Date:
January 11th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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 2586)
---------------------------------------
Vector Time (GMT): 2007/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6522854
22 A = 6723556
99 meter
Y = -1303803
91 meter E =
0031569
Z = -941464
68 I = 51
55132
XDOT = 147
322560 Wp = 65
18157
YDOT = -4905
571444 meter/sec RA = 197
75564 deg
ZDOT = 5940
776583 TA = 284
51061
MA = 284
86062
Ha = 193
975 n
mi
Hp = 171
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21400440
36 X = -6503216
69
Y = -4277571
88 feet Y = -1376636
24 meter
Z = -3088794
87 Z = -973104
76
XDOT = 483
341732 XDOT = 173
307486
YDOT = -16094
394502 feet/sec YDOT = -4903
779098 meter/sec
ZDOT = 19490
736821 ZDOT = 5941
555067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2879783
97 X = -877758
15
Y = -21615638
17 feet Y = -6588446
51 meter
Z = -3207515
14 Z = -977650
62
XDOT = 13771
993619 XDOT = 4197
703655
YDOT = -4648
617060 feet/sec YDOT = -1416
898480 meter/sec
ZDOT = 19493
015499 ZDOT = 5941
471124
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 07010
50188517
00020000 00000-0 20000-3 0 9002
2 25544 51
6296 198
7260 0023110 75
8329 284
5401 15
76884327 25872
Satellite: ISS
Catalog Number: 25544
Epoch time: 07010
50188517 = yrday
fracday
Element set: 900
Inclination: 51
6296 deg
RA of node: 198
7260 deg
Eccentricity:
0023110
Arg of perigee: 75
8329 deg
Mean anomaly: 284
5401 deg
Mean motion: 15
76884327 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2587
Checksum: 296
Coasting Arc #2 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2007/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -997231
76 A = 6711820
39 meter
Y = 4070576
25 meter E =
0038109
Z = -5275064
53 I = 51
53923
XDOT = -7478
079315 Wp = 84
32028
YDOT = -1735
483371 meter/sec RA = 192
59925 deg
ZDOT = 78
678439 TA = 186
40518
MA = 186
45403
Ha = 194
013 n
mi
Hp = 170
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3271757
74 X = -1017050
28
Y = 13354908
95 feet Y = 4059314
22 meter
Z = -17306642
17 Z = -5279956
89
XDOT = -24534
380956 XDOT = -7458
499313
YDOT = -5693
843080 feet/sec YDOT = -1818
997944 meter/sec
ZDOT = 258
131360 ZDOT = 42
397618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13638864
55 X = -4157125
91
Y = 1556547
39 feet Y = 474435
65 meter
Z = -17324444
84 Z = -5280490
79
XDOT = -2878
178863 XDOT = -877
268917
YDOT = -24014
582267 feet/sec YDOT = -7319
644675 meter/sec
ZDOT = 121
957640 ZDOT = 37
172689
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 07011
51584291
00020000 00000-0 20000-3 0 9014
2 25544 51
6294 193
4945 0023197 79
8709 280
5071 15
76918111 26030
Satellite: ISS
Catalog Number: 25544
Epoch time: 07011
51584291 = yrday
fracday
Element set: 901
Inclination: 51
6294 deg
RA of node: 193
4945 deg
Eccentricity:
0023197
Arg of perigee: 79
8709 deg
Mean anomaly: 280
5071 deg
Mean motion: 15
76918111 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2603
Checksum: 296
Coasting Arc #3 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2007/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6410366
69 A = 6723171
77 meter
Y = 1710369
02 meter E =
0029400
Z = -1091795
64 I = 51
60673
XDOT = -2166
281726 Wp = 99
81734
YDOT = 4437
365228 meter/sec RA = 187
44668 deg
ZDOT = -5906
996864 TA = 92
13949
MA = 91
80280
Ha = 193
934 n
mi
Hp = 170
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21031386
77 X = 6396068
39
Y = 5611446
92 feet Y = 1781973
46 meter
Z = -3582006
70 Z = -1060688
