ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 10763.91
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 71.3
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.07
ET - UTC (sec) : 65.18
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
------------------------------------------------------------------------
There are no maneuvers.
Coasting Arc #1 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2008/184/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4296743.47 A = 6717958.24 meter
Y = 618998.18 meter E = .0005093
Z = 5128217.00 I = 51.33111
XDOT = -2540.661787 Wp = 331.63404
YDOT = 7158.913367 meter/sec RA = 297.22551 deg
ZDOT = 1269.550509 TA = 106.20574
MA = 106.14968
Ha = 189.038 n.mi
Hp = 183.694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14096927.40 X = 4264590.64
Y = 2030833.93 feet Y = 666865.83 meter
Z = 16824858.92 Z = 5149012.47
XDOT = -8335.504551 XDOT = -2626.692259
YDOT = 23487.248580 feet/sec YDOT = 7130.020908 meter/sec
ZDOT = 4165.191958 ZDOT = 1257.000811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3218205.95 X = 980909.17
Y = -13776334.36 feet Y = -4199026.71 meter
Z = 16905007.79 Z = 5152646.37
XDOT = 21683.738796 XDOT = 6609.203585
YDOT = 10098.138754 feet/sec YDOT = 3077.912692 meter/sec
ZDOT = 4117.422809 ZDOT = 1254.990472
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 08184.50805226 .00020000 00000-0 20000-3 0 9008
2 25544 51.6406 297.5896 0008984 320.0195 40.0306 15.74933236 30941
Satellite: ISS
Catalog Number: 25544
Epoch time: 08184.50805226 = yrday.fracday
Element set: 900
Inclination: 51.6406 deg
RA of node: 297.5896 deg
Eccentricity: .0008984
Arg of perigee: 320.0195 deg
Mean anomaly: 40.0306 deg
Mean motion: 15.74933236 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3094
Checksum: 291
Coasting Arc #2 (Orbit 3108)
---------------------------------------
Vector Time (GMT): 2008/185/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1903837.27 A = 6729298.03 meter
Y = -6394627.81 meter E = .0015478
Z = -794701.11 I = 51.35741
XDOT = 4847.230589 Wp = 5.09913
YDOT = 706.529659 meter/sec RA = 292.04405 deg
ZDOT = 5951.229895 TA = 346.19121
MA = 346.23349
Ha = 189.327 n.mi
Hp = 183.447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6246185.28 X = 1979061.97
Y = -20979750.03 feet Y = -6372917.23 meter
Z = -2607287.12 Z = -785271.12
XDOT = 15902.987496 XDOT = 4810.060241
YDOT = 2318.010691 feet/sec YDOT = 760.525004 meter/sec
ZDOT = 19525.032464 ZDOT = 5974.687272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20504083.58 X = -6249644.67
Y = -7676766.61 feet Y = -2339878.46 meter
Z = -2571478.04 Z = -783786.51
XDOT = 2829.563917 XDOT = 862.451082
YDOT = -14101.336923 feet/sec YDOT = -4298.087494 meter/sec
ZDOT = 19615.450940 ZDOT = 5978.789447
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 08185.45984221 .00020000 00000-0 20000-3 0 9017
2 25544 51.6411 292.6958 0008993 324.6787 35.3779 15.74918788 31092
Satellite: ISS
Catalog Number: 25544
Epoch time: 08185.45984221 = yrday.fracday
Element set: 901
Inclination: 51.6411 deg
RA of node: 292.6958 deg
Eccentricity: .0008993
Arg of perigee: 324.6787 deg
Mean anomaly: 35.3779 deg
Mean motion: 15.74918788 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3109
Checksum: 341
Coasting Arc #3 (Orbit 3124)
---------------------------------------
Vector Time (GMT): 2008/186/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4180069.51 A = 6717443.55 meter
Y = -645514.05 meter E = .0013436
Z = -5228060.04 I = 51.30796
XDOT = 1822.297118 Wp = 49.01843
YDOT = -7457.153590 meter/sec RA = 286.89286 deg
ZDOT = -528.462088 TA = 215.88837
