Date:
December 7th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12665 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3786)
---------------------------------------
Vector Time (GMT): 2007/339/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4863447
35 A = 6716458
39 meter
Y = -2460329
80 meter E =
0010003
Z = 3918029
37 I = 51
34848
XDOT = 106
632467 Wp = 102
03157
YDOT = 6590
892456 meter/sec RA = 298
07224 deg
ZDOT = 3995
758072 TA = 306
33463
MA = 306
42693
Ha = 184
793 n
mi
Hp = 179
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15956192
09 X = 4871564
18
Y = -8071948
15 feet Y = -2405898
97 meter
Z = 12854427
06 Z = 3941675
99
XDOT = 349
844053 XDOT = 13
513092
YDOT = 21623
662914 feet/sec YDOT = 6591
563834 meter/sec
ZDOT = 13109
442492 ZDOT = 3996
050555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9498614
85 X = 2895177
81
Y = -15073669
88 feet Y = -4594454
58 meter
Z = 12944245
84 Z = 3945406
13
XDOT = 10223
970871 XDOT = 3116
266321
YDOT = 17731
375687 feet/sec YDOT = 5404
523309 meter/sec
ZDOT = 13111
216321 ZDOT = 3996
298735
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 07339
93621092
00020000 00000-0 20000-3 0 9003
2 25544 51
6366 298
3847 0001079 268
8901 91
2140 15
77140841 37871
Satellite: ISS
Catalog Number: 25544
Epoch time: 07339
93621092 = yrday
fracday
Element set: 900
Inclination: 51
6366 deg
RA of node: 298
3847 deg
Eccentricity:
0001079
Arg of perigee: 268
8901 deg
Mean anomaly: 91
2140 deg
Mean motion: 15
77140841 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3787
Checksum: 306
Coasting Arc #2 (Orbit 3801)
---------------------------------------
Vector Time (GMT): 2007/340/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 323512
52 A = 6720163
11 meter
Y = -6176948
66 meter E =
0004274
Z = -2625402
96 I = 51
34868
XDOT = 5334
415175 Wp = 47
28815
YDOT = -1931
341153 meter/sec RA = 292
84190 deg
ZDOT = 5209
532491 TA = 282
69223
MA = 282
74001
Ha = 184
910 n
mi
Hp = 179
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1061392
77 X = 405314
07
Y = -20265579
58 feet Y = -6172873
27 meter
Z = -8613526
76 Z = -2623633
32
XDOT = 17501
362124 XDOT = 5330
307729
YDOT = -6336
421107 feet/sec YDOT = -1871
712277 meter/sec
ZDOT = 17091
642030 ZDOT = 5235
437456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9744716
41 X = -2970189
56
Y = -17803545
15 feet Y = -5426520
56 meter
Z = -8607403
54 Z = -2623536
60
XDOT = 10147
440658 XDOT = 3092
939913
YDOT = -13851
958674 feet/sec YDOT = -4222
077004 meter/sec
ZDOT = 17190
118953 ZDOT = 5239
548257
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 07340
88665119
00020000 00000-0 20000-3 0 9018
2 25544 51
6366 293
4797 0000887 264
2844 95
8219 15
77169456 38021
Satellite: ISS
Catalog Number: 25544
Epoch time: 07340
88665119 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 293
4797 deg
Eccentricity:
0000887
Arg of perigee: 264
2844 deg
Mean anomaly: 95
8219 deg
Mean motion: 15
77169456 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3802
Checksum: 331
Coasting Arc #3 (Orbit 3817)
---------------------------------------
Vector Time (GMT): 2007/341/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4439403
82 A = 6712077
17 meter
Y = 781801
61 meter E =
0012542
Z = -4984508
45 I = 51
31213
XDOT = 794
545127 Wp = 75
33862
YDOT = -7422
856553 meter/sec RA = 287
69844 deg
ZDOT = -1872
696156 TA = 176
50294
MA = 176
49416
Ha = 184
881 n
mi
Hp = 178
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14564973
18 X = -4423601
75
Y = 2564965
92 feet Y = 732246
72 meter
Z = -16353374
17 Z = -5006037
04
XDOT = 2606
775350 XDOT = 886
586993
YDOT = -24353
203913 feet/sec YDOT = -7413
456611 meter/sec
