Date:
November 1st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 997)
---------------------------------------
Vector Time (GMT): 2008/305/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1471418
52 A = 6725420
71 meter
Y = -4014950
73 meter E =
0010773
Z = -5200356
86 I = 51
82356
XDOT = 6556
496294 Wp = 75
81671
YDOT = 3858
841358 meter/sec RA = 37
14653 deg
ZDOT = -1123
447601 TA = 183
46975
MA = 183
47723
Ha = 191
393 n
mi
Hp = 187
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4827488
57 X = 1541468
16
Y = -13172410
54 feet Y = -3998104
61 meter
Z = -17061538
27 Z = -5193038
49
XDOT = 21510
814612 XDOT = 6518
316478
YDOT = 12660
240677 feet/sec YDOT = 3931
946458 meter/sec
ZDOT = -3685
851710 ZDOT = -1091
687745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2775733
97 X = 846043
71
Y = 13786553
68 feet Y = 4202141
56 meter
Z = -17033477
97 Z = -5191804
08
XDOT = -23964
704958 XDOT = -7304
442071
YDOT = 420
848635 feet/sec YDOT = 128
274664 meter/sec
ZDOT = -3562
467818 ZDOT = -1085
840191
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 08305
49690195
00020000 00000-0 20000-3 0 9008
2 25544 51
6441 37
5933 0003842 277
2623 82
8102 15
72272330 9988
Satellite: ISS
Catalog Number: 25544
Epoch time: 08305
49690195 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 37
5933 deg
Eccentricity:
0003842
Arg of perigee: 277
2623 deg
Mean anomaly: 82
8102 deg
Mean motion: 15
72272330 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 998
Checksum: 288
Coasting Arc #2 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2008/306/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6099117
39 A = 6736111
91 meter
Y = -2410832
38 meter E =
0010578
Z = 1513119
27 I = 51
83497
XDOT = 545
512619 Wp = 124
11484
YDOT = -5034
196398 meter/sec RA = 32
01488 deg
ZDOT = -5799
140376 TA = 39
27039
MA = 39
19371
Ha = 191
481 n
mi
Hp = 187
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20010227
66 X = -6079056
43
Y = -7909555
05 feet Y = -2478924
15 meter
Z = 4964302
06 Z = 1483537
53
XDOT = 1789
739563 XDOT = 629
937239
YDOT = -16516
392381 feet/sec YDOT = -5027
623814 meter/sec
ZDOT = -19026
051103 ZDOT = -5796
285392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21123073
93 X = 6438312
94
Y = -4232370
97 feet Y = -1290026
67 meter
Z = 4849469
10 Z = 1478118
18
XDOT = 7060
654041 XDOT = 2152
087352
YDOT = 13362
525030 feet/sec YDOT = 4072
897629 meter/sec
ZDOT = -19015
359876 ZDOT = -5795
881690
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 08306
51384137
00020000 00000-0 20000-3 0 9019
2 25544 51
6437 32
3849 0003682 281
1343 78
9405 15
72287129 10141
Satellite: ISS
Catalog Number: 25544
Epoch time: 08306
51384137 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 32
3849 deg
Eccentricity:
0003682
Arg of perigee: 281
1343 deg
Mean anomaly: 78
9405 deg
Mean motion: 15
72287129 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1014
Checksum: 282
Coasting Arc #3 (Orbit 1029)
---------------------------------------
Vector Time (GMT): 2008/307/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 562492
58 A = 6726537
03 meter
Y = 4595557
65 meter E =
0003166
Z = 4878780
14 I = 51
77841
XDOT = -7165
926644 Wp = 140
67953
YDOT = -1590
615030 meter/sec RA = 26
93586 deg
ZDOT = 2321
245605 TA = 286
73446
MA = 286
76920
Ha = 191
422 n
mi
Hp = 187
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1845448
11 X = 487361
69
Y = 15077288
89 feet Y = 4601427
41 meter
Z = 16006496
53 Z = 4881330
57
XDOT = -23510
