Date:
August 12th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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
226/08:06:18
565 -0
9 9
6 9
6
N/A 9
2 0
0 196
8
000/00:16:33
129 2
8 -0
2 187
4
Coasting Arc #1 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2008/224/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1712891
87 A = 6733591
34 meter
Y = -6212085
09 meter E =
0012385
Z = -1965802
20 I = 51
98474
XDOT = 4319
167638 Wp = 86
87187
YDOT = 2963
218379 meter/sec RA = 91
61901 deg
ZDOT = -5630
141805 TA = 114
86604
MA = 114
73722
Ha = 195
182 n
mi
Hp = 182
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5619723
99 X = 1791778
52
Y = -20380856
59 feet Y = -6192489
27 meter
Z = -6449482
29 Z = -1957290
06
XDOT = 14170
497501 XDOT = 4313
061398
YDOT = 9721
845075 feet/sec YDOT = 3011
484219 meter/sec
ZDOT = -18471
593847 ZDOT = -5609
174018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18922650
62 X = -5767623
91
Y = 9450390
49 feet Y = 2880479
02 meter
Z = -6417152
66 Z = -1955948
13
XDOT = -1653
568255 XDOT = -504
007604
YDOT = -15732
289377 feet/sec YDOT = -4795
201802 meter/sec
ZDOT = -18390
298878 ZDOT = -5605
363098
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 08224
50716127
00020000 00000-0 20000-3 0 9004
2 25544 51
6423 92
2159 0010002 53
1634 307
0444 15
72917973 37245
Satellite: ISS
Catalog Number: 25544
Epoch time: 08224
50716127 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 92
2159 deg
Eccentricity:
0010002
Arg of perigee: 53
1634 deg
Mean anomaly: 307
0444 deg
Mean motion: 15
72917973 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3724
Checksum: 261
Coasting Arc #2 (Orbit 3739)
---------------------------------------
Vector Time (GMT): 2008/225/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4055346
28 A = 6724109
25 meter
Y = -1845870
42 meter E =
0015690
Z = 5027355
05 I = 51
95323
XDOT = 1020
547298 Wp = 55
54024
YDOT = -7403
276776 meter/sec RA = 86
48133 deg
ZDOT = -1882
173177 TA = 52
59794
MA = 52
45522
Ha = 195
222 n
mi
Hp = 182
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13304941
87 X = -4058825
73
Y = -6056005
30 feet Y = -1891239
59 meter
Z = 16493947
00 Z = 5007645
79
XDOT = 3348
252291 XDOT = 1112
399212
YDOT = -24288
965799 feet/sec YDOT = -7391
350669 meter/sec
ZDOT = -6175
108848 ZDOT = -1876
993061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4717765
03 X = 1437974
78
Y = 13926652
86 feet Y = 4244843
79 meter
Z = 16417612
47 Z = 5004088
28
XDOT = -19047
077991 XDOT = -5805
549372
YDOT = 13758
965820 feet/sec YDOT = 4193
732782 meter/sec
ZDOT = -6155
756015 ZDOT = -1876
274433
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 08225
52366894
00020000 00000-0 20000-3 0 9010
2 25544 51
6425 87
0036 0010073 55
8961 304
3156 15
73002901 37408
Satellite: ISS
Catalog Number: 25544
Epoch time: 08225
52366894 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 87
0036 deg
Eccentricity:
0010073
Arg of perigee: 55
8961 deg
Mean anomaly: 304
3156 deg
Mean motion: 15
73002901 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3740
Checksum: 270
Coasting Arc #3 (Orbit 3752)
---------------------------------------
Vector Time (GMT): 2008/226/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3102191
61 A = 6736941
42 meter
Y = 5158756
30 meter E =
0011237
Z = -3017618
65 I = 51
97328
XDOT = -3260
316081 Wp = 29
82501
YDOT = 4868
698838 meter/sec RA = 82
06049 deg
ZDOT = 4988
979772 TA = 295
50122
MA = 295
61740
Ha = 196
834 n
mi
Hp = 187
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10177794
00 X = 3058933
82
Y = 16925053
48 feet Y = 5193205
21 meter
Z = -9900323
67 Z = -3002653
03
XDOT = -10696
575068 XDOT = -3338
751511
YDOT = 15973
421384 feet/sec YDOT = 4831
801084 meter/sec
ZDOT = 16368
043870 ZDOT = 4972
951348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17747423
