Date:
July 17th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6619 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 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
202/01:19:29
707 -1
0 3
4 3
4
N/A 3
2 0
1 186
9
000/00:04:59
415 0
0 0
2 172
6
204/22:30:58
096 2
2 11
1 11
1
N/A -10
7 -0
0 187
3
000/00:19:56
192 2
0 0
5 179
5
Coasting Arc #1 (Orbit 1540)
---------------------------------------
Vector Time (GMT): 2007/197/12:47:21
841
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2446116
69 A = 6705850
47 meter
Y = -3494596
63 meter E =
0022446
Z = -5193358
51 I = 51
37564
XDOT = 5581
832317 Wp = 87
26919
YDOT = -5218
809849 meter/sec RA = 311
60373 deg
ZDOT = 886
978557 TA = 191
19264
MA = 191
24265
Ha = 185
219 n
mi
Hp = 172
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8025317
22 X = -2381629
99
Y = -11465212
04 feet Y = -3521589
17 meter
Z = -17038577
79 Z = -5205085
34
XDOT = 18313
098152 XDOT = 5635
466286
YDOT = -17122
079556 feet/sec YDOT = -5156
090908 meter/sec
ZDOT = 2910
034635 ZDOT = 914
223985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4824250
48 X = -1470431
55
Y = 13078853
71 feet Y = 3986434
61 meter
Z = -17083329
01 Z = -5206998
68
XDOT = -23573
858086 XDOT = -7185
311945
YDOT = -4779
058911 feet/sec YDOT = -1456
657156 meter/sec
ZDOT = 3012
561816 ZDOT = 918
228842
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 07197
54720373
00020000 00000-0 20000-3 0 9004
2 25544 51
6358 312
1054 0008355 70
7109 289
4960 15
79113360 15416
Satellite: ISS
Catalog Number: 25544
Epoch time: 07197
54720373 = yrday
fracday
Element set: 900
Inclination: 51
6358 deg
RA of node: 312
1054 deg
Eccentricity:
0008355
Arg of perigee: 70
7109 deg
Mean anomaly: 289
4960 deg
Mean motion: 15
79113360 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1541
Checksum: 282
Coasting Arc #2 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2007/198/12:47:21
841
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5093881
79 A = 6715001
96 meter
Y = 3655435
20 meter E =
0012138
Z = -2412496
23 I = 51
38824
XDOT = -1338
058670 Wp = 96
58261
YDOT = -5377
836407 meter/sec RA = 306
43984 deg
ZDOT = -5347
639577 TA = 110
77765
MA = 110
64756
Ha = 185
184 n
mi
Hp = 172
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16712210
61 X = -5122659
61
Y = 11992897
65 feet Y = 3598311
94 meter
Z = -7915013
87 Z = -2437311
23
XDOT = -4389
956266 XDOT = -1251
846162
YDOT = -17643
820232 feet/sec YDOT = -5392
316648 meter/sec
ZDOT = -17544
749269 ZDOT = -5353
930969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19507245
22 X = 5945808
34
Y = 6411409
45 feet Y = 1954197
60 meter
Z = -8008510
16 Z = -2440993
90
XDOT = -11267
236543 XDOT = -3434
253698
YDOT = 12434
447934 feet/sec YDOT = 3790
019730 meter/sec
ZDOT = -17569
146276 ZDOT = -5355
075785
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 07198
55974371
00020000 00000-0 20000-3 0 9016
2 25544 51
6354 306
8653 0008325 74
6128 285
5957 15
79131959 15572
Satellite: ISS
Catalog Number: 25544
Epoch time: 07198
55974371 = yrday
fracday
Element set: 901
Inclination: 51
6354 deg
RA of node: 306
8653 deg
Eccentricity:
0008325
Arg of perigee: 74
6128 deg
Mean anomaly: 285
5957 deg
Mean motion: 15
79131959 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1557
Checksum: 330
