Date:
February 9th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12852 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 806)
---------------------------------------
Vector Time (GMT): 2008/039/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -885763
36 A = 6709267
84 meter
Y = -4330490
13 meter E =
0015329
Z = -5059789
46 I = 51
43344
XDOT = 6775
380586 Wp = 80
39121
YDOT = -3272
709208 meter/sec RA = 324
32364 deg
ZDOT = 1621
579994 TA = 205
20245
MA = 205
27732
Ha = 185
109 n
mi
Hp = 176
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2906047
75 X = -812694
48
Y = -14207644
77 feet Y = -4339986
79 meter
Z = -16600359
13 Z = -5063914
81
XDOT = 22228
938932 XDOT = 6803
595852
YDOT = -10737
234933 feet/sec YDOT = -3196
785250 meter/sec
ZDOT = 5320
144337 ZDOT = 1654
562443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5200643
22 X = 1585156
05
Y = -13517276
46 feet Y = -4120065
87 meter
Z = -16616580
70 Z = -5064733
80
XDOT = 23518
224403 XDOT = 7168
354798
YDOT = 2380
667415 feet/sec YDOT = 725
627428 meter/sec
ZDOT = 5445
982011 ZDOT = 1659
935317
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 08039
54220430
00020000 00000-0 20000-3 0 9009
2 25544 51
6407 324
8051 0005721 18
4029 341
7342 15
78127916 8073
Satellite: ISS
Catalog Number: 25544
Epoch time: 08039
54220430 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 324
8051 deg
Eccentricity:
0005721
Arg of perigee: 18
4029 deg
Mean anomaly: 341
7342 deg
Mean motion: 15
78127916 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 807
Checksum: 264
Coasting Arc #2 (Orbit 822)
---------------------------------------
Vector Time (GMT): 2008/040/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5770132
27 A = 6717033
84 meter
Y = 2135086
03 meter E =
0006715
Z = -2704656
72 I = 51
43760
XDOT = 306
166255 Wp = 65
96830
YDOT = -5703
334923 meter/sec RA = 319
17892 deg
ZDOT = -5162
824682 TA = 145
00704
MA = 144
96290
Ha = 185
081 n
mi
Hp = 176
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18930880
14 X = -5780439
86
Y = 7004875
42 feet Y = 2070503
39 meter
Z = -8873545
66 Z = -2732712
46
XDOT = 1004
482465 XDOT = 394
998535
YDOT = -18711
728749 feet/sec YDOT = -5699
414705 meter/sec
ZDOT = -16938
401188 ZDOT = -5161
121379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19774721
52 X = -6027335
12
Y = -3807186
94 feet Y = -1160430
58 meter
Z = -8980647
60 Z = -2737301
39
XDOT = 10371
181008 XDOT = 3161
135971
YDOT = -13983
357961 feet/sec YDOT = -4262
127506 meter/sec
ZDOT = -16932
472547 ZDOT = -5161
017632
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 08040
55535989
00020000 00000-0 20000-3 0 9011
2 25544 51
6409 319
5700 0005643 21
7976 338
3429 15
78180126 8236
Satellite: ISS
Catalog Number: 25544
Epoch time: 08040
55535989 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 319
5700 deg
Eccentricity:
0005643
Arg of perigee: 21
7976 deg
Mean anomaly: 338
3429 deg
Mean motion: 15
78180126 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 823
Checksum: 299
Coasting Arc #3 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2008/041/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1301811
61 A = 6714489
12 meter
Y = 5504070
66 meter E =
0015677
Z = 3611693
02 I = 51
40716
XDOT = -6196
835067 Wp = 67
34863
YDOT = 1411
240670 meter/sec RA = 313
94622 deg
ZDOT = -4363
310721 TA = 69
13315
MA = 68
96536
Ha = 185
109 n
mi
Hp = 176
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4271035
45 X = -1380806
85
Y = 18057974
61 feet Y = 5489071
53 meter
