Date:
May 3rd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5812 51 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
There are no maneuvers
Coasting Arc #1 (Orbit 355)
---------------------------------------
Vector Time (GMT): 2007/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -106239
78 A = 6710782
16 meter
Y = -4330968
38 meter E =
0023199
Z = -5144866
08 I = 51
50201
XDOT = 7392
011364 Wp = 115
42293
YDOT = -1695
813549 meter/sec RA = 339
42787 deg
ZDOT = 1269
556854 TA = 166
78596
MA = 166
72509
Ha = 188
117 n
mi
Hp = 175
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -348555
70 X = -32809
01
Y = -14209213
86 feet Y = -4331745
59 meter
Z = -16879481
89 Z = -5145204
05
XDOT = 24252
005786 XDOT = 7404
257394
YDOT = -5563
692745 feet/sec YDOT = -1613
083529 meter/sec
ZDOT = 4165
212774 ZDOT = 1305
497669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9194676
96 X = -2802537
54
Y = -10836099
84 feet Y = -3302843
23 meter
Z = -16881262
22 Z = -5145408
73
XDOT = 14438
330121 XDOT = 4400
803021
YDOT = -18977
991768 feet/sec YDOT = -5784
491891 meter/sec
ZDOT = 4300
373967 ZDOT = 1310
753985
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 07122
51366528
00020000 00000-0 20000-3 0 9007
2 25544 51
6338 339
8656 0010307 137
7825 222
4136 15
77480189 3566
Satellite: ISS
Catalog Number: 25544
Epoch time: 07122
51366528 = yrday
fracday
Element set: 900
Inclination: 51
6338 deg
RA of node: 339
8656 deg
Eccentricity:
0010307
Arg of perigee: 137
7825 deg
Mean anomaly: 222
4136 deg
Mean motion: 15
77480189 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 356
Checksum: 295
Coasting Arc #2 (Orbit 371)
---------------------------------------
Vector Time (GMT): 2007/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6247695
03 A = 6720029
56 meter
Y = 1036970
12 meter E =
0016157
Z = -2233626
31 I = 51
50650
XDOT = 1056
371923 Wp = 139
65726
YDOT = -5331
438842 meter/sec RA = 334
28762 deg
ZDOT = -5463
970306 TA = 65
49086
MA = 65
32248
Ha = 187
944 n
mi
Hp = 175
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20497687
12 X = -6247975
46
Y = 3402132
94 feet Y = 967103
49 meter
Z = -7328170
30 Z = -2263978
86
XDOT = 3465
787148 XDOT = 1142
453869
YDOT = -17491
597251 feet/sec YDOT = -5319
144195 meter/sec
ZDOT = -17926
411765 ZDOT = -5458
629632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13407861
77 X = -4086716
27
Y = 15819994
28 feet Y = 4821934
26 meter
Z = -7442364
50 Z = -2268432
70
XDOT = -7433
470389 XDOT = -2265
721774
YDOT = -14672
465203 feet/sec YDOT = -4472
167394 meter/sec
ZDOT = -17906
917997 ZDOT = -5458
028606
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 07123
52725057
00020000 00000-0 20000-3 0 9016
2 25544 51
6333 334
6330 0010248 142
3074 217
8810 15
77483920 3726
Satellite: ISS
Catalog Number: 25544
Epoch time: 07123
52725057 = yrday
fracday
Element set: 901
Inclination: 51
6333 deg
RA of node: 334
6330 deg
Eccentricity:
0010248
Arg of perigee: 142
3074 deg
Mean anomaly: 217
8810 deg
Mean motion: 15
77483920 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 372
Checksum: 264
Coasting Arc #3 (Orbit 387)
---------------------------------------
Vector Time (GMT): 2007/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1841421
77 A = 6714586
30 meter
Y = 4944115
74 meter E =
0016674
Z = 4136169
62 I = 51
46347
XDOT = -6741
354569 Wp = 109
62493
YDOT = 596
773832 meter/sec RA = 329
06717 deg
ZDOT = -3708
055175 TA = 18
30556
MA = 18
24562
Ha = 187
772 n
mi
Hp = 175
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6041409
99 X = -1916663
