Date:
September 24th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3552 09 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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
267/19:33:56
053 0
7 10
2 10
2
N/A -8
3 0
0 189
0
000/00:01:52
106 -5
9 0
0 181
4
Coasting Arc #1 (Orbit 2565)
---------------------------------------
Vector Time (GMT): 2007/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2011073
40 A = 6711945
86 meter
Y = -3685761
97 meter E =
0020942
Z = -5252910
15 I = 51
48685
XDOT = 6946
353208 Wp = 62
38041
YDOT = -3284
636175 meter/sec RA = 336
74743 deg
ZDOT = -346
213082 TA = 204
27237
MA = 204
37116
Ha = 188
400 n
mi
Hp = 177
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6598009
85 X = -1944191
31
Y = -12092394
91 feet Y = -3707876
94 meter
Z = -17233957
19 Z = -5262517
58
XDOT = 22789
872730 XDOT = 6984
248084
YDOT = -10776
365402 feet/sec YDOT = -3206
746246 meter/sec
ZDOT = -1135
869691 ZDOT = -312
375417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5918858
96 X = 1804068
21
Y = 12387651
93 feet Y = 3775756
31 meter
Z = -17270848
77 Z = -5264154
71
XDOT = -22379
073415 XDOT = -6821
141577
YDOT = 9248
934049 feet/sec YDOT = 2819
075098 meter/sec
ZDOT = -1007
813497 ZDOT = -307
181554
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 07262
51637699
00020000 00000-0 20000-3 0 9002
2 25544 51
6353 337
1650 0009650 22
0216 338
1362 15
76879361 25661
Satellite: ISS
Catalog Number: 25544
Epoch time: 07262
51637699 = yrday
fracday
Element set: 900
Inclination: 51
6353 deg
RA of node: 337
1650 deg
Eccentricity:
0009650
Arg of perigee: 22
0216 deg
Mean anomaly: 338
1362 deg
Mean motion: 15
76879361 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2566
Checksum: 295
Coasting Arc #2 (Orbit 2581)
---------------------------------------
Vector Time (GMT): 2007/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6126647
68 A = 6723631
87 meter
Y = 2684006
40 meter E =
0011166
Z = -697681
23 I = 51
50037
XDOT = -1370
518847 Wp = 86
57160
YDOT = -4659
690598 meter/sec RA = 331
58321 deg
ZDOT = -5972
208609 TA = 101
04598
MA = 100
92038
Ha = 188
500 n
mi
Hp = 177
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20100550
14 X = -6152816
07
Y = 8805795
28 feet Y = 2615348
46 meter
Z = -2288980
41 Z = -727508
15
XDOT = -4496
452910 XDOT = -1289
299605
YDOT = -15287
698811 feet/sec YDOT = -4674
562356 meter/sec
ZDOT = -19593
860266 ZDOT = -5978
669363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20345346
18 X = 6201261
52
Y = -8192155
61 feet Y = -2496969
03 meter
Z = -2401885
30 Z = -732094
64
XDOT = 3322
894712 XDOT = 1012
818308
YDOT = 13930
039685 feet/sec YDOT = 4245
876096 meter/sec
ZDOT = -19618
923095 ZDOT = -5979
847759
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 07263
53033400
00020000 00000-0 20000-3 0 9016
2 25544 51
6350 331
9346 0009798 26
7887 333
3782 15
76922929 25820
Satellite: ISS
Catalog Number: 25544
Epoch time: 07263
53033400 = yrday
fracday
Element set: 901
Inclination: 51
6350 deg
RA of node: 331
9346 deg
Eccentricity:
0009798
Arg of perigee: 26
7887 deg
Mean anomaly: 333
3782 deg
Mean motion: 15
76922929 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2582
Checksum: 308
Coasting Arc #3 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2007/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 427648
