Date:
January 24th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6565 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
032/20:36:28
062 -2
1 6
4 6
4
N/A 4
8 -0
1 191
5
000/00:08:52
124 3
6 -0
0 176
2
Coasting Arc #1 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2007/024/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5071727
14 A = 6715075
52 meter
Y = 1557297
79 meter E =
0032578
Z = 4103775
40 I = 51
88931
XDOT = 1072
799068 Wp = 120
54101
YDOT = -6625
194545 meter/sec RA = 125
57662 deg
ZDOT = 3801
536700 TA = 290
50049
MA = 290
84987
Ha = 192
815 n
mi
Hp = 171
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16639524
73 X = -5108699
23
Y = 5109244
70 feet Y = 1500376
09 meter
Z = 13463830
07 Z = 4079047
55
XDOT = 3519
681983 XDOT = 1128
336293
YDOT = -21736
202574 feet/sec YDOT = -6612
887471 meter/sec
ZDOT = 12472
233267 ZDOT = 3806
883026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14265909
00 X = -4348249
06
Y = -10096844
97 feet Y = -3077518
35 meter
Z = 13371254
49 Z = 4075558
37
XDOT = 18569
531135 XDOT = 5659
993090
YDOT = -9526
519842 feet/sec YDOT = -2903
683248 meter/sec
ZDOT = 12491
428051 ZDOT = 3807
387270
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 07024
56829726
00020000 00000-0 20000-3 0 9007
2 25544 51
6345 126
1471 0022622 128
2207 232
0999 15
77466206 28091
Satellite: ISS
Catalog Number: 25544
Epoch time: 07024
56829726 = yrday
fracday
Element set: 900
Inclination: 51
6345 deg
RA of node: 126
1471 deg
Eccentricity:
0022622
Arg of perigee: 128
2207 deg
Mean anomaly: 232
0999 deg
Mean motion: 15
77466206 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2809
Checksum: 290
Coasting Arc #2 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2007/025/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1476923
52 A = 6719987
24 meter
Y = 6138807
90 meter E =
0023488
Z = -2337292
12 I = 51
92134
XDOT = -5383
024240 Wp = 117
54061
YDOT = 762
296879 meter/sec RA = 120
38756 deg
ZDOT = 5434
491774 TA = 216
29041
MA = 216
44994
Ha = 192
623 n
mi
Hp = 171
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4845549
60 X = -1534104
75
Y = 20140445
87 feet Y = 6121972
50 meter
Z = -7668281
23 Z = -2344605
57
XDOT = -17660
840683 XDOT = -5417
547758
YDOT = 2500
974013 feet/sec YDOT = 701
907647 meter/sec
ZDOT = 17829
697422 ZDOT = 5408
257510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18721396
97 X = -5706281
80
Y = 8844027
69 feet Y = 2695659
64 meter
Z = -7694928
05 Z = -2345414
07
XDOT = -12410
639448 XDOT = -3782
762904
YDOT = -10931
545515 feet/sec YDOT = -3331
935073 meter/sec
ZDOT = 17731
359996 ZDOT = 5404
518527
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 07025
51855319
00020000 00000-0 20000-3 0 9011
2 25544 51
6344 121
2420 0022398 131
4260 228
8834 15
77442595 28248
Satellite: ISS
Catalog Number: 25544
Epoch time: 07025
51855319 = yrday
fracday
Element set: 901
Inclination: 51
6344 deg
RA of node: 121
2420 deg
Eccentricity:
0022398
Arg of perigee: 131
4260 deg
Mean anomaly: 228
8834 deg
Mean motion: 15
77442595 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2824
Checksum: 281
Coasting Arc #3 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2007/026/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4303832