81
XDOT = -7107
223509 XDOT = -2187
044989
YDOT = 14558
284868 feet/sec YDOT = 4413
025079 meter/sec
ZDOT = -19379
910972 ZDOT = -5917
570659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2256924
85 X = 687910
69
Y = 21668800
44 feet Y = 6604650
37 meter
Z = -3465215
15 Z = -1056197
58
XDOT = -14516
776137 XDOT = -4424
713367
YDOT = -1517
866729 feet/sec YDOT = -462
645779 meter/sec
ZDOT = -19418
959133 ZDOT = -5918
898744
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 07012
52977832
00020000 00000-0 20000-3 0 9024
2 25544 51
6295 188
2630 0023207 83
1011 277
2793 15
76995303 26199
Satellite: ISS
Catalog Number: 25544
Epoch time: 07012
52977832 = yrday
fracday
Element set: 902
Inclination: 51
6295 deg
RA of node: 188
2630 deg
Eccentricity:
0023207
Arg of perigee: 83
1011 deg
Mean anomaly: 277
2793 deg
Mean motion: 15
76995303 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2619
Checksum: 295
Coasting Arc #4 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2007/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2735147
38 A = 6713391
12 meter
Y = -3732029
34 meter E =
0029156
Z = 4841094
72 I = 51
60132
XDOT = 7051
726313 Wp = 81
35829
YDOT = 2125
467749 meter/sec RA = 182
25640 deg
ZDOT = -2329
413411 TA = 31
35849
MA = 31
18495
Ha = 193
903 n
mi
Hp = 170
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8973580
65 X = 2753159
12
Y = -12244190
74 feet Y = -3701343
20 meter
Z = 15882856
69 Z = 4854425
37
XDOT = 23135
585017 XDOT = 7038
750754
YDOT = 6973
319386 feet/sec YDOT = 2204
251770 meter/sec
ZDOT = -7642
432450 ZDOT = -2295
187561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14672097
55 X = 4472055
33
Y = 3687924
17 feet Y = 1124079
29 meter
Z = 15932333
85 Z = 4856175
36
XDOT = 2426
042841 XDOT = 739
457858
YDOT = 23037
718951 feet/sec YDOT = 7021
896736 meter/sec
ZDOT = -7513
887976 ZDOT = -2290
233055
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 07013
54369512
00020000 00000-0 20000-3 0 9038
2 25544 51
6287 183
0315 0023180 87
5649 272
8169 15
76965630 26354
Satellite: ISS
Catalog Number: 25544
Epoch time: 07013
54369512 = yrday
fracday
Element set: 903
Inclination: 51
6287 deg
RA of node: 183
0315 deg
Eccentricity:
0023180
Arg of perigee: 87
5649 deg
Mean anomaly: 272
8169 deg
Mean motion: 15
76965630 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2635
Checksum: 304
Coasting Arc #5 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2007/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5711900
35 A = 6720016
22 meter
Y = -2001449
41 meter E =
0036529
Z = 2887178
53 I = 51
65287
XDOT = 4051
588915 Wp = 88
00398
YDOT = -4201
917043 meter/sec RA = 177
13940 deg
ZDOT = 5049
347025 TA = 305
29349
MA = 305
63460
Ha = 193
915 n
mi
Hp = 170
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18739830
53 X = -5703120
65
Y = -6566435
08 feet Y = -2065274
33 meter
Z = 9472370
52 Z = 2859451
35
XDOT = 13292
614550 XDOT = 4073
745544
YDOT = -13785
817070 feet/sec YDOT = -4156
486663 meter/sec
ZDOT = 16566
099164 ZDOT = 5069
082838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1243912
61 X = -379144
56
Y = -19867432
43 feet Y = -6055593
41 meter
Z = 9368187
19 Z = 2855423
45
XDOT = 16380
539123 XDOT = 4992
788325
YDOT = 6903
948045 feet/sec YDOT = 2104
323364 meter/sec
ZDOT = 16639
530728 ZDOT = 5071
728966
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 07014
55758851
00020000 00000-0 20000-3 0 9049
2 25544 51
6290 177
8003 0023179 91
5279 268
8541 15
77031248 26512
Satellite: ISS
Catalog Number: 25544