94 A = 6712877
00 meter
Y = 4479315
94 meter E =
0015181
Z = 4976774
79 I = 51
44014
XDOT = -6932
036965 Wp = 38
58773
YDOT = 2789
014836 meter/sec RA = 326
38994 deg
ZDOT = -1899
766812 TA = 69
86189
MA = 69
69863
Ha = 188
469 n
mi
Hp = 176
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1403047
71 X = 353352
49
Y = 14695918
42 feet Y = 4483682
75 meter
Z = 16328001
27 Z = 4978671
83
XDOT = -22742
903430 XDOT = -6953
480214
YDOT = 9150
311142 feet/sec YDOT = 2711
376981 meter/sec
ZDOT = -6232
830749 ZDOT = -1933
494756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1117875
26 X = -340728
38
Y = -14711786
29 feet Y = -4484152
46 meter
Z = 16335724
22 Z = 4979128
74
XDOT = 21753
062281 XDOT = 6630
333383
YDOT = -8769
451776 feet/sec YDOT = -2672
928901 meter/sec
ZDOT = -6360
532897 ZDOT = -1938
690427
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 07264
54427587
00020000 00000-0 20000-3 0 9022
2 25544 51
6355 326
7040 0009782 29
3699 330
8014 15
76977827 25985
Satellite: ISS
Catalog Number: 25544
Epoch time: 07264
54427587 = yrday
fracday
Element set: 902
Inclination: 51
6355 deg
RA of node: 326
7040 deg
Eccentricity:
0009782
Arg of perigee: 29
3699 deg
Mean anomaly: 330
8014 deg
Mean motion: 15
76977827 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2598
Checksum: 329
Coasting Arc #4 (Orbit 2613)
---------------------------------------
Vector Time (GMT): 2007/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5844094
50 A = 6720882
65 meter
Y = -2083878
38 meter E =
0022197
Z = 2549555
29 I = 51
44304
XDOT = -302
025829 Wp = 58
83099
YDOT = 5627
905945 meter/sec RA = 321
25608 deg
ZDOT = 5269
953794 TA = 330
24992
MA = 330
37595
Ha = 188
594 n
mi
Hp = 176
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19173538
39 X = 5854577
14
Y = -6836871
32 feet Y = -2018467
75 meter
Z = 8364682
71 Z = 2577971
35
XDOT = -990
898389 XDOT = -390
535897
YDOT = 18464
258349 feet/sec YDOT = 5624
033749 meter/sec
ZDOT = 17289
874651 ZDOT = 5268
271445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19098344
65 X = -5821175
45
Y = 6914375
73 feet Y = 2107501
72 meter
Z = 8472304
33 Z = 2582358
36
XDOT = 1517
463505 XDOT = 462
522876
YDOT = -17075
730149 feet/sec YDOT = -5204
682549 meter/sec
ZDOT = 17284
150595 ZDOT = 5268
209101
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 07265
55820826
00020000 00000-0 20000-3 0 9038
2 25544 51
6349 321
4738 0009994 34
4606 325
7205 15
76953359 26142
Satellite: ISS
Catalog Number: 25544
Epoch time: 07265
55820826 = yrday
fracday
Element set: 903
Inclination: 51
6349 deg
RA of node: 321
4738 deg
Eccentricity:
0009994
Arg of perigee: 34
4606 deg
Mean anomaly: 325
7205 deg
Mean motion: 15
76953359 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2614
Checksum: 312
Coasting Arc #5 (Orbit 2628)
---------------------------------------
Vector Time (GMT): 2007/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 877865
06 A = 6716598
90 meter
Y = -5310081
52 meter E =
0014277
Z = -4025243
26 I = 51
40686
XDOT = 6386
865435 Wp = 66
55317
YDOT = -1866
843255 meter/sec RA = 316
03427 deg
ZDOT = 3872
065432 TA = 243
42633
MA = 243
57272
Ha = 188
705 n
mi
Hp = 176
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2880134
72 X = 956731
79
Y = -17421527
