Date:
November 10th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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 1108)
---------------------------------------
Vector Time (GMT): 2008/312/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6695235
32 A = 6736497
96 meter
Y = -518381
19 meter E =
0007288
Z = -488691
78 I = 51
66909
XDOT = 801
644933 Wp = 140
19549
YDOT = -4738
067546 meter/sec RA = 1
12889 deg
ZDOT = -6011
598087 TA = 45
11345
MA = 45
05431
Ha = 191
928 n
mi
Hp = 187
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21965995
13 X = -6686567
06
Y = -1700725
68 feet Y = -593202
71 meter
Z = -1603319
48 Z = -521196
79
XDOT = 2630
068679 XDOT = 883
771000
YDOT = -15544
841029 feet/sec YDOT = -4728
643876 meter/sec
ZDOT = -19723
090837 ZDOT = -6007
504153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14332732
99 X = 4368617
02
Y = -16719753
42 feet Y = -5096180
84 meter
Z = -1729350
68 Z = -527106
09
XDOT = 9709
755430 XDOT = 2959
533455
YDOT = 10344
696729 feet/sec YDOT = 3153
063563 meter/sec
ZDOT = -19707
568326 ZDOT = -6006
866826
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
55162482
00020000 00000-0 20000-3 0 9006
2 25544 51
6430 1
4599 0003803 315
9219 44
1640 15
72440313 11093
Satellite: ISS
Catalog Number: 25544
Epoch time: 08312
55162482 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 1
4599 deg
Eccentricity:
0003803
Arg of perigee: 315
9219 deg
Mean anomaly: 44
1640 deg
Mean motion: 15
72440313 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1109
Checksum: 251
Coasting Arc #2 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2008/313/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 307022
55 A = 6724496
28 meter
Y = 4165774
65 meter E =
0002962
Z = 5269864
60 I = 51
59866
XDOT = -7679
380682 Wp = 358
64282
YDOT = 549
573938 meter/sec RA = 356
00027 deg
ZDOT = 15
877468 TA = 91
22337
MA = 91
18944
Ha = 192
027 n
mi
Hp = 186
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1007291
84 X = 234816
75
Y = 13667239
68 feet Y = 4168804
28 meter
Z = 17289582
02 Z = 5271180
72
XDOT = -25194
818512 XDOT = -7685
032486
YDOT = 1803
064101 feet/sec YDOT = 463
667062 meter/sec
ZDOT = 52
091432 ZDOT = -21
443520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11692952
83 X = -3564012
02
Y = -7134140
73 feet Y = -2174486
09 meter
Z = 17294988
11 Z = 5271512
38
XDOT = 12525
449617 XDOT = 3817
757043
YDOT = -20776
814504 feet/sec YDOT = -6332
773061 meter/sec
ZDOT = -92
524719 ZDOT = -28
201534
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
56846860
00020000 00000-0 20000-3 0 9018
2 25544 51
6422 356
2504 0003781 320
3366 39
7519 15
72458081 11253
Satellite: ISS
Catalog Number: 25544
Epoch time: 08313
56846860 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 356
2504 deg
Eccentricity:
0003781
Arg of perigee: 320
3366 deg
Mean anomaly: 39
7519 deg
Mean motion: 15
72458081 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1125
Checksum: 283
Coasting Arc #3 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2008/314/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6547788
85 A = 6736475
87 meter
Y = -1463858
74 meter E =
0012740
Z = -512780
65 I = 51
61027
XDOT = 1489
811482 Wp = 23
79425
YDOT = 4581
516644 meter/sec RA = 350
86943 deg
ZDOT = 6007
681855 TA = 330
62641
MA = 330
69796
Ha = 192
189 n
mi
Hp = 186
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21482246
88 X = 6566162
37
Y = -4802686
17 feet Y = -1390534
86 meter
Z = -1682351
21 Z = -480925
99