MA = 215.97869
Ha = 189.413 n.mi
Hp = 183.016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13714138.80 X = -4147144.11
Y = -2117828.23 feet Y = -692072.85 meter
Z = -17152427.95 Z = -5248286.59
XDOT = 5978.665086 XDOT = 1908.115878
YDOT = -24465.727001 feet/sec YDOT = -7436.295678 meter/sec
ZDOT = -1733.799501 ZDOT = -519.402558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2809685.26 X = -856392.07
Y = 13490272.38 feet Y = 4111835.02 meter
Z = -17230403.47 Z = -5251826.98
XDOT = -23144.707514 XDOT = -7054.506850
YDOT = -7023.713063 feet/sec YDOT = -2140.827742 meter/sec
ZDOT = -1699.512979 ZDOT = -518.011556
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 08186.47506800 .00020000 00000-0 20000-3 0 9024
2 25544 51.6409 287.4760 0009063 328.6572 31.4051 15.74964571 31256
Satellite: ISS
Catalog Number: 25544
Epoch time: 08186.47506800 = yrday.fracday
Element set: 902
Inclination: 51.6409 deg
RA of node: 287.4760 deg
Eccentricity: .0009063
Arg of perigee: 328.6572 deg
Mean anomaly: 31.4051 deg
Mean motion: 15.74964571 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3125
Checksum: 292
Coasting Arc #4 (Orbit 3140)
---------------------------------------
Vector Time (GMT): 2008/187/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1279954.12 A = 6729379.68 meter
Y = 6605120.12 meter E = .0004850
Z = 110769.41 I = 51.34080
XDOT = -4740.461868 Wp = 97.12446
YDOT = -814.083777 meter/sec RA = 281.72163 deg
ZDOT = -6008.871655 TA = 81.66759
MA = 81.61260
Ha = 189.596 n.mi
Hp = 182.896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4199324.53 X = -1354256.57
Y = 21670341.61 feet Y = 6590391.48 meter
Z = 363416.70 Z = 104372.14
XDOT = -15552.696418 XDOT = -4701.816913
YDOT = -2670.878532 feet/sec YDOT = -866.877261 meter/sec
ZDOT = -19714.145851 ZDOT = -6031.806630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21515853.67 X = 6558032.20
Y = 4931835.55 feet Y = 1503223.47 meter
Z = 339326.97 Z = 103426.86
XDOT = -2832.012711 XDOT = -863.197474
YDOT = 13771.797197 feet/sec YDOT = 4197.643786 meter/sec
ZDOT = -19802.576399 ZDOT = -6035.825287
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 08187.49027787 .00020000 00000-0 20000-3 0 9030
2 25544 51.6406 282.2548 0009041 332.4843 27.5841 15.74980686 31416
Satellite: ISS
Catalog Number: 25544
Epoch time: 08187.49027787 = yrday.fracday
Element set: 903
Inclination: 51.6406 deg
RA of node: 282.2548 deg
Eccentricity: .0009041
Arg of perigee: 332.4843 deg
Mean anomaly: 27.5841 deg
Mean motion: 15.74980686 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3141
Checksum: 308
Coasting Arc #5 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2008/188/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4133205.36 A = 6717169.11 meter
Y = 790166.90 meter E = .0009098
Z = 5237151.50 I = 51.29578
XDOT = -1096.984477 Wp = 351.99157
YDOT = 7618.511957 meter/sec RA = 276.55394 deg
ZDOT = -274.875731 TA = 100.68085
MA = 100.57839
Ha = 189.620 n.mi
Hp = 182.551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13560385.02 X = 4098621.73
Y = 2592411.10 feet Y = 836192.68 meter
Z = 17182255.56 Z = 5257146.35
XDOT = -3599.030436 XDOT = -1180.759083
YDOT = 24995.117969 feet/sec YDOT = 7605.776478 meter/sec
ZDOT = -901.823264 ZDOT = -280.407204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2815939.59 X = 858298.39
Y = -13417133.49 feet Y = -4089542.29 meter
Z = 17259361.42 Z = 5260653.36
XDOT = 23953.521342 XDOT = 7301.033305
YDOT = 3803.513124 feet/sec YDOT = 1159.310800 meter/sec
ZDOT = -922.479126 ZDOT = -281.171638
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 08188.50547049 .00020000 00000-0 20000-3 0 9042