28 feet Y = -5299823
95 meter
Z = -13206178
69 Z = -4020786
79
XDOT = 20954
282923 XDOT = 6388
456331
YDOT = -6124
813828 feet/sec YDOT = -1795
412639 meter/sec
ZDOT = 12703
626744 ZDOT = 3903
096680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2583417
58 X = -787425
68
Y = 17480291
77 feet Y = 5327992
93 meter
Z = -13189893
77 Z = -4020279
62
XDOT = -19472
953906 XDOT = -5935
356351
YDOT = 6755
716853 feet/sec YDOT = 2059
142497 meter/sec
ZDOT = 12821
200216 ZDOT = 3907
901826
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 07266
50875621
00020000 00000-0 20000-3 0 9048
2 25544 51
6345 316
5704 0010092 38
2420 321
9459 15
77000341 26293
Satellite: ISS
Catalog Number: 25544
Epoch time: 07266
50875621 = yrday
fracday
Element set: 904
Inclination: 51
6345 deg
RA of node: 316
5704 deg
Eccentricity:
0010092
Arg of perigee: 38
2420 deg
Mean anomaly: 321
9459 deg
Mean motion: 15
77000341 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2629
Checksum: 273
Coasting Arc #6 (Orbit 2644)
---------------------------------------
Vector Time (GMT): 2007/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5233278
17 A = 6716250
19 meter
Y = 1041629
47 meter E =
0017377
Z = -4097871
06 I = 51
38621
XDOT = 1653
286236 Wp = 53
99131
YDOT = -6499
132360 meter/sec RA = 310
90941 deg
ZDOT = -3764
431793 TA = 177
22437
MA = 177
21471
Ha = 188
789 n
mi
Hp = 176
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17169547
81 X = -5224630
19
Y = 3417419
52 feet Y = 983156
04 meter
Z = -13444458
86 Z = -4123273
36
XDOT = 5424
167442 XDOT = 1744
124537
YDOT = -21322
612729 feet/sec YDOT = -6480
136754 meter/sec
ZDOT = -12350
498010 ZDOT = -3756
179014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16949650
35 X = 5166253
43
Y = -4072191
27 feet Y = -1241203
90 meter
Z = -13540761
18 Z = -4127224
01
XDOT = -4966
620035 XDOT = -1513
825787
YDOT = 20281
984434 feet/sec YDOT = 6181
948856 meter/sec
ZDOT = -12319
952915 ZDOT = -3755
121648
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 07267
52266163
00020000 00000-0 20000-3 0 9057
2 25544 51
6349 311
3393 0010126 42
1165 318
0776 15
76998319 26459
Satellite: ISS
Catalog Number: 25544
Epoch time: 07267
52266163 = yrday
fracday
Element set: 905
Inclination: 51
6349 deg
RA of node: 311
3393 deg
Eccentricity:
0010126
Arg of perigee: 42
1165 deg
Mean anomaly: 318
0776 deg
Mean motion: 15
76998319 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2645
Checksum: 298
Coasting Arc #7 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2007/267/19:34:52
106
Vector Time (MET): N/A
Weight (LBS) : 508517
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5299841
43 A = 6722738
85 meter
Y = 1727525
85 meter E =
0008167
Z = -3767221
21 I = 51
38378
XDOT = 896
301013 Wp = 65
74235
YDOT = -6388
001015 meter/sec RA = 309
27520 deg
ZDOT = -4194
108886 TA = 160
03520
MA = 160
00323
Ha = 188
989 n
mi
Hp = 181
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17387931
20 X = -5300464
51
Y = 5667735
74 feet Y = 1668256
24 meter
Z = -12359649
63 Z = -3792969
48
XDOT = 2940
620122 XDOT = 988
040202
YDOT = -20958
008581 feet/sec YDOT = -6377
465474 meter/sec
ZDOT = -13760
199756 ZDOT = -4189
531300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12738816
42 X = -3882791
24
Y = -13029409
17 feet Y = -3971363