33 A = 6710850
79 meter
Y = 358230
26 meter E =
0032456
Z = -5159086
12 I = 51
90347
XDOT = -2223
473545 Wp = 114
47100
YDOT = 7229
346632 meter/sec RA = 115
27639 deg
ZDOT = -1372
738275 TA = 142
52686
MA = 142
30015
Ha = 192
534 n
mi
Hp = 171
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14120184
80 X = 4324568
33
Y = 1175296
11 feet Y = 406474
39 meter
Z = -16926135
58 Z = -5138127
93
XDOT = -7294
860712 XDOT = -2297
479426
YDOT = 23718
328846 feet/sec YDOT = 7204
068816 meter/sec
ZDOT = -4503
734498 ZDOT = -1383
719077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8171909
49 X = 2490798
01
Y = 11689247
08 feet Y = 3562882
51 meter
Z = -16847445
00 Z = -5135101
24
XDOT = -22042
754771 XDOT = -6718
631654
YDOT = 8955
109497 feet/sec YDOT = 2729
517375 meter/sec
ZDOT = -4544
012965 ZDOT = -1385
015152
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 07026
53213862
00020000 00000-0 20000-3 0 9026
2 25544 51
6339 116
0087 0022392 135
4331 224
8639 15
77474383 28407
Satellite: ISS
Catalog Number: 25544
Epoch time: 07026
53213862 = yrday
fracday
Element set: 902
Inclination: 51
6339 deg
RA of node: 116
0087 deg
Eccentricity:
0022392
Arg of perigee: 135
4331 deg
Mean anomaly: 224
8639 deg
Mean motion: 15
77474383 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2840
Checksum: 285
Coasting Arc #4 (Orbit 2855)
---------------------------------------
Vector Time (GMT): 2007/027/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2299335
20 A = 6722204
25 meter
Y = -6298342
35 meter E =
0034792
Z = 10046
98 I = 51
95295
XDOT = 4478
829272 Wp = 137
34876
YDOT = 1606
103728 meter/sec RA = 110
12281 deg
ZDOT = -6079
644639 TA = 42
54221
MA = 42
27317
Ha = 192
427 n
mi
Hp = 171
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7543750
65 X = 2369544
46
Y = -20663852
84 feet Y = -6272237
34 meter
Z = 32962
54 Z = 21386
98
XDOT = 14694
321760 XDOT = 4490
070175
YDOT = 5269
369186 feet/sec YDOT = 1656
251892 meter/sec
ZDOT = -19946
340678 ZDOT = -6057
859297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20589087
69 X = 6275553
93
Y = -7745189
45 feet Y = -2360733
74 meter
Z = 74720
18 Z = 22774
71
XDOT = 5086
819094 XDOT = 1550
462460
YDOT = 13161
891905 feet/sec YDOT = 4011
744653 meter/sec
ZDOT = -19864
381274 ZDOT = -6054
663412
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 07027
54570423
00020000 00000-0 20000-3 0 9038
2 25544 51
6336 110
7758 0022471 138
8105 221
4761 15
77516989 28569
Satellite: ISS
Catalog Number: 25544
Epoch time: 07027
54570423 = yrday
fracday
Element set: 903
Inclination: 51
6336 deg
RA of node: 110
7758 deg
Eccentricity:
0022471
Arg of perigee: 138
8105 deg
Mean anomaly: 221
4761 deg
Mean motion: 15
77516989 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2856
Checksum: 299
Coasting Arc #5 (Orbit 2871)
---------------------------------------
Vector Time (GMT): 2007/028/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3522875
58 A = 6710392
51 meter
Y = -2437480
25 meter E =
0022749
Z = 5147751
14 I = 51
92339
XDOT = 2944
975592 Wp = 132
06476
YDOT = -7016
124350 meter/sec RA = 104
97053 deg
ZDOT = -1318
030642 TA = 330
39312
MA = 330
52172
Ha = 192
245 n
mi
Hp = 171
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11557990
76 X = -3520363
95
Y = -7996982