2 25544 51.6410 277.0335 0009202 336.5783 23.4961 15.75037886 31575
Satellite: ISS
Catalog Number: 25544
Epoch time: 08188.50547049 = yrday.fracday
Element set: 904
Inclination: 51.6410 deg
RA of node: 277.0335 deg
Eccentricity: .0009202
Arg of perigee: 336.5783 deg
Mean anomaly: 23.4961 deg
Mean motion: 15.75037886 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3157
Checksum: 299
Coasting Arc #6 (Orbit 3172)
---------------------------------------
Vector Time (GMT): 2008/189/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 633126.73 A = 6729144.25 meter
Y = -6661346.55 meter E = .0018590
Z = 588173.30 I = 51.33370
XDOT = 4763.901312 Wp = 23.24254
YDOT = 985.119908 meter/sec RA = 271.39604 deg
ZDOT = 5981.721189 TA = 343.19645
MA = 343.25795
Ha = 189.888 n.mi
Hp = 182.332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2077187.42 X = 704710.71
Y = -21854811.51 feet Y = -6653866.39 meter
Z = 1929702.43 Z = 591422.05
XDOT = 15629.597481 XDOT = 4723.473793
YDOT = 3232.020697 feet/sec YDOT = 1038.165818 meter/sec
ZDOT = 19625.069519 ZDOT = 6004.765807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21855990.58 X = -6661705.93
Y = -2053526.46 feet Y = -625914.86 meter
Z = 1941635.93 Z = 591810.63
XDOT = 3073.417627 XDOT = 936.777693
YDOT = -13925.422849 feet/sec YDOT = -4244.468885 meter/sec
ZDOT = 19713.946529 ZDOT = 6008.810902
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 08189.52064976 .00020000 00000-0 20000-3 0 9059
2 25544 51.6408 271.8125 0009263 341.3523 18.7300 15.75018188 31730
Satellite: ISS
Catalog Number: 25544
Epoch time: 08189.52064976 = yrday.fracday
Element set: 905
Inclination: 51.6408 deg
RA of node: 271.8125 deg
Eccentricity: .0009263
Arg of perigee: 341.3523 deg
Mean anomaly: 18.7300 deg
Mean motion: 15.75018188 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3173
Checksum: 291
Coasting Arc #7 (Orbit 3187)
---------------------------------------
Vector Time (GMT): 2008/190/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206948.92 A = 6717459.20 meter
Y = -937518.29 meter E = .0013710
Z = -5161483.42 I = 51.29491
XDOT = 370.872287 Wp = 59.86023
YDOT = -7608.667100 meter/sec RA = 266.21485 deg
ZDOT = 1088.674623 TA = 220.53374
MA = 220.63592
Ha = 189.942 n.mi
Hp = 181.923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13802325.85 X = -4171079.48
Y = -3075847.41 feet Y = -984361.67 meter
Z = -16934000.73 Z = -5181833.55
XDOT = 1216.772594 XDOT = 450.637517
YDOT = -24962.818570 feet/sec YDOT = -7604.073926 meter/sec
ZDOT = 3571.767135 ZDOT = 1090.669192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2831784.69 X = -863127.97
Y = 13757958.97 feet Y = 4193425.89 meter
Z = -17012494.74 Z = -5185408.40
XDOT = -23976.878915 XDOT = -7308.152693
YDOT = -545.881754 feet/sec YDOT = -166.384759 meter/sec
ZDOT = 3578.776595 ZDOT = 1090.811106
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 08190.47236412 .00020000 00000-0 20000-3 0 9062
2 25544 51.6403 266.9183 0009314 344.8507 15.2377 15.75063507 31888
Satellite: ISS
Catalog Number: 25544
Epoch time: 08190.47236412 = yrday.fracday
Element set: 906
Inclination: 51.6403 deg
RA of node: 266.9183 deg
Eccentricity: .0009314
Arg of perigee: 344.8507 deg
Mean anomaly: 15.2377 deg
Mean motion: 15.75063507 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3188
Checksum: 292
Coasting Arc #8 (Orbit 3203)
---------------------------------------
Vector Time (GMT): 2008/191/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -39132.53 A = 6728360.43 meter
Y = 6597802.45 meter E = .0004100
Z = -1328263.51 I = 51.33416