Epoch time: 07014
55758851 = yrday
fracday
Element set: 904
Inclination: 51
6290 deg
RA of node: 177
8003 deg
Eccentricity:
0023179
Arg of perigee: 91
5279 deg
Mean anomaly: 268
8541 deg
Mean motion: 15
77031248 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2651
Checksum: 303
Coasting Arc #6 (Orbit 2665)
---------------------------------------
Vector Time (GMT): 2007/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4260578
60 A = 6717265
33 meter
Y = 3608322
05 meter E =
0029361
Z = -3762983
78 I = 51
67363
XDOT = -5881
710103 Wp = 97
33046
YDOT = -2550
281887 meter/sec RA = 171
93195 deg
ZDOT = 4238
498068 TA = 217
23697
MA = 217
44092
Ha = 193
829 n
mi
Hp = 170
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13978276
26 X = -4282330
98
Y = 11838326
95 feet Y = 3560556
80 meter
Z = -12345747
30 Z = -3783733
82
XDOT = -19296
949156 XDOT = -5873
345029
YDOT = -8367
066557 feet/sec YDOT = -2616
008264 meter/sec
ZDOT = 13905
833557 ZDOT = 4209
944922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16448824
53 X = -5013601
72
Y = -7940983
15 feet Y = -2420411
66 meter
Z = -12423068
33 Z = -3786551
23
XDOT = -752
402919 XDOT = -229
332410
YDOT = -19903
243382 feet/sec YDOT = -6066
508583 meter/sec
ZDOT = 13798
471496 ZDOT = 4205
774112
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 07015
50809502
00020000 00000-0 20000-3 0 9056
2 25544 51
6300 172
8959 0023263 95
0430 265
3391 15
77052638 26668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07015
50809502 = yrday
fracday
Element set: 905
Inclination: 51
6300 deg
RA of node: 172
8959 deg
Eccentricity:
0023263
Arg of perigee: 95
0430 deg
Mean anomaly: 265
3391 deg
Mean motion: 15
77052638 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2666
Checksum: 286
Coasting Arc #7 (Orbit 2681)
---------------------------------------
Vector Time (GMT): 2007/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4427350
47 A = 6715089
23 meter
Y = 2529924
10 meter E =
0031487
Z = -4395968
19 I = 51
69483
XDOT = -5614
674985 Wp = 90
80421
YDOT = 4034
882657 meter/sec RA = 166
82609 deg
ZDOT = -3353
680964 TA = 145
50849
MA = 145
30377
Ha = 193
774 n
mi
Hp = 170
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14525428
04 X = 4420085
98
Y = 8300275
93 feet Y = 2579393
24 meter
Z = -14422467
80 Z = -4374477
67
XDOT = -18420
849689 XDOT = -5643
084965
YDOT = 13237
803993 feet/sec YDOT = 3971
937892 meter/sec
ZDOT = -11002
890302 ZDOT = -3381
025099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1404372
08 X = -428052
61
Y = 16740287
95 feet Y = 5102439
77 meter
Z = -14341573
00 Z = -4371311
45
XDOT = -18500
100274 XDOT = -5638
830563
YDOT = -11006
208149 feet/sec YDOT = -3354
692244 meter/sec
ZDOT = -11104
890631 ZDOT = -3384
770664
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 07016
52194672
00020000 00000-0 20000-3 0 9065
2 25544 51
6303 167
6642 0023222 98
6559 261
7238 15
77092891 26821
Satellite: ISS
Catalog Number: 25544
Epoch time: 07016
52194672 = yrday
fracday
Element set: 906
Inclination: 51
6303 deg
RA of node: 167
6642 deg
Eccentricity:
0023222
Arg of perigee: 98
6559 deg
Mean anomaly: 261
7238 deg
Mean motion: 15
77092891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2682
Checksum: 308
Coasting Arc #8 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2007/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5398893
01 A = 6721579
99 meter
Y = -3445064
11 meter E =
0037178
Z = 1988461
20 I = 51
74423
XDOT = 4178
871486 Wp = 106
20526
YDOT = 3269
644865 meter/sec RA = 161