32 X = 5409414
63
Y = -8730687
62 feet Y = -2661113
59 meter
Z = -9842021
83 Z = -2999848
25
XDOT = 14342
816509 XDOT = 4371
690472
YDOT = 10838
120546 feet/sec YDOT = 3303
459142 meter/sec
ZDOT = 16306
532599 ZDOT = 4970
231136
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 08226
34957788
00020000 00000-0 20000-3 0 9020
2 25544 51
6414 82
7688 0008326 9
2353 350
8961 15
70958162 37537
Satellite: ISS
Catalog Number: 25544
Epoch time: 08226
34957788 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 82
7688 deg
Eccentricity:
0008326
Arg of perigee: 9
2353 deg
Mean anomaly: 350
8961 deg
Mean motion: 15
70958162 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3753
Checksum: 319
Coasting Arc #4 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2008/227/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1771054
82 A = 6734796
39 meter
Y = -5327174
81 meter E =
0012144
Z = -3735194
53 I = 51
96160
XDOT = 4493
313996 Wp = 38
69863
YDOT = 4511
085512 meter/sec RA = 77
02067 deg
ZDOT = -4301
477458 TA = 185
99627
MA = 186
01082
Ha = 196
862 n
mi
Hp = 187
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5810547
30 X = 1848637
06
Y = -17477607
63 feet Y = -5306935
77 meter
Z = -12254575
22 Z = -3726402
88
XDOT = 14741
843819 XDOT = 4463
431768
YDOT = 14800
149317 feet/sec YDOT = 4561
165594 meter/sec
ZDOT = -14112
458851 ZDOT = -4279
721575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17027283
77 X = -5189916
09
Y = -7079610
08 feet Y = -2157865
15 meter
Z = -12221070
78 Z = -3724982
37
XDOT = 15277
062998 XDOT = 4656
448802
YDOT = -12517
535561 feet/sec YDOT = -3815
344839 meter/sec
ZDOT = -14027
967419 ZDOT = -4275
724469
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 08227
36737965
00020000 00000-0 20000-3 0 9037
2 25544 51
6421 77
5654 0008410 12
8777 347
2598 15
70977752 37693
Satellite: ISS
Catalog Number: 25544
Epoch time: 08227
36737965 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 77
5654 deg
Eccentricity:
0008410
Arg of perigee: 12
8777 deg
Mean anomaly: 347
2598 deg
Mean motion: 15
70977752 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3769
Checksum: 332
Coasting Arc #5 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2008/228/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4438416
06 A = 6732508
06 meter
Y = -2519756
38 meter E =
0016006
Z = 4387564
40 I = 51
94544
XDOT = 539
500746 Wp = 44
84814
YDOT = -6888
201757 meter/sec RA = 71
88056 deg
ZDOT = -3391
544761 TA = 79
27009
MA = 79
08992
Ha = 197
019 n
mi
Hp = 186
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14561732
48 X = -4431223
42
Y = -8266917
27 feet Y = -2569349
34 meter
Z = 14394896
32 Z = 4366020
35
XDOT = 1770
015572 XDOT = 632
960791
YDOT = -22599
087129 feet/sec YDOT = -6881
645992 meter/sec
ZDOT = -11127
115358 ZDOT = -3388
697308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9020671
36 X = -2749500
63
Y = 14191913
20 feet Y = 4325695
14 meter
Z = 14311397
62 Z = 4362113
99
XDOT = -21437
569478 XDOT = -6534
171177
YDOT = -2354
071840 feet/sec YDOT = -717
521097 meter/sec
ZDOT = -11116
724683 ZDOT = -3388
377683
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 08228
38517256
00020000 00000-0 20000-3 0 9040
2 25544 51
6414 72
3619 0008468 16
4213 343
7221 15
70991940 37854
Satellite: ISS
Catalog Number: 25544
Epoch time: 08228
38517256 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 72
3619 deg
Eccentricity:
0008468
Arg of perigee: 16
4213 deg
Mean anomaly: 343
7221 deg
Mean motion: 15
70991940 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3785
Checksum: 296
Coasting Arc #6 (Orbit 3800)
---------------------------------------
Vector Time (GMT): 2008/229/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 931855
51 A = 6738900
30 meter
Y = 6326673
53 meter E =
0020619
Z = 2086182
53 I = 51
95701