87
Y = 16220852
18 feet Y = 4923102
85 meter
Z = 13570110
32 Z = 4127041
52
XDOT = -22117
305018 XDOT = -6729
513341
YDOT = 1957
919396 feet/sec YDOT = 521
454784 meter/sec
ZDOT = -12165
535351 ZDOT = -3740
776487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6099154
07 X = 1859022
16
Y = 16227488
81 feet Y = 4946138
59 meter
Z = 13536303
06 Z = 4125865
17
XDOT = -14100
034904 XDOT = -4297
690639
YDOT = 15568
219467 feet/sec YDOT = 4745
193294 meter/sec
ZDOT = -12288
706098 ZDOT = -3745
597619
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 07124
54081213
00020000 00000-0 20000-3 0 9029
2 25544 51
6334 329
3988 0010066 146
2682 213
9126 15
77567405 3888
Satellite: ISS
Catalog Number: 25544
Epoch time: 07124
54081213 = yrday
fracday
Element set: 902
Inclination: 51
6334 deg
RA of node: 329
3988 deg
Eccentricity:
0010066
Arg of perigee: 146
2682 deg
Mean anomaly: 213
9126 deg
Mean motion: 15
77567405 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 388
Checksum: 289
Coasting Arc #4 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2007/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5339467
89 A = 6714747
15 meter
Y = 120227
19 meter E =
0018980
Z = 4064438
90 I = 51
43888
XDOT = -3048
232483 Wp = 126
03341
YDOT = 5971
078801 meter/sec RA = 323
94119 deg
ZDOT = 3804
493403 TA = 284
72391
MA = 284
93418
Ha = 187
618 n
mi
Hp = 175
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17517939
28 X = 5317982
03
Y = 394446
15 feet Y = 179815
53 meter
Z = 13334773
29 Z = 4090326
27
XDOT = -10000
762740 XDOT = -3133
257232
YDOT = 19590
153545 feet/sec YDOT = 5936
515944 meter/sec
ZDOT = 12481
933738 ZDOT = 3789
478980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13177694
15 X = 4016561
18
Y = -11435552
54 feet Y = -3485556
42 meter
Z = 13432292
36 Z = 4094162
71
XDOT = 4882
337307 XDOT = 1488
136411
YDOT = 20311
244246 feet/sec YDOT = 6190
867246 meter/sec
ZDOT = 12426
070803 ZDOT = 3787
466381
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 07125
55435441
00020000 00000-0 20000-3 0 9038
2 25544 51
6321 324
1646 0010057 150
0455 210
1287 15
77560245 4040
Satellite: ISS
Catalog Number: 25544
Epoch time: 07125
55435441 = yrday
fracday
Element set: 903
Inclination: 51
6321 deg
RA of node: 324
1646 deg
Eccentricity:
0010057
Arg of perigee: 150
0455 deg
Mean anomaly: 210
1287 deg
Mean motion: 15
77560245 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 404
Checksum: 250
Coasting Arc #5 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2007/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3333045
60 A = 6719653
04 meter
Y = -5368549
77 meter E =
0009869
Z = -2301426
69 I = 51
43261
XDOT = 5375
104072 Wp = 119
42527
YDOT = 1022
666657 meter/sec RA = 318
71590 deg
ZDOT = 5411
543559 TA = 214
61856
MA = 214
68284
Ha = 187
577 n
mi
Hp = 175
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10935188
98 X = 3404009
83
Y = -17613352
26 feet Y = -5330880
73 meter
Z = -7550612
49 Z = -2285062
82
XDOT = 17634
855880 XDOT = 5336
980372
YDOT = 3355
205568 feet/sec YDOT = 1082
560287 meter/sec
ZDOT = 17754
408003 ZDOT = 5437
563637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4066538
30 X = -1239480
87
Y = -20351646
92 feet Y = -6203181
98 meter
Z = -7489594
03 Z = -2282828
26
XDOT = 13590
155466 XDOT = 4142
279386
YDOT = -9270
038310 feet/sec YDOT = -2825
507677 meter/sec
ZDOT = 17852
536367 ZDOT = 5441
453085
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 07126
50452843
00020000 00000-0 20000-3 0 9040
2 25544 51
6315 319
2570 0010177 153
9191 206
2489 15
