Date:
January 21st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2008/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3939176
05 A = 6713634
42 meter
Y = -2489358
23 meter E =
0006872
Z = -4839298
37 I = 51
94813
XDOT = 1504
195628 Wp = 51
47524
YDOT = 7143
869459 meter/sec RA = 93
32984 deg
ZDOT = -2448
564448 TA = 194
69771
MA = 194
71770
Ha = 183
447 n
mi
Hp = 181
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12923805
95 X = 3990227
87
Y = -8167185
79 feet Y = -2445022
45 meter
Z = -15876963
14 Z = -4820038
15
XDOT = 4935
025026 XDOT = 1436
094556
YDOT = 23437
891926 feet/sec YDOT = 7160
309570 meter/sec
ZDOT = -8033
347927 ZDOT = -2441
422226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12539780
00 X = 3822124
94
Y = 8877264
13 feet Y = 2705790
11 meter
Z = -15803599
00 Z = -4816936
98
XDOT = -19078
724761 XDOT = -5815
195307
YDOT = 12687
845522 feet/sec YDOT = 3867
255315 meter/sec
ZDOT = -8005
297530 ZDOT = -2440
014687
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 08014
52004876
00020000 00000-0 20000-3 0 9004
2 25544 51
6382 93
9655 0006063 276
4356 83
6118 15
76964852 4129
Satellite: ISS
Catalog Number: 25544
Epoch time: 08014
52004876 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 93
9655 deg
Eccentricity:
0006063
Arg of perigee: 276
4356 deg
Mean anomaly: 83
6118 deg
Mean motion: 15
76964852 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 412
Checksum: 295
Coasting Arc #2 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2008/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1122775
89 A = 6722953
21 meter
Y = -6519698
75 meter E =
0008591
Z = 1168156
87 I = 51
98072
XDOT = 4571
603353 Wp = 136
04153
YDOT = -1851
564677 meter/sec RA = 88
16383 deg
ZDOT = -5920
209457 TA = 31
20712
MA = 31
15615
Ha = 183
589 n
mi
Hp = 181
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3683647
93 X = -1055462
83
Y = -21390087
77 feet Y = -6531877
97 meter
Z = 3832535
65 Z = 1162865
58
XDOT = 14998
698665 XDOT = 4620
727203
YDOT = -6074
687259 feet/sec YDOT = -1800
167404 meter/sec
ZDOT = -19423
259374 ZDOT = -5897
881520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18122353
15 X = 5523693
24
Y = -11951787
09 feet Y = -3642904
70 meter
Z = 3811633
26 Z = 1161785
82
XDOT = 10739
223656 XDOT = 3273
315370
YDOT = 10095
765157 feet/sec YDOT = 3077
189220 meter/sec
ZDOT = -19338
096977 ZDOT = -5894
251959
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 08015
53394185
00020000 00000-0 20000-3 0 9012
2 25544 51
6382 88
7352 0005902 282
3625 77
6879 15
77040339 4281
Satellite: ISS
Catalog Number: 25544
Epoch time: 08015
53394185 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 88
7352 deg
Eccentricity:
0005902
Arg of perigee: 282
3625 deg
Mean anomaly: 77
6879 deg
Mean motion: 15
77040339 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 428
Checksum: 305
Coasting Arc #3 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2008/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4084709
41 A = 6711262
66 meter
Y = 682043
47 meter E =
0003647
Z = 5284056
78 I = 51
94013
XDOT = -1061
732214 Wp = 291
46382
YDOT = -7628
782367 meter/sec RA = 83
03983 deg
ZDOT = 165
341236 TA = 156
98243
MA = 156
96608
Ha = 183
761 n
mi
Hp = 181
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13401277
58 X = -4117701
44
Y = 2237675
42 feet Y = 636181
03 meter
Z = 17336144
29 Z = 5264133
24
XDOT = -3483
373407 XDOT = -977
150287
YDOT = -25028