XDOT = -5207
284421 Wp = 51
07190
YDOT = -1079
341757 meter/sec RA = 66
83164 deg
ZDOT = 5575
350230 TA = 332
11942
MA = 332
22976
Ha = 197
089 n
mi
Hp = 186
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3057268
73 X = 850906
29
Y = 20756802
90 feet Y = 6336641
39 meter
Z = 6844430
89 Z = 2090512
97
XDOT = -17084
266473 XDOT = -5221
911514
YDOT = -3541
147498 feet/sec YDOT = -1137
654570 meter/sec
ZDOT = 18291
831463 ZDOT = 5550
018205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20849882
45 X = 6355044
17
Y = -2288443
94 feet Y = -697517
71 meter
Z = 6861735
87 Z = 2091457
09
XDOT = -4308
443464 XDOT = -1313
213568
YDOT = 15533
500306 feet/sec YDOT = 4734
610893 meter/sec
ZDOT = 18193
816951 ZDOT = 5545
475407
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 08229
40295684
00020000 00000-0 20000-3 0 9053
2 25544 51
6418 67
1579 0008536 20
0388 340
1107 15
70979954 38019
Satellite: ISS
Catalog Number: 25544
Epoch time: 08229
40295684 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 67
1579 deg
Eccentricity:
0008536
Arg of perigee: 20
0388 deg
Mean anomaly: 340
1107 deg
Mean motion: 15
70979954 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3801
Checksum: 304
Coasting Arc #7 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2008/230/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4267464
90 A = 6729198
15 meter
Y = -633846
69 meter E =
0017971
Z = -5177842
08 I = 51
91229
XDOT = 2643
629510 Wp = 72
52993
YDOT = 7093
715868 meter/sec RA = 61
70968 deg
ZDOT = 1319
450167 TA = 210
01929
MA = 210
12243
Ha = 197
088 n
mi
Hp = 186
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14000869
08 X = 4299388
06
Y = -2079549
50 feet Y = -585946
91 meter
Z = -16987670
87 Z = -5157033
59
XDOT = 8673
325164 XDOT = 2557
700434
YDOT = 23273
346025 feet/sec YDOT = 7122
797992 meter/sec
ZDOT = 4328
904747 ZDOT = 1332
084007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1827405
30 X = -556993
13
Y = -14132721
28 feet Y = -4307653
45 meter
Z = -16907294
34 Z = -5153343
32
XDOT = 22393
580590 XDOT = 6825
563364
YDOT = -8097
989917 feet/sec YDOT = -2468
267327 meter/sec
ZDOT = 4378
375341 ZDOT = 1334
528804
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 08230
35711955
00020000 00000-0 20000-3 0 9064
2 25544 51
6421 62
2793 0008485 22
7838 337
3699 15
71019537 38162
Satellite: ISS
Catalog Number: 25544
Epoch time: 08230
35711955 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 62
2793 deg
Eccentricity:
0008485
Arg of perigee: 22
7838 deg
Mean anomaly: 337
3699 deg
Mean motion: 15
71019537 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3816
Checksum: 308
Coasting Arc #8 (Orbit 3831)
---------------------------------------
Vector Time (GMT): 2008/231/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3569769
99 A = 6740733
09 meter
Y = -5713690
68 meter E =
0011894
Z = -206368
80 I = 51
93599
XDOT = 4116
317278 Wp = 95
01134
YDOT = -2364
017805 meter/sec RA = 56
62941 deg
ZDOT = -6050
411342 TA = 87
21731
MA = 87
08118
Ha = 197
143 n
mi
Hp = 186
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11711843
80 X = -3504610
79
Y = -18745704
33 feet Y = -5753245
58 meter
Z = -677062
99 Z = -223552
14
XDOT = 13504
977947 XDOT = 4171
837543
YDOT = -7755
963927 feet/sec YDOT = -2317
676429 meter/sec
ZDOT = -19850
430911 ZDOT = -6030
279679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18753480
98 X = -5716061
00
Y = 11695321
87 feet Y = 3564734
11 meter
Z = -743994
58 Z = -226769
55
XDOT = -6894
137183 XDOT = -2101
333013
YDOT = -12255
937997 feet/sec YDOT = -3735
609902 meter/sec
ZDOT = -19772
826271 ZDOT = -6026
757447
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 08231
37488602
00020000 00000-0 20000-3 0 9078
2 25544 51
6422 57
0753 0008359 26
8428 333
3165 15
70988831 38324
Satellite: ISS
Catalog Number: 25544