46 feet Y = -2476861
52 meter
Z = 16888947
30 Z = 5130643
12
XDOT = 9661
993413 XDOT = 3029
614665
YDOT = -23018
780676 feet/sec YDOT = -6982
718612 meter/sec
ZDOT = -4324
247514 ZDOT = -1303
519343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1769252
01 X = -539268
01
Y = -14020829
73 feet Y = -4273548
90 meter
Z = 16824431
66 Z = 5128086
77
XDOT = 22613
827731 XDOT = 6892
694693
YDOT = -7933
671804 feet/sec YDOT = -2418
183166 meter/sec
ZDOT = -4270
666393 ZDOT = -1301
699116
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 07028
55924697
00020000 00000-0 20000-3 0 9047
2 25544 51
6344 105
5428 0022202 142
8252 217
4456 15
77600227 28727
Satellite: ISS
Catalog Number: 25544
Epoch time: 07028
55924697 = yrday
fracday
Element set: 904
Inclination: 51
6344 deg
RA of node: 105
5428 deg
Eccentricity:
0022202
Arg of perigee: 142
8252 deg
Mean anomaly: 217
4456 deg
Mean motion: 15
77600227 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2872
Checksum: 286
Coasting Arc #6 (Orbit 2887)
---------------------------------------
Vector Time (GMT): 2007/029/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2787539
44 A = 6719776
60 meter
Y = 5679796
09 meter E =
0029446
Z = 2267023
09 I = 51
96064
XDOT = -3650
349601 Wp = 118
64307
YDOT = -4002
724984 meter/sec RA = 99
86045 deg
ZDOT = 5472
814516 TA = 266
71569
MA = 267
05261
Ha = 192
103 n
mi
Hp = 171
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9145470
60 X = -2861857
10
Y = 18634501
62 feet Y = 5648208
49 meter
Z = 7437739
80 Z = 2253301
63
XDOT = -11976
212601 XDOT = -3631
904632
YDOT = -13132
299815 feet/sec YDOT = -4043
442705 meter/sec
ZDOT = 17955
428202 ZDOT = 5455
125852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19930757
08 X = -6074894
76
Y = 5865340
59 feet Y = 1787755
81 meter
Z = 7386945
13 Z = 2251540
88
XDOT = 1907
805168 XDOT = 581
499015
YDOT = -16325
661392 feet/sec YDOT = -4976
061592 meter/sec
ZDOT = 17888
532315 ZDOT = 5452
424650
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 07029
57277327
00020000 00000-0 20000-3 0 9052
2 25544 51
6340 100
3099 0022268 146
0913 214
1680 15
77591710 28888
Satellite: ISS
Catalog Number: 25544
Epoch time: 07029
57277327 = yrday
fracday
Element set: 905
Inclination: 51
6340 deg
RA of node: 100
3099 deg
Eccentricity:
0022268
Arg of perigee: 146
0913 deg
Mean anomaly: 214
1680 deg
Mean motion: 15
77591710 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2888
Checksum: 292
Coasting Arc #7 (Orbit 2902)
---------------------------------------
Vector Time (GMT): 2007/030/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2874513
29 A = 6714492
78 meter
Y = 4477838
12 meter E =
0028562
Z = -4126029
14 I = 51
94660
XDOT = -3449
842568 Wp = 139
40128
YDOT = 5719
443103 meter/sec RA = 94
67358 deg
ZDOT = 3797
144182 TA = 169
50357
MA = 169
44381
Ha = 191
911 n
mi
Hp = 171
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9430817
88 X = 2844270
79
Y = 14691069
95 feet Y = 4509813
87 meter
Z = -13536841
02 Z = -4112138
12
XDOT = -11318
381127 XDOT = -3531
987137
YDOT = 18764
577108 feet/sec YDOT = 5680
405351 meter/sec
ZDOT = 12457
822119 ZDOT = 3780
186369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4075472
11 X = -1242203
90
Y = 17017124
12 feet Y = 5186819