Coasting Arc #3 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2007/199/12:47:21
841
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -28278
53 A = 6711767
40 meter
Y = 5639628
09 meter E =
0020400
Z = 3624121
67 I = 51
36107
XDOT = -5740
650405 Wp = 81
87337
YDOT = 2777
287658 meter/sec RA = 301
19812 deg
ZDOT = -4343
008485 TA = 54
32873
MA = 54
13899
Ha = 185
210 n
mi
Hp = 172
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -92777
31 X = -108944
58
Y = 18502716
85 feet Y = 5638860
47 meter
Z = 11890162
97 Z = 3623788
94
XDOT = -18834
154873 XDOT = -5750
182628
YDOT = 9111
836147 feet/sec YDOT = 2713
039624 meter/sec
ZDOT = -14248
715502 ZDOT = -4370
918926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14862218
14 X = 4530004
09
Y = -11022188
17 feet Y = -3359562
95 meter
Z = 11889531
26 Z = 3623929
13
XDOT = 17768
905502 XDOT = 5415
962397
YDOT = 8392
276158 feet/sec YDOT = 2557
965773 meter/sec
ZDOT = -14354
017996 ZDOT = -4375
104685
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 07199
57226073
00020000 00000-0 20000-3 0 9029
2 25544 51
6351 301
6255 0008458 77
5864 282
6248 15
79165421 15736
Satellite: ISS
Catalog Number: 25544
Epoch time: 07199
57226073 = yrday
fracday
Element set: 902
Inclination: 51
6351 deg
RA of node: 301
6255 deg
Eccentricity:
0008458
Arg of perigee: 77
5864 deg
Mean anomaly: 282
6248 deg
Mean motion: 15
79165421 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1573
Checksum: 307
Coasting Arc #4 (Orbit 1588)
---------------------------------------
Vector Time (GMT): 2007/200/12:47:21
841
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4653027
24 A = 6707375
35 meter
Y = -887381
39 meter E =
0014722
Z = 4737187
24 I = 51
33301
XDOT = -1236
942780 Wp = 98
89841
YDOT = 7178
869355 meter/sec RA = 296
04817 deg
ZDOT = 2550
758856 TA = 326
01364
MA = 326
10786
Ha = 184
956 n
mi
Hp = 172
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15265837
40 X = 4639592
18
Y = -2911356
28 feet Y = -835424
18 meter
Z = 15541952
87 Z = 4759758
61
XDOT = -4058
211219 XDOT = -1329
516970
YDOT = 23552
720982 feet/sec YDOT = 7164
519321 meter/sec
ZDOT = 8368
631418 ZDOT = 2544
525679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11646278
33 X = -3549785
64
Y = -10160067
40 feet Y = -3096788
54 meter
Z = 15627262
00 Z = 4763189
46
XDOT = 20338
181179 XDOT = 6199
077623
YDOT = -10431
409881 feet/sec YDOT = -3179
493732 meter/sec
ZDOT = 8345
851737 ZDOT = 2543
815609
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 07200
58475281
00020000 00000-0 20000-3 0 9031
2 25544 51
6350 296
3850 0008305 81
0610 279
1496 15
79229554 15897
Satellite: ISS
Catalog Number: 25544
Epoch time: 07200
58475281 = yrday
fracday
Element set: 903
Inclination: 51
6350 deg
RA of node: 296
3850 deg
Eccentricity:
0008305
Arg of perigee: 81
0610 deg
Mean anomaly: 279
1496 deg
Mean motion: 15
79229554 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1589
Checksum: 300
Coasting Arc #5 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2007/201/12:47:21
841
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1954800
25 A = 6717283
55 meter
Y = -6396673
85 meter E =
0018205
Z = -559209
42 I = 51
35417
XDOT = 4762
903734 Wp = 58
54772
YDOT = 945
364411 meter/sec RA = 290
82608 deg
ZDOT = 5987
772472 TA = 295
32867
MA = 295
