Date:
March 17th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10010 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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
077/02:55:34
797 -0
4 0
8 0
8
N/A -0
3 -0
0 186
1
000/00:05:09
593 0
7 -0
1 180
6
080/02:40:34
734 0
0 0
6 0
6
N/A -0
5 -0
0 186
6
000/00:05:09
467 0
3 -0
1 180
4
Coasting Arc #1 (Orbit 1389)
---------------------------------------
Vector Time (GMT): 2008/076/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1107489
26 A = 6718902
40 meter
Y = 5465068
24 meter E =
0005039
Z = -3753833
17 I = 51
87360
XDOT = -6185
805770 Wp = 109
40803
YDOT = 1674
878386 meter/sec RA = 133
34999 deg
ZDOT = 4266
363023 TA = 205
36520
MA = 205
38995
Ha = 185
840 n
mi
Hp = 180
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3633494
95 X = -1150283
09
Y = 17930013
90 feet Y = 5452444
31 meter
Z = -12315725
61 Z = -3759317
30
XDOT = -20294
638354 XDOT = -6224
799614
YDOT = 5495
007827 feet/sec YDOT = 1605
487236 meter/sec
ZDOT = 13997
254012 ZDOT = 4236
218193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7743551
25 X = -2360234
42
Y = 16559670
73 feet Y = 5047387
64 meter
Z = -12336105
56 Z = -3760044
97
XDOT = -19888
993435 XDOT = -6062
165199
YDOT = 1033
628523 feet/sec YDOT = 315
049974 meter/sec
ZDOT = 13881
876591 ZDOT = 4231
195985
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 08076
48719014
00020000 00000-0 20000-3 0 9004
2 25544 51
6377 134
2564 0001167 259
3152 100
7882 15
76501764 13909
Satellite: ISS
Catalog Number: 25544
Epoch time: 08076
48719014 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 134
2564 deg
Eccentricity:
0001167
Arg of perigee: 259
3152 deg
Mean anomaly: 100
7882 deg
Mean motion: 15
76501764 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1390
Checksum: 285
Coasting Arc #2 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2008/077/02:58:09
593
Vector Time (MET): N/A
Weight (LBS) : 567143
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5007710
02 A = 6724710
91 meter
Y = 4255725
43 meter E =
0013378
Z = 1392888
11 I = 51
90179
XDOT = -2197
972575 Wp = 54
88227
YDOT = -4511
185761 meter/sec RA = 130
07523 deg
ZDOT = 5849
319818 TA = 320
39416
MA = 320
49181
Ha = 186
101 n
mi
Hp = 180
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16429494
82 X = -5061692
28
Y = 13962353
79 feet Y = 4199424
58 meter
Z = 4569842
87 Z = 1368429
87
XDOT = -7211
196112 XDOT = -2175
778805
YDOT = -14800
478220 feet/sec YDOT = -4535
640442 meter/sec
ZDOT = 19190
681819 ZDOT = 5838
696355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4055056
03 X = 1235981
08
Y = -21196130
51 feet Y = -6460580
58 meter
Z = 4476567
76 Z = 1364457
85
XDOT = 13439
781637 XDOT = 4096
445443
YDOT = 6637
887295 feet/sec YDOT = 2023
228047 meter/sec
ZDOT = 19149
415160 ZDOT = 5836
741741
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 08077
18447684
00020000 00000-0 20000-3 0 9014
2 25544 51
6355 130
6597 0001463 301
6190 58
4832 15
76345008 14017
Satellite: ISS
Catalog Number: 25544
Epoch time: 08077
18447684 = yrday
fracday
Element set: 901
Inclination: 51
6355 deg
RA of node: 130
6597 deg
Eccentricity:
0001463
Arg of perigee: 301
6190 deg
Mean anomaly: 58
4832 deg
Mean motion: 15
76345008 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1401
Checksum: 283
Coasting Arc #3 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2008/078/02:58:09
593
Vector Time (MET): N/A
Weight (LBS) : 567143
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1540609
58 A = 6715283
90 meter
Y = 4413965
65 meter E =
0010738
Z = -4830557
28 I = 51
88797
XDOT = -5609
177108 Wp = 105
49175
YDOT = 4656
205503 meter/sec RA = 124
90654 deg
ZDOT = 2467
426033 TA = 188
54543
MA = 188
56372
Ha = 186
091 n
mi
Hp = 180
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5054493
39 X = 1514602
93
Y = 14481514
61 feet Y = 4431047
92 meter
Z = -15848285
04 Z = -4823136
60
XDOT = -18402
812033 XDOT = -5672