Z = 11849386
55 Z = 3605176
82
XDOT = -20330
823709 XDOT = -6190
959434
YDOT = 4630
054691 feet/sec YDOT = 1341
976793 meter/sec
ZDOT = -14315
323888 ZDOT = -4393
400174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12848686
30 X = -3916279
58
Y = 13409699
18 feet Y = 4087276
31 meter
Z = 11825031
96 Z = 3604269
74
XDOT = -18844
884917 XDOT = -5743
920923
YDOT = -5270
682796 feet/sec YDOT = -1606
504116 meter/sec
ZDOT = -14430
275688 ZDOT = -4398
348030
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 08041
56848114
00020000 00000-0 20000-3 0 9021
2 25544 51
6401 314
3346 0005658 26
2005 333
9446 15
78230766 8399
Satellite: ISS
Catalog Number: 25544
Epoch time: 08041
56848114 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 314
3346 deg
Eccentricity:
0005658
Arg of perigee: 26
2005 deg
Mean anomaly: 333
9446 deg
Mean motion: 15
78230766 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 839
Checksum: 282
Coasting Arc #4 (Orbit 854)
---------------------------------------
Vector Time (GMT): 2008/042/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4854276
05 A = 6710526
47 meter
Y = -143281
56 meter E =
0009966
Z = 4621969
26 I = 51
37554
XDOT = -2502
986460 Wp = 82
44310
YDOT = 6724
398664 meter/sec RA = 308
80798 deg
ZDOT = 2833
344544 TA = 339
49467
MA = 339
53465
Ha = 184
919 n
mi
Hp = 175
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15926102
53 X = 4833065
08
Y = -470083
84 feet Y = -89116
71 meter
Z = 15163941
14 Z = 4645499
50
XDOT = -8211
897835 XDOT = -2591
757387
YDOT = 22061
675407 feet/sec YDOT = 6695
912600 meter/sec
ZDOT = 9295
749817 ZDOT = 2820
969342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14045870
08 X = 4281181
20
Y = 7337432
12 feet Y = 2236449
31 meter
Z = 15253932
44 Z = 4649398
61
XDOT = -17463
953249 XDOT = -5323
012950
YDOT = 14176
199218 feet/sec YDOT = 4320
905522 meter/sec
ZDOT = 9249
113858 ZDOT = 2819
129904
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 08042
58156662
00020000 00000-0 20000-3 0 9035
2 25544 51
6404 309
0985 0005620 29
4150 330
7331 15
78289290 8559
Satellite: ISS
Catalog Number: 25544
Epoch time: 08042
58156662 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 309
0985 deg
Eccentricity:
0005620
Arg of perigee: 29
4150 deg
Mean anomaly: 330
7331 deg
Mean motion: 15
78289290 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 855
Checksum: 286
Coasting Arc #5 (Orbit 869)
---------------------------------------
Vector Time (GMT): 2008/043/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2880316
87 A = 6719273
39 meter
Y = -5958169
73 meter E =
0015088
Z = -1122857
87 I = 51
38848
XDOT = 4824
463067 Wp = 35
30668
YDOT = 1232
630468 meter/sec RA = 303
58787 deg
ZDOT = 5886
253831 TA = 312
33183
MA = 312
45954
Ha = 184
961 n
mi
Hp = 175
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9449858
50 X = 2952182
56
Y = -19547800
95 feet Y = -5925558
58 meter
Z = -3683916
90 Z = -1108690
78
XDOT = 15828
290901 XDOT = 4781
726968
YDOT = 4044
063216 feet/sec YDOT = 1286
341503 meter/sec
ZDOT = 19311
856400 ZDOT = 5909
587012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17605236
44 X = 5366076
07
Y = -12722571
12 feet Y = -3877839
68 meter
Z = -3630347
84 Z = -1106530
02
XDOT = 10995
582783 XDOT = 3351
453632
YDOT = 9728
167489 feet/sec YDOT = 2965
145451 meter/sec
ZDOT = 19401
237205 ZDOT = 5913
497100
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 08043
53130272
00020000 00000-0 20000-3 0 9041
2 25544 51
6406 304
1895 0005552 31
6956 328
4543 15
78355025 8706