258017 XDOT = -7158
884004
YDOT = -5218
553248 feet/sec YDOT = -1670
709320 meter/sec
ZDOT = 7615
635186 ZDOT = 2286
449687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9855943
00 X = -3004091
43
Y = -11543974
26 feet Y = -3518603
35 meter
Z = 16016719
26 Z = 4881896
03
XDOT = 21625
323121 XDOT = 6591
398487
YDOT = -8069
448482 feet/sec YDOT = -2459
567897 meter/sec
ZDOT = 7480
651104 ZDOT = 2280
102457
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 08307
53076532
00020000 00000-0 20000-3 0 9020
2 25544 51
6442 27
1754 0003773 286
5678 73
5070 15
72347033 10303
Satellite: ISS
Catalog Number: 25544
Epoch time: 08307
53076532 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 27
1754 deg
Eccentricity:
0003773
Arg of perigee: 286
5678 deg
Mean anomaly: 73
5070 deg
Mean motion: 15
72347033 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1030
Checksum: 275
Coasting Arc #4 (Orbit 1044)
---------------------------------------
Vector Time (GMT): 2008/308/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6232723
63 A = 6734297
71 meter
Y = 355468
57 meter E =
0005051
Z = -2517778
31 I = 51
77695
XDOT = 1846
680935 Wp = 4
71487
YDOT = 5248
534594 meter/sec RA = 21
78404 deg
ZDOT = 5318
118469 TA = 326
85380
MA = 326
88543
Ha = 191
627 n
mi
Hp = 187
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20448568
35 X = 6240516
67
Y = 1166235
48 feet Y = 425210
21 meter
Z = -8260427
53 Z = -2487480
14
XDOT = 6058
664485 XDOT = 1762
018707
YDOT = 17219
601686 feet/sec YDOT = 5268
711567 meter/sec
ZDOT = 17447
895239 ZDOT = 5326
884494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17487749
64 X = -5330266
09
Y = 10752184
27 feet Y = 3277265
77 meter
Z = -8142963
95 Z = -2481975
41
XDOT = -13944
008622 XDOT = -4250
133828
YDOT = -9453
512336 feet/sec YDOT = -2881
430560 meter/sec
ZDOT = 17482
255215 ZDOT = 5328
591389
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 08308
48412188
00020000 00000-0 20000-3 0 9037
2 25544 51
6439 22
2928 0003889 292
9603 67
1149 15
72315516 10458
Satellite: ISS
Catalog Number: 25544
Epoch time: 08308
48412188 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 22
2928 deg
Eccentricity:
0003889
Arg of perigee: 292
9603 deg
Mean anomaly: 67
1149 deg
Mean motion: 15
72315516 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1045
Checksum: 297
Coasting Arc #5 (Orbit 1060)
---------------------------------------
Vector Time (GMT): 2008/309/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2623641
16 A = 6728532
73 meter
Y = -4393026
22 meter E =
0007197
Z = -4376668
89 I = 51
72950
XDOT = 6867
577264 Wp = 46
17978
YDOT = -726
750857 meter/sec RA = 16
71489 deg
ZDOT = -3385
939155 TA = 189
70678
MA = 189
72069
Ha = 191
608 n
mi
Hp = 187
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8607746
60 X = -2553061
17
Y = -14412815
69 feet Y = -4421970
44 meter
Z = -14359149
90 Z = -4389243
56
XDOT = 22531
421469 XDOT = 6891
642081
YDOT = -2384
353204 feet/sec YDOT = -649
818915 meter/sec
ZDOT = -11108
724261 ZDOT = -3352
517418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15348595
86 X = 4678252
02
Y = 6695657
32 feet Y = 2040836
35 meter
Z = -14408210
21 Z = -4391622
47
XDOT = -16435
617310 XDOT = -5009
576156
YDOT = 14039
684762 feet/sec YDOT = 4279
295916 meter/sec
ZDOT = -10979
229270 ZDOT = -3346
469081
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 08309
50102234
00020000 00000-0 20000-3 0 9040
2 25544 51
6430 17
0837 0003788 296
5074 63
5699 15
72345109 10619