XDOT = 4887
832945 XDOT = 1409
284475
YDOT = 15031
222584 feet/sec YDOT = 4597
726405 meter/sec
ZDOT = 19710
242308 ZDOT = 6014
723889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8109182
77 X = -2471678
91
Y = 20474220
97 feet Y = 6240542
55 meter
Z = -1558993
88 Z = -475181
34
XDOT = -13622
576900 XDOT = -4152
161439
YDOT = -3909
545911 feet/sec YDOT = -1191
629594 meter/sec
ZDOT = 19737
870800 ZDOT = 6016
103020
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
52174790
00020000 00000-0 20000-3 0 9022
2 25544 51
6427 351
3663 0003889 325
6725 34
4185 15
72455954 11400
Satellite: ISS
Catalog Number: 25544
Epoch time: 08314
52174790 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 351
3663 deg
Eccentricity:
0003889
Arg of perigee: 325
6725 deg
Mean anomaly: 34
4185 deg
Mean motion: 15
72455954 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1140
Checksum: 294
Coasting Arc #4 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2008/315/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2233781
41 A = 6724841
39 meter
Y = -3677234
48 meter E =
0013401
Z = -5179740
52 I = 51
54288
XDOT = 7101
317523 Wp = 65
97036
YDOT = -2724
695753 meter/sec RA = 345
75527 deg
ZDOT = -1125
062459 TA = 193
24253
MA = 193
27775
Ha = 192
197 n
mi
Hp = 186
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7328679
15 X = -2167332
90
Y = -12064417
58 feet Y = -3701842
40 meter
Z = -16993899
34 Z = -5190431
15
XDOT = 23298
285837 XDOT = 7136
723247
YDOT = -8939
290527 feet/sec YDOT = -2645
086754 meter/sec
ZDOT = -3691
149799 ZDOT = -1090
477144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14054435
95 X = 4283792
08
Y = 559897
05 feet Y = 170656
62 meter
Z = -17035600
08 Z = -5192450
90
XDOT = -5255
493687 XDOT = -1601
874476
YDOT = 23380
875121 feet/sec YDOT = 7126
490737 meter/sec
ZDOT = -3557
304488 ZDOT = -1084
266408
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
53856525
00020000 00000-0 20000-3 0 9038
2 25544 51
6431 346
1564 0003832 328
7161 31
3773 15
72476065 11565
Satellite: ISS
Catalog Number: 25544
Epoch time: 08315
53856525 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 346
1564 deg
Eccentricity:
0003832
Arg of perigee: 328
7161 deg
Mean anomaly: 31
3773 deg
Mean motion: 15
72476065 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1156
Checksum: 285
Coasting Arc #5 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2008/316/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5728661
43 A = 6735548
35 meter
Y = 3228616
75 meter E =
0011120
Z = 1439059
23 I = 51
54961
XDOT = -3517
445798 Wp = 107
27849
YDOT = -3642
031736 meter/sec RA = 340
60160 deg
ZDOT = -5797
748440 TA = 56
87999
MA = 56
77332
Ha = 192
318 n
mi
Hp = 186
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18794820
97 X = -5771329
52
Y = 10592574
65 feet Y = 3164316
95 meter
Z = 4721322
94 Z = 1411124
80
XDOT = -11540
176501 XDOT = -3448
293143
YDOT = -11948
923017 feet/sec YDOT = -3680
979084 meter/sec
ZDOT = -19021
484383 ZDOT = -5814
668903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1078461
05 X = 328714
93
Y = -21570658
06 feet Y = -6574736
58 meter
Z = 4613291
26 Z = 1406131
18
XDOT = 14631
338646 XDOT = 4459
632019
YDOT = -3374
731220 feet/sec YDOT = -1028
618076 meter/sec
ZDOT = -19087
322976 ZDOT = -5817
816043
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
55536879
00020000 00000-0 20000-3 0 9049
2 25544 51
6416 340
9461 0003845 335
4062 24
6916 15
72516139 11724
Satellite: ISS
Catalog Number: 25544