43 meter
Z = -13484136
64 Z = -4109964
85
XDOT = -20198
583049 XDOT = -6156
528113
YDOT = 5001
197673 feet/sec YDOT = 1524
365051 meter/sec
ZDOT = 12394
875665 ZDOT = 3777
958103
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 07030
52293499
00020000 00000-0 20000-3 0 9068
2 25544 51
6337 95
4035 0022236 149
2941 210
9530 15
77643840 29037
Satellite: ISS
Catalog Number: 25544
Epoch time: 07030
52293499 = yrday
fracday
Element set: 906
Inclination: 51
6337 deg
RA of node: 95
4035 deg
Eccentricity:
0022236
Arg of perigee: 149
2941 deg
Mean anomaly: 210
9530 deg
Mean motion: 15
77643840 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2903
Checksum: 287
Coasting Arc #8 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2007/031/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3252974
76 A = 6714220
69 meter
Y = -4116059
83 meter E =
0024477
Z = -4193951
85 I = 51
94707
XDOT = 2946
040323 Wp = 133
91912
YDOT = 6074
877067 meter/sec RA = 89
58198 deg
ZDOT = -3706
868589 TA = 98
54435
MA = 98
26690
Ha = 191
858 n
mi
Hp = 172
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10672489
36 X = 3319132
18
Y = -13504133
30 feet Y = -4079312
98 meter
Z = -13759684
53 Z = -4177989
06
XDOT = 9665
486623 XDOT = 2895
897965
YDOT = 19930
699038 feet/sec YDOT = 6107
541296 meter/sec
ZDOT = -12161
642352 ZDOT = -3692
678431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17162110
23 X = 5231011
20
Y = -1832264
59 feet Y = -558474
25 meter
Z = -13700267
98 Z = -4175841
68
XDOT = -7486
255497 XDOT = -2281
810676
YDOT = 19674
682539 feet/sec YDOT = 5996
843238 meter/sec
ZDOT = -12107
610969 ZDOT = -3690
399823
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 07031
53642207
00020000 00000-0 20000-3 0 9076
2 25544 51
6341 90
1693 0022172 153
1634 207
0683 15
77638367 29197
Satellite: ISS
Catalog Number: 25544
Epoch time: 07031
53642207 = yrday
fracday
Element set: 907
Inclination: 51
6341 deg
RA of node: 90
1693 deg
Eccentricity:
0022172
Arg of perigee: 153
1634 deg
Mean anomaly: 207
0683 deg
Mean motion: 15
77638367 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2919
Checksum: 285
Coasting Arc #9 (Orbit 2934)
---------------------------------------
Vector Time (GMT): 2007/032/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2288391
87 A = 6719626
47 meter
Y = -5908108
31 meter E =
0033164
Z = 2173777
79 I = 51
96432
XDOT = 4003
508453 Wp = 138
37494
YDOT = -3598
519577 meter/sec RA = 84
39608 deg
ZDOT = -5542
419905 TA = 17
29275
MA = 17
18005
Ha = 191
577 n
mi
Hp = 172
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7507847
34 X = -2232715
95
Y = -19383557
44 feet Y = -5933387
22 meter
Z = 7131816
88 Z = 2162796
01
XDOT = 13134
870254 XDOT = 4070
373227
YDOT = -11806
166590 feet/sec YDOT = -3553
375899 meter/sec
ZDOT = -18183
792340 ZDOT = -5522
809339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8170216
38 X = 2490281
95
Y = -19129414
98 feet Y = -5830645
69 meter
Z = 7089846
93 Z = 2160985
34
XDOT = 16321
836940 XDOT = 4974
895899
YDOT = 230
223682 feet/sec YDOT = 70
172178 meter/sec
ZDOT = -18110
611717 ZDOT = -5520
114451
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 07032
54988809
00020000 00000-0 20000-3 0 9080
2 25544 51
6341 84
9359 0021964 156
7489 203
4675 15
77703729 29356