51713
Ha = 185
149 n
mi
Hp = 172
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6413386
64 X = 2028900
02
Y = -20986462
78 feet Y = -6374399
81 meter
Z = -1834676
57 Z = -549533
70
XDOT = 15626
324586 XDOT = 4722
891323
YDOT = 3101
589276 feet/sec YDOT = 998
401608 meter/sec
ZDOT = 19644
922807 ZDOT = 6010
813322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20348232
33 X = -6202141
21
Y = 8224535
87 feet Y = 2506838
53 meter
Z = -1798787
68 Z = -548270
49
XDOT = -6760
906811 XDOT = -2060
724396
YDOT = -12522
803056 feet/sec YDOT = -3816
950372 meter/sec
ZDOT = 19732
215177 ZDOT = 6014
379186
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 07201
53394581
00020000 00000-0 20000-3 0 9041
2 25544 51
6345 291
4727 0008384 82
6558 277
5560 15
79199936 16047
Satellite: ISS
Catalog Number: 25544
Epoch time: 07201
53394581 = yrday
fracday
Element set: 904
Inclination: 51
6345 deg
RA of node: 291
4727 deg
Eccentricity:
0008384
Arg of perigee: 82
6558 deg
Mean anomaly: 277
5560 deg
Mean motion: 15
79199936 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1604
Checksum: 320
Coasting Arc #6 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2007/202/01:21:59
415
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3762322
26 A = 6706971
90 meter
Y = 1904311
37 meter E =
0013829
Z = 5204063
19 I = 51
30958
XDOT = -2824
980566 Wp = 79
82440
YDOT = 7160
929616 meter/sec RA = 288
10362 deg
ZDOT = -574
333731 TA = 15
66676
MA = 15
62401
Ha = 186
865 n
mi
Hp = 172
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12343576
97 X = 3715468
16
Y = 6247740
71 feet Y = 1946121
30 meter
Z = 17073698
14 Z = 5222226
78
XDOT = -9268
308944 XDOT = -2902
055192
YDOT = 23493
863568 feet/sec YDOT = 7128
908202 meter/sec
ZDOT = -1884
297018 ZDOT = -588
243907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4965961
93 X = 1513625
19
Y = 12821009
45 feet Y = 3907843
68 meter
Z = 17142644
59 Z = 5225078
07
XDOT = -21625
927814 XDOT = -6591
582798
YDOT = 10981
297775 feet/sec YDOT = 3347
099562 meter/sec
ZDOT = -1936
120401 ZDOT = -590
129498
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 07202
10347595
00020000 00000-0 20000-3 0 9059
2 25544 51
6351 288
5259 0011093 83
8325 276
4104 15
78653530 16133
Satellite: ISS
Catalog Number: 25544
Epoch time: 07202
10347595 = yrday
fracday
Element set: 905
Inclination: 51
6351 deg
RA of node: 288
5259 deg
Eccentricity:
0011093
Arg of perigee: 83
8325 deg
Mean anomaly: 276
4104 deg
Mean motion: 15
78653530 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1613
Checksum: 284
Coasting Arc #7 (Orbit 1628)
---------------------------------------
Vector Time (GMT): 2007/203/01:21:59
415
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2932819
20 A = 6717275
56 meter
Y = -5698560
46 meter E =
0024981
Z = 1978512
35 I = 51
33634
XDOT = 3690
210278 Wp = 76
35975
YDOT = 3852
391493 meter/sec RA = 282
93290 deg
ZDOT = 5572
734991 TA = 305
83591
MA = 306
06773
Ha = 186
991 n
mi
Hp = 172
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9622110
25 X = 2986712
17
Y = -18696064
51 feet Y = -5665462
91 meter
Z = 6491182
26 Z = 1992890
22
XDOT = 12106
989101 XDOT = 3619
786808
YDOT = 12639
079703 feet/sec YDOT = 3893
263153 meter/sec
ZDOT = 18283
251282 ZDOT = 5590
491291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19474694
