Date:
July 3rd 2008
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
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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