Date:
January 31st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9902 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 632)
---------------------------------------
Vector Time (GMT): 2008/028/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1525977
94 A = 6712472
18 meter
Y = -4565772
75 meter E =
0012572
Z = -4689274
74 I = 51
74355
XDOT = 7166
688300 Wp = 43
29085
YDOT = 454
508405 meter/sec RA = 21
33709 deg
ZDOT = -2770
099510 TA = 199
40594
MA = 199
45385
Ha = 185
072 n
mi
Hp = 178
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5006489
30 X = -1452030
04
Y = -14979569
38 feet Y = -4582423
55 meter
Z = -15384759
65 Z = -4696508
30
XDOT = 23512
756891 XDOT = 7174
529717
YDOT = 1491
169309 feet/sec YDOT = 534
694287 meter/sec
ZDOT = -9088
252984 ZDOT = -2735
265203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9027095
69 X = 2751458
77
Y = -12926646
64 feet Y = -3940041
90 meter
Z = -15412871
68 Z = -4697843
29
XDOT = 12010
324255 XDOT = 3660
746833
YDOT = 19082
531522 feet/sec YDOT = 5816
355608 meter/sec
ZDOT = -8954
979085 ZDOT = -2729
477625
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 08028
52197361
00020000 00000-0 20000-3 0 9001
2 25544 51
6382 21
7147 0005757 341
0535 19
0421 15
77551467 6331
Satellite: ISS
Catalog Number: 25544
Epoch time: 08028
52197361 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 21
7147 deg
Eccentricity:
0005757
Arg of perigee: 341
0535 deg
Mean anomaly: 19
0421 deg
Mean motion: 15
77551467 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 633
Checksum: 274
Coasting Arc #2 (Orbit 648)
---------------------------------------
Vector Time (GMT): 2008/029/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6541307
52 A = 6721221
49 meter
Y = -842808
75 meter E =
0010480
Z = 1280679
15 I = 51
74598
XDOT = -516
610683 Wp = 98
01660
YDOT = -4965
743359 meter/sec RA = 16
14839 deg
ZDOT = -5867
377994 TA = 67
93504
MA = 67
82378
Ha = 185
140 n
mi
Hp = 178
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21460982
68 X = -6537618
17
Y = -2765120
59 feet Y = -915936
79 meter
Z = 4201703
25 Z = 1248910
82
XDOT = -1694
916940 XDOT = -432
542285
YDOT = -16291
808922 feet/sec YDOT = -4971
050150 meter/sec
ZDOT = -19249
927801 ZDOT = -5869
683621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11008337
86 X = -3355341
38
Y = -18655913
24 feet Y = -5686322
36 meter
Z = 4080119
90 Z = 1243620
55
XDOT = 10525
407290 XDOT = 3208
144142
YDOT = -10451
812848 feet/sec YDOT = -3185
712556 meter/sec
ZDOT = -19259
227868 ZDOT = -5870
212654
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 08029
53549788
00020000 00000-0 20000-3 0 9018
2 25544 51
6383 16
4818 0005937 345
0426 15
0563 15
77620249 6496
Satellite: ISS
Catalog Number: 25544
Epoch time: 08029
53549788 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 16
4818 deg
Eccentricity:
0005937
Arg of perigee: 345
0426 deg
Mean anomaly: 15
0563 deg
Mean motion: 15
77620249 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 649
Checksum: 306
Coasting Arc #3 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2008/030/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -700040
84 A = 6709773
10 meter
Y = 4101393
41 meter E =
0005773
Z = 5262962
68 I = 51
67875
XDOT = -7579
429432 Wp = 11
13521
YDOT = -1401
584552 meter/sec RA = 11
00337 deg
ZDOT = 89
635150 TA = 78
04791
MA = 77
98319
Ha = 185
239 n
mi
Hp = 178
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2296721
91 X = -771417
43
Y = 13456015
12 feet Y = 4093165
81 meter
Z = 17266937
92 Z = 5259388
75
XDOT = -24866
894463 XDOT = -7563
628807
YDOT = -4598
374515 feet/sec YDOT = -1486
253703 meter/sec
ZDOT = 294
078577 ZDOT = 52
853031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11979907
49 X = -3651475
80
Y = 6578700
52 feet Y = 2005187
92 meter
Z = 17253664
41 Z = 5258916
91
XDOT = -11543
598430 XDOT = -3518
488801
YDOT = -21375
234684 feet/sec YDOT = -6515
171532 meter/sec
ZDOT = 153
266407 ZDOT = 46
715601
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 08030
54899823
00020000 00000-0 20000-3 0 9020
2 25544 51
6380 11
2489 0005876 348
2774 11
8253 15
77628918 6652
Satellite: ISS
Catalog Number: 25544
Epoch time: 08030
54899823 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 11
2489 deg
Eccentricity:
0005876
Arg of perigee: 348
2774 deg
Mean anomaly: 11
8253 deg
Mean motion: 15
77628918 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 665
Checksum: 314
Coasting Arc #4 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2008/031/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6427315
63 A = 6721025
15 meter
Y = 1560757
44 meter E =
0017026
Z = 1135388
94 I = 51
68882
XDOT = -2136
316721 Wp = 39
68336
YDOT = 4473
533714 meter/sec RA = 5
85431 deg
ZDOT = 5908
475305 TA = 332
76852
MA = 332
85770
Ha = 185
087 n
mi
Hp = 178
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21086993
55 X = 6403869
87
Y = 5120595
29 feet Y = 1632500
18 meter
Z = 3725029
34 Z = 1166555
60
XDOT = -7008
913128 XDOT = -2214
883628
YDOT = 14676
947882 feet/sec YDOT = 4449
204531 meter/sec
ZDOT = 19384
761498 ZDOT = 5897
906663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9566761
94 X = 2915949
04
Y = 19453931
28 feet Y = 5929558
25 meter
Z = 3844380
35 Z = 1171767
13
XDOT = -14410
766053 XDOT = -4392
401493
YDOT = 3241
623928 feet/sec YDOT = 988
046973 meter/sec
ZDOT = 19344
768716 ZDOT = 5896
285505
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 08031
56247038
00020000 00000-0 20000-3 0 9039
2 25544 51
6381 6
0162 0005663 352
1067 8
0008 15
77720304 6812
Satellite: ISS
Catalog Number: 25544
Epoch time: 08031
56247038 = yrday
fracday
Element set: 903
Inclination: 51
6381 deg
RA of node: 6
0162 deg
Eccentricity:
0005663
Arg of perigee: 352
1067 deg
Mean anomaly: 8
0008 deg
Mean motion: 15
77720304 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 681
Checksum: 253
Coasting Arc #5 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2008/032/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2987353
45 A = 6711970
59 meter
Y = -3713815
67 meter E =
0010505
Z = -4733675
65 I = 51
62897
XDOT = 6894
034686 Wp = 77
27851
YDOT = 2177
412343 meter/sec RA =
65980 deg
ZDOT = 2649
616663 TA = 218
71811
MA = 218
79346
Ha = 185
339 n
mi
Hp = 178
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9801028
39 X = 3051654
89
Y = -12184434
61 feet Y = -3680049
49 meter
Z = -15530431
92 Z = -4719007
40
XDOT = 22618
224036 XDOT = 6856
302981
YDOT = 7143
741282 feet/sec YDOT = 2254
294187 meter/sec
ZDOT = 8692
968055 ZDOT = 2683
015912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15684823
04 X = 4780734
06
Y = -485177
82 feet Y = -147882
20 meter
Z = -15474684
12 Z = -4716683
72
XDOT = 9316
703200 XDOT = 2839
731135
YDOT = 20602
847177 feet/sec YDOT = 6279
747820 meter/sec
ZDOT = 8820
919162 ZDOT = 2688
616161
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 08032
51258042
00020000 00000-0 20000-3 0 9043
2 25544 51
6383 1
1098 0005907 355
7559 4
3555 15
77695463 6963
Satellite: ISS
Catalog Number: 25544
Epoch time: 08032
51258042 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 1
1098 deg
Eccentricity:
0005907
Arg of perigee: 355
7559 deg
Mean anomaly: 4
3555 deg
Mean motion: 15
77695463 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 696
Checksum: 298
Coasting Arc #6 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2008/033/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5354982
60 A = 6716421
63 meter
Y = -2263068
14 meter E =
0007777
Z = -3373897
18 I = 51
61638
XDOT = 4628
929763 Wp = 38
60067
YDOT = -4043
309332 meter/sec RA = 355
54097 deg
ZDOT = -4634
610327 TA = 181
21662
MA = 181
21852
Ha = 185
320 n
mi
Hp = 177
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17568840
54 X = -5312889
14
Y = -7424764
23 feet Y = -2322714
96 meter
Z = -11069216
48 Z = -3399809
17
XDOT = 15186
777439 XDOT = 4696
312331
YDOT = -13265
450564 feet/sec YDOT = -3991
168861 meter/sec
ZDOT = -15205
414459 ZDOT = -4611
960061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6139526
86 X = -1871327
79
Y = -17996908
39 feet Y = -5485457
68 meter
Z = -11168542
14 Z = -3404171
64
XDOT = 18757
318142 XDOT = 5717
230570
YDOT = 2984
245038 feet/sec YDOT = 909
597888 meter/sec
ZDOT = -15119
165696 ZDOT = -4608
321704
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 08033
52600385
00020000 00000-0 20000-3 0 9057
2 25544 51
6390 355
8760 0005947 359
8051
3111 15
77767736 7128
Satellite: ISS
Catalog Number: 25544
Epoch time: 08033
52600385 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 355
8760 deg
Eccentricity:
0005947
Arg of perigee: 359
8051 deg
Mean anomaly:
3111 deg
Mean motion: 15
77767736 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 712
Checksum: 287
Coasting Arc #7 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2008/034/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4926233
97 A = 6717227
19 meter
Y = 3340023
55 meter E =
0014219
Z = 3108317
01 I = 51
59030
XDOT = -5144
930194 Wp = 69
99177
YDOT = -3037
536174 meter/sec RA = 350
32352 deg
ZDOT = -4867
284112 TA = 73
79636
MA = 73
63994
Ha = 185
381 n
mi
Hp = 177
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16162184
93 X = -4978315
80
Y = 10958082
50 feet Y = 3284644
13 meter
Z = 10197890
45 Z = 3084259
67
XDOT = -16879
692236 XDOT = -5086
937756
YDOT = -9965
669862 feet/sec YDOT = -3094
745050 meter/sec
ZDOT = -15968
779895 ZDOT = -4892
137025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19061028
82 X = -5809801
58
Y = -4453635
09 feet Y = -1357467
98 meter
Z = 10106190
11 Z = 3080366
75
XDOT = -4421
647529 XDOT = -1347
718167
YDOT = -17699
303679 feet/sec YDOT = -5394
747761 meter/sec
ZDOT = -16064
133194 ZDOT = -4896
347797
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 08034
53940106
00020000 00000-0 20000-3 0 9068
2 25544 51
6391 350
6426 0005958 3
0437 357
0763 15
77806658 7288
Satellite: ISS
Catalog Number: 25544
Epoch time: 08034
53940106 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 350
6426 deg
Eccentricity:
0005958
Arg of perigee: 3
0437 deg
Mean anomaly: 357
0763 deg
Mean motion: 15
77806658 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 728
Checksum: 298
Coasting Arc #8 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2008/035/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3448787
13 A = 6710744
66 meter
Y = 3079436
54 meter E =
0006477
Z = 4857852
53 I = 51
54158
XDOT = -6431
675088 Wp = 69
24415
YDOT = 3584
108492 meter/sec RA = 345
19755 deg
ZDOT = 2293
920274 TA = 358
43009
MA = 358
43213
Ha = 185
171 n
mi
Hp = 177
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11314918
41 X = 3390498
13
Y = 10103138
25 feet Y = 3117676
57 meter
Z = 15937836
38 Z = 4874464
94
XDOT = -21101
296219 XDOT = -6482
418282
YDOT = 11758
886130 feet/sec YDOT = 3511
901952 meter/sec
ZDOT = 7525
985152 ZDOT = 2262
553035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 474579
69 X = 144651
89
Y = 15094252
97 feet Y = 4600728
31 meter
Z = 16001678
38 Z = 4877311
57
XDOT = -22019
699924 XDOT = -6711
604537
YDOT = -7159
925379 feet/sec YDOT = -2182
345256 meter/sec
ZDOT = 7406
345235 ZDOT = 2257
454028
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 08035
55277021
00020000 00000-0 20000-3 0 9071
2 25544 51
6399 345
4094 0005804 5
4515 354
6712 15
77879195 7443
Satellite: ISS
Catalog Number: 25544
Epoch time: 08035
55277021 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 345
4094 deg
Eccentricity:
0005804
Arg of perigee: 5
4515 deg
Mean anomaly: 354
6712 deg
Mean motion: 15
77879195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 744
Checksum: 306
Coasting Arc #9 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2008/036/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6035502
02 A = 6720939
91 meter
Y = -2837761
18 meter E =
0016012
Z = -758554
31 I = 51
54766
XDOT = 2661
828699 Wp = 28
75515
YDOT = 4081
386138 meter/sec RA = 339
99993 deg
ZDOT = 5976
295655 TA = 322
94782
MA = 323
05827
Ha = 185
407 n
mi
Hp = 177
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19801515
82 X = 6070470
55
Y = -9310240
09 feet Y = -2770073
20 meter
Z = -2488695
23 Z = -729149
94
XDOT = 8733
033791 XDOT = 2586
961288
YDOT = 13390
374468 feet/sec YDOT = 4110
733279 meter/sec
ZDOT = 19607
269208 ZDOT = 5989
044814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20565772
25 X = 6268447
38
Y = 7508362
42 feet Y = 2288548
87 meter
Z = -2376490
88 Z = -724354
42
XDOT = -2884
949292 XDOT = -879
332544
YDOT = 14052
030708 feet/sec YDOT = 4283
058960 meter/sec
ZDOT = 19656
436075 ZDOT = 5991
281716
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 08036
50278219
00020000 00000-0 20000-3 0 9088
2 25544 51
6397 340
5024 0005898 9
9906 350
1375 15
77875874 7598
Satellite: ISS
Catalog Number: 25544
Epoch time: 08036
50278219 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 340
5024 deg
Eccentricity:
0005898
Arg of perigee: 9
9906 deg
Mean anomaly: 350
1375 deg
Mean motion: 15
77875874 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 759
Checksum: 328
Coasting Arc #10 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2008/037/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1128723
70 A = 6709112
53 meter
Y = -4067538
89 meter E =
0016729
Z = -5228136
35 I = 51
48189
XDOT = 7141
982812 Wp = 74
45946
YDOT = -2794
911518 meter/sec RA = 334
82739 deg
ZDOT = 638
654722 TA = 201
59371
MA = 201
66434
Ha = 185
382 n
mi
Hp = 176
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3703161
74 X = -1057759
43
Y = -13344943
85 feet Y = -4079763
97 meter
Z = -17152678
31 Z = -5233447
28
XDOT = 23431
702140 XDOT = 7169
602770
YDOT = -9169
657211 feet/sec YDOT = -2714
891390 meter/sec
ZDOT = 2095
323890 ZDOT = 673
416365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6726406
87 X = 2050208
81
Y = -12076639
22 feet Y = -3680959
63 meter
Z = -17173396
35 Z = -5234451
21
XDOT = 22295
380557 XDOT = 6795
631994
YDOT = 9278
101533 feet/sec YDOT = 2827
965347 meter/sec
ZDOT = 2228
024924 ZDOT = 679
101997
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 08037
51610098
00020000 00000-0 20000-3 0 9096
2 25544 51
6405 335
2682 0005890 13
3881 346
7439 15
77916592 7755
Satellite: ISS
Catalog Number: 25544
Epoch time: 08037
51610098 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 335
2682 deg
Eccentricity:
0005890
Arg of perigee: 13
3881 deg
Mean anomaly: 346
7439 deg
Mean motion: 15
77916592 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 775
Checksum: 313
Coasting Arc #11 (Orbit 790)
---------------------------------------
Vector Time (GMT): 2008/038/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6173632
02 A = 6719341
02 meter
Y = 1899958
02 meter E =
0006201
Z = -1856506
00 I = 51
49181
XDOT = 77
277078 Wp = 89
00843
YDOT = -5243
164451 meter/sec RA = 329
67438 deg
ZDOT = -5638
929800 TA = 111
66253
MA = 111
59647
Ha = 185
394 n
mi
Hp = 176
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20254698
24 X = -6185400
53
Y = 6233458
08 feet Y = 1830855
16 meter
Z = -6090898
95 Z = -1886525
13
XDOT = 253
533720 XDOT = 163
293243
YDOT = -17201
983108 feet/sec YDOT = -5241
819328 meter/sec
ZDOT = -18500
425852 ZDOT = -5638
345497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18998310
63 X = -5790685
08
Y = -9314679
95 feet Y = -2839114
45 meter
Z = -6205544
37 Z = -1891449
93
XDOT = 11368
677078 XDOT = 3465
172773
YDOT = -10898
086672 feet/sec YDOT = -3321
736818 meter/sec
ZDOT = -18498
716159 ZDOT = -5638
408685
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 08038
52939294
00020000 00000-0 20000-3 0 9102
2 25544 51
6411 330
0343 0005882 17
5132 342
6235 15
77968508 7916
Satellite: ISS
Catalog Number: 25544
Epoch time: 08038
52939294 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 330
0343 deg
Eccentricity:
0005882
Arg of perigee: 17
5132 deg
Mean anomaly: 342
6235 deg
Mean motion: 15
77968508 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 791
Checksum: 290
Coasting Arc #12 (Orbit 806)
---------------------------------------
Vector Time (GMT): 2008/039/12:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1174341
47 A = 6712829
29 meter
Y = 5031963
15 meter E =
0014277
Z = 4280501
24 I = 51
44502
XDOT = -6734
398641 Wp = 53
21270
YDOT = 1402
740938 meter/sec RA = 324
45452 deg
ZDOT = -3480
145735 TA = 72
12374
MA = 71
96809
Ha = 185
437 n
mi
Hp = 176
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3852826
35 X = -1251315
68
Y = 16509065
45 feet Y = 5018400
70 meter
Z = 14043639
25 Z = 4274609
39
XDOT = -22094
483730 XDOT = -6732
678364
YDOT = 4602
168431 feet/sec YDOT = 1327
442605 meter/sec
ZDOT = -11417
800967 ZDOT = -3512
856345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14013645
25 X = -4271359
07
Y = 9572327
36 feet Y = 2917645
38 meter
Z = 14021612
32 Z = 4273787
44
XDOT = -18699
670031 XDOT = -5699
659426
YDOT = -10388
883909 feet/sec YDOT = -3166
531816 meter/sec
ZDOT = -11542
789065 ZDOT = -3518
242107
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 08039
54265831
00020000 00000-0 20000-3 0 9115
2 25544 51
6407 324
8005 0005840 21
4608 338
6801 15
78001574 8077
Satellite: ISS
Catalog Number: 25544
Epoch time: 08039
54265831 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 324
8005 deg
Eccentricity:
0005840
Arg of perigee: 21
4608 deg
Mean anomaly: 338
6801 deg
Mean motion: 15
78001574 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 807
Checksum: 274
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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