Epoch time: 08316
55536879 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 340
9461 deg
Eccentricity:
0003845
Arg of perigee: 335
4062 deg
Mean anomaly: 24
6916 deg
Mean motion: 15
72516139 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1172
Checksum: 295
Coasting Arc #6 (Orbit 1187)
---------------------------------------
Vector Time (GMT): 2008/317/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3816216
72 A = 6725802
09 meter
Y = 2554886
42 meter E =
0003866
Z = 4910404
53 I = 51
48903
XDOT = -5827
587325 Wp = 86
27628
YDOT = 4546
696327 meter/sec RA = 335
49905 deg
ZDOT = 2162
162026 TA = 342
69060
MA = 342
70377
Ha = 192
313 n
mi
Hp = 186
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12520396
07 X = 3763509
17
Y = 8382173
28 feet Y = 2597266
59 meter
Z = 16110251
07 Z = 4928816
52
XDOT = -19119
380989 XDOT = -5888
499890
YDOT = 14916
982701 feet/sec YDOT = 4481
188182 meter/sec
ZDOT = 7093
707435 ZDOT = 2133
702808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13612958
45 X = -4149229
74
Y = 6276813
50 feet Y = 1913172
75 meter
Z = 16181789
48 Z = 4932209
43
XDOT = -2356
733683 XDOT = -718
332427
YDOT = -23125
664128 feet/sec YDOT = -7048
702426 meter/sec
ZDOT = 6983
732066 ZDOT = 2128
641534
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 08317
57215877
00020000 00000-0 20000-3 0 9055
2 25544 51
6409 335
7353 0003895 339
8300 20
2708 15
72525697 11883
Satellite: ISS
Catalog Number: 25544
Epoch time: 08317
57215877 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 335
7353 deg
Eccentricity:
0003895
Arg of perigee: 339
8300 deg
Mean anomaly: 20
2708 deg
Mean motion: 15
72525697 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1188
Checksum: 310
Coasting Arc #7 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2008/318/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4335346
28 A = 6733937
39 meter
Y = -4595010
21 meter E =
0008464
Z = -2320307
45 I = 51
49114
XDOT = 5074
048729 Wp = 20
48292
YDOT = 2062
739281 meter/sec RA = 330
32708 deg
ZDOT = 5409
329478 TA = 313
37531
MA = 313
44579
Ha = 192
453 n
mi
Hp = 186
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14223577
05 X = 4397678
26
Y = -15075492
83 feet Y = -4546181
14 meter
Z = -7612557
26 Z = -2299094
58
XDOT = 16647
141499 XDOT = 5024
327226
YDOT = 6767
517325 feet/sec YDOT = 2119
201734 meter/sec
ZDOT = 17747
143957 ZDOT = 5433
859511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5831487
59 X = 1777437
42
Y = 19920204
03 feet Y = 6071678
19 meter
Z = -7530662
63 Z = -2295345
97
XDOT = -12730
631933 XDOT = -3880
296613
YDOT = 10454
732227 feet/sec YDOT = 3186
602383 meter/sec
ZDOT = 17842
358939 ZDOT = 5438
351004
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 08318
52538628
00020000 00000-0 20000-3 0 9064
2 25544 51
6415 330
8514 0003874 343
8391 16
2647 15
72577023 12032
Satellite: ISS
Catalog Number: 25544
Epoch time: 08318
52538628 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 330
8514 deg
Eccentricity:
0003874
Arg of perigee: 343
8391 deg
Mean anomaly: 16
2647 deg
Mean motion: 15
72577023 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1203
Checksum: 288
Coasting Arc #8 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2008/319/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4901232
40 A = 6727323
16 meter
Y = -977909
44 meter E =
0011322
Z = -4514356
13 I = 51
44285
XDOT = 4007
747543 Wp = 48
81506
YDOT = -5785
700509 meter/sec RA = 325
23257 deg
ZDOT = -3095
597794 TA = 190
18599