91 meter
Z = -12457181
53 Z = -3796948
93
XDOT = 19183
340569 XDOT = 5847
082206
YDOT = -5627
429944 feet/sec YDOT = -1715
240647 meter/sec
ZDOT = -13743
595157 ZDOT = -4189
047804
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 07267
83952281
00020000 00000-0 20000-3 0 9065
2 25544 51
6345 309
7053 0002283 39
4045 320
7285 15
75114410 26502
Satellite: ISS
Catalog Number: 25544
Epoch time: 07267
83952281 = yrday
fracday
Element set: 906
Inclination: 51
6345 deg
RA of node: 309
7053 deg
Eccentricity:
0002283
Arg of perigee: 39
4045 deg
Mean anomaly: 320
7285 deg
Mean motion: 15
75114410 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2650
Checksum: 279
Coasting Arc #8 (Orbit 2665)
---------------------------------------
Vector Time (GMT): 2007/268/19:34:52
106
Vector Time (MET): N/A
Weight (LBS) : 508517
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -657995
54 A = 6724068
72 meter
Y = 5777092
12 meter E =
0014217
Z = 3366724
46 I = 51
37047
XDOT = -5826
284021 Wp = 83
31206
YDOT = 2035
584801 meter/sec RA = 304
06064 deg
ZDOT = -4613
355679 TA = 56
78902
MA = 56
65280
Ha = 189
014 n
mi
Hp = 181
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2158778
00 X = -738901
96
Y = 18953714
29 feet Y = 5769282
00 meter
Z = 11045683
92 Z = 3363330
80
XDOT = -19115
105056 XDOT = -5826
202250
YDOT = 6678
427826 feet/sec YDOT = 1970
431995 meter/sec
ZDOT = -15135
681363 ZDOT = -4641
659908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17870780
77 X = -5447013
98
Y = 6693853
15 feet Y = 2040286
44 meter
Z = 11033506
50 Z = 3363012
78
XDOT = -14154
539662 XDOT = -4314
303689
YDOT = -12564
960465 feet/sec YDOT = -3829
799950 meter/sec
ZDOT = -15242
873701 ZDOT = -4646
027904
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 07268
85463786
00020000 00000-0 20000-3 0 9076
2 25544 51
6341 304
4832 0002263 42
7212 317
4127 15
75120023 26668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07268
85463786 = yrday
fracday
Element set: 907
Inclination: 51
6341 deg
RA of node: 304
4832 deg
Eccentricity:
0002263
Arg of perigee: 42
7212 deg
Mean anomaly: 317
4127 deg
Mean motion: 15
75120023 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2666
Checksum: 276
Coasting Arc #9 (Orbit 2681)
---------------------------------------
Vector Time (GMT): 2007/269/19:34:52
106
Vector Time (MET): N/A
Weight (LBS) : 508517
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4877939
76 A = 6720929
85 meter
Y = -1785371
36 meter E =
0011079
Z = 4256303
40 I = 51
34494
XDOT = -570
631623 Wp = 97
49827
YDOT = 6836
666240 meter/sec RA = 298
94617 deg
ZDOT = 3512
493721 TA = 316
75523
MA = 316
84216
Ha = 188
902 n
mi
Hp = 181
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16003739
38 X = 4876864
91
Y = -5857517
59 feet Y = -1730829
05 meter
Z = 13964250
01 Z = 4279998
28
XDOT = -1872
150994 XDOT = -664
101100
YDOT = 22430
007348 feet/sec YDOT = 6829
762859 meter/sec
ZDOT = 11523
929531 ZDOT = 3509
493822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12688299
71 X = 3867393
75
Y = 11266027
44 feet Y = 3433885
16 meter
Z = 14053972
42 Z = 4283650
79
XDOT = -19860
853445 XDOT = -6053
588130
YDOT = 7968
130592 feet/sec YDOT = 2428
686204 meter/sec
ZDOT = 11513
380859 ZDOT = 3509
278486
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 07269
86974051