812703
YDOT = 15276
264772 feet/sec YDOT = 4593
124830 meter/sec
ZDOT = 8095
229766 ZDOT = 2440
022350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13227608
35 X = -4031775
03
Y = -7823694
60 feet Y = -2384662
11 meter
Z = -15819307
43 Z = -4821724
91
XDOT = 3808
108822 XDOT = 1160
711569
YDOT = -22584
033999 feet/sec YDOT = -6883
613563 meter/sec
ZDOT = 7990
701393 ZDOT = 2435
565785
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 08078
13539174
00020000 00000-0 20000-3 0 9027
2 25544 51
6352 125
7581 0001307 306
5466 53
5578 15
76381801 14169
Satellite: ISS
Catalog Number: 25544
Epoch time: 08078
13539174 = yrday
fracday
Element set: 902
Inclination: 51
6352 deg
RA of node: 125
7581 deg
Eccentricity:
0001307
Arg of perigee: 306
5466 deg
Mean anomaly: 53
5578 deg
Mean motion: 15
76381801 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1416
Checksum: 288
Coasting Arc #4 (Orbit 1431)
---------------------------------------
Vector Time (GMT): 2008/079/02:58:09
593
Vector Time (MET): N/A
Weight (LBS) : 567143
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4761350
92 A = 6721715
07 meter
Y = -3771810
97 meter E =
0003386
Z = -2879544
70 I = 51
92576
XDOT = 1375
129645 Wp = 109
05749
YDOT = 5614
754757 meter/sec RA = 119
81506 deg
ZDOT = -5086
683149 TA = 103
90893
MA = 103
87127
Ha = 186
087 n
mi
Hp = 180
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15621230
06 X = 4817162
08
Y = -12374707
90 feet Y = -3718255
01 meter
Z = -9447325
15 Z = -2856278
60
XDOT = 4511
580201 XDOT = 1336
952128
YDOT = 18421
111407 feet/sec YDOT = 5629
918347 meter/sec
ZDOT = -16688
593007 ZDOT = -5080
096101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3770858
20 X = -1149357
58
Y = 19611381
51 feet Y = 5977549
08 meter
Z = -9358553
33 Z = -2852487
05
XDOT = -14098
504110 XDOT = -4297
224053
YDOT = -10652
936673 feet/sec YDOT = -3247
015098 meter/sec
ZDOT = -16662
668228 ZDOT = -5078
781276
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 08079
14967808
00020000 00000-0 20000-3 0 9039
2 25544 51
6353 120
5307 0001360 317
2683 42
8375 15
76432519 14325
Satellite: ISS
Catalog Number: 25544
Epoch time: 08079
14967808 = yrday
fracday
Element set: 903
Inclination: 51
6353 deg
RA of node: 120
5307 deg
Eccentricity:
0001360
Arg of perigee: 317
2683 deg
Mean anomaly: 42
8375 deg
Mean motion: 15
76432519 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1432
Checksum: 286
Coasting Arc #5 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2008/080/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4426210
76 A = 6714596
67 meter
Y = 161443
47 meter E =
0004400
Z = 5043724
54 I = 51
91317
XDOT = 1793
678989 Wp = 115
20678
YDOT = -7275
334290 meter/sec RA = 114
72506 deg
ZDOT = 1803
900125 TA = 317
47654
MA = 317
51062
Ha = 186
569 n
mi
Hp = 180
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14521688
85 X = -4452188
25
Y = 529670
19 feet Y = 111802
32 meter
Z = 16547652
70 Z = 5022159
20
XDOT = 5884
773586 XDOT = 1866
136697
YDOT = -23869
206987 feet/sec YDOT = -7254
871032 meter/sec
ZDOT = 5918
307498 ZDOT = 1812
790429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11182662
70 X = 3408475
59
Y = -9425366
90 feet Y = -2872851
83 meter
Z = 16464972
55 Z = 5018523
63
XDOT = 9417
161100 XDOT = 2870
350703
YDOT = 21587
110437 feet/sec YDOT = 6579
751261 meter/sec
ZDOT = 5951
539758 ZDOT = 1814
029318
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 08080
16394701
00020000 00000-0 20000-3 0 9040
2 25544 51
6346 115
3020 0001368 339
4893 20
6216 15
76315582 14483
Satellite: ISS
Catalog Number: 25544
Epoch time: 08080
16394701 = yrday
fracday
Element set: 904
Inclination: 51
6346 deg
RA of node: 115
3020 deg
Eccentricity:
0001368
Arg of perigee: 339
4893 deg
Mean anomaly: 20
6216 deg
Mean motion: 15
76315582 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1448
Checksum: 275