Epoch time: 08231
37488602 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 57
0753 deg
Eccentricity:
0008359
Arg of perigee: 26
8428 deg
Mean anomaly: 333
3165 deg
Mean motion: 15
70988831 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3832
Checksum: 304
Coasting Arc #9 (Orbit 3847)
---------------------------------------
Vector Time (GMT): 2008/232/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2606953
07 A = 6728768
47 meter
Y = 3320128
05 meter E =
0009111
Z = 5233167
55 I = 51
87938
XDOT = -5283
016191 Wp = 50
78676
YDOT = -5535
189059 meter/sec RA = 51
53997 deg
ZDOT = 884
576476 TA = 30
84625
MA = 30
79275
Ha = 197
283 n
mi
Hp = 186
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8552995
64 X = -2669307
06
Y = 10892808
58 feet Y = 3290627
10 meter
Z = 17169184
89 Z = 5220351
56
XDOT = -17332
730287 XDOT = -5225
025248
YDOT = -18160
069091 feet/sec YDOT = -5593
942522 meter/sec
ZDOT = 2902
153794 ZDOT = 859
052827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11034431
60 X = 3363294
75
Y = 8469756
21 feet Y = 2581581
69 meter
Z = 17119943
69 Z = 5218158
84
XDOT = -17253
051496 XDOT = -5258
730096
YDOT = 16842
346572 feet/sec YDOT = 5133
547235 meter/sec
ZDOT = 2803
004108 ZDOT = 854
355652
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 08232
39264118
00020000 00000-0 20000-3 0 9086
2 25544 51
6424 51
8712 0008534 29
9592 330
2056 15
71044508 38481
Satellite: ISS
Catalog Number: 25544
Epoch time: 08232
39264118 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 51
8712 deg
Eccentricity:
0008534
Arg of perigee: 29
9592 deg
Mean anomaly: 330
2056 deg
Mean motion: 15
71044508 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3848
Checksum: 289
Coasting Arc #10 (Orbit 3862)
---------------------------------------
Vector Time (GMT): 2008/233/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5369623
07 A = 6739330
80 meter
Y = 3675081
65 meter E =
0016284
Z = -1729653
59 I = 51
89567
XDOT = -1528
292788 Wp = 34
58764
YDOT = 4910
424760 meter/sec RA = 46
42081 deg
ZDOT = 5728
174780 TA = 306
35742
MA = 306
50759
Ha = 197
297 n
mi
Hp = 186
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17616873
59 X = 5336530
95
Y = 12057354
49 feet Y = 3734942
79 meter
Z = -5674716
50 Z = -1703648
54
XDOT = -5014
083950 XDOT = -1610
914685
YDOT = 16110
317453 feet/sec YDOT = 4892
872688 meter/sec
ZDOT = 18793
224343 ZDOT = 5720
549555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11455110
70 X = 3491517
74
Y = -18045741
00 feet Y = -5500341
86 meter
Z = -5573877
48 Z = -1698917
86
XDOT = 14958
053439 XDOT = 4559
214688
YDOT = 3739
817553 feet/sec YDOT = 1139
896390 meter/sec
ZDOT = 18764
186018 ZDOT = 5719
323898
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 08233
34677897
00020000 00000-0 20000-3 0 9095
2 25544 51
6423 46
9924 0008593 32
2989 327
8698 15
71049642 38637
Satellite: ISS
Catalog Number: 25544
Epoch time: 08233
34677897 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 46
9924 deg
Eccentricity:
0008593
Arg of perigee: 32
2989 deg
Mean anomaly: 327
8698 deg
Mean motion: 15
71049642 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3863
Checksum: 344
Coasting Arc #11 (Orbit 3878)
---------------------------------------
Vector Time (GMT): 2008/234/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -76854
84 A = 6731314
66 meter
Y = -4907696
24 meter E =
0018239
Z = -4624244
43 I = 51
84740
XDOT = 6562
204450 Wp = 54
38277
YDOT = 2684
101132 meter/sec RA = 41
36114 deg
ZDOT = -2955
441629 TA = 186
31192
MA = 186
33493
Ha = 197
250 n
mi
Hp = 186
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -252148
41 X = 493
28
Y = -16101365
61 feet Y = -4908123
25 meter
Z = -15171405
62 Z = -4624429
86
XDOT = 21529
542158 XDOT = 6546
059693
YDOT = 8806
106076 feet/sec YDOT = 2757
393175 meter/sec
ZDOT = -9696