ZDOT = -6144
016261 ZDOT = -1868
613615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10773056
61 X = -3283627
66
Y = 9998623
39 feet Y = 3047580
41 meter
Z = -16435301
10 Z = -5009479
77
XDOT = -10248
531232 XDOT = -3123
752320
YDOT = -21112
976948 feet/sec YDOT = -6435
235374 meter/sec
ZDOT = -6129
205851 ZDOT = -1868
181943
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 07341
90042549
00020000 00000-0 20000-3 0 9029
2 25544 51
6369 288
2489 0000718 265
6832 94
4250 15
77226535 38188
Satellite: ISS
Catalog Number: 25544
Epoch time: 07341
90042549 = yrday
fracday
Element set: 902
Inclination: 51
6369 deg
RA of node: 288
2489 deg
Eccentricity:
0000718
Arg of perigee: 265
6832 deg
Mean anomaly: 94
4250 deg
Mean motion: 15
77226535 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3818
Checksum: 309
Coasting Arc #4 (Orbit 3833)
---------------------------------------
Vector Time (GMT): 2007/342/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1005644
87 A = 6722663
99 meter
Y = 6616971
09 meter E =
0012428
Z = 562060
06 I = 51
34088
XDOT = -4853
134518 Wp = 131
21395
YDOT = -222
776041 meter/sec RA = 282
49373 deg
ZDOT = -5983
154005 TA = 42
63408
MA = 42
53769
Ha = 184
688 n
mi
Hp = 179
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3299359
80 X = -1082292
54
Y = 21709222
73 feet Y = 6605296
75 meter
Z = 1844029
08 Z = 556989
38
XDOT = -15922
357344 XDOT = -4821
217093
YDOT = -730
892522 feet/sec YDOT = -276
867162 meter/sec
ZDOT = -19629
770359 ZDOT = -6006
653477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9326504
55 X = 2842718
59
Y = 19881169
39 feet Y = 6059780
43 meter
Z = 1825372
98 Z = 556373
68
XDOT = -12095
774311 XDOT = -3686
792010
YDOT = 7508
361235 feet/sec YDOT = 2288
548504 meter/sec
ZDOT = -19719
310942 ZDOT = -6010
445975
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 07342
91416892
00020000 00000-0 20000-3 0 9038
2 25544 51
6368 283
0166 0000929 280
1578 79
9482 15
77302754 38346
Satellite: ISS
Catalog Number: 25544
Epoch time: 07342
91416892 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 283
0166 deg
Eccentricity:
0000929
Arg of perigee: 280
1578 deg
Mean anomaly: 79
9482 deg
Mean motion: 15
77302754 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3834
Checksum: 316
Coasting Arc #5 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2007/343/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4052568
58 A = 6710954
50 meter
Y = 1210512
03 meter E =
0002304
Z = 5208800
54 I = 51
29586
XDOT = -1463
123519 Wp = 59
24941
YDOT = 7543
248422 meter/sec RA = 277
31006 deg
ZDOT = -613
323659 TA = 36
61043
MA = 36
59469
Ha = 184
736 n
mi
Hp = 179
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13295828
69 X = 4013427
48
Y = 3971496
16 feet Y = 1255610
43 meter
Z = 17089240
63 Z = 5228393
34
XDOT = -4800
274011 XDOT = -1544
385067
YDOT = 24748
190360 feet/sec YDOT = 7526
432691 meter/sec
ZDOT = -2012
216730 ZDOT = -620
627752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13106135
12 X = 3994749
98
Y = -4268508
49 feet Y = -1301041
39 meter
Z = 17164004
34 Z = 5231588
52
XDOT = 9874
811968 XDOT = 3009
842688
YDOT = 22101
816163 feet/sec YDOT = 6736
633567 meter/sec
ZDOT = -2039
288917 ZDOT = -621
575262
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 07343
92788827
00020000 00000-0 20000-3 0 9041
2 25544 51
6367 277
7848 0000645 263
6937 96
4154 15
77257839 38503
Satellite: ISS
Catalog Number: 25544
Epoch time: 07343
92788827 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 277
7848 deg
Eccentricity:
0000645
Arg of perigee: 263
6937 deg
Mean anomaly: 96
4154 deg
Mean motion: 15
77257839 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3850