62877 deg
ZDOT = -5605
672313 TA = 51
60905
MA = 51
27572
Ha = 193
664 n
mi
Hp = 170
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17712903
58 X = 5427355
55
Y = -11302703
78 feet Y = -3384531
84 meter
Z = 6523822
84 Z = 2014757
15
XDOT = 13710
208286 XDOT = 4169
230093
YDOT = 10727
181314 feet/sec YDOT = 3316
322255 meter/sec
ZDOT = -18391
313363 ZDOT = -5585
394672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17869461
28 X = 5446611
80
Y = 10994999
93 feet Y = 3351275
98 meter
Z = 6621983
16 Z = 2018380
47
XDOT = -2844
660328 XDOT = -867
052468
YDOT = 15801
092937 feet/sec YDOT = 4816
173127 meter/sec
ZDOT = -18314
859865 ZDOT = -5582
369287
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 07017
53577678
00020000 00000-0 20000-3 0 9079
2 25544 51
6299 162
4316 0023150 102
6257 257
7498 15
77109116 26986
Satellite: ISS
Catalog Number: 25544
Epoch time: 07017
53577678 = yrday
fracday
Element set: 907
Inclination: 51
6299 deg
RA of node: 162
4316 deg
Eccentricity:
0023150
Arg of perigee: 102
6257 deg
Mean anomaly: 257
7498 deg
Mean motion: 15
77109116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2698
Checksum: 317
Coasting Arc #9 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2007/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2806691
87 A = 6711509
78 meter
Y = -3216243
60 meter E =
0026837
Z = 5158873
68 I = 51
73902
XDOT = 6587
440826 Wp = 109
18580
YDOT = -3862
879130 meter/sec RA = 156
50545 deg
ZDOT = 1162
088489 TA = 329
69065
MA = 329
84557
Ha = 193
615 n
mi
Hp = 170
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9208306
66 X = -2795579
03
Y = -10551980
33 feet Y = -3247568
16 meter
Z = 16925438
57 Z = 5145265
66
XDOT = 21612
338667 XDOT = 6624
501422
YDOT = -12673
487958 feet/sec YDOT = -3789
007642 meter/sec
ZDOT = 3812
626277 ZDOT = 1194
178986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5227720
75 X = 1593409
28
Y = -13059364
02 feet Y = -3980494
15 meter
Z = 16873992
36 Z = 5143192
87
XDOT = 20091
391214 XDOT = 6123
856042
YDOT = 13181
425671 feet/sec YDOT = 4017
698544 meter/sec
ZDOT = 3932
476523 ZDOT = 1198
618844
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 07018
54958362
00020000 00000-0 20000-3 0 9085
2 25544 51
6313 157
2005 0022993 106
2530 254
1166 15
77182192 27145
Satellite: ISS
Catalog Number: 25544
Epoch time: 07018
54958362 = yrday
fracday
Element set: 908
Inclination: 51
6313 deg
RA of node: 157
2005 deg
Eccentricity:
0022993
Arg of perigee: 106
2530 deg
Mean anomaly: 254
1166 deg
Mean motion: 15
77182192 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2714
Checksum: 282
Coasting Arc #10 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2007/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5910242
48 A = 6723106
68 meter
Y = 3203109
57 meter E =
0030508
Z = 29594
07 I = 51
80534
XDOT = -2224
735956 Wp = 88
74799
YDOT = -4210
184444 meter/sec RA = 151
34567 deg
ZDOT = 6051
784261 TA = 271
57295
MA = 271
92238
Ha = 193
510 n
mi
Hp = 170
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19390559
30 X = -5945764
60
Y = 10508889
67 feet Y = 3136819
33 meter
Z = 97093
40 Z = 797
01
XDOT = -7299
002479 XDOT = -2206
889354
YDOT = -13812
941088 feet/sec YDOT = -4234
963568 meter/sec
ZDOT = 19854
935240 ZDOT = 6041
019684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18333489
87 X = -5588047
71
Y = -12260628
79 feet Y = -3737039
66 meter
Z = -10502
30 Z = -3201
10
XDOT = 7875
647704 XDOT = 2400
497420
YDOT = -11654
952803 feet/sec YDOT = -3552
429614 meter/sec
ZDOT = 19814