Satellite: ISS
Catalog Number: 25544
Epoch time: 08043
53130272 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 304
1895 deg
Eccentricity:
0005552
Arg of perigee: 31
6956 deg
Mean anomaly: 328
4543 deg
Mean motion: 15
78355025 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 870
Checksum: 279
Coasting Arc #6 (Orbit 885)
---------------------------------------
Vector Time (GMT): 2008/044/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3477250
45 A = 6707609
99 meter
Y = -2376946
52 meter E =
0018487
Z = -5235577
05 I = 51
33435
XDOT = 3929
647622 Wp = 78
17409
YDOT = -6604
318051 meter/sec RA = 298
40589 deg
ZDOT = 393
350130 TA = 195
55115
MA = 195
60802
Ha = 184
895 n
mi
Hp = 175
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11408302
01 X = -3424979
39
Y = -7798380
97 feet Y = -2415538
79 meter
Z = -17177090
04 Z = -5252342
43
XDOT = 12892
544691 XDOT = 4001
295258
YDOT = -21667
710140 feet/sec YDOT = -6559
973895 meter/sec
ZDOT = 1290
518799 ZDOT = 412
614135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6471943
43 X = -1972648
36
Y = -12118672
18 feet Y = -3693771
28 meter
Z = -17241469
08 Z = -5255199
77
XDOT = 20506
573409 XDOT = 6250
403575
YDOT = -12868
579758 feet/sec YDOT = -3922
343110 meter/sec
ZDOT = 1363
518332 ZDOT = 415
600388
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 08044
54432111
00020000 00000-0 20000-3 0 9051
2 25544 51
6404 298
9528 0005533 34
4665 325
6858 15
78413368 8864
Satellite: ISS
Catalog Number: 25544
Epoch time: 08044
54432111 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 298
9528 deg
Eccentricity:
0005533
Arg of perigee: 34
4665 deg
Mean anomaly: 325
6858 deg
Mean motion: 15
78413368 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 886
Checksum: 307
Coasting Arc #7 (Orbit 901)
---------------------------------------
Vector Time (GMT): 2008/045/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3813850
75 A = 6718172
44 meter
Y = 5229702
95 meter E =
0007952
Z = -1802712
22 I = 51
35737
XDOT = -3110
100975 Wp = 101
08493
YDOT = -4208
283746 meter/sec RA = 293
23598 deg
ZDOT = -5651
073493 TA = 99
00594
MA = 98
91593
Ha = 184
874 n
mi
Hp = 175
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12512633
70 X = -3863289
49
Y = 17157818
07 feet Y = 5186777
94 meter
Z = -5914410
18 Z = -1821359
59
XDOT = -10203
743357 XDOT = -3035
360574
YDOT = -13806
705205 feet/sec YDOT = -4242
644564 meter/sec
ZDOT = -18540
267364 ZDOT = -5666
000801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18793666
02 X = -5728309
40
Y = 9844414
74 feet Y = 3000577
61 meter
Z = -5985197
30 Z = -1824288
14
XDOT = -2210
537173 XDOT = -673
771730
YDOT = -15482
702356 feet/sec YDOT = -4719
127678 meter/sec
ZDOT = -18597
809464 ZDOT = -5668
612325
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 08045
55730602
00020000 00000-0 20000-3 0 9060
2 25544 51
6403 293
7163 0005323 38
0166 322
1374 15
78419045 9026
Satellite: ISS
Catalog Number: 25544
Epoch time: 08045
55730602 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 293
7163 deg
Eccentricity:
0005323
Arg of perigee: 38
0166 deg
Mean anomaly: 322
1374 deg
Mean motion: 15
78419045 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 902
Checksum: 268
Coasting Arc #8 (Orbit 917)
---------------------------------------
Vector Time (GMT): 2008/046/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1970418
08 A = 6711469
81 meter
Y = 4836531
42 meter E =
0014942
Z = 4208654
64 I = 51
32554
XDOT = -4639
188412 Wp = 61
24581
YDOT = 5015