00020000 00000-0 20000-3 0 9081
2 25544 51
6338 299
2602 0002285 46
8091 313
3264 15
75141797 26820
Satellite: ISS
Catalog Number: 25544
Epoch time: 07269
86974051 = yrday
fracday
Element set: 908
Inclination: 51
6338 deg
RA of node: 299
2602 deg
Eccentricity:
0002285
Arg of perigee: 46
8091 deg
Mean anomaly: 313
3264 deg
Mean motion: 15
75141797 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2682
Checksum: 313
Coasting Arc #10 (Orbit 2696)
---------------------------------------
Vector Time (GMT): 2007/270/19:34:52
106
Vector Time (MET): N/A
Weight (LBS) : 508517
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 308363
07 A = 6725603
16 meter
Y = -6136309
13 meter E =
0007086
Z = -2734966
12 I = 51
34830
XDOT = 5371
246316 Wp = 54
79473
YDOT = -2012
869735 meter/sec RA = 293
73212 deg
ZDOT = 5135
161628 TA = 273
82391
MA = 273
90493
Ha = 188
993 n
mi
Hp = 181
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1011689
87 X = 390243
50
Y = -20132247
80 feet Y = -6132403
26 meter
Z = -8972985
95 Z = -2733268
64
XDOT = 17622
199199 XDOT = 5368
409179
YDOT = -6603
903329 feet/sec YDOT = -1952
820835 meter/sec
ZDOT = 16847
643137 ZDOT = 5161
248897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18093753
66 X = 5514976
12
Y = -8890954
47 feet Y = -2709962
92 meter
Z = -8967296
23 Z = -2733231
89
XDOT = 13664
881627 XDOT = 4165
055920
YDOT = 10761
444563 feet/sec YDOT = 3280
088303 meter/sec
ZDOT = 16946
416262 ZDOT = 5165
267677
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 07270
82138833
00020000 00000-0 20000-3 0 9090
2 25544 51
6341 294
3636 0002299 49
0883 311
0480 15
75165762 26975
Satellite: ISS
Catalog Number: 25544
Epoch time: 07270
82138833 = yrday
fracday
Element set: 909
Inclination: 51
6341 deg
RA of node: 294
3636 deg
Eccentricity:
0002299
Arg of perigee: 49
0883 deg
Mean anomaly: 311
0480 deg
Mean motion: 15
75165762 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2697
Checksum: 307
Coasting Arc #11 (Orbit 2712)
---------------------------------------
Vector Time (GMT): 2007/271/19:34:52
106
Vector Time (MET): N/A
Weight (LBS) : 508517
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4525251
97 A = 6719122
44 meter
Y = 1675033
79 meter E =
0013498
Z = -4688770
96 I = 51
31694
XDOT = 137
880308 Wp = 67
56320
YDOT = -7198
804096 meter/sec RA = 288
60916 deg
ZDOT = -2705
928919 TA = 175
65648
MA = 175
64475
Ha = 188
995 n
mi
Hp = 181
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14846627
19 X = -4520868
41
Y = 5495517
68 feet Y = 1624454
09 meter
Z = -15383106
83 Z = -4710744
57
XDOT = 452
363214 XDOT = 231
513370
YDOT = -23618
123676 feet/sec YDOT = -7196
738872 meter/sec
ZDOT = -8877
719550 ZDOT = -2705
031217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12169765
51 X = -3709344
53
Y = -9997658
19 feet Y = -3047286
22 meter
Z = -15466307
49 Z = -4714130
52
XDOT = 19941
243259 XDOT = 6078
090945
YDOT = -10549
550109 feet/sec YDOT = -3215
502873 meter/sec
ZDOT = -8875
194203 ZDOT = -2705
159193
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 07271
83646707
00020000 00000-0 20000-3 0 9108
2 25544 51
6346 289
1404 0002383 51
7220 308
4157 15
75196030 27136
Satellite: ISS
Catalog Number: 25544
Epoch time: 07271
83646707 = yrday
fracday
Element set: 910
Inclination: 51
6346 deg
RA of node: 289