Coasting Arc #6 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2008/081/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1635719
35 A = 6725124
59 meter
Y = 6468353
43 meter E =
0011082
Z = -799220
49 I = 51
96069
XDOT = -4810
584679 Wp = 34
27988
YDOT = -481
260411 meter/sec RA = 109
56917 deg
ZDOT = 5999
442401 TA = 317
03438
MA = 317
12088
Ha = 186
369 n
mi
Hp = 180
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5366533
29 X = -1704045
47
Y = 21221632
00 feet Y = 6449679
77 meter
Z = -2622114
46 Z = -807333
40
XDOT = -15782
758133 XDOT = -4833
989572
YDOT = -1578
938355 feet/sec YDOT = -535
185331 meter/sec
ZDOT = 19683
209977 ZDOT = 5976
015992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9208850
29 X = -2806857
57
Y = -19854327
80 feet Y = -6051599
11 meter
Z = -2652465
31 Z = -808471
43
XDOT = 11892
452752 XDOT = 3624
819599
YDOT = -8112
378706 feet/sec YDOT = -2472
653029 meter/sec
ZDOT = 19593
315809 ZDOT = 5972
042658
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 08081
11486131
00020000 00000-0 20000-3 0 9056
2 25544 51
6349 110
4005 0001172 343
1190 16
9935 15
76379733 14631
Satellite: ISS
Catalog Number: 25544
Epoch time: 08081
11486131 = yrday
fracday
Element set: 905
Inclination: 51
6349 deg
RA of node: 110
4005 deg
Eccentricity:
0001172
Arg of perigee: 343
1190 deg
Mean anomaly: 16
9935 deg
Mean motion: 15
76379733 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1463
Checksum: 269
Coasting Arc #7 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2008/082/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4008064
75 A = 6713209
10 meter
Y = 1059795
60 meter E =
0014999
Z = -5292857
35 I = 51
92953
XDOT = -1937
866398 Wp = 85
91797
YDOT = 7445
958443 meter/sec RA = 104
44484 deg
ZDOT = 24
549454 TA = 184
30778
MA = 184
32071
Ha = 186
384 n
mi
Hp = 180
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13149818
73 X = 4021627
72
Y = 3477019
67 feet Y = 1104691
34 meter
Z = -17365017
54 Z = -5273353
41
XDOT = -6357
829391 XDOT = -2021
103492
YDOT = 24428
997517 feet/sec YDOT = 7423
822714 meter/sec
ZDOT = 80
542828 ZDOT = 14
932362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12381455
97 X = -3773867
78
Y = 5856901
33 feet Y = 1785183
52 meter
Z = -17290097
96 Z = -5270021
86
XDOT = -10413
639697 XDOT = -3174
077380
YDOT = -21893
641876 feet/sec YDOT = -6673
182044 meter/sec
ZDOT = 44
531146 ZDOT = 13
573093
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 08082
12914841
00020000 00000-0 20000-3 0 9063
2 25544 51
6350 105
1728 0001124 354
2761 5
8391 15
76422363 14798
Satellite: ISS
Catalog Number: 25544
Epoch time: 08082
12914841 = yrday
fracday
Element set: 906
Inclination: 51
6350 deg
RA of node: 105
1728 deg
Eccentricity:
0001124
Arg of perigee: 354
2761 deg
Mean anomaly: 5
8391 deg
Mean motion: 15
76422363 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1479
Checksum: 273
Coasting Arc #8 (Orbit 1494)
---------------------------------------
Vector Time (GMT): 2008/083/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1733960
08 A = 6724801
99 meter
Y = -6436999
15 meter E =
0009212
Z = -855025
38 I = 51
97490
XDOT = 4421
107677 Wp = 136
41586
YDOT = 1980
569684 meter/sec RA = 99
31989 deg
ZDOT = -5989
187966 TA = 52
87779
MA = 52
79366
Ha = 186
317 n
mi
Hp = 179
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5688845
42 X = 1809964
30
Y = -21118763
62 feet Y = -6417184
14 meter
Z = -2805201
38 Z = -846416
57
XDOT = 14504
946446 XDOT = 4427
726477
YDOT = 6497
932034 feet/sec YDOT = 2030
045472 meter/sec
ZDOT = -19649
566817 ZDOT = -5967
694318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9552368
98 X = 2911562
07
Y = 19679872
99 feet Y = 5998425
29 meter
Z = -2772929
83 Z = -845189
01
XDOT = -13858
377076 XDOT = -4224
033333
YDOT = 3990
460656 feet/sec YDOT = 1216
292408 meter/sec
ZDOT = -19566
911241 ZDOT = -5963
994546
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 08083
14341042
00020000 00000-0 20000-3 0 9074
2 25544 51
6347 99
9435 0001335 355