877502 meter/sec RA = 288
00201 deg
ZDOT = -3575
526602 TA = 65
26664
MA = 65
11120
Ha = 184
727 n
mi
Hp = 175
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6464626
23 X = 1895744
24
Y = 15867885
23 feet Y = 4858148
01 meter
Z = 13807922
06 Z = 4218045
66
XDOT = -15220
434421 XDOT = -4677
562954
YDOT = 16456
291018 feet/sec YDOT = 4963
785083 meter/sec
ZDOT = -11730
730320 ZDOT = -3598
156357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1019366
47 X = -310702
90
Y = 17074384
08 feet Y = 5204272
27 meter
Z = 13844355
75 Z = 4219759
63
XDOT = -19493
666354 XDOT = -5941
669505
YDOT = 8461
774926 feet/sec YDOT = 2579
148997 meter/sec
ZDOT = -11816
777917 ZDOT = -3601
753909
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 08046
57025435
00020000 00000-0 20000-3 0 9075
2 25544 51
6403 288
4792 0005495 39
5556 320
6010 15
78549462 9188
Satellite: ISS
Catalog Number: 25544
Epoch time: 08046
57025435 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 288
4792 deg
Eccentricity:
0005495
Arg of perigee: 39
5556 deg
Mean anomaly: 320
6010 deg
Mean motion: 15
78549462 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 918
Checksum: 305
Coasting Arc #9 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2008/047/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4158060
69 A = 6711596
11 meter
Y = -3198458
88 meter E =
0013601
Z = 4174003
67 I = 51
31724
XDOT = 1462
648517 Wp = 85
15792
YDOT = 6649
467889 meter/sec RA = 282
85912 deg
ZDOT = 3629
313434 TA = 327
74413
MA = 327
82724
Ha = 184
754 n
mi
Hp = 175
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13641931
39 X = 4173241
21
Y = -10493631
51 feet Y = -3151876
43 meter
Z = 13694237
77 Z = 4194239
78
XDOT = 4798
715608 XDOT = 1370
554278
YDOT = 21815
839532 feet/sec YDOT = 6665
308932 meter/sec
ZDOT = 11907
196306 ZDOT = 3636
195499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16684400
89 X = 5085405
39
Y = -3966382
36 feet Y = -1208953
34 meter
Z = 13771322
40 Z = 4197499
07
XDOT = -4975
367325 XDOT = -1516
491961
YDOT = 20608
893579 feet/sec YDOT = 6281
590763 meter/sec
ZDOT = 11934
229370 ZDOT = 3637
553112
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 08047
58317213
00020000 00000-0 20000-3 0 9086
2 25544 51
6395 283
2418 0005529 43
9926 316
1679 15
78530773 9348
Satellite: ISS
Catalog Number: 25544
Epoch time: 08047
58317213 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 283
2418 deg
Eccentricity:
0005529
Arg of perigee: 43
9926 deg
Mean anomaly: 316
1679 deg
Mean motion: 15
78530773 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 934
Checksum: 316
Coasting Arc #10 (Orbit 948)
---------------------------------------
Vector Time (GMT): 2008/048/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -614730
57 A = 6717659
40 meter
Y = -6430818
05 meter E =
0012632
Z = -1827445
78 I = 51
33224
XDOT = 4830
962358 Wp = 41
33785
YDOT = -2056
350793 meter/sec RA = 277
62299 deg
ZDOT = 5642
750092 TA = 298
25898
MA = 298
38643
Ha = 184
702 n
mi
Hp = 175
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2016832
57 X = -533897
32
Y = -21098484
43 feet Y = -6437240
28 meter
Z = -5995557
03 Z = -1830236
00
XDOT = 15849
614034 XDOT = 4826
187045
YDOT = -6746
557720 feet/sec YDOT = -2002
355163 meter/sec
ZDOT = 18512
959621 ZDOT = 5666
206570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6548380
52 X = 1995946
38
Y = -20154304
11 feet Y = -6143031
89 meter
Z = -6006921
12 Z = -1830909
56
XDOT = 15659
266537 XDOT = 4772
944440
YDOT = -425
788906 feet/sec YDOT = -129