MA = 190
20896
Ha = 192
527 n
mi
Hp = 186
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16080158
80 X = -4868002
38
Y = -3208364
30 feet Y = -1032531
52 meter
Z = -14810879
68 Z = -4538086
45
XDOT = 13148
778027 XDOT = 4087
184639
YDOT = -18981
957052 feet/sec YDOT = -5740
439042 meter/sec
ZDOT = -10156
160742 ZDOT = -3075
935270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10620387
72 X = 3237094
18
Y = -12382951
73 feet Y = -3774323
69 meter
Z = -14902923
77 Z = -4542411
16
XDOT = 9196
276503 XDOT = 2803
025078
YDOT = 20028
054812 feet/sec YDOT = 6104
551107 meter/sec
ZDOT = -10080
349721 ZDOT = -3072
490595
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 08319
54214938
00020000 00000-0 20000-3 0 9073
2 25544 51
6403 325
6399 0004002 346
8656 13
2401 15
72566620 12196
Satellite: ISS
Catalog Number: 25544
Epoch time: 08319
54214938 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 325
6399 deg
Eccentricity:
0004002
Arg of perigee: 346
8656 deg
Mean anomaly: 13
2401 deg
Mean motion: 15
72566620 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1219
Checksum: 281
Coasting Arc #9 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2008/320/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2612739
14 A = 6732053
88 meter
Y = 5385491
22 meter E =
0012691
Z = 3073515
99 I = 51
43533
XDOT = -5952
329120 Wp = 76
75113
YDOT = -90
602043 meter/sec RA = 320
04578 deg
ZDOT = -4881
457538 TA = 67
50391
MA = 67
36960
Ha = 192
580 n
mi
Hp = 186
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8571978
82 X = -2687697
34
Y = 17668934
46 feet Y = 5355854
56 meter
Z = 10083713
86 Z = 3060641
61
XDOT = -19528
638844 XDOT = -5927
159797
YDOT = -297
250798 feet/sec YDOT = -157
023067 meter/sec
ZDOT = -16015
280638 ZDOT = -4910
313521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11468670
37 X = -3495650
73
Y = -15972982
25 feet Y = -4868564
99 meter
Z = 10034181
04 Z = 3058418
38
XDOT = 8308
701575 XDOT = 2532
492240
YDOT = -16137
615531 feet/sec YDOT = -4918
745214 meter/sec
ZDOT = -16127
137821 ZDOT = -4915
551608
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 08320
55889777
00020000 00000-0 20000-3 0 9086
2 25544 51
6400 320
4289 0004190 350
2071 9
9009 15
72619269 12354
Satellite: ISS
Catalog Number: 25544
Epoch time: 08320
55889777 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 320
4289 deg
Eccentricity:
0004190
Arg of perigee: 350
2071 deg
Mean anomaly: 9
9009 deg
Mean motion: 15
72619269 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1235
Checksum: 292
Coasting Arc #10 (Orbit 1250)
---------------------------------------
Vector Time (GMT): 2008/321/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5347157
64 A = 6729067
62 meter
Y = -853734
25 meter E =
0010198
Z = 3984923
58 I = 51
40358
XDOT = -1914
269442 Wp = 79
55696
YDOT = 6347
763637 meter/sec RA = 314
95576 deg
ZDOT = 3921
940184 TA = 329
76449
MA = 329
82330
Ha = 192
460 n
mi
Hp = 185
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17543168
12 X = 5336948
46
Y = -2800965
40 feet Y = -793996
82 meter
Z = 13073896
26 Z = 4010875
61
XDOT = -6280
411555 XDOT = -2004
161292
YDOT = 20825
996185 feet/sec YDOT = 6325
854077 meter/sec
ZDOT = 12867
257820 ZDOT = 3912
422933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5524040
28 X = -1683727
48
Y = 16806369
17 feet Y = 5122581
32 meter
Z = 13174439
36 Z = 4015569
12
XDOT = -14365
352472 XDOT = -4378
559433
YDOT = -14796
738517 feet/sec YDOT = -4510
045900 meter/sec
ZDOT = 12830