XDOT = -4896.889216 Wp = 60.21464
YDOT = -1197.088981 meter/sec RA = 261.06982 deg
ZDOT = -5813.376030 TA = 134.42628
MA = 134.39272
Ha = 190.131 n.mi
Hp = 181.814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -128387.55 X = -106454.87
Y = 21646333.50 feet Y = 6596988.58 meter
Z = -4357819.91 Z = -1328616.39
XDOT = -16065.909502 XDOT = -4854.899088
YDOT = -3927.457286 feet/sec YDOT = -1251.613365 meter/sec
ZDOT = -19072.756004 ZDOT = -5837.063107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21636689.27 X = 6594862.89
Y = -653618.27 feet Y = -199222.85 meter
Z = -4358588.35 Z = -1328497.73
XDOT = -3414.734107 XDOT = -1040.810956
YDOT = 14506.604823 feet/sec YDOT = 4421.613150 meter/sec
ZDOT = -19164.134017 ZDOT = -5841.228048
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 08191.48751229 .00020000 00000-0 20000-3 0 9073
2 25544 51.6395 261.6966 0009283 348.8255 11.2701 15.75070106 32047
Satellite: ISS
Catalog Number: 25544
Epoch time: 08191.48751229 = yrday.fracday
Element set: 907
Inclination: 51.6395 deg
RA of node: 261.6966 deg
Eccentricity: .0009283
Arg of perigee: 348.8255 deg
Mean anomaly: 11.2701 deg
Mean motion: 15.75070106 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3204
Checksum: 292
Coasting Arc #9 (Orbit 3219)
---------------------------------------
Vector Time (GMT): 2008/192/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4384738.36 A = 6718122.65 meter
Y = 1141912.33 meter E = .0013108
Z = 4960879.18 I = 51.30679
XDOT = 271.542891 Wp = 15.42298
YDOT = 7448.625796 meter/sec RA = 255.87369 deg
ZDOT = -1940.908395 TA = 93.48815
MA = 93.33822
Ha = 190.119 n.mi
Hp = 181.486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14385624.53 X = 4347544.46
Y = 3746431.52 feet Y = 1190736.41 meter
Z = 16275850.34 Z = 4982089.97
XDOT = 890.888750 XDOT = 197.659543
YDOT = 24437.748675 feet/sec YDOT = 7451.249481 meter/sec
ZDOT = -6367.809695 ZDOT = -1939.767788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2995918.76 X = 913156.04
Y = -14468442.98 feet Y = -4409981.42 meter
Z = 16357685.50 Z = 4985822.54
XDOT = 23301.031188 XDOT = 7102.154306
YDOT = -2419.098030 feet/sec YDOT = -737.341079 meter/sec
ZDOT = -6362.743241 ZDOT = -1939.364140
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 08192.50264325 .00020000 00000-0 20000-3 0 9084
2 25544 51.6402 256.4742 0009464 352.2290 7.8726 15.75134894 32200
Satellite: ISS
Catalog Number: 25544
Epoch time: 08192.50264325 = yrday.fracday
Element set: 908
Inclination: 51.6402 deg
RA of node: 256.4742 deg
Eccentricity: .0009464
Arg of perigee: 352.2290 deg
Mean anomaly: 7.8726 deg
Mean motion: 15.75134894 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3220
Checksum: 286
Coasting Arc #10 (Orbit 3235)
---------------------------------------
Vector Time (GMT): 2008/193/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -492756.48 A = 6727181.63 meter
Y = -6376083.85 meter E = .0019240
Z = 2047545.23 I = 51.34508
XDOT = 5179.852230 Wp = 41.21770
YDOT = 1384.493227 meter/sec RA = 250.74239 deg
ZDOT = 5542.702372 TA = 341.76602
MA = 341.83491
Ha = 190.343 n.mi
Hp = 181.294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1616655.13 X = -431368.07
Y = -20918910.27 feet Y = -6381251.18 meter
Z = 6717668.08 Z = 2045299.65
XDOT = 16994.265848 XDOT = 5137.060227
YDOT = 4542.300615 feet/sec YDOT = 1442.177276 meter/sec
ZDOT = 18184.719067 ZDOT = 5567.762310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20753800.06 X = -6325758.26
Y = 3101304.05 feet Y = 945277.47 meter
Z = 6708438.08 Z = 2044731.93
XDOT = 3586.617402 XDOT = 1093.200984
YDOT = -15651.070970 feet/sec YDOT = -4770.446432 meter/sec