77605702 4190
Satellite: ISS
Catalog Number: 25544
Epoch time: 07126
50452843 = yrday
fracday
Element set: 904
Inclination: 51
6315 deg
RA of node: 319
2570 deg
Eccentricity:
0010177
Arg of perigee: 153
9191 deg
Mean anomaly: 206
2489 deg
Mean motion: 15
77605702 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 419
Checksum: 282
Coasting Arc #6 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2007/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3966007
92 A = 6710293
10 meter
Y = -1774285
65 meter E =
0019269
Z = -5127928
87 I = 51
38010
XDOT = 4424
368425 Wp = 110
93491
YDOT = -6159
730467 meter/sec RA = 313
56698 deg
ZDOT = -1301
279499 TA = 146
62551
MA = 146
50390
Ha = 187
417 n
mi
Hp = 175
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13011837
02 X = -3920962
11
Y = -5821147
15 feet Y = -1818383
32 meter
Z = -16823913
60 Z = -5147086
66
XDOT = 14515
644438 XDOT = 4499
240021
YDOT = -20209
089458 feet/sec YDOT = -6109
835924 meter/sec
ZDOT = -4269
289695 ZDOT = -1279
604602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13317621
54 X = -4059211
04
Y = 4836757
35 feet Y = 1474243
64 meter
Z = -16896285
40 Z = -5149987
79
XDOT = -3320
618621 XDOT = -1012
124556
YDOT = -23652
073533 feet/sec YDOT = -7209
152013 meter/sec
ZDOT = -4188
355112 ZDOT = -1276
610638
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 07127
51802660
00020000 00000-0 20000-3 0 9059
2 25544 51
6309 314
0228 0010179 157
3189 202
8427 15
77637021 4354
Satellite: ISS
Catalog Number: 25544
Epoch time: 07127
51802660 = yrday
fracday
Element set: 905
Inclination: 51
6309 deg
RA of node: 314
0228 deg
Eccentricity:
0010179
Arg of perigee: 157
3189 deg
Mean anomaly: 202
8427 deg
Mean motion: 15
77637021 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 435
Checksum: 275
Coasting Arc #7 (Orbit 450)
---------------------------------------
Vector Time (GMT): 2007/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4222077
73 A = 6721639
18 meter
Y = 5214003
70 meter E =
0021415
Z = -91476
47 I = 51
40073
XDOT = -3694
718074 Wp = 146
93446
YDOT = -3085
699516 meter/sec RA = 308
37545 deg
ZDOT = -6028
231258 TA = 34
06509
MA = 33
92782
Ha = 187
101 n
mi
Hp = 176
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13851961
06 X = -4279623
31
Y = 17106311
35 feet Y = 5166468
32 meter
Z = -300119
65 Z = -112126
64
XDOT = -12121
778459 XDOT = -3630
654570
YDOT = -10123
686076 feet/sec YDOT = -3126
657099 meter/sec
ZDOT = -19777
661609 ZDOT = -6046
024978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2380165
27 X = 725474
37
Y = 21881161
76 feet Y = 6669378
11 meter
Z = -377303
93 Z = -115002
24
XDOT = -14051
232291 XDOT = -4282
815602
YDOT = 1216
744383 feet/sec YDOT = 370
863688 meter/sec
ZDOT = -19845
052975 ZDOT = -6048
772147
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 07128
53150095
00020000 00000-0 20000-3 0 9061
2 25544 51
6314 308
7888 0009887 161
2780 198
8750 15
77711924 4513
Satellite: ISS
Catalog Number: 25544
Epoch time: 07128
53150095 = yrday
fracday
Element set: 906
Inclination: 51
6314 deg
RA of node: 308
7888 deg
Eccentricity:
0009887
Arg of perigee: 161
2780 deg
Mean anomaly: 198
8750 deg
Mean motion: 15
77711924 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 451
Checksum: 316
Coasting Arc #8 (Orbit 466)
---------------------------------------
Vector Time (GMT): 2007/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2486795
48 A = 6710404
44 meter
Y = 3611109
74 meter E =
0009553
Z = 5072760
90 I = 51
34479
XDOT = -5090
193618 Wp = 137
08760
YDOT = 5599
010647 meter/sec RA = 303