Satellite: ISS
Catalog Number: 25544
Epoch time: 08309
50102234 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 17
0837 deg
Eccentricity:
0003788
Arg of perigee: 296
5074 deg
Mean anomaly: 63
5699 deg
Mean motion: 15
72345109 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1061
Checksum: 281
Coasting Arc #6 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2008/310/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5604957
39 A = 6731876
30 meter
Y = 1573459
17 meter E =
0009621
Z = 3374392
78 I = 51
71306
XDOT = -4089
691928 Wp = 77
78267
YDOT = -4578
241305 meter/sec RA = 11
54831 deg
ZDOT = -4645
186503 TA = 62
50795
MA = 62
41018
Ha = 191
732 n
mi
Hp = 187
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18388967
83 X = -5638527
97
Y = 5162267
63 feet Y = 1510593
47 meter
Z = 11070842
45 Z = 3347081
94
XDOT = -13417
624436 XDOT = -4015
627468
YDOT = -15020
476721 feet/sec YDOT = -4623
560314 meter/sec
ZDOT = -15240
113200 ZDOT = -4664
874834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11679526
87 X = 3559919
79
Y = -15189537
53 feet Y = -4629771
04 meter
Z = 10965094
58 Z = 3342160
83
XDOT = 18564
642077 XDOT = 5658
502905
YDOT = 3186
459488 feet/sec YDOT = 971
232852 meter/sec
ZDOT = -15316
761531 ZDOT = -4668
548915
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 08310
51790886
00020000 00000-0 20000-3 0 9050
2 25544 51
6435 11
8742 0003858 303
7377 56
3418 15
72404804 10770
Satellite: ISS
Catalog Number: 25544
Epoch time: 08310
51790886 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 11
8742 deg
Eccentricity:
0003858
Arg of perigee: 303
7377 deg
Mean anomaly: 56
3418 deg
Mean motion: 15
72404804 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1077
Checksum: 292
Coasting Arc #7 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2008/311/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4429213
20 A = 6730656
53 meter
Y = 3449613
06 meter E =
0008635
Z = 3704430
46 I = 51
68001
XDOT = -5757
847390 Wp = 83
16129
YDOT = 2766
632257 meter/sec RA = 6
48033 deg
ZDOT = 4300
540394 TA = 321
42563
MA = 321
48730
Ha = 191
679 n
mi
Hp = 187
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14531539
37 X = 4372314
11
Y = 11317628
14 feet Y = 3498824
86 meter
Z = 12153643
23 Z = 3725809
80
XDOT = -18890
575428 XDOT = -5809
247988
YDOT = 9076
877483 feet/sec YDOT = 2701
957193 meter/sec
ZDOT = 14109
384496 ZDOT = 4272
443498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18363567
76 X = -5597215
45
Y = -79705
40 feet Y = -24294
21 meter
Z = 12236764
81 Z = 3729765
91
XDOT = 9421
626448 XDOT = 2871
711741
YDOT = -17460
447852 feet/sec YDOT = -5321
944505 meter/sec
ZDOT = 14000
677069 ZDOT = 4267
406371
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 08311
53478300
00020000 00000-0 20000-3 0 9068
2 25544 51
6433 6
6647 0003803 307
0381 53
0433 15
72414074 10935
Satellite: ISS
Catalog Number: 25544
Epoch time: 08311
53478300 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 6
6647 deg
Eccentricity:
0003803
Arg of perigee: 307
0381 deg
Mean anomaly: 53
0433 deg
Mean motion: 15
72414074 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1093
Checksum: 255
Coasting Arc #8 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2008/312/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4314089
85 A = 6729411
38 meter
Y = -3146162
20 meter E =
0004393
Z = -4099414
17 I = 51
64593
XDOT = 5903
066968 Wp = 87
84364
YDOT = 3144
474994 meter/sec RA = 1
30785 deg
ZDOT = 3802
573936 TA = 221