803888 ZDOT = 3910
829025
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 08321
57563294
00020000 00000-0 20000-3 0 9093
2 25544 51
6397 315
2185 0004121 352
7573 7
3529 15
72631496 12517
Satellite: ISS
Catalog Number: 25544
Epoch time: 08321
57563294 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 315
2185 deg
Eccentricity:
0004121
Arg of perigee: 352
7573 deg
Mean anomaly: 7
3529 deg
Mean motion: 15
72631496 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1251
Checksum: 292
Coasting Arc #11 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2008/322/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 720438
81 A = 6730045
33 meter
Y = -5545266
83 meter E =
0006406
Z = -3747375
70 I = 51
38664
XDOT = 6095
849589 Wp = 63
01260
YDOT = -2055
092605 meter/sec RA = 309
76171 deg
ZDOT = 4221
408068 TA = 251
55179
MA = 251
62143
Ha = 192
760 n
mi
Hp = 185
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2363644
39 X = 800597
63
Y = -18193132
66 feet Y = -5536761
89 meter
Z = -12294539
68 Z = -3743681
63
XDOT = 19999
506524 XDOT = 6097
869826
YDOT = -6742
429808 feet/sec YDOT = -1986
914435 meter/sec
ZDOT = 13849
764004 ZDOT = 4251
026761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15228083
32 X = 4641519
80
Y = 10248158
20 feet Y = 3123638
62 meter
Z = -12280607
83 Z = -3743129
27
XDOT = -2040
998583 XDOT = -622
096368
YDOT = 19733
644809 feet/sec YDOT = 6014
814938 meter/sec
ZDOT = 13964
443095 ZDOT = 4256
362255
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 08322
52881003
00020000 00000-0 20000-3 0 9102
2 25544 51
6396 310
3335 0004232 358
5346 1
5803 15
72612259 12667
Satellite: ISS
Catalog Number: 25544
Epoch time: 08322
52881003 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 310
3335 deg
Eccentricity:
0004232
Arg of perigee: 358
5346 deg
Mean anomaly: 1
5803 deg
Mean motion: 15
72612259 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1266
Checksum: 261
Coasting Arc #12 (Orbit 1281)
---------------------------------------
Vector Time (GMT): 2008/323/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5158013
11 A = 6730938
79 meter
Y = 2699888
91 meter E =
0006743
Z = -3386937
90 I = 51
37249
XDOT = -206
513976 Wp = 49
37026
YDOT = -6160
728028 meter/sec RA = 304
66908 deg
ZDOT = -4598
173876 TA = 170
69640
MA = 170
68390
Ha = 192
792 n
mi
Hp = 185
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16922615
18 X = -5171367
05
Y = 8857903
23 feet Y = 2642134
62 meter
Z = -11112000
98 Z = -3412028
00
XDOT = -677
539292 XDOT = -115
271045
YDOT = -20212
362298 feet/sec YDOT = -6162
526859 meter/sec
ZDOT = -15085
872297 ZDOT = -4598
955986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -792514
99 X = -241558
57
Y = -19027410
85 feet Y = -5799554
83 meter
Z = -11209080
09 Z = -3416527
61
XDOT = 17134
068185 XDOT = 5222
463983
YDOT = 8172
307174 feet/sec YDOT = 2490
919227 meter/sec
ZDOT = -15089
344148 ZDOT = -4599
232096
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 08323
54551790
00020000 00000-0 20000-3 0 9113
2 25544 51
6397 305
1221 0004258 2
7693 357
3492 15
72657857 12822
Satellite: ISS
Catalog Number: 25544
Epoch time: 08323
54551790 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 305
1221 deg
Eccentricity:
0004258
Arg of perigee: 2
7693 deg
Mean anomaly: 357
3492 deg
Mean motion: 15
72657857 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1282
Checksum: 297
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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