73 X = 5935886
96
Y = -7884371
26 feet Y = -2403156
36 meter
Z = 6544939
72 Z = 1994897
63
XDOT = 249
152928 XDOT = 75
941813
YDOT = 15991
627920 feet/sec YDOT = 4874
248190 meter/sec
ZDOT = 18350
880264 ZDOT = 5593
348305
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 07203
11632642
00020000 00000-0 20000-3 0 9062
2 25544 51
6349 283
2876 0011148 86
9236 273
3205 15
78641477 16295
Satellite: ISS
Catalog Number: 25544
Epoch time: 07203
11632642 = yrday
fracday
Element set: 906
Inclination: 51
6349 deg
RA of node: 283
2876 deg
Eccentricity:
0011148
Arg of perigee: 86
9236 deg
Mean anomaly: 273
3205 deg
Mean motion: 15
78641477 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1629
Checksum: 299
Coasting Arc #8 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2007/204/01:21:59
415
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2648788
21 A = 6711646
72 meter
Y = -4659605
43 meter E =
0018279
Z = -4056946
40 I = 51
31245
XDOT = 3822
071153 Wp = 97
97355
YDOT = -5482
222825 meter/sec RA = 277
69399 deg
ZDOT = 3813
324791 TA = 211
38565
MA = 211
49486
Ha = 186
887 n
mi
Hp = 172
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8690250
02 X = -2576779
11
Y = -15287419
40 feet Y = -4688822
56 meter
Z = -13310191
59 Z = -4069639
82
XDOT = 12539
603520 XDOT = 3864
565735
YDOT = -17986
295358 feet/sec YDOT = -5439
245140 meter/sec
ZDOT = 12510
908107 ZDOT = 3831
994905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3175267
95 X = 967821
67
Y = -17258276
68 feet Y = -5260322
73 meter
Z = -13358757
32 Z = -4071749
23
XDOT = 19837
660482 XDOT = 6046
518915
YDOT = -6057
667911 feet/sec YDOT = -1846
377179 meter/sec
ZDOT = 12580
932887 ZDOT = 3834
668344
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 07204
06585212
00020000 00000-0 20000-3 0 9078
2 25544 51
6347 278
3766 0010998 90
4329 269
8096 15
78683753 16449
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
06585212 = yrday
fracday
Element set: 907
Inclination: 51
6347 deg
RA of node: 278
3766 deg
Eccentricity:
0010998
Arg of perigee: 90
4329 deg
Mean anomaly: 269
8096 deg
Mean motion: 15
78683753 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1644
Checksum: 329
Coasting Arc #9 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2007/204/22:40:56
192
Vector Time (MET): N/A
Weight (LBS) : 508148
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2393036
64 A = 6720783
66 meter
Y = -5320298
65 meter E =
0006815
Z = -3341527
71 I = 51
31735
XDOT = 3969
973012 Wp = 78
66606
YDOT = -4691
834890 meter/sec RA = 273
07963 deg
ZDOT = 4636
431222 TA = 241
78656
MA = 241
85539
Ha = 187
289 n
mi
Hp = 179
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7851170
07 X = -2317133
93
Y = -17455048
07 feet Y = -5346634
08 meter
Z = -10963017
43 Z = -3352969
41
XDOT = 13024
845839 XDOT = 3999
619872
YDOT = -15393
159087 feet/sec YDOT = -4647
275291 meter/sec
ZDOT = 15211
388524 ZDOT = 4655
788662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15689511
99 X = 4782163
26
Y = -10917607
07 feet Y = -3327686
63 meter
Z = -11006924
87 Z = -3354910
70
XDOT = 16746
057396 XDOT = 5104
198294
YDOT = 8686
987874 feet/sec YDOT = 2647
793904 meter/sec
ZDOT = 15284
106660 ZDOT = 4658
595710
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 07204
95206369