Satellite: ISS
Catalog Number: 25544
Epoch time: 07032
54988809 = yrday
fracday
Element set: 908
Inclination: 51
6341 deg
RA of node: 84
9359 deg
Eccentricity:
0021964
Arg of perigee: 156
7489 deg
Mean anomaly: 203
4675 deg
Mean motion: 15
77703729 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2935
Checksum: 338
Coasting Arc #10 (Orbit 2939)
---------------------------------------
Vector Time (GMT): 2007/032/20:40:54
124
Vector Time (MET): N/A
Weight (LBS) : 478859
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2668009
57 A = 6722590
76 meter
Y = 5676337
01 meter E =
0015486
Z = -2448132
03 I = 51
96136
XDOT = -3711
233929 Wp = 146
07775
YDOT = 4059
598357 meter/sec RA = 82
60623 deg
ZDOT = 5371
862625 TA = 186
42763
MA = 186
44752
Ha = 191
520 n
mi
Hp = 176
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8753312
24 X = 2616229
85
Y = 18623152
90 feet Y = 5705882
80 meter
Z = -8031929
24 Z = -2435296
74
XDOT = -12175
964333 XDOT = -3782
447754
YDOT = 13318
892248 feet/sec YDOT = 4017
698798 meter/sec
ZDOT = 17624
221212 ZDOT = 5353
661319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19753334
01 X = 6020816
21
Y = -5833631
57 feet Y = -1778090
90 meter
Z = -7983027
29 Z = -2433226
72
XDOT = 10850
611810 XDOT = 3307
266480
YDOT = 12732
956952 feet/sec YDOT = 3881
005279 meter/sec
ZDOT = 17556
388441 ZDOT = 5351
187197
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 07032
86659267
00020000 00000-0 20000-3 0 9099
2 25544 51
6340 83
3009 0017192 164
5110 195
6584 15
76463196 29403
Satellite: ISS
Catalog Number: 25544
Epoch time: 07032
86659267 = yrday
fracday
Element set: 909
Inclination: 51
6340 deg
RA of node: 83
3009 deg
Eccentricity:
0017192
Arg of perigee: 164
5110 deg
Mean anomaly: 195
6584 deg
Mean motion: 15
76463196 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2940
Checksum: 304
Coasting Arc #11 (Orbit 2955)
---------------------------------------
Vector Time (GMT): 2007/033/20:40:54
124
Vector Time (MET): N/A
Weight (LBS) : 478859
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3393563
67 A = 6714130
27 meter
Y = -2893966
60 meter E =
0021267
Z = -5028994
67 I = 51
92881
XDOT = 3030
645483 Wp = 129
45274
YDOT = 6815
757747 meter/sec RA = 77
50925 deg
ZDOT = -1895
580789 TA = 122
41848
MA = 122
21258
Ha = 191
381 n
mi
Hp = 176
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11133739
06 X = 3450101
31
Y = -9494641
07 feet Y = -2855701
61 meter
Z = -16499326
33 Z = -5012372
05
XDOT = 9943
062608 XDOT = 2963
413545
YDOT = 22361
409931 feet/sec YDOT = 6849
272258 meter/sec
ZDOT = -6219
097078 ZDOT = -1881
021515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7872867
59 X = -2399650
04
Y = -12416525
83 feet Y = -3784557
07 meter
Z = -16437273
68 Z = -5010081
02
XDOT = 22608
945384 XDOT = 6891
206553
YDOT = -6256
636323 feet/sec YDOT = -1907
022751 meter/sec
ZDOT = -6163
574600 ZDOT = -1878
657538
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 07033
88082752
00020000 00000-0 20000-3 0 9103
2 25544 51
6346 78
0719 0017122 168
1029 192
0543 15
76502918 29569
Satellite: ISS
Catalog Number: 25544
Epoch time: 07033
88082752 = yrday
fracday
Element set: 910
Inclination: 51
6346 deg
RA of node: 78
0719 deg
Eccentricity:
0017122
Arg of perigee: 168
1029 deg