813540 feet/sec YDOT = -7640
182352 meter/sec
ZDOT = 542
458122 ZDOT = 160
388195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7646725
57 X = -2330721
95
Y = -11347319
23 feet Y = -3458662
90 meter
Z = 17260048
24 Z = 5260862
70
XDOT = 20487
047667 XDOT = 6244
452129
YDOT = -13017
670122 feet/sec YDOT = -3967
785853 meter/sec
ZDOT = 522
744669 ZDOT = 159
332575
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 08016
54779989
00020000 00000-0 20000-3 0 9024
2 25544 51
6387 83
5043 0006013 286
2537 73
7966 15
77108449 4444
Satellite: ISS
Catalog Number: 25544
Epoch time: 08016
54779989 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 83
5043 deg
Eccentricity:
0006013
Arg of perigee: 286
2537 deg
Mean anomaly: 73
7966 deg
Mean motion: 15
77108449 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 444
Checksum: 320
Coasting Arc #4 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2008/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 697727
15 A = 6723019
90 meter
Y = 6618306
80 meter E =
0011740
Z = 900121
92 I = 51
97454
XDOT = -4850
493440 Wp = 29
34955
YDOT = -305
468095 meter/sec RA = 77
91037 deg
ZDOT = 5983
283441 TA = 340
44710
MA = 340
49209
Ha = 184
038 n
mi
Hp = 181
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2289131
06 X = 619295
76
Y = 21713604
97 feet Y = 6625670
55 meter
Z = 2953155
91 Z = 903321
68
XDOT = -15913
692387 XDOT = -4875
782743
YDOT = -1002
191912 feet/sec YDOT = -359
851116 meter/sec
ZDOT = 19630
195016 ZDOT = 5959
658372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18610374
71 X = -5672442
21
Y = 11414831
22 feet Y = 3479240
56 meter
Z = 2966053
46 Z = 904053
09
XDOT = -5174
474858 XDOT = -1577
179937
YDOT = -13532
730527 feet/sec YDOT = -4124
776265 meter/sec
ZDOT = 19539
842872 ZDOT = 5955
744108
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 08017
56162822
00020000 00000-0 20000-3 0 9030
2 25544 51
6383 78
2735 0005848 293
5796 66
4755 15
77101416 4602
Satellite: ISS
Catalog Number: 25544
Epoch time: 08017
56162822 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 78
2735 deg
Eccentricity:
0005848
Arg of perigee: 293
5796 deg
Mean anomaly: 66
4755 deg
Mean motion: 15
77101416 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 460
Checksum: 304
Coasting Arc #5 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2008/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4409460
61 A = 6712675
42 meter
Y = 1195517
52 meter E =
0006875
Z = -4924161
72 I = 51
93306
XDOT = 472
268208 Wp = 96
74370
YDOT = 7361
100517 meter/sec RA = 72
74643 deg
ZDOT = 2211
903233 TA = 194
64387
MA = 194
66380
Ha = 184
136 n
mi
Hp = 180
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14466734
30 X = 4419684
94
Y = 3922301
57 feet Y = 1244884
44 meter
Z = -16155386
23 Z = -4902715
72
XDOT = 1549
436378 XDOT = 379
175209
YDOT = 24150
592248 feet/sec YDOT = 7365
860884 meter/sec
ZDOT = 7256
900371 ZDOT = 2213
972355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2994395
48 X = 912691
74
Y = 14776701
43 feet Y = 4503938
60 meter
Z = -16073271
15 Z = -4899133
05
XDOT = -19855
351368 XDOT = -6051
911097
YDOT = 11920
043265 feet/sec YDOT = 3633
229187 meter/sec
ZDOT = 7265
539344 ZDOT = 2214
536392
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 08018
51205831
00020000 00000-0 20000-3 0 9045
2 25544 51
6384 73
3696 0005839 297
2845 62
7725 15
77177990 4753
Satellite: ISS
Catalog Number: 25544
Epoch time: 08018