17821 deg
ZDOT = -1495
649043 TA = 327
25987
MA = 327
31903
Ha = 187
109 n
mi
Hp = 176
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8158777
83 X = 2421588
11
Y = 11847472
91 feet Y = 3638553
45 meter
Z = 16642916
32 Z = 5084683
70
XDOT = -16700
110294 XDOT = -5145
158647
YDOT = 18369
457503 feet/sec YDOT = 5541
782055 meter/sec
ZDOT = -4906
985050 ZDOT = -1520
510277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14133173
79 X = 4307791
37
Y = 2381253
50 feet Y = 725806
07 meter
Z = 16688258
28 Z = 5086581
12
XDOT = 1887
484727 XDOT = 575
305345
YDOT = 23717
565139 feet/sec YDOT = 7229
113854 meter/sec
ZDOT = -4999
986480 ZDOT = -1523
995879
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 07129
54495597
00020000 00000-0 20000-3 0 9073
2 25544 51
6306 303
5544 0010139 165
1964 194
9499 15
77674350 4670
Satellite: ISS
Catalog Number: 25544
Epoch time: 07129
54495597 = yrday
fracday
Element set: 907
Inclination: 51
6306 deg
RA of node: 303
5544 deg
Eccentricity:
0010139
Arg of perigee: 165
1964 deg
Mean anomaly: 194
9499 deg
Mean motion: 15
77674350 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 467
Checksum: 325
Coasting Arc #9 (Orbit 482)
---------------------------------------
Vector Time (GMT): 2007/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4523262
31 A = 6718849
23 meter
Y = -4316187
11 meter E =
0016667
Z = 2457486
09 I = 51
35931
XDOT = 2047
749508 Wp = 112
55985
YDOT = 5190
152740 meter/sec RA = 298
02734 deg
ZDOT = 5311
647193 TA = 275
36744
MA = 275
55757
Ha = 186
965 n
mi
Hp = 176
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14840099
44 X = 4559252
31
Y = -14160718
86 feet Y = -4265404
39 meter
Z = 8062618
42 Z = 2479547
28
XDOT = 6718
338280 XDOT = 1963
757193
YDOT = 17028
060172 feet/sec YDOT = 5212
581841 meter/sec
ZDOT = 17426
664018 ZDOT = 5321
391515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -328825
71 X = -100226
08
Y = -20477001
64 feet Y = -6241390
10 meter
Z = 8145219
64 Z = 2482662
95
XDOT = 15496
292371 XDOT = 4723
269915
YDOT = 6743
013270 feet/sec YDOT = 2055
270445 meter/sec
ZDOT = 17463
992035 ZDOT = 5323
024772
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 07130
55838560
00020000 00000-0 20000-3 0 9088
2 25544 51
6305 298
3195 0010139 169
2664 190
8719 15
77748939 4837
Satellite: ISS
Catalog Number: 25544
Epoch time: 07130
55838560 = yrday
fracday
Element set: 908
Inclination: 51
6305 deg
RA of node: 298
3195 deg
Eccentricity:
0010139
Arg of perigee: 169
2664 deg
Mean anomaly: 190
8719 deg
Mean motion: 15
77748939 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 483
Checksum: 327
Coasting Arc #10 (Orbit 497)
---------------------------------------
Vector Time (GMT): 2007/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1140818
94 A = 6714780
27 meter
Y = -5352988
11 meter E =
0014321
Z = -3906048
31 I = 51
33407
XDOT = 5178
344502 Wp = 146
79974
YDOT = -4035
083621 meter/sec RA = 292
79335 deg
ZDOT = 4012
535990 TA = 165
12826
MA = 165
08610
Ha = 186
841 n
mi
Hp = 176
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3742844
30 X = -1061901
29
Y = -17562296
95 feet Y = -5365303
94 meter
Z = -12815119
12 Z = -3911399
01
XDOT = 16989
319231 XDOT = 5203
588255
YDOT = -13238
463324 feet/sec YDOT = -3977
035524 meter/sec
ZDOT = 13164
488157 ZDOT = 4037
753632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15532984
56 X = -4734453
69
Y = -8979753
93 feet Y = -2737029
00 meter
Z = -12835920
13 Z = -3912388
46
XDOT = 765
866915 XDOT = 233
436236
YDOT = -20300
419934 feet/sec YDOT = -6187
567996 meter/sec