016634 ZDOT = 6039
312270
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 07019
50000901
00020000 00000-0 20000-3 0 9090
2 25544 51
6327 152
2965 0023114 109
6964 250
6698 15
77189545 27290
Satellite: ISS
Catalog Number: 25544
Epoch time: 07019
50000901 = yrday
fracday
Element set: 909
Inclination: 51
6327 deg
RA of node: 152
2965 deg
Eccentricity:
0023114
Arg of perigee: 109
6964 deg
Mean anomaly: 250
6698 deg
Mean motion: 15
77189545 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2729
Checksum: 302
Coasting Arc #11 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2007/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1055268
54 A = 6711436
15 meter
Y = 4189595
10 meter E =
0037028
Z = -5168116
84 I = 51
79124
XDOT = -6799
238717 Wp = 108
45291
YDOT = 3321
770037 meter/sec RA = 146
18647 deg
ZDOT = 1300
631977 TA = 174
01862
MA = 173
97429
Ha = 193
387 n
mi
Hp = 170
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3462167
12 X = 1033446
48
Y = 13745390
74 feet Y = 4201274
10 meter
Z = -16955763
92 Z = -5163043
17
XDOT = -22307
213639 XDOT = -6842
195934
YDOT = 10898
195659 feet/sec YDOT = 3245
496873 meter/sec
ZDOT = 4267
165280 ZDOT = 1267
498207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10339310
19 X = -3151421
74
Y = 9730597
13 feet Y = 2965886
00 meter
Z = -16936187
36 Z = -5162149
91
XDOT = -19587
693646 XDOT = -5970
329023
YDOT = -13579
411577 feet/sec YDOT = -4139
004649 meter/sec
ZDOT = 4143
308451 ZDOT = 1262
880416
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 07020
51377348
00020000 00000-0 20000-3 0 9107
2 25544 51
6331 147
0654 0023050 113
3489 247
0104 15
77239508 27450
Satellite: ISS
Catalog Number: 25544
Epoch time: 07020
51377348 = yrday
fracday
Element set: 910
Inclination: 51
6331 deg
RA of node: 147
0654 deg
Eccentricity:
0023050
Arg of perigee: 113
3489 deg
Mean anomaly: 247
0104 deg
Mean motion: 15
77239508 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2745
Checksum: 269
Coasting Arc #12 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2007/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5837785
45 A = 6720848
42 meter
Y = -2488978
22 meter E =
0028891
Z = -2205003
48 I = 51
84666
XDOT = 235
677766 Wp = 121
77213
YDOT = 5376
692485 meter/sec RA = 141
06831 deg
ZDOT = -5512
448231 TA = 82
89659
MA = 82
56816
Ha = 193
355 n
mi
Hp = 170
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19152839
41 X = 5875894
88
Y = -8165939
05 feet Y = -2423483
66 meter
Z = -7234263
39 Z = -2176551
90
XDOT = 773
221016 XDOT = 202
315013
YDOT = 17640
067207 feet/sec YDOT = 5379
141702 meter/sec
ZDOT = -18085
460077 ZDOT = -5511
384107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16611769
05 X = 5063267
21
Y = 12613136
01 feet Y = 3844483
86 meter
Z = -7127854
78 Z = -2172570
14
XDOT = -13963
115573 XDOT = -4255
957627
YDOT = 8298
620536 feet/sec YDOT = 2529
419540 meter/sec
ZDOT = -18080
765052 ZDOT = -5511
017188
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 07021
52751562
00020000 00000-0 20000-3 0 9114
2 25544 51
6335 141
8324 0022993 117
1583 243
1930 15
77259460 27613
Satellite: ISS
Catalog Number: 25544
Epoch time: 07021
52751562 = yrday
fracday
Element set: 911
Inclination: 51
6335 deg
RA of node: 141
8324 deg
Eccentricity:
0022993
Arg of perigee: 117
1583 deg
Mean anomaly: 243
1930 deg
Mean motion: 15
77259460 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2761
Checksum: 279
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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