51205831 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 73
3696 deg
Eccentricity:
0005839
Arg of perigee: 297
2845 deg
Mean anomaly: 62
7725 deg
Mean motion: 15
77177990 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 475
Checksum: 320
Coasting Arc #6 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2008/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -40127
49 A = 6719281
60 meter
Y = -6062599
44 meter E =
0001304
Z = -2897800
18 I = 51
94696
XDOT = 5277
545607 Wp = 329
55127
YDOT = 2391
281824 meter/sec RA = 67
64938 deg
ZDOT = -5073
887559 TA = 243
65464
MA = 243
66802
Ha = 184
143 n
mi
Hp = 180
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -131651
85 X = 41745
22
Y = -19890418
12 feet Y = -6062589
97 meter
Z = -9507218
44 Z = -2897797
15
XDOT = 17314
782176 XDOT = 5275
061392
YDOT = 7845
412809 feet/sec YDOT = 2450
285197 meter/sec
ZDOT = -16646
612727 ZDOT = -5048
255256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17603836
77 X = 5365649
45
Y = -9259587
07 feet Y = -2822322
14 meter
Z = -9507799
24 Z = -2897977
21
XDOT = 410
938438 XDOT = 125
254036
YDOT = 17780
245120 feet/sec YDOT = 5419
418713 meter/sec
ZDOT = -16548
367270 ZDOT = -5043
942344
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 08019
52581963
00020000 00000-0 20000-3 0 9051
2 25544 51
6391 68
1385 0005697 302
2832 57
7780 15
77249257 4912
Satellite: ISS
Catalog Number: 25544
Epoch time: 08019
52581963 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 68
1385 deg
Eccentricity:
0005697
Arg of perigee: 302
2832 deg
Mean anomaly: 57
7780 deg
Mean motion: 15
77249257 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 491
Checksum: 315
Coasting Arc #7 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2008/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4790530
75 A = 6716788
89 meter
Y = -2879594
58 meter E =
0008498
Z = 3722778
28 I = 51
92617
XDOT = 478
141750 Wp = 56
41389
YDOT = -6373
342604 meter/sec RA = 62
46013 deg
ZDOT = -4302
958304 TA = 78
82286
MA = 78
72734
Ha = 184
265 n
mi
Hp = 180
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15716964
39 X = -4776058
86
Y = -9447488
79 feet Y = -2933084
65 meter
Z = 12213839
51 Z = 3699541
07
XDOT = 1568
706528 XDOT = 570
276479
YDOT = -20909
916680 feet/sec YDOT = -6367
479966 meter/sec
ZDOT = -14117
317270 ZDOT = -4300
412686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 768443
66 X = 234221
63
Y = -18380888
99 feet Y = -5602494
96 meter
Z = 12124698
10 Z = 3695607
98
XDOT = 17821
436279 XDOT = 5431
973778
YDOT = -8586
481281 feet/sec YDOT = -2617
159495 meter/sec
ZDOT = -14108
200978 ZDOT = -4300
179658
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 08020
53954611
00020000 00000-0 20000-3 0 9069
2 25544 51
6385 62
9072 0005797 306
8606 53
2027 15
77319405 5076
Satellite: ISS
Catalog Number: 25544
Epoch time: 08020
53954611 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 62
9072 deg
Eccentricity:
0005797
Arg of perigee: 306
8606 deg
Mean anomaly: 53
2027 deg
Mean motion: 15
77319405 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 507
Checksum: 287
Coasting Arc #8 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2008/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -980666
45 A = 6714063
94 meter
Y = 4931726
80 meter E =
0004327
Z = 4445282
71 I = 51
90230
XDOT = -5660
971143 Wp = 85
19534
YDOT = -4079
554492 meter/sec RA = 57
36801 deg
ZDOT = 3274
765750 TA = 332
11860
MA = 332
14179
Ha = 184
439 n
mi