00020000 00000-0 20000-3 0 9080
2 25544 51
6342 273
7929 0002230 56
4762 303
6615 15
76281048 16585
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
95206369 = yrday
fracday
Element set: 908
Inclination: 51
6342 deg
RA of node: 273
7929 deg
Eccentricity:
0002230
Arg of perigee: 56
4762 deg
Mean anomaly: 303
6615 deg
Mean motion: 15
76281048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1658
Checksum: 297
Coasting Arc #10 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2007/205/22:40:56
192
Vector Time (MET): N/A
Weight (LBS) : 508148
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3481136
73 A = 6716693
68 meter
Y = 3581859
21 meter E =
0012285
Z = -4502852
58 I = 51
30411
XDOT = -2706
539833 Wp = 67
42084
YDOT = -6507
702692 meter/sec RA = 267
95171 deg
ZDOT = -3086
280853 TA = 171
66271
MA = 171
64227
Ha = 187
275 n
mi
Hp = 179
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11421052
27 X = -3499056
94
Y = 11751506
60 feet Y = 3542831
68 meter
Z = -14773138
39 Z = -4519806
85
XDOT = -8879
723863 XDOT = -2618
576060
YDOT = -21350
730617 feet/sec YDOT = -6537
476436 meter/sec
ZDOT = -10125
593351 ZDOT = -3099
216508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13816989
04 X = -4211418
26
Y = -8702953
49 feet Y = -2652660
22 meter
Z = -14836892
35 Z = -4522284
79
XDOT = 18467
834573 XDOT = 5628
995978
YDOT = -11984
372486 feet/sec YDOT = -3652
836734 meter/sec
ZDOT = -10175
295360 ZDOT = -3101
430026
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 07205
96642238
00020000 00000-0 20000-3 0 9092
2 25544 51
6347 268
5653 0002280 57
7720 302
3665 15
76316858 16746
Satellite: ISS
Catalog Number: 25544
Epoch time: 07205
96642238 = yrday
fracday
Element set: 909
Inclination: 51
6347 deg
RA of node: 268
5653 deg
Eccentricity:
0002280
Arg of perigee: 57
7720 deg
Mean anomaly: 302
3665 deg
Mean motion: 15
76316858 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1674
Checksum: 310
Coasting Arc #11 (Orbit 1689)
---------------------------------------
Vector Time (GMT): 2007/206/22:40:56
192
Vector Time (MET): N/A
Weight (LBS) : 508148
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2361860
23 A = 6723898
59 meter
Y = 5967172
55 meter E =
0015728
Z = 1984463
23 I = 51
33012
XDOT = -4049
464672 Wp = 105
52771
YDOT = 3464
971615 meter/sec RA = 262
73357 deg
ZDOT = -5566
998519 TA = 52
23914
MA = 52
09675
Ha = 187
304 n
mi
Hp = 179
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7748885
28 X = 2285318
80
Y = 19577337
76 feet Y = 5993155
90 meter
Z = 6510706
12 Z = 1995752
14
XDOT = -13285
645249 XDOT = -4060
866262
YDOT = 11368
017111 feet/sec YDOT = 3419
625405 meter/sec
ZDOT = -18264
430835 ZDOT = -5586
697792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17391704
86 X = -5300991
64
Y = 11843934
26 feet Y = 3610031
16 meter
Z = 6554120
41 Z = 1997695
90
XDOT = -13134
261993 XDOT = -4003
323055
YDOT = -9079
891956 feet/sec YDOT = -2767
551068 meter/sec
ZDOT = -18338
591472 ZDOT = -5589
602681
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 07206
98076457
00020000 00000-0 20000-3 0 9101
2 25544 51
6342 263
3375 0002262 63
7649 296
3748 15
76302609 16903
Satellite: ISS
Catalog Number: 25544
Epoch time: 07206
98076457 = yrday
fracday
Element set: 910
Inclination: 51
6342 deg
RA of node: 263
3375 deg
Eccentricity:
