09339.46062550 .00016717 00000-0 10270-3 0 9188
2 25544 51.6410 146.6409 0007544 48.7561 311.4252 15.76444230 32942
Satellite: ISS
Catalog Number: 25544
Epoch time: 09339.46062550 = yrday.fracday
Element set: 918
Inclination: 51.6410 deg
RA of node: 146.6409 deg
Eccentricity: .0007544
Arg of perigee: 48.7561 deg
Mean anomaly: 311.4252 deg
Mean motion: 15.76444230 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3294
Checksum: 304
|