Hp = 180
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3217409
63 X = -1057334
70
Y = 16180206
04 feet Y = 4920331
17 meter
Z = 14584260
85 Z = 4440333
19
XDOT = -18572
739972 XDOT = -5630
840008
YDOT = -13384
365131 feet/sec YDOT = -4142
690650 meter/sec
ZDOT = 10743
982121 ZDOT = 3247
338118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15708268
18 X = -4787880
14
Y = 5093030
56 feet Y = 1552355
71 meter
Z = 14565809
53 Z = 4439658
74
XDOT = 2848
566611 XDOT = 868
243103
YDOT = -21662
491949 feet/sec YDOT = -6602
727546 meter/sec
ZDOT = 10638
690983 ZDOT = 3242
673012
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 08021
55324087
00020000 00000-0 20000-3 0 9071
2 25544 51
6381 57
6751 0005584 312
1734 47
8957 15
77344484 5237
Satellite: ISS
Catalog Number: 25544
Epoch time: 08021
55324087 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 57
6751 deg
Eccentricity:
0005584
Arg of perigee: 312
1734 deg
Mean anomaly: 47
8957 deg
Mean motion: 15
77344484 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 523
Checksum: 300
Coasting Arc #9 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2008/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4999647
75 A = 6721011
63 meter
Y = 4086556
95 meter E =
0009780
Z = -1842517
15 I = 51
91042
XDOT = -1875
449104 Wp = 3
58470
YDOT = 4853
469730 meter/sec RA = 52
18507 deg
ZDOT = 5686
762061 TA = 336
01177
MA = 336
05730
Ha = 184
464 n
mi
Hp = 179
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16403043
81 X = 4962530
01
Y = 13407339
07 feet Y = 4142258
51 meter
Z = -6045003
79 Z = -1818319
32
XDOT = -6153
048243 XDOT = -1957
206381
YDOT = 15923
457119 feet/sec YDOT = 4832
039656 meter/sec
ZDOT = 18657
355844 ZDOT = 5677
453342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3218206
10 X = -980909
22
Y = 20966039
83 feet Y = 6390448
94 meter
Z = -5952056
90 Z = -1814186
94
XDOT = -15368
794011 XDOT = -4684
408414
YDOT = 2917
063696 feet/sec YDOT = 889
121014 meter/sec
ZDOT = 18622
224231 ZDOT = 5676
053946
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 08022
50354802
00020000 00000-0 20000-3 0 9086
2 25544 51
6389 52
7703 0005566 315
6756 44
3963 15
77423311 5382
Satellite: ISS
Catalog Number: 25544
Epoch time: 08022
50354802 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 52
7703 deg
Eccentricity:
0005566
Arg of perigee: 315
6756 deg
Mean anomaly: 44
3963 deg
Mean motion: 15
77423311 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 538
Checksum: 290
Coasting Arc #10 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2008/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2384051
22 A = 6710539
49 meter
Y = -3472199
51 meter E =
0012484
Z = -5234197
91 I = 51
85626
XDOT = 5669
059642 Wp = 61
64106
YDOT = 5142
185592 meter/sec RA = 47
06424 deg
ZDOT = -824
715205 TA = 200
50465
MA = 200
55480
Ha = 184
538 n
mi
Hp = 179
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7821690
34 X = 2448126
68
Y = -11391730
68 feet Y = -3445181
03 meter
Z = -17172565
31 Z = -5222461
18
XDOT = 18599
277042 XDOT = 5615
143792
YDOT = 16870
687637 feet/sec YDOT = 5205
278844 meter/sec
ZDOT = -2705
758548 ZDOT = -797
306347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13850069
41 X = 4221501
16
Y = 808775
12 feet Y = 246514
66 meter
Z = -17128012
94 Z = -5220618
34
XDOT = -4615
865655 XDOT = -1406
915852
YDOT = 23673
189052 feet/sec YDOT = 7215
588023 meter/sec
ZDOT = -2600
420998 ZDOT = -792
608320