Checksum: 346
Coasting Arc #6 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2007/344/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1535335
31 A = 6721462
03 meter
Y = -6333090
43 meter E =
0013366
Z = 1620746
24 I = 51
33089
XDOT = 4486
192849 Wp = 62
66441
YDOT = 2559
554787 meter/sec RA = 272
14673 deg
ZDOT = 5721
747819 TA = 315
34248
MA = 315
45006
Ha = 184
640 n
mi
Hp = 178
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5037189
35 X = 1598165
41
Y = -20777855
73 feet Y = -6315570
42 meter
Z = 5317408
91 Z = 1628356
50
XDOT = 14718
480475 XDOT = 4429
442605
YDOT = 8397
489458 feet/sec YDOT = 2609
403649 meter/sec
ZDOT = 18772
138514 ZDOT = 5743
404556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8083232
96 X = -2463769
41
Y = -19785133
67 feet Y = -6030508
74 meter
Z = 5345767
81 Z = 1629390
03
XDOT = 15321
791852 XDOT = 4670
082157
YDOT = -1138
871825 feet/sec YDOT = -347
128132 meter/sec
ZDOT = 18854
909225 ZDOT = 5746
976332
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 07344
94157356
00020000 00000-0 20000-3 0 9052
2 25544 51
6376 272
5532 0000788 257
4008 102
7069 15
77367681 38664
Satellite: ISS
Catalog Number: 25544
Epoch time: 07344
94157356 = yrday
fracday
Element set: 905
Inclination: 51
6376 deg
RA of node: 272
5532 deg
Eccentricity:
0000788
Arg of perigee: 257
4008 deg
Mean anomaly: 102
7069 deg
Mean motion: 15
77367681 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3866
Checksum: 318
Coasting Arc #7 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2007/345/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3798268
02 A = 6713567
65 meter
Y = -3209209
11 meter E =
0009539
Z = -4520096
28 I = 51
30511
XDOT = 2082
120779 Wp = 112
27078
YDOT = -6755
305661 meter/sec RA = 266
92450 deg
ZDOT = 3048
117863 TA = 188
20706
MA = 188
22268
Ha = 184
628 n
mi
Hp = 178
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12461509
26 X = -3740141
94
Y = -10528901
28 feet Y = -3251357
74 meter
Z = -14829712
22 Z = -4538407
72
XDOT = 6831
104918 XDOT = 2142
697602
YDOT = -22163
076314 feet/sec YDOT = -6731
684017 meter/sec
ZDOT = 10000
386688 ZDOT = 3058
378866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16217432
29 X = -4943073
36
Y = -1028506
76 feet Y = -313488
86 meter
Z = -14899812
19 Z = -4541462
76
XDOT = -7910
268874 XDOT = -2411
049953
YDOT = -20628
062366 feet/sec YDOT = -6287
433409 meter/sec
ZDOT = 10038
800530 ZDOT = 3059
826402
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 07345
89188036
00020000 00000-0 20000-3 0 9067
2 25544 51
6381 267
6490 0000736 263
8246 96
2835 15
77384935 38812
Satellite: ISS
Catalog Number: 25544
Epoch time: 07345
89188036 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 267
6490 deg
Eccentricity:
0000736
Arg of perigee: 263
8246 deg
Mean anomaly: 96
2835 deg
Mean motion: 15
77384935 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3881
Checksum: 331
Coasting Arc #8 (Orbit 3896)
---------------------------------------
Vector Time (GMT): 2007/346/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2141601
55 A = 6716764
56 meter
Y = 5263068
00 meter E =
0004732
Z = -3586476
86 I = 51
31905
XDOT = -4228
668489 Wp = 79
83063
YDOT = -4707
943219 meter/sec RA = 261
78855 deg
ZDOT = -4387
798272 TA = 143
30626
MA = 143
27385
Ha = 184
536 n
mi
Hp = 178
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7026251
81 X = -2182872
33
Y = 17267283
46 feet Y = 5238889
20 meter
Z = -11766656
38 Z = -3596980
21
XDOT = -13873
584282 XDOT = -4154
394107
YDOT = -15446
007935 feet/sec YDOT = -4754
814611 meter/sec
ZDOT = -14395
663623 ZDOT = -4408
161503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5066063