1404 deg
Eccentricity:
0002383
Arg of perigee: 51
7220 deg
Mean anomaly: 308
4157 deg
Mean motion: 15
75196030 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2713
Checksum: 276
Coasting Arc #12 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2007/272/19:34:52
106
Vector Time (MET): N/A
Weight (LBS) : 508517
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 96695
20 A = 6727136
62 meter
Y = 6422430
91 meter E =
0015596
Z = 1978012
98 I = 51
33545
XDOT = -5010
179868 Wp = 104
76078
YDOT = 1800
796256 meter/sec RA = 283
40213 deg
ZDOT = -5569
483421 TA = 53
09576
MA = 52
95295
Ha = 189
044 n
mi
Hp = 181
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 317241
47 X = 15262
38
Y = 21070967
55 feet Y = 6423056
95 meter
Z = 6489543
89 Z = 1978284
76
XDOT = -16437
597992 XDOT = -5002
888118
YDOT = 5908
124198 feet/sec YDOT = 1744
810212 meter/sec
ZDOT = -18272
583403 ZDOT = -5593
805757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17885684
39 X = -5451556
60
Y = 11142936
64 feet Y = 3396367
09 meter
Z = 6491359
84 Z = 1978566
48
XDOT = -12695
263693 XDOT = -3869
516374
YDOT = -9616
604478 feet/sec YDOT = -2931
141045 meter/sec
ZDOT = -18364
687040 ZDOT = -5597
556610
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 07272
85153446
00020000 00000-0 20000-3 0 9115
2 25544 51
6343 283
9172 0002343 57
5205 302
6185 15
75175113 27293
Satellite: ISS
Catalog Number: 25544
Epoch time: 07272
85153446 = yrday
fracday
Element set: 911
Inclination: 51
6343 deg
RA of node: 283
9172 deg
Eccentricity:
0002343
Arg of perigee: 57
5205 deg
Mean anomaly: 302
6185 deg
Mean motion: 15
75175113 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2729
Checksum: 280
Coasting Arc #13 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2007/273/19:34:52
106
Vector Time (MET): N/A
Weight (LBS) : 508517
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4251193
65 A = 6717717
98 meter
Y = -1443890
55 meter E =
0006774
Z = 4991958
24 I = 51
29935
XDOT = 391
462902 Wp = 106
42463
YDOT = 7477
725324 meter/sec RA = 278
26703 deg
ZDOT = 1825
572658 TA = 325
88531
MA = 325
92883
Ha = 188
858 n
mi
Hp = 181
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13947485
74 X = 4242772
98
Y = -4737173
73 feet Y = -1396398
38 meter
Z = 16377815
75 Z = 5012590
49
XDOT = 1284
327107 XDOT = 298
948286
YDOT = 24533
219567 feet/sec YDOT = 7481
585609 meter/sec
ZDOT = 5989
411608 ZDOT = 1827
249696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11382985
63 X = 3469534
02
Y = 9210592
38 feet Y = 2807388
56 meter
Z = 16455960
87 Z = 5015776
87
XDOT = -19435
163025 XDOT = -5923
837690
YDOT = 13282
250679 feet/sec YDOT = 4048
430007 meter/sec
ZDOT = 5996
688742 ZDOT = 1827
790729
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 07273
86658725
00020000 00000-0 20000-3 0 9128
2 25544 51
6349 278
6939 0002345 58
4800 301
6592 15
75223898 27457
Satellite: ISS
Catalog Number: 25544
Epoch time: 07273
86658725 = yrday
fracday
Element set: 912
Inclination: 51
6349 deg
RA of node: 278
6939 deg
Eccentricity:
0002345
Arg of perigee: 58
4800 deg
Mean anomaly: 301
6592 deg
Mean motion: 15
75223898 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2745
Checksum: 327
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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