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 08023
51717574
00020000 00000-0 20000-3 0 9098
2 25544 51
6389 47
5378 0005638 319
6745 40
4001 15
77434274 5542
Satellite: ISS
Catalog Number: 25544
Epoch time: 08023
51717574 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 47
5378 deg
Eccentricity:
0005638
Arg of perigee: 319
6745 deg
Mean anomaly: 40
4001 deg
Mean motion: 15
77434274 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 554
Checksum: 302
Coasting Arc #11 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2008/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4741366
65 A = 6722140
79 meter
Y = -4739732
11 meter E =
0005730
Z = -458208
36 I = 51
87410
XDOT = 3659
492814 Wp = 132
56208
YDOT = -3082
078130 meter/sec RA = 41
91526 deg
ZDOT = -6037
141848 TA = 52
41060
MA = 52
35858
Ha = 184
595 n
mi
Hp = 179
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15555664
85 X = -4685788
02
Y = -15550302
20 feet Y = -4792441
99 meter
Z = -1503308
28 Z = -481106
46
XDOT = 12006
210019 XDOT = 3723
011564
YDOT = -10111
804887 feet/sec YDOT = -3040
800162 meter/sec
ZDOT = -19806
895828 ZDOT = -6019
210432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4781087
34 X = 1457275
42
Y = -21462975
79 feet Y = -6541915
02 meter
Z = -1591357
02 Z = -485045
62
XDOT = 13469
832907 XDOT = 4105
605070
YDOT = 4452
258343 feet/sec YDOT = 1357
048343 meter/sec
ZDOT = -19738
611817 ZDOT = -6016
328882
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 08024
53076916
00020000 00000-0 20000-3 0 9101
2 25544 51
6378 42
3047 0005547 324
9445 35
1354 15
77496665 5703
Satellite: ISS
Catalog Number: 25544
Epoch time: 08024
53076916 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 42
3047 deg
Eccentricity:
0005547
Arg of perigee: 324
9445 deg
Mean anomaly: 35
1354 deg
Mean motion: 15
77496665 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 570
Checksum: 296
Coasting Arc #12 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2008/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4016584
36 A = 6711143
24 meter
Y = 1928088
69 meter E =
0008218
Z = 5019612
18 I = 51
81447
XDOT = -5002
190773 Wp = 12
02633
YDOT = -5559
395525 meter/sec RA = 36
74676 deg
ZDOT = -1858
795139 TA = 95
89176
MA = 95
79808
Ha = 184
734 n
mi
Hp = 179
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13177770
22 X = -4062229
74
Y = 6325750
28 feet Y = 1882917
61 meter
Z = 16468543
91 Z = 4999989
32
XDOT = -16411
387051 XDOT = -4930
623540
YDOT = -18239
486629 feet/sec YDOT = -5614
932668 meter/sec
ZDOT = -6098
409250 ZDOT = -1882
921437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12590815
78 X = -3837680
65
Y = -7589490
15 feet Y = -2313276
60 meter
Z = 16393678
06 Z = 4996793
07
XDOT = 5644
801767 XDOT = 1720
535578
YDOT = -22797
966226 feet/sec YDOT = -6948
820106 meter/sec
ZDOT = -6191
237333 ZDOT = -1887
089139
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 08025
54432715
00020000 00000-0 20000-3 0 9117
2 25544 51
6373 37
0715 0005605 329
2136 30
8699 15
77564639 5869
Satellite: ISS
Catalog Number: 25544
Epoch time: 08025
54432715 = yrday
fracday
Element set: 911
Inclination: 51
6373 deg
RA of node: 37
0715 deg
Eccentricity:
0005605
Arg of perigee: 329
2136 deg
Mean anomaly: 30
8699 deg
Mean motion: 15
77564639 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 586
Checksum: 298
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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