16 X = 1544136
05
Y = 17914560
96 feet Y = 5460358
18 meter
Z = -11806142
66 Z = -3598512
28
XDOT = -19054
751374 XDOT = -5807
888219
YDOT = -4141
269138 feet/sec YDOT = -1262
258833 meter/sec
ZDOT = -14473
746752 ZDOT = -4411
598010
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 07346
90551242
00020000 00000-0 20000-3 0 9074
2 25544 51
6379 262
4169 0000760 269
6166 90
4911 15
77436342 38975
Satellite: ISS
Catalog Number: 25544
Epoch time: 07346
90551242 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 262
4169 deg
Eccentricity:
0000760
Arg of perigee: 269
6166 deg
Mean anomaly: 90
4911 deg
Mean motion: 15
77436342 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3897
Checksum: 311
Coasting Arc #9 (Orbit 3912)
---------------------------------------
Vector Time (GMT): 2007/347/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3580057
92 A = 6718520
43 meter
Y = 4858778
89 meter E =
0012591
Z = 2939016
34 I = 51
33041
XDOT = -2869
778123 Wp = 97
92479
YDOT = 5137
035281 meter/sec RA = 256
55313 deg
ZDOT = -4980
371038 TA = 47
96691
MA = 47
85981
Ha = 184
459 n
mi
Hp = 178
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11745596
86 X = 3511183
05
Y = 15940875
61 feet Y = 4898427
62 meter
Z = 9642442
07 Z = 2956241
62
XDOT = -9415
282557 XDOT = -2902
814227
YDOT = 16853
790291 feet/sec YDOT = 5104
759765 meter/sec
ZDOT = -16339
799993 ZDOT = -4994
391948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19093438
06 X = 5819679
92
Y = 5121626
00 feet Y = 1561071
61 meter
Z = 9708595
16 Z = 2959179
80
XDOT = 3644
691009 XDOT = 1110
901819
YDOT = 17588
341470 feet/sec YDOT = 5360
926480 meter/sec
ZDOT = -16392
701515 ZDOT = -4996
495422
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 07347
91911708
00020000 00000-0 20000-3 0 9084
2 25544 51
6376 257
1844 0000757 265
9042 94
2036 15
77462585 39138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07347
91911708 = yrday
fracday
Element set: 908
Inclination: 51
6376 deg
RA of node: 257
1844 deg
Eccentricity:
0000757
Arg of perigee: 265
9042 deg
Mean anomaly: 94
2036 deg
Mean motion: 15
77462585 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3913
Checksum: 314
Coasting Arc #10 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2007/348/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2922798
33 A = 6711606
78 meter
Y = -3561258
40 meter E =
0005697
Z = 4877881
36 I = 51
31674
XDOT = 3950
251342 Wp = 127
41056
YDOT = 6247
317463 meter/sec RA = 251
41061 deg
ZDOT = 2188
928922 TA = 301
23041
MA = 301
28622
Ha = 184
231 n
mi
Hp = 178
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9589233
36 X = 2938707
81
Y = -11683918
64 feet Y = -3528485
62 meter
Z = 16003547
76 Z = 4892118
53
XDOT = 12960
142197 XDOT = 3869
465892
YDOT = 20496
448369 feet/sec YDOT = 6291
039466 meter/sec
ZDOT = 7181
525334 ZDOT = 2207
923711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -158649
48 X = -48356
36
Y = -15057040
24 feet Y = -4589385
87 meter
Z = 16057436
34 Z = 4894306
60
XDOT = 21936
490548 XDOT = 6686
242319
YDOT = 7523
449891 feet/sec YDOT = 2293
147527 meter/sec
ZDOT = 7254
581291 ZDOT = 2211
196378
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 07348
93269181
00020000 00000-0 20000-3 0 9099
2 25544 51
6384 251
9520 0000899 273
0037 87
1025 15
77554594 39299
Satellite: ISS
Catalog Number: 25544
Epoch time: 07348
93269181 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 251
9520 deg
Eccentricity:
0000899
Arg of perigee: 273
0037 deg
Mean anomaly: 87
1025 deg
Mean motion: 15
77554594 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3929
Checksum: 320
Coasting Arc #11 (Orbit 3943)
---------------------------------------