0002262
Arg of perigee: 63
7649 deg
Mean anomaly: 296
3748 deg
Mean motion: 15
76302609 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1690
Checksum: 306
Coasting Arc #12 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2007/207/22:40:56
192
Vector Time (MET): N/A
Weight (LBS) : 508148
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3639746
86 A = 6714051
19 meter
Y = -2427002
54 meter E =
0005948
Z = 5088609
11 I = 51
30265
XDOT = 2722
595017 Wp = 106
30933
YDOT = 7070
707457 meter/sec RA = 257
58721 deg
ZDOT = 1421
938916 TA = 330
00324
MA = 330
03731
Ha = 187
110 n
mi
Hp = 179
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11941426
70 X = 3641896
20
Y = -7962606
76 feet Y = -2386289
70 meter
Z = 16694911
78 Z = 5106295
60
XDOT = 8932
398349 XDOT = 2636
419534
YDOT = 23197
859111 feet/sec YDOT = 7100
670969 meter/sec
ZDOT = 4665
153923 ZDOT = 1434
957031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10548724
08 X = 3215251
10
Y = 9617419
70 feet Y = 2931389
52 meter
Z = 16761578
57 Z = 5108929
15
XDOT = -19717
469695 XDOT = -6009
884763
YDOT = 13391
699455 feet/sec YDOT = 4081
789994 meter/sec
ZDOT = 4715
250211 ZDOT = 1437
208264
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 07207
99508678
00020000 00000-0 20000-3 0 9119
2 25544 51
6344 258
1096 0002239 63
7634 296
3760 15
76363993 17060
Satellite: ISS
Catalog Number: 25544
Epoch time: 07207
99508678 = yrday
fracday
Element set: 911
Inclination: 51
6344 deg
RA of node: 258
1096 deg
Eccentricity:
0002239
Arg of perigee: 63
7634 deg
Mean anomaly: 296
3760 deg
Mean motion: 15
76363993 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1706
Checksum: 321
Coasting Arc #13 (Orbit 1720)
---------------------------------------
Vector Time (GMT): 2007/208/22:40:56
192
Vector Time (MET): N/A
Weight (LBS) : 508148
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2372883
50 A = 6725275
64 meter
Y = -6270024
02 meter E =
0013306
Z = -456676
85 I = 51
34822
XDOT = 4369
687372 Wp = 45
27356
YDOT = -2081
915439 meter/sec RA = 252
39395 deg
ZDOT = 5995
125866 TA = 309
73398
MA = 309
85116
Ha = 187
149 n
mi
Hp = 179
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7785050
85 X = -2300376
39
Y = -20570944
96 feet Y = -6296153
46 meter
Z = -1498283
63 Z = -468029
06
XDOT = 14336
244659 XDOT = 4363
520143
YDOT = -6830
431230 feet/sec YDOT = -2033
086625 meter/sec
ZDOT = 19669
048118 ZDOT = 6016
338132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17918665
98 X = 5461609
39
Y = -12749875
11 feet Y = -3886161
93 meter
Z = -1541992
64 Z = -469999
36
XDOT = 9292
349518 XDOT = 2832
308133
YDOT = 10715
658755 feet/sec YDOT = 3266
132789 meter/sec
ZDOT = 19749
107069 ZDOT = 6019
527834
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 07208
94599898
00020000 00000-0 20000-3 0 9120
2 25544 51
6343 253
2083 0002205 64
6697 295
4696 15
76393138 17212
Satellite: ISS
Catalog Number: 25544
Epoch time: 07208
94599898 = yrday
fracday
Element set: 912
Inclination: 51
6343 deg
RA of node: 253
2083 deg
Eccentricity:
0002205
Arg of perigee: 64
6697 deg
Mean anomaly: 295
4696 deg
Mean motion: 15
76393138 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1721
Checksum: 324
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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