330805 ZDOT = -2923
601671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16072103
66 X = -4898777
20
Y = 985022
82 feet Y = 300234
96 meter
Z = -15172551
39 Z = -4624593
66
XDOT = 7767
388974 XDOT = 2367
500159
YDOT = -20833
069716 feet/sec YDOT = -6349
919649 meter/sec
ZDOT = -9573
032272 ZDOT = -2917
860237
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 08234
36451659
00020000 00000-0 20000-3 0 9106
2 25544 51
6419 41
7882 0008533 35
4676 324
7052 15
71064452 38793
Satellite: ISS
Catalog Number: 25544
Epoch time: 08234
36451659 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 41
7882 deg
Eccentricity:
0008533
Arg of perigee: 35
4676 deg
Mean anomaly: 324
7052 deg
Mean motion: 15
71064452 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3879
Checksum: 301
Coasting Arc #12 (Orbit 3894)
---------------------------------------
Vector Time (GMT): 2008/235/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5754277
90 A = 6735571
30 meter
Y = -936746
82 meter E =
0019200
Z = 3364711
22 I = 51
83999
XDOT = -1790
988448 Wp = 69
67687
YDOT = -5855
138857 meter/sec RA = 36
21515 deg
ZDOT = -4665
097974 TA = 70
84965
MA = 70
64190
Ha = 197
324 n
mi
Hp = 185
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18878864
49 X = -5759720
58
Y = -3073316
34 feet Y = -1001124
93 meter
Z = 11039078
81 Z = 3336743
62
XDOT = -5875
946352 XDOT = -1702
719964
YDOT = -19209
773152 feet/sec YDOT = -5874
673136 meter/sec
ZDOT = -15305
439547 ZDOT = -4673
584280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1776377
25 X = -541439
78
Y = 19107012
26 feet Y = 5823817
34 meter
Z = 10930902
31 Z = 3331739
02
XDOT = -17377
798457 XDOT = -5296
752970
YDOT = 7212
416808 feet/sec YDOT = 2198
344643 meter/sec
ZDOT = -15338
743894 ZDOT = -4675
249139
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 08235
38224417
00020000 00000-0 20000-3 0 9110
2 25544 51
6426 36
5843 0008662 38
6859 321
4921 15
71123540 38952
Satellite: ISS
Catalog Number: 25544
Epoch time: 08235
38224417 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 36
5843 deg
Eccentricity:
0008662
Arg of perigee: 38
6859 deg
Mean anomaly: 321
4921 deg
Mean motion: 15
71123540 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3895
Checksum: 294
Coasting Arc #13 (Orbit 3910)
---------------------------------------
Vector Time (GMT): 2008/236/08:14:35
129
Vector Time (MET): N/A
Weight (LBS) : 661191
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3029556
47 A = 6735432
13 meter
Y = 4951732
01 meter E =
0019297
Z = 3393782
98 I = 51
81409
XDOT = -6127
102979 Wp = 70
70674
YDOT = 558
731243 meter/sec RA = 31
16499 deg
ZDOT = 4639
268140 TA = 329
24292
MA = 329
35586
Ha = 197
326 n
mi
Hp = 185
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9939489
74 X = 2957473
82
Y = 16245839
93 feet Y = 4985207
09 meter
Z = 11134458
61 Z = 3408325
71
XDOT = -20102
043893 XDOT = -6155
432209
YDOT = 1833
107752 feet/sec YDOT = 490
055881 meter/sec
ZDOT = 15220
695997 ZDOT = 4609
433798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15344919
06 X = 4677131
33
Y = -11224524
82 feet Y = -3421235
17 meter
Z = 11191087
59 Z = 3411043
50
XDOT = 2728
933730 XDOT = 831
779001
YDOT = 18840
080277 feet/sec YDOT = 5742
456469 meter/sec
ZDOT = 15105
431510 ZDOT = 4604
135524
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 08236
39996400
00020000 00000-0 20000-3 0 9121
2 25544 51
6415 31
3799 0008605 42
4093 317
7732 15
71087648 39118
Satellite: ISS
Catalog Number: 25544
Epoch time: 08236
39996400 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 31
3799 deg
Eccentricity:
0008605
Arg of perigee: 42
4093 deg
Mean anomaly: 317
7732 deg
Mean motion: 15
71087648 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3911
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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