20898
MA = 221
24215
Ha = 191
929 n
mi
Hp = 187
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14153838
08 X = 4368864
70
Y = -10322054
48 feet Y = -3097613
28 meter
Z = -13449521
56 Z = -4078322
89
XDOT = 19367
017612 XDOT = 5848
993643
YDOT = 10316
519009 feet/sec YDOT = 3210
184145 meter/sec
ZDOT = 12475
636273 ZDOT = 3831
120238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4627468
07 X = -1410452
27
Y = 16960209
72 feet Y = 5169471
92 meter
Z = -13367998
98 Z = -4074566
09
XDOT = -20266
203088 XDOT = -6177
138701
YDOT = 4381
663519 feet/sec YDOT = 1335
531040 meter/sec
ZDOT = 12586
514931 ZDOT = 3836
369751
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 08312
48809197
00020000 00000-0 20000-3 0 9076
2 25544 51
6427 1
7811 0003731 313
9376 46
1478 15
72441625 11088
Satellite: ISS
Catalog Number: 25544
Epoch time: 08312
48809197 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 1
7811 deg
Eccentricity:
0003731
Arg of perigee: 313
9376 deg
Mean anomaly: 46
1478 deg
Mean motion: 15
72441625 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1108
Checksum: 286
Coasting Arc #9 (Orbit 1123)
---------------------------------------
Vector Time (GMT): 2008/313/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5743247
92 A = 6732809
35 meter
Y = -1945817
85 meter E =
0002129
Z = -2928739
36 I = 51
62874
XDOT = 3996
666048 Wp = 55
67950
YDOT = -4245
171519 meter/sec RA = 356
23342 deg
ZDOT = -5018
419598 TA = 158
01247
MA = 158
00333
Ha = 192
022 n
mi
Hp = 186
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18842676
91 X = -5706835
02
Y = -6383916
82 feet Y = -2009838
60 meter
Z = -9608724
94 Z = -2956552
21
XDOT = 13112
421417 XDOT = 4068
218314
YDOT = -13927
728080 feet/sec YDOT = -4200
078461 meter/sec
ZDOT = -16464
631228 ZDOT = -4998
829528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18524143
86 X = 5646159
05
Y = -7111320
30 feet Y = -2167530
43 meter
Z = -9716670
21 Z = -2961641
08
XDOT = -1759
903320 XDOT = -536
418532
YDOT = 17802
806207 feet/sec YDOT = 5426
295332 meter/sec
ZDOT = -16389
010454 ZDOT = -4995
370386
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 08313
50494213
00020000 00000-0 20000-3 0 9080
2 25544 51
6432 356
5713 0003769 319
5052 40
5829 15
72442108 11243
Satellite: ISS
Catalog Number: 25544
Epoch time: 08313
50494213 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 356
5713 deg
Eccentricity:
0003769
Arg of perigee: 319
5052 deg
Mean anomaly: 40
5829 deg
Mean motion: 15
72442108 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1124
Checksum: 275
Coasting Arc #10 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2008/314/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2585874
58 A = 6727207
63 meter
Y = 4129790
58 meter E =
0008393
Z = 4637114
94 I = 51
58059
XDOT = -7047
226999 Wp = 36
32056
YDOT = -1189
152714 meter/sec RA = 351
06207 deg
ZDOT = -2861
532583 TA = 82
04892
MA = 81
95368
Ha = 192
098 n
mi
Hp = 186
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8483840
50 X = -2654389
25
Y = 13549181
70 feet Y = 4100490
81 meter
Z = 15213631
69 Z = 4624385
95
XDOT = -23120
823488 XDOT = -7019
504751
YDOT = -3901
419666 feet/sec YDOT = -1267
803916 meter/sec
ZDOT = -9388
230259 ZDOT = -2895
701565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2352743
58 X = -717116
24
Y = -15859068
22 feet Y = -4833843
99 meter
Z = 15164597
47 Z = 4622169
31
XDOT = 18863
602674 XDOT = 5749
626095
YDOT = -11931
523325 feet/sec YDOT = -3636
728309 meter/sec