Vector Time (GMT): 2007/349/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3240554
99 A = 6721809
31 meter
Y = -5833625
89 meter E =
0010140
Z = -764318
86 I = 51
36213
XDOT = 3905
230371 Wp = 35
42880
YDOT = -2943
444875 meter/sec RA = 246
20112 deg
ZDOT = 5955
822876 TA = 316
19463
MA = 316
27502
Ha = 184
342 n
mi
Hp = 178
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10631742
09 X = -3171368
73
Y = -19139192
54 feet Y = -5869476
70 meter
Z = -2507607
80 Z = -779893
98
XDOT = 12812
435600 XDOT = 3908
921863
YDOT = -9656
971376 feet/sec YDOT = -2899
754301 meter/sec
ZDOT = 19540
101299 ZDOT = 5974
803175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20529998
59 X = -6257543
57
Y = -7586654
45 feet Y = -2312412
28 meter
Z = -2567598
08 Z = -782603
90
XDOT = 2779
356440 XDOT = 847
147843
YDOT = -14107
071130 feet/sec YDOT = -4299
835281 meter/sec
ZDOT = 19612
133713 ZDOT = 5977
778356
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 07349
88289575
00020000 00000-0 20000-3 0 9105
2 25544 51
6387 247
0467 0000794 283
5147 76
5929 15
77554371 39445
Satellite: ISS
Catalog Number: 25544
Epoch time: 07349
88289575 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 247
0467 deg
Eccentricity:
0000794
Arg of perigee: 283
5147 deg
Mean anomaly: 76
5929 deg
Mean motion: 15
77554371 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3944
Checksum: 342
Coasting Arc #12 (Orbit 3959)
---------------------------------------
Vector Time (GMT): 2007/350/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3935949
62 A = 6709872
79 meter
Y = 1526628
31 meter E =
0014184
Z = -5227604
59 I = 51
33543
XDOT = -3357
445396 Wp = 93
19150
YDOT = -6906
737686 meter/sec RA = 241
02133 deg
ZDOT = 511
300501 TA = 181
68677
MA = 181
69156
Ha = 184
262 n
mi
Hp = 178
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12913220
53 X = -3927333
23
Y = 5008623
06 feet Y = 1482662
89 meter
Z = -17150933
71 Z = -5246704
45
XDOT = -11015
240799 XDOT = -3282
447485
YDOT = -22659
900543 feet/sec YDOT = -6943
863251 meter/sec
ZDOT = 1677
495081 ZDOT = 495
171585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6240337
15 X = -1902054
76
Y = 12263716
26 feet Y = 3737980
72 meter
Z = -17223575
47 Z = -5249745
80
XDOT = -22408
621045 XDOT = -6830
147695
YDOT = -9135
887008 feet/sec YDOT = -2784
618360 meter/sec
ZDOT = 1615
268453 ZDOT = 492
333824
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 07350
89641908
00020000 00000-0 20000-3 0 9111
2 25544 51
6387 241
8146 0000803 288
6282 71
4796 15
77623903 39600
Satellite: ISS
Catalog Number: 25544
Epoch time: 07350
89641908 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 241
8146 deg
Eccentricity:
0000803
Arg of perigee: 288
6282 deg
Mean anomaly: 71
4796 deg
Mean motion: 15
77623903 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3960
Checksum: 313
Coasting Arc #13 (Orbit 3975)
---------------------------------------
Vector Time (GMT): 2007/351/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2491144
31 A = 6720641
25 meter
Y = 6017289
23 meter E =
0007251
Z = -1647084
70 I = 51
38750
XDOT = -5133
739470 Wp = 146
52355
YDOT = 565
262384 meter/sec RA = 235
85752 deg
ZDOT = -5717
377638 TA = 51
76408
MA = 51
69884
Ha = 184
220 n
mi
Hp = 178
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8173045
65 X = 2431674
22
Y = 19741762
56 feet Y = 6044814
23 meter
Z = -5403821
19 Z = -1635126
61
XDOT = -16842
977264 XDOT = -5111
904561
YDOT = 1854
535382 feet/sec YDOT = 507
976522 meter/sec
ZDOT = -18757
800648 ZDOT = -5742
264464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19412316
50 X = 5916874
07
Y = 8955189
66 feet Y = 2729541
81 meter