5760 4
5393 15
76485258 14954
Satellite: ISS
Catalog Number: 25544
Epoch time: 08083
14341042 = yrday
fracday
Element set: 907
Inclination: 51
6347 deg
RA of node: 99
9435 deg
Eccentricity:
0001335
Arg of perigee: 355
5760 deg
Mean anomaly: 4
5393 deg
Mean motion: 15
76485258 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1495
Checksum: 300
Coasting Arc #9 (Orbit 1510)
---------------------------------------
Vector Time (GMT): 2008/084/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3763673
12 A = 6714324
88 meter
Y = -2392116
71 meter E =
0006441
Z = 5016561
59 I = 51
94287
XDOT = 2020
168216 Wp = 48
06078
YDOT = -7189
346435 meter/sec RA = 94
16390 deg
ZDOT = -1906
798830 TA = 60
28372
MA = 60
21964
Ha = 186
543 n
mi
Hp = 179
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12348008
91 X = -3761014
03
Y = -7848151
93 feet Y = -2434188
99 meter
Z = 16458535
40 Z = 4998284
24
XDOT = 6627
848477 XDOT = 2109
673386
YDOT = -23587
094604 feet/sec YDOT = -7166
255461 meter/sec
ZDOT = -6255
901673 ZDOT = -1896
766839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14497392
90 X = 4418805
36
Y = -2490723
06 feet Y = -759172
39 meter
Z = 16388169
46 Z = 4995114
05
XDOT = 10646
825566 XDOT = 3245
152432
YDOT = 20931
324550 feet/sec YDOT = 6379
867723 meter/sec
ZDOT = -6218
247251 ZDOT = -1895
321762
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 08084
15765200
00020000 00000-0 20000-3 0 9083
2 25544 51
6349 94
7149 0001091 7
1382 352
9798 15
76446767 15110
Satellite: ISS
Catalog Number: 25544
Epoch time: 08084
15765200 = yrday
fracday
Element set: 908
Inclination: 51
6349 deg
RA of node: 94
7149 deg
Eccentricity:
0001091
Arg of perigee: 7
1382 deg
Mean anomaly: 352
9798 deg
Mean motion: 15
76446767 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1511
Checksum: 305
Coasting Arc #10 (Orbit 1526)
---------------------------------------
Vector Time (GMT): 2008/085/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1808281
82 A = 6722361
58 meter
Y = 5990807
59 meter E =
0014286
Z = 2436495
68 I = 51
97317
XDOT = -4269
991980 Wp = 70
74602
YDOT = -3488
182566 meter/sec RA = 89
06849 deg
ZDOT = 5386
834298 TA = 316
67972
MA = 316
79194
Ha = 186
275 n
mi
Hp = 179
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5932683
14 X = -1886973
69
Y = 19654880
55 feet Y = 5970146
50 meter
Z = 7993752
22 Z = 2427519
50
XDOT = -14009
160041 XDOT = -4256
837651
YDOT = -11444
168523 feet/sec YDOT = -3535
858193 meter/sec
ZDOT = 17673
340874 ZDOT = 5366
122709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9025744
22 X = -2751046
84
Y = -18454958
25 feet Y = -5625071
27 meter
Z = 7959999
41 Z = 2426207
82
XDOT = 16778
484469 XDOT = 5114
082066
YDOT = -587
828977 feet/sec YDOT = -179
170272 meter/sec
ZDOT = 17593
518877 ZDOT = 5362
504554
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 08085
17186465
00020000 00000-0 20000-3 0 9097
2 25544 51
6363 89
4866 0001000 4
0723 356
0449 15
76553466 15278
Satellite: ISS
Catalog Number: 25544
Epoch time: 08085
17186465 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node: 89
4866 deg
Eccentricity:
0001000
Arg of perigee: 4
0723 deg
Mean anomaly: 356
0449 deg
Mean motion: 15
76553466 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1527
Checksum: 297
Coasting Arc #11 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2008/086/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3726266
12 A = 6717176
76 meter
Y = 3652865
48 meter E =
0008132
Z = -4237792
89 I = 51
95456
XDOT = -2172
579046 Wp = 102
54729
YDOT = 6428
189201 meter/sec RA = 83
89066 deg
ZDOT = 3634
678237 TA = 204
27359
MA = 204
31192
Ha = 186
305 n
mi
Hp = 179
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12225282
53 X = 3705728
82
Y = 11984466
79 feet Y = 3694419
72 meter
Z = -13903519
99 Z = -4219740
61
XDOT = -7127
884010 XDOT = -2261
955304
YDOT = 21089
859582 feet/sec YDOT = 6403
394590 meter/sec
ZDOT = 11924