ZDOT = -9520
751544 ZDOT = -2901
925071
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 08314
52177767
00020000 00000-0 20000-3 0 9096
2 25544 51
6429 351
3619 0003940 322
9060 37
1829 15
72488301 11400
Satellite: ISS
Catalog Number: 25544
Epoch time: 08314
52177767 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 351
3619 deg
Eccentricity:
0003940
Arg of perigee: 322
9060 deg
Mean anomaly: 37
1829 deg
Mean motion: 15
72488301 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1140
Checksum: 288
Coasting Arc #11 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2008/315/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6405039
11 A = 6734716
46 meter
Y = 78743
12 meter E =
0014079
Z = 2053189
15 I = 51
57645
XDOT = -1848
300938 Wp = 53
36722
YDOT = 5004
481403 meter/sec RA = 345
97421 deg
ZDOT = 5555
972532 TA = 329
56316
MA = 329
64481
Ha = 192
278 n
mi
Hp = 186
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21013907
85 X = 6393708
21
Y = 258343
57 feet Y = 150304
63 meter
Z = 6736184
89 Z = 2084278
30
XDOT = -6063
979455 XDOT = -1931
115259
YDOT = 16418
902241 feet/sec YDOT = 4983
349620 meter/sec
ZDOT = 18228
256339 ZDOT = 5546
792016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15822759
89 X = -4822777
22
Y = 13771470
91 feet Y = 4197544
33 meter
Z = 6856683
59 Z = 2089917
16
XDOT = -5324
199137 XDOT = -1622
815897
YDOT = -15204
237550 feet/sec YDOT = -4634
251605 meter/sec
ZDOT = 18193
038393 ZDOT = 5545
238102
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 08315
53860457
00020000 00000-0 20000-3 0 9105
2 25544 51
6425 346
1518 0003891 332
0802 28
0151 15
72445838 11569
Satellite: ISS
Catalog Number: 25544
Epoch time: 08315
53860457 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 346
1518 deg
Eccentricity:
0003891
Arg of perigee: 332
0802 deg
Mean anomaly: 28
0151 deg
Mean motion: 15
72445838 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1156
Checksum: 276
Coasting Arc #12 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2008/316/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 622803
49 A = 6725607
61 meter
Y = -4442380
33 meter E =
0011044
Z = -5020481
42 I = 51
51859
XDOT = 7397
104954 Wp = 87
95025
YDOT = -1031
045460 meter/sec RA = 340
80987 deg
ZDOT = 1833
807000 TA = 199
76308
MA = 199
80591
Ha = 192
325 n
mi
Hp = 186
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2043318
54 X = 696822
09
Y = -14574738
61 feet Y = -4435001
83 meter
Z = -16471395
75 Z = -5017276
02
XDOT = 24268
717041 XDOT = 7399
175871
YDOT = -3382
695079 feet/sec YDOT = -948
315210 meter/sec
ZDOT = 6016
427165 ZDOT = 1869
748445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8318553
81 X = 2535495
20
Y = 12157237
07 feet Y = 3705525
86 meter
Z = -16459291
71 Z = -5016792
11
XDOT = -14620
558902 XDOT = -4456
346353
YDOT = 18320
872250 feet/sec YDOT = 5584
201862 meter/sec
ZDOT = 6155
648724 ZDOT = 1876
241731
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 08316
49186457
00020000 00000-0 20000-3 0 9113
2 25544 51
6434 341
2675 0003938 333
3027 26
7932 15
72476873 11716
Satellite: ISS
Catalog Number: 25544
Epoch time: 08316
49186457 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 341
2675 deg
Eccentricity:
0003938
Arg of perigee: 333
3027 deg
Mean anomaly: 26
7932 deg
Mean motion: 15
72476873 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1171
Checksum: 301
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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