Date:
March 21st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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
There are no maneuvers
Coasting Arc #1 (Orbit 1449)
---------------------------------------
Vector Time (GMT): 2008/080/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2935987
41 A = 6714561
53 meter
Y = -3230019
53 meter E =
0004199
Z = 5100244
26 I = 51
91754
XDOT = 4161
914504 Wp = 46
66406
YDOT = -6289
649110 meter/sec RA = 114
02141 deg
ZDOT = -1583
815295 TA = 58
49175
MA = 58
45074
Ha = 186
452 n
mi
Hp = 180
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9632504
62 X = -2924426
36
Y = -10597176
93 feet Y = -3262786
25 meter
Z = 16733084
83 Z = 5086009
83
XDOT = 13654
575145 XDOT = 4239
630803
YDOT = -20635
331726 feet/sec YDOT = -6242
673833 meter/sec
ZDOT = -5196
244405 ZDOT = -1563
407569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11261191
39 X = 3432411
13
Y = -8950275
67 feet Y = -2728044
02 meter
Z = 16678116
38 Z = 5083489
87
XDOT = 18958
904325 XDOT = 5778
674038
YDOT = 14293
393135 feet/sec YDOT = 4356
626228 meter/sec
ZDOT = -5118
727722 ZDOT = -1560
188210
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
29086815
00020000 00000-0 20000-3 0 9004
2 25544 51
6382 114
6530 0000895 274
1102 85
9960 15
76227791 14500
Satellite: ISS
Catalog Number: 25544
Epoch time: 08080
29086815 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 114
6530 deg
Eccentricity:
0000895
Arg of perigee: 274
1102 deg
Mean anomaly: 85
9960 deg
Mean motion: 15
76227791 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1450
Checksum: 286
Coasting Arc #2 (Orbit 1465)
---------------------------------------
Vector Time (GMT): 2008/081/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3552943
30 A = 6723784
94 meter
Y = 5300484
27 meter E =
0013277
Z = 2098857
74 I = 51
96029
XDOT = -3128
477450 Wp = 67
95545
YDOT = -4311
474450 meter/sec RA = 108
92153 deg
ZDOT = 5569
409823 TA = 315
41781
MA = 315
52453
Ha = 186
284 n
mi
Hp = 180
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11656638
13 X = -3622145
87
Y = 17390040
25 feet Y = 5260366
52 meter
Z = 6886016
22 Z = 2081429
02
XDOT = -10264
033628 XDOT = -3107
088329
YDOT = -14145
257381 feet/sec YDOT = -4346
338675 meter/sec
ZDOT = 18272
341939 ZDOT = 5554
264227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16735117
60 X = -5100863
85
Y = -12614835
21 feet Y = -3845001
77 meter
Z = 6819802
29 Z = 2078675
74
XDOT = 13763
090890 XDOT = 4194
990103
YDOT = -8370
614428 feet/sec YDOT = -2551
363278 meter/sec
ZDOT = 18213
753321 ZDOT = 5551
552012
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
30524119
00020000 00000-0 20000-3 0 9012
2 25544 51
6387 109
4258 0000923 275
0739 85
0320 15
76293109 14666
Satellite: ISS
Catalog Number: 25544
Epoch time: 08081
30524119 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 109
4258 deg
Eccentricity:
0000923
Arg of perigee: 275
0739 deg
Mean anomaly: 85
0320 deg
Mean motion: 15
76293109 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1466
Checksum: 280
Coasting Arc #3 (Orbit 1480)
---------------------------------------
Vector Time (GMT): 2008/082/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2575730
76 A = 6716870
90 meter
Y = 4282916
73 meter E =
0008829
Z = -4496329
62 I = 51
94523
XDOT = -3986
435648 Wp = 111
45897
YDOT = 5754
332844 meter/sec RA = 103
74902 deg
ZDOT = 3199
408258 TA = 190
39574
MA = 190
41401
Ha = 186
217 n
mi
Hp = 180
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8450560
23 X = 2549489
38
Y = 14051564
09 feet Y = 4311572
83 meter
Z = -14751737
61 Z = -4483880
95
XDOT = -13078
857112 XDOT = -4066
027315
YDOT = 18879
044763 feet/sec YDOT = 5709
309559 meter/sec
ZDOT = 10496
746252 ZDOT = 3179
848280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14354983
67 X = -4375399
02
Y = 8013348
29 feet Y = 2442468
56 meter
Z = -14703498
79 Z = -4481626
43
XDOT = -17800
402819 XDOT = -5425
562779
YDOT = -12774
618321 feet/sec YDOT = -3893
703664 meter/sec
ZDOT = 10422
406042 ZDOT = 3176
749362
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
25620233
00020000 00000-0 20000-3 0 9022
2 25544 51
6385 104
5261 0000989 283
2577 76
8477 15
76307353 14812
Satellite: ISS
Catalog Number: 25544
Epoch time: 08082
25620233 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 104
5261 deg
Eccentricity:
0000989
Arg of perigee: 283
2577 deg
Mean anomaly: 76
8477 deg
Mean motion: 15
76307353 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1481
Checksum: 296
Coasting Arc #4 (Orbit 1496)
---------------------------------------
Vector Time (GMT): 2008/083/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3428621
06 A = 6720490
71 meter
Y = -4650079
65 meter E =
0004055
Z = -3436970
68 I = 51
96348
XDOT = 2815
416092 Wp = 84
22854
YDOT = 5482
931504 meter/sec RA = 98
66652 deg
ZDOT = -4613
827983 TA = 136
24753
MA = 136
21539
Ha = 186
221 n
mi
Hp = 180
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11248756
75 X = 3497060
36
Y = -15256166
85 feet Y = -4611356
51 meter
Z = -11276150
52 Z = -3420147
74
XDOT = 9236
929435 XDOT = 2776
309031
YDOT = 17988
620419 feet/sec YDOT = 5514
196005 meter/sec
ZDOT = -15137
230916 ZDOT = -4600
246177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15033105
91 X = 4582090
68
Y = 11607311
18 feet Y = 3537908
45 meter
Z = -11212171
05 Z = -3417469
73
XDOT = -17320
255777 XDOT = -5279
213961
YDOT = 7874
637175 feet/sec YDOT = 2400
189411 meter/sec
ZDOT = -15084
513672 ZDOT = -4597
759767
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
27054311
00020000 00000-0 20000-3 0 9034
2 25544 51
6388 99
2983 0000959 286
2659 73
8400 15
76320625 14974
Satellite: ISS
Catalog Number: 25544
Epoch time: 08083
27054311 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 99
2983 deg
Eccentricity:
0000959
Arg of perigee: 286
2659 deg
Mean anomaly: 73
8400 deg
Mