Date:
October 31st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 966)
---------------------------------------
Vector Time (GMT): 2008/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2470612
88 A = 6734254
83 meter
Y = -5692137
05 meter E =
0003268
Z = -2611744
20 I = 51
89470
XDOT = 5608
892393 Wp = 175
73531
YDOT = -18
550047 meter/sec RA = 47
26312 deg
ZDOT = -5268
980314 TA = 33
80300
MA = 33
78217
Ha = 191
457 n
mi
Hp = 187
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8105685
29 X = -2394091
05
Y = -18674990
31 feet Y = -5719337
01 meter
Z = -8568714
58 Z = -2623560
98
XDOT = 18401
877931 XDOT = 5634
279564
YDOT = -60
859735 feet/sec YDOT = 44
313788 meter/sec
ZDOT = -17286
680821 ZDOT = -5241
669736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17748775
32 X = 5409826
72
Y = 9931953
33 feet Y = 3027259
37 meter
Z = -8614960
49 Z = -2625839
96
XDOT = -13929
293779 XDOT = -4245
648744
YDOT = 9999
747215 feet/sec YDOT = 3047
922951 meter/sec
ZDOT = -17180
838009 ZDOT = -5236
719425
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 08303
52653525
00020000 00000-0 20000-3 0 9006
2 25544 51
6430 47
6826 0003812 265
8192 94
2534 15
72220185 9673
Satellite: ISS
Catalog Number: 25544
Epoch time: 08303
52653525 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 47
6826 deg
Eccentricity:
0003812
Arg of perigee: 265
8192 deg
Mean anomaly: 94
2534 deg
Mean motion: 15
72220185 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 967
Checksum: 281
Coasting Arc #2 (Orbit 982)
---------------------------------------
Vector Time (GMT): 2008/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4535521
01 A = 6727037
31 meter
Y = 1042670
15 meter E =
0004378
Z = 4856934
29 I = 51
85009
XDOT = -3981
695500 Wp = 30
72277
YDOT = -6137
198567 meter/sec RA = 42
11698 deg
ZDOT = -2396
060143 TA = 82
61789
MA = 82
56813
Ha = 191
570 n
mi
Hp = 187
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14880318
26 X = -4570438
10
Y = 3420833
83 feet Y = 991755
99 meter
Z = 15934823
78 Z = 4834815
21
XDOT = -13063
305445 XDOT = -3901
132407
YDOT = -20135
165903 feet/sec YDOT = -6181
273681 meter/sec
ZDOT = -7861
089709 ZDOT = -2415
208301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9604062
71 X = 2927318
31
Y = -11983742
78 feet Y = -3652644
80 meter
Z = 15849178
94 Z = 4830829
74
XDOT = 21837
816449 XDOT = 6656
166454
YDOT = 6985
651116 feet/sec YDOT = 2129
226460 meter/sec
ZDOT = -7935
774223 ZDOT = -2418
823983
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 08304
54351337
00020000 00000-0 20000-3 0 9016
2 25544 51
6435 42
4743 0003733 272
7181 87
3554 15
72247819 9832
Satellite: ISS
Catalog Number: 25544
Epoch time: 08304
54351337 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 42
4743 deg
Eccentricity:
0003733
Arg of perigee: 272
7181 deg
Mean anomaly: 87
3554 deg
Mean motion: 15
72247819 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 983
Checksum: 290
Coasting Arc #3 (Orbit 998)
---------------------------------------
Vector Time (GMT): 2008/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4395825
46 A = 6736055
35 meter
Y = 4851526
41 meter E =
0011184
Z = 1558957
12 I = 51
85823
XDOT = -4550
938409 Wp = 51
76346
YDOT = 2257
508377 meter/sec RA = 37
04377 deg
ZDOT = 5785
832673 TA = 325
36624
MA = 325
43902
Ha = 191
450 n
mi
Hp = 187
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14421999
56 X = 4333674
83
Y = 15917081
40 feet Y = 4900335
51 meter
Z = 5114688
72 Z = 1580161
93
XDOT = -14930
900292 XDOT = -4603
951391
YDOT = 7406
523546 feet/sec YDOT = 2206
320512 meter/sec
ZDOT = 18982
390660 ZDOT = 5763
594849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21224869
29 X = -6469340
16
Y = -3162470
60 feet Y = -963921
04 meter
Z = 5197239
22 Z = 1584118
51
XDOT = 6688
359292 XDOT = 2038
611912
YDOT = -13722
308467 feet/sec YDOT = -4182
559621 meter/sec
ZDOT = 18896
373763 ZDOT = 5759
614723
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 08305
56047910
00020000 00000-0 20000-3 0 9029
2 25544 51
6436 37
2658 0003730 277
2694 82
8044 15
72259110 9994
Satellite: ISS
Catalog Number: 25544
Epoch time: 08305
56047910 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 37
2658 deg
Eccentricity:
0003730
Arg of perigee: 277
2694 deg
Mean anomaly: 82
8044 deg
Mean motion: 15
72259110 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 999
Checksum: 295
Coasting Arc #4 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2008/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3262082
28 A = 6725466
70 meter
Y = -2781416
38 meter E =
0010520
Z = -5191289
60 I = 51
79818
XDOT = 5920
310127 Wp = 97
68013
YDOT = 4767
894748 meter/sec RA = 31
91128 deg
ZDOT = 1166
244410 TA = 183
44281
MA = 183
45005
Ha = 191
456 n
mi
Hp = 187
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10702369
68 X = 3318161
13
Y = -9125381
84 feet Y = -2744624
07 meter
Z = -17031790
03 Z = -5175305
89
XDOT = 19423
589656 XDOT = 5860
889176
YDOT = 15642
699305 feet/sec YDOT = 4833
766775 meter/sec
ZDOT = 3826
261187 ZDOT = 1194
861994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2312377
21 X = -704812
57
Y = 13948677
79 feet Y = 4251556
99 meter
Z = -16970046
60 Z = -5172470
20
XDOT = -23896
161010 XDOT = -7283
549876
YDOT = 826
452978 feet/sec YDOT = 251
902868 meter/sec
ZDOT = 3937
532423 ZDOT = 1200
159883
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 08306
51387336
00020000 00000-0 20000-3 0 9035
2 25544 51
6433 32
3835 0003777 282
4731 77
6008 15
72286100 10145
Satellite: ISS
Catalog Number: 25544
Epoch time: 08306
51387336 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 32
3835 deg
Eccentricity:
0003777
Arg of perigee: 282
4731 deg
Mean anomaly: 77
6008 deg
Mean motion: 15
72286100 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1014
Checksum: 272
Coasting Arc #5 (Orbit 1029)
---------------------------------------
Vector Time (GMT): 2008/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5812901
17 A = 6736947
97 meter
Y = -3361939
34 meter E =
0008232
Z = -480643
50 I = 51
81055
XDOT = 2759
051154 Wp = 152
67214
YDOT = -3915
924683 meter/sec RA = 26
81561 deg
ZDOT = -6025
091554 TA = 32
53953
MA = 32
48881
Ha = 191
509 n
mi
Hp = 187
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19071198
07 X = -5772540
45
Y = -11029984
71 feet Y = -3426716
86 meter
Z = -1576914
36 Z = -508785
43
XDOT = 9052
005097 XDOT = 2831
904123
YDOT = -12847
521926 feet/sec YDOT = -3884
663682 meter/sec
ZDOT = -19767
360740 ZDOT = -6011
511019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21594545
69 X = 6582017
53
Y = -4323195
05 feet Y = -1317709
85 meter
Z = -1686237
95 Z = -513965
33
XDOT = 1299
609484 XDOT = 396
120971
YDOT = 14124
241758 feet/sec YDOT = 4305
068888 meter/sec
ZDOT = -19715
010589 ZDOT = -6009
135228
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 08307
53081633
00020000 00000-0 20000-3 0 9040
2 25544 51
6425 27
1748 0003723 286
2198 73
8555 15
72285046 10302
Satellite: ISS
Catalog Number: 25544
Epoch time: 08307
53081633 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 27
1748 deg
Eccentricity:
0003723
Arg of perigee: 286
2198 deg
Mean anomaly: 73
8555 deg
Mean motion: 15
72285046 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1030
Checksum: 284
Coasting Arc #6 (Orbit 1045)
---------------------------------------
Vector Time (GMT): 2008/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1458960
13 A = 6724827
81 meter
Y = 3901018
18 meter E =
0001803
Z = 5280909
21 I = 51
74412
XDOT = -7174
839780 Wp = 315
88070
YDOT = -2788
151920 meter/sec RA = 21
69810 deg
ZDOT = 78
700831 TA = 133
38083
MA = 133
36581
Ha = 191
537 n
mi
Hp = 187
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4786614
59 X = -1528127
76
Y = 12798616
06 feet Y = 3884316
20 meter
Z = 17325817
63 Z = 5273653
65
XDOT = -23539
500590 XDOT = -7143
511280
YDOT = -9147
480054 feet/sec YDOT = -2868
209962 meter/sec
ZDOT = 258
204825 ZDOT = 43
920649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5013703
37 X = -1528176
79
Y = -12749232
10 feet Y = -3885965
94 meter
Z = 17297978
73 Z = 5272423
92
XDOT = 22628
199609 XDOT = 6897
075241
YDOT = -8737
244647 feet/sec YDOT = -2663
112168 meter/sec
ZDOT = 123
191412 ZDOT = 37
548742
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 08308
54774498
00020000 00000-0 20000-3 0 9051
2 25544 51
6432 21
9653 0003875 291
0500 69
0247 15
72342253 10462
Satellite: ISS
Catalog Number: 25544
Epoch time: 08308
54774498 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 21
9653 deg
Eccentricity:
0003875
Arg of perigee: 291
0500 deg
Mean anomaly: 69
0247 deg
Mean motion: 15
72342253 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1046
Checksum: 285
Coasting Arc #7 (Orbit 1060)
---------------------------------------
Vector Time (GMT): 2008/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6544902
62 A = 6736912
33 meter
Y = 1444414
91 meter E =
0010887
Z = -612742
75 I = 51
75590
XDOT = -498
839742 Wp = 19
80655
YDOT = 4791
035475 meter/sec RA = 16
57736 deg
ZDOT = 6006
602863 TA = 333
53672
MA = 333
59228
Ha = 191
789 n
mi
Hp = 187
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21472777
63 X = 6531241
15
Y = 4738894
06 feet Y = 1517527
44 meter
Z = -2010310
86 Z = -580980
13
XDOT = -1636
613326 XDOT = -581
556341
YDOT = 15718
620325 feet/sec YDOT = 4784
994366 meter/sec
ZDOT = 19706
702307 ZDOT = 6003
978773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18876069
34 X = -5753425
93
Y = 11300953
36 feet Y = 3444530
58 meter
Z = -1887089
19 Z = -575184
79
XDOT = -8693
266750 XDOT = -2649
707705
YDOT = -11255
271136 feet/sec YDOT = -3430
606642 meter/sec
ZDOT = 19696
878743 ZDOT = 6003
608641
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 08309
50110734
00020000 00000-0 20000-3 0 9066
2 25544 51
6425 17
0821 0003890 299
3299 60
7475 15
72286514 10615
Satellite: ISS
Catalog Number: 25544
Epoch time: 08309
50110734 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 17
0821 deg
Eccentricity:
0003890
Arg of perigee: 299
3299 deg
Mean anomaly: 60
7475 deg
Mean motion: 15
72286514 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1061
Checksum: 283
Coasting Arc #8 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2008/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -604280
50 A = 6725394
04 meter
Y = -4282790
14 meter E =
0011625
Z = -5160138
93 I = 51
68844
XDOT = 7564
196370 Wp = 67
42293
YDOT = 493
248204 meter/sec RA = 11
47682 deg
ZDOT = -1293
126967 TA = 190
18997
MA = 190
21356
Ha = 191
750 n
mi
Hp = 187
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1982547
58 X = -531277
28
Y = -14051148
75 feet Y = -4289139
18 meter
Z = -16929589
66 Z = -5162897
40
XDOT = 24816
917223 XDOT = 7564
400481
YDOT = 1618
268386 feet/sec YDOT = 577
836608 meter/sec
ZDOT = -4242
542544 ZDOT = -1256
378955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11168020
29 X = 3404012
58
Y = 8733149
96 feet Y = 2661864
11 meter
Z = -16940593
16 Z = -5163492
80
XDOT = -18262
402209 XDOT = -5566
380193
YDOT = 15387
645369 feet/sec YDOT = 4690
154308 meter/sec
ZDOT = -4100
064181 ZDOT = -1249
699562
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 08310
51801505
00020000 00000-0 20000-3 0 9073
2 25544 51
6419 11
8727 0003831 301
8319 58
2470 15
72326888 10775
Satellite: ISS
Catalog Number: 25544
Epoch time: 08310
51801505 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 11
8727 deg
Eccentricity:
0003831
Arg of perigee: 301
8319 deg
Mean anomaly: 58
2470 deg
Mean motion: 15
72326888 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1077
Checksum: 280
Coasting Arc #9 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2008/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6504826
79 A = 6735653
43 meter
Y = 575535
07 meter E =
0010324
Z = 1632410
55 I = 51
69509
XDOT = -1869
864645 Wp = 111
99617
YDOT = -4772
055554 meter/sec RA = 6
33191 deg
ZDOT = -5743
473109 TA = 50
00215
MA = 49
91156
Ha = 191
850 n
mi
Hp = 187
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21341295
24 X = -6518709
15
Y = 1888238
43 feet Y = 502716
69 meter
Z = 5355677
64 Z = 1600775
85
XDOT = -6134
726527 XDOT = -1788
462540
YDOT = -15656
350242 feet/sec YDOT = -4792
510200 meter/sec
ZDOT = -18843
415713 ZDOT = -5752
359436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13685113
07 X = 4171222
46
Y = -16523679
38 feet Y = -5036417
48 meter
Z = 5233097
55 Z = 1595048
13
XDOT = 14164
895679 XDOT = 4317
460203
YDOT = 5726
077335 feet/sec YDOT = 1745
308372 meter/sec
ZDOT = -18878
208257 ZDOT = -5754
077877
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 08311
53490993
00020000 00000-0 20000-3 0 9082
2 25544 51
6425 6
6633 0003871 309
3883 50
6936 15
72393090 10933
Satellite: ISS
Catalog Number: 25544
Epoch time: 08311
53490993 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 6
6633 deg
Eccentricity:
0003871
Arg of perigee: 309
3883 deg
Mean anomaly: 50
6936 deg
Mean motion: 15
72393090 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1093
Checksum: 297
Coasting Arc #10 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2008/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2622110
84 A = 6726560
99 meter
Y = 3879057
93 meter E =
0003254
Z = 4827204
89 I = 51
63508
XDOT = -7089
803789 Wp = 107
46742
YDOT = 1768
299837 meter/sec RA = 1
24467 deg
ZDOT = 2427
868718 TA = 318
80757
MA = 318
83212
Ha = 191
873 n
mi
Hp = 187
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8602725
84 X = 2555089
57
Y = 12726568
03 feet Y = 3908005
14 meter
Z = 15837286
39 Z = 4839780
56
XDOT = -23260
511119 XDOT = -7120
844640
YDOT = 5801
508653 feet/sec YDOT = 1688
843984 meter/sec
ZDOT = 7965
448551 ZDOT = 2393
350415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15081747
95 X = -4596916
78
Y = -2637793
19 feet Y = -803999
36 meter
Z = 15886314
60 Z = 4842148
69
XDOT = 11713
291539 XDOT = 3570
211261
YDOT = -19758
700475 feet/sec YDOT = -6022
451905 meter/sec
ZDOT = 7831
780540 ZDOT = 2387
126709
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 08312
55179365
00020000 00000-0 20000-3 0 9093
2 25544 51
6423 1
4538 0003806 312
8273 47
2570 15
72396004 11090
Satellite: ISS
Catalog Number: 25544
Epoch time: 08312
55179365 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 1
4538 deg
Eccentricity:
0003806
Arg of perigee: 312
8273 deg
Mean anomaly: 47
2570 deg
Mean motion: 15
72396004 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1109
Checksum: 275
Coasting Arc #11 (Orbit 1123)
---------------------------------------
Vector Time (GMT): 2008/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5712616
86 A = 6733846
39 meter
Y = -2444576
92 meter E =
0006242
Z = -2587159
73 I = 51
63031
XDOT = 4046
751675 Wp = 13
73909
YDOT = 3897
797012 meter/sec RA = 356
08007 deg
ZDOT = 5261
044747 TA = 316
90298
MA = 316
95183
Ha = 192
092 n
mi
Hp = 187
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18742181
30 X = 5752096
17
Y = -8020265
50 feet Y = -2380474
42 meter
Z = -8488056
85 Z = -2559311
30
XDOT = 13276
744342 XDOT = 3977
307341
YDOT = 12788
047938 feet/sec YDOT = 3942
661891 meter/sec
ZDOT = 17260
645494 ZDOT = 5280
535581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6852109
51 X = -2088522
98
Y = 19247347
31 feet Y = 5866591
46 meter
Z = -8380295
00 Z = -2554313
92
XDOT = -16931
265749 XDOT = -5160
649800
YDOT = 1508
372861 feet/sec YDOT = 459
752048 meter/sec
ZDOT = 17336
477263 ZDOT = 5284
158270
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 08313
50511241
00020000 00000-0 20000-3 0 9104
2 25544 51
6423 356
5699 0003759 318
3352 41
7523 15
72418036 11242
Satellite: ISS
Catalog Number: 25544
Epoch time: 08313
50511241 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 356
5699 deg
Eccentricity:
0003759
Arg of perigee: 318
3352 deg
Mean anomaly: 41
7523 deg
Mean motion: 15
72418036 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1124
Checksum: 268
Coasting Arc #12 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2008/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4332874
81 A = 6728455
91 meter
Y = -2792977
35 meter E =
0008784
Z = -4333103
31 I = 51
58386
XDOT = 5811
881923 Wp = 44
54039
YDOT = -3680
417388 meter/sec RA = 351
00057 deg
ZDOT = -3437
353287 TA = 190
66676
MA = 190
68540
Ha = 192
166 n
mi
Hp = 186
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14215468
52 X = -4280271
25
Y = -9163311
51 feet Y = -2841135
99 meter
Z = -14216218
21 Z = -4354025
16
XDOT = 19067
854078 XDOT = 5869
303479
YDOT = -12074
860197 feet/sec YDOT = -3615
104547 meter/sec
ZDOT = -11277
405796 ZDOT = -3408
978884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16245767
54 X = 4951709
95
Y = -4450040
12 feet Y = -1356372
23 meter
Z = -14297512
49 Z = -4357881
81
XDOT = -4045
736590 XDOT = -1233
140512
YDOT = 21131
255692 feet/sec YDOT = 6440
806735 meter/sec
ZDOT = -11167
699241 ZDOT = -3403
914729
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 08314
52197392
00020000 00000-0 20000-3 0 9115
2 25544 51
6430 351
3602 0003758 323
7286 36
3621 15
72417841 11402
Satellite: ISS
Catalog Number: 25544
Epoch time: 08314
52197392 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 351
3602 deg
Eccentricity:
0003758
Arg of perigee: 323
7286 deg
Mean anomaly: 36
3621 deg
Mean motion: 15
72417841 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1140
Checksum: 269
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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