ZDOT = 18281.413589 ZDOT = 5572.174862
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 08193.51776163 .00020000 00000-0 20000-3 0 9095
2 25544 51.6398 251.2529 0009478 357.0195 3.0910 15.75119966 32365
Satellite: ISS
Catalog Number: 25544
Epoch time: 08193.51776163 = yrday.fracday
Element set: 909
Inclination: 51.6398 deg
RA of node: 251.2529 deg
Eccentricity: .0009478
Arg of perigee: 357.0195 deg
Mean anomaly: 3.0910 deg
Mean motion: 15.75119966 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3236
Checksum: 312
Coasting Arc #11 (Orbit 3250)
---------------------------------------
Vector Time (GMT): 2008/194/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4674626.63 A = 6719296.00 meter
Y = -1254980.51 meter E = .0012218
Z = -4667240.18 I = 51.32899
XDOT = -824.243734 Wp = 61.04445
YDOT = -7138.918776 meter/sec RA = 245.53705 deg
ZDOT = 2756.407612 TA = 236.20005
MA = 236.31646
Ha = 190.407 n.mi
Hp = 180.883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15336701.55 X = -4637573.23
Y = -4117390.13 feet Y = -1307046.96 meter
Z = -15312467.79 Z = -4689859.69
XDOT = -2704.211726 XDOT = -757.744064
YDOT = -23421.649528 feet/sec YDOT = -7147.764553 meter/sec
ZDOT = 9043.332060 ZDOT = 2752.563854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2783313.04 X = -848353.81
Y = 15547982.83 feet Y = 4739025.17 meter
Z = -15399752.73 Z = -4693844.63
XDOT = -21961.757033 XDOT = -6693.943544
YDOT = 4973.929759 feet/sec YDOT = 1516.053791 meter/sec
ZDOT = 9027.871801 ZDOT = 2751.695325
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 08194.46942025 .00020000 00000-0 20000-3 0 9104
2 25544 51.6389 246.3579 0009589 1.0272 359.0910 15.75157109 32512
Satellite: ISS
Catalog Number: 25544
Epoch time: 08194.46942025 = yrday.fracday
Element set: 910
Inclination: 51.6389 deg
RA of node: 246.3579 deg
Eccentricity: .0009589
Arg of perigee: 1.0272 deg
Mean anomaly: 359.0910 deg
Mean motion: 15.75157109 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3251
Checksum: 298
Coasting Arc #12 (Orbit 3266)
---------------------------------------
Vector Time (GMT): 2008/195/11:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 661904.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 896068.95 A = 6725524.78 meter
Y = 6067913.11 meter E = .0008685
Z = -2772845.94 I = 51.36306
XDOT = -5551.132667 Wp = 34.80092
YDOT = -1512.678157 meter/sec RA = 240.41610 deg
ZDOT = -5104.983292 TA = 177.02626
MA = 177.02109
Ha = 190.605 n.mi
Hp = 180.758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2939858.76 X = 841619.94
Y = 19907851.40 feet Y = 6077629.50 meter
Z = -9097263.59 Z = -2768624.06
XDOT = -18212.377518 XDOT = -5509.006065
YDOT = -4962.854845 feet/sec YDOT = -1574.517686 meter/sec
ZDOT = -16748.632849 ZDOT = -5131.848570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19490713.21 X = 5940769.39
Y = -5038176.65 feet Y = -1535636.24 meter
Z = -9080440.32 Z = -2767718.21
XDOT = -3426.693800 XDOT = -1044.456270
YDOT = 17111.861662 feet/sec YDOT = 5215.695435 meter/sec
ZDOT = -16852.312868 ZDOT = -5136.584962
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 08195.48450864 .00020000 00000-0 20000-3 0 9113
2 25544 51.6386 241.1356 0009622 5.2119 354.9144 15.75167384 32675
Satellite: ISS
Catalog Number: 25544
Epoch time: 08195.48450864 = yrday.fracday
Element set: 911
Inclination: 51.6386 deg
RA of node: 241.1356 deg
Eccentricity: .0009622
Arg of perigee: 5.2119 deg
Mean anomaly: 354.9144 deg
Mean motion: 15.75167384 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 3267
Checksum: 300
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