ZDOT = 13259
011531 ZDOT = 4041
346715
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 07131
50845666
00020000 00000-0 20000-3 0 9090
2 25544 51
6311 293
4119 0010138 172
2926 187
8397 15
77777064 4985
Satellite: ISS
Catalog Number: 25544
Epoch time: 07131
50845666 = yrday
fracday
Element set: 909
Inclination: 51
6311 deg
RA of node: 293
4119 deg
Eccentricity:
0010138
Arg of perigee: 172
2926 deg
Mean anomaly: 187
8397 deg
Mean motion: 15
77777064 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 498
Checksum: 317
Coasting Arc #11 (Orbit 513)
---------------------------------------
Vector Time (GMT): 2007/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4454657
78 A = 6712975
99 meter
Y = 2524118
57 meter E =
0011454
Z = -4345650
76 I = 51
31875
XDOT = -634
692520 Wp = 125
65069
YDOT = -6897
801657 meter/sec RA = 287
65695 deg
ZDOT = -3368
680833 TA = 110
33859
MA = 110
21548
Ha = 186
531 n
mi
Hp = 176
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14615018
97 X = -4461441
17
Y = 8281228
91 feet Y = 2474266
33 meter
Z = -14257384
37 Z = -4367308
07
XDOT = -2082
324540 XDOT = -541
148529
YDOT = -22630
582864 feet/sec YDOT = -6904
375983 meter/sec
ZDOT = -11052
102471 ZDOT = -3371
537247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3244235
75 X = -988843
06
Y = 16411212
90 feet Y = 5002137
69 meter
Z = -14338673
80 Z = -4370427
77
XDOT = -17242
208174 XDOT = -5255
425052
YDOT = -13038
541904 feet/sec YDOT = -3974
147572 meter/sec
ZDOT = -11063
697351 ZDOT = -3372
214952
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 07132
52184304
00020000 00000-0 20000-3 0 9100
2 25544 51
6313 288
1777 0009978 176
0213 184
1033 15
77822409 5149
Satellite: ISS
Catalog Number: 25544
Epoch time: 07132
52184304 = yrday
fracday
Element set: 910
Inclination: 51
6313 deg
RA of node: 288
1777 deg
Eccentricity:
0009978
Arg of perigee: 176
0213 deg
Mean anomaly: 184
1033 deg
Mean motion: 15
77822409 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 514
Checksum: 281
Coasting Arc #12 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2007/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 45484
96 A = 6719874
13 meter
Y = 6462540
31 meter E =
0020344
Z = 1793497
26 I = 51
33385
XDOT = -4992
157530 Wp = 140
95310
YDOT = 1611
030798 meter/sec RA = 282
42695 deg
ZDOT = -5659
354632 TA = 19
01880
MA = 18
94294
Ha = 186
403 n
mi
Hp = 176
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 149228
87 X = -35496
10
Y = 21202560
06 feet Y = 6462596
08 meter
Z = 5884177
35 Z = 1793521
79
XDOT = -16378
469586 XDOT = -4982
308740
YDOT = 5285
534113 feet/sec YDOT = 1555
260995 meter/sec
ZDOT = -18567
436457 ZDOT = -5683
582914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16347885
42 X = 4982835
48
Y = 13502116
85 feet Y = 4115445
22 meter
Z = 5885052
94 Z = 1793764
14
XDOT = -5391
081335 XDOT = -1643
201591
YDOT = 14687
163215 feet/sec YDOT = 4476
647348 meter/sec
ZDOT = -18658
521883 ZDOT = -5687
117470
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 07133
53520673
00020000 00000-0 20000-3 0 9116
2 25544 51
6305 282
9419 0009983 180
7132 179
4021 15
77840066 5304
Satellite: ISS
Catalog Number: 25544
Epoch time: 07133
53520673 = yrday
fracday
Element set: 911
Inclination: 51
6305 deg
RA of node: 282
9419 deg
Eccentricity:
0009983
Arg of perigee: 180
7132 deg
Mean anomaly: 179
4021 deg
Mean motion: 15
77840066 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 530
Checksum: 282
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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