797367 ZDOT = 3623
906446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17175837
83 X = -5235195
37
Y = -84527
83 feet Y = -25764
08 meter
Z = -13833882
15 Z = -4216567
28
XDOT = -9467
877964 XDOT = -2885
809203
YDOT = -18922
541791 feet/sec YDOT = -5767
590738 meter/sec
ZDOT = 11884
194817 ZDOT = 3622
302580
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 08086
12266996
00020000 00000-0 20000-3 0 9103
2 25544 51
6370 84
5856 0001119 8
7220 351
3964 15
76551654 15429
Satellite: ISS
Catalog Number: 25544
Epoch time: 08086
12266996 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 84
5856 deg
Eccentricity:
0001119
Arg of perigee: 8
7220 deg
Mean anomaly: 351
3964 deg
Mean motion: 15
76551654 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1542
Checksum: 294
Coasting Arc #12 (Orbit 1557)
---------------------------------------
Vector Time (GMT): 2008/087/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2045424
99 A = 6718430
25 meter
Y = -5128071
03 meter E =
0006911
Z = -3836008
83 I = 51
95526
XDOT = 4290
470949 Wp = 66
70084
YDOT = 4835
140755 meter/sec RA = 78
80832 deg
ZDOT = -4179
215118 TA = 159
72989
MA = 159
70244
Ha = 186
240 n
mi
Hp = 179
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6710711
90 X = 2121250
58
Y = -16824380
00 feet Y = -5104774
03 meter
Z = -12585330
81 Z = -3825887
82
XDOT = 14076
348259 XDOT = 4256
386746
YDOT = 15863
322686 feet/sec YDOT = 4882
928589 meter/sec
ZDOT = -13711
335688 ZDOT = -4158
454802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7086418
46 X = 2159940
35
Y = 16698432
71 feet Y = 5089682
29 meter
Z = -12547070
84 Z = -3824347
19
XDOT = -20006
702368 XDOT = -6098
042882
YDOT = -1744
004538 feet/sec YDOT = -531
572583 meter/sec
ZDOT = -13631
185628 ZDOT = -4154
785379
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 08087
13683703
00020000 00000-0 20000-3 0 9115
2 25544 51
6374 79
3567 0001085 12
2710 347
8481 15
76594790 15589
Satellite: ISS
Catalog Number: 25544
Epoch time: 08087
13683703 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 79
3567 deg
Eccentricity:
0001085
Arg of perigee: 12
2710 deg
Mean anomaly: 347
8481 deg
Mean motion: 15
76594790 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1558
Checksum: 306
Coasting Arc #13 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2008/088/02:43:09
467
Vector Time (MET): N/A
Weight (LBS) : 567060
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3784986
30 A = 6720980
05 meter
Y = -4698972
45 meter E =
0013643
Z = 2947977
69 I = 51
95758
XDOT = 2567
541905 Wp = 93
28938
YDOT = -5239
472542 meter/sec RA = 73
62522 deg
ZDOT = -5035
927025 TA = 52
83422
MA = 52
70971
Ha = 186
280 n
mi
Hp = 179
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12417934
05 X = -3746481
13
Y = -15416576
27 feet Y = -4741083
00 meter
Z = 9671842
80 Z = 2929683
75
XDOT = 8423
693914 XDOT = 2650
403361
YDOT = -17189
870544 feet/sec YDOT = -5210
297570 meter/sec
ZDOT = -16522
070292 ZDOT = -5023
252552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19752024
81 X = 6020417
16
Y = 1759403
82 feet Y = 536266
28 meter
Z = 9601170
10 Z = 2926436
65
XDOT = 6556
679295 XDOT = 1998
475849
YDOT = 16634
826908 feet/sec YDOT = 5070
295242 meter/sec
ZDOT = -16474
019333 ZDOT = -5021
281093
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 08088
15097924
00020000 00000-0 20000-3 0 9123
2 25544 51
6379 74
1282 0001047 20
3950 339
7256 15
76626772 15749
Satellite: ISS
Catalog Number: 25544
Epoch time: 08088
15097924 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 74
1282 deg
Eccentricity:
0001047
Arg of perigee: 20
3950 deg
Mean anomaly: 339
7256 deg
Mean motion: 15
76626772 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1574
Checksum: 304
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 may contain past, current and future orbital data 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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