Mean anomaly: 192
0543 deg
Mean motion: 15
76502918 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2956
Checksum: 294
Coasting Arc #12 (Orbit 2971)
---------------------------------------
Vector Time (GMT): 2007/034/20:40:54
124
Vector Time (MET): N/A
Weight (LBS) : 478859
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2627009
49 A = 6724832
92 meter
Y = -6114784
48 meter E =
0028389
Z = 830167
93 I = 51
95708
XDOT = 4106
356144 Wp = 151
88998
YDOT = -2586
993617 meter/sec RA = 72
35230 deg
ZDOT = -6003
105597 TA = 19
06726
MA = 18
96120
Ha = 191
274 n
mi
Hp = 176
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8618797
55 X = -2562470
54
Y = -20061628
86 feet Y = -6143800
31 meter
Z = 2723648
07 Z = 817563
05
XDOT = 13472
297062 XDOT = 4164
140156
YDOT = -8487
511868 feet/sec YDOT = -2540
750927 meter/sec
ZDOT = -19695
228337 ZDOT = -5983
017221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20949519
57 X = -6385413
57
Y = 6174945
33 feet Y = 1882123
34 meter
Z = 2675548
98 Z = 815507
33
XDOT = -6353
521488 XDOT = -1936
553349
YDOT = -12970
670666 feet/sec YDOT = -3953
460419 meter/sec
ZDOT = -19620
122645 ZDOT = -5980
213382
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 07034
89504557
00020000 00000-0 20000-3 0 9118
2 25544 51
6345 72
8432 0017195 172
0897 188
0547 15
76488225 29720
Satellite: ISS
Catalog Number: 25544
Epoch time: 07034
89504557 = yrday
fracday
Element set: 911
Inclination: 51
6345 deg
RA of node: 72
8432 deg
Eccentricity:
0017195
Arg of perigee: 172
0897 deg
Mean anomaly: 188
0547 deg
Mean motion: 15
76488225 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2972
Checksum: 320
Coasting Arc #13 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2007/035/20:40:54
124
Vector Time (MET): N/A
Weight (LBS) : 478859
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3815715
02 A = 6712758
98 meter
Y = 1605862
22 meter E =
0017320
Z = 5281151
74 I = 51
90732
XDOT = -2978
901049 Wp = 168
19875
YDOT = -7109
709539 meter/sec RA = 67
22585 deg
ZDOT = -7
025039 TA = 281
77048
MA = 281
96473
Ha = 191
005 n
mi
Hp = 176
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12518750
07 X = -3859042
57
Y = 5268576
83 feet Y = 1562950
56 meter
Z = 17326613
33 Z = 5262510
27
XDOT = -9773
297405 XDOT = -2899
143744
YDOT = -23325
818696 feet/sec YDOT = -7142
575326 meter/sec
ZDOT = -23
048028 ZDOT = -21
302330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3949161
96 X = 1203704
57
Y = 13087968
42 feet Y = 3989212
78 meter
Z = 17256817
11 Z = 5259877
86
XDOT = -23249
466955 XDOT = -7086
437528
YDOT = 7045
439120 feet/sec YDOT = 2147
449844 meter/sec
ZDOT = -77
553043 ZDOT = -23
638167
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 07035
90924296
00020000 00000-0 20000-3 0 9128
2 25544 51
6345 67
6144 0017032 176
3901 183
7389 15
76577572 29882
Satellite: ISS
Catalog Number: 25544
Epoch time: 07035
90924296 = yrday
fracday
Element set: 912
Inclination: 51
6345 deg
RA of node: 67
6144 deg
Eccentricity:
0017032
Arg of perigee: 176
3901 deg
Mean anomaly: 183
7389 deg
Mean motion: 15
76577572 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2988
Checksum: 322
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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