780459 meter/sec
ZDOT = 18602
490803 ZDOT = 5670
039197
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 08048
53274804
00020000 00000-0 20000-3 0 9091
2 25544 51
6386 278
3317 0005356 45
6379 314
5224 15
78595110 9490
Satellite: ISS
Catalog Number: 25544
Epoch time: 08048
53274804 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 278
3317 deg
Eccentricity:
0005356
Arg of perigee: 45
6379 deg
Mean anomaly: 314
5224 deg
Mean motion: 15
78595110 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 949
Checksum: 313
Coasting Arc #11 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2008/049/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4207935
56 A = 6706864
16 meter
Y = 210365
38 meter E =
0019518
Z = -5234945
99 I = 51
29248
XDOT = 50
623778 Wp = 77
70854
YDOT = -7686
375290 meter/sec RA = 272
44794 deg
ZDOT = -346
557931 TA = 188
96513
MA = 189
00004
Ha = 184
637 n
mi
Hp = 174
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13805562
85 X = -4184545
54
Y = 690175
13 feet Y = 163440
73 meter
Z = -17175019
64 Z = -5255330
67
XDOT = 166
088510 XDOT = 138
253712
YDOT = -25217
766701 feet/sec YDOT = -7685
319216 meter/sec
ZDOT = -1137
001085 ZDOT = -346
099315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12938049
93 X = -3943517
62
Y = -4581707
77 feet Y = -1396504
53 meter
Z = -17253000
45 Z = -5258714
54
XDOT = 9428
189558 XDOT = 2873
712177
YDOT = -22308
705178 feet/sec YDOT = -6799
693338 meter/sec
ZDOT = -1136
081501 ZDOT = -346
277641
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 08049
54559684
00020000 00000-0 20000-3 0 9107
2 25544 51
6372 273
0934 0005320 49
8089 310
3542 15
78671552 9657
Satellite: ISS
Catalog Number: 25544
Epoch time: 08049
54559684 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 273
0934 deg
Eccentricity:
0005320
Arg of perigee: 49
8089 deg
Mean anomaly: 310
3542 deg
Mean motion: 15
78671552 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 965
Checksum: 306
Coasting Arc #12 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2008/050/12:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -702453
56 A = 6718132
65 meter
Y = 6558715
59 meter E =
0010500
Z = -1268134
75 I = 51
33050
XDOT = -4755
287569 Wp = 113
00960
YDOT = -1629
907078 meter/sec RA = 267
26283 deg
ZDOT = -5838
009836 TA = 80
98363
MA = 80
86482
Ha = 184
597 n
mi
Hp = 174
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2304637
66 X = -769581
76
Y = 21518095
78 feet Y = 6550485
02 meter
Z = -4160547
07 Z = -1271710
26
XDOT = -15601
337169 XDOT = -4708
349217
YDOT = -5347
464167 feet/sec YDOT = -1682
821015 meter/sec
ZDOT = -19153
575576 ZDOT = -5860
996235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9974279
88 X = -3040160
51
Y = 19202748
61 feet Y = 5852997
78 meter
Z = -4173504
47 Z = -1272084
16
XDOT = -11073
463592 XDOT = -3375
191703
YDOT = -9903
670550 feet/sec YDOT = -3018
638784 meter/sec
ZDOT = -19241
720551 ZDOT = -5864
876424
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 08050
55841160
00020000 00000-0 20000-3 0 9114
2 25544 51
6367 267
8561 0005207 53
4678 306
6967 15
78697029 9811
Satellite: ISS
Catalog Number: 25544
Epoch time: 08050
55841160 = yrday
fracday
Element set: 911
Inclination: 51
6367 deg
RA of node: 267
8561 deg
Eccentricity:
0005207
Arg of perigee: 53
4678 deg
Mean anomaly: 306
6967 deg
Mean motion: 15
78697029 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 981
Checksum: 317
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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