Z = -5357582
86 Z = -1632991
26
XDOT = -10395
906442 XDOT = -3168
672284
YDOT = 11291
930953 feet/sec YDOT = 3441
780555 meter/sec
ZDOT = -18852
609687 ZDOT = -5746
275433
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 07351
90991587
00020000 00000-0 20000-3 0 9126
2 25544 51
6390 236
5810 0000832 288
8790 71
2285 15
77651087 39763
Satellite: ISS
Catalog Number: 25544
Epoch time: 07351
90991587 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 236
5810 deg
Eccentricity:
0000832
Arg of perigee: 288
8790 deg
Mean anomaly: 71
2285 deg
Mean motion: 15
77651087 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3976
Checksum: 321
Coasting Arc #14 (Orbit 3991)
---------------------------------------
Vector Time (GMT): 2007/352/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4992459
76 A = 6712934
62 meter
Y = 470036
02 meter E =
0008451
Z = 4458507
72 I = 51
37966
XDOT = 2205
345375 Wp = 63
04258
YDOT = 6674
653441 meter/sec RA = 230
63695 deg
ZDOT = -3164
756452 TA = 58
69634
MA = 58
61362
Ha = 184
106 n
mi
Hp = 178
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16379461
16 X = 4965173
80
Y = 1542112
94 feet Y = 525711
59 meter
Z = 14627649
99 Z = 4482695
15
XDOT = 7235
385088 XDOT = 2145
918482
YDOT = 21898
469293 feet/sec YDOT = 6698
982864 meter/sec
ZDOT = -10383
059226 ZDOT = -3154
186524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12855049
03 X = 3918218
94
Y = -10134345
16 feet Y = -3088948
41 meter
Z = 14719910
57 Z = 4486628
74
XDOT = 19655
282391 XDOT = 5990
930073
YDOT = 9870
779153 feet/sec YDOT = 3008
613486 meter/sec
ZDOT = -10342
037714 ZDOT = -3152
253095
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 07352
92338683
00020000 00000-0 20000-3 0 9132
2 25544 51
6394 231
3483 0000781 300
9558 59
1530 15
77676182 39926
Satellite: ISS
Catalog Number: 25544
Epoch time: 07352
92338683 = yrday
fracday
Element set: 913
Inclination: 51
6394 deg
RA of node: 231
3483 deg
Eccentricity:
0000781
Arg of perigee: 300
9558 deg
Mean anomaly: 59
1530 deg
Mean motion: 15
77676182 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3992
Checksum: 310
Coasting Arc #15 (Orbit 4007)
---------------------------------------
Vector Time (GMT): 2007/353/21:09:12
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1193899
02 A = 6715489
96 meter
Y = -5454273
90 meter E =
0010945
Z = 3722814
21 I = 51
40845
XDOT = 6252
688919 Wp = 94
86170
YDOT = 1534
226453 meter/sec RA = 225
50506 deg
ZDOT = 4241
427759 TA = 310
35354
MA = 310
44907
Ha = 184
083 n
mi
Hp = 178
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3916991
54 X = -1150904
80
Y = -17894599
40 feet Y = -5467384
77 meter
Z = 12213957
39 Z = 3717118
00
XDOT = 20514
071257 XDOT = 6214
463843
YDOT = 5033
551354 feet/sec YDOT = 1603
933378 meter/sec
ZDOT = 13915
445403 ZDOT = 4271
711112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15410090
06 X = -4696995
45
Y = -9931419
77 feet Y = -3027096
75 meter
Z = 12191648
42 Z = 3716014
44
XDOT = 17352
593967 XDOT = 5289
070641
YDOT = -9654
108565 feet/sec YDOT = -2942
572291 meter/sec
ZDOT = 14031
068964 ZDOT = 4276
669820
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 07353
93682920
00020000 00000-0 20000-3 0 9141
2 25544 51
6395 226
1147 0000876 299
3047 60
8030 15
77751893 40081
Satellite: ISS
Catalog Number: 25544
Epoch time: 07353
93682920 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 226
1147 deg
Eccentricity:
0000876
Arg of perigee: 299
3047 deg
Mean anomaly: 60
8030 deg
Mean motion: 15
77751893 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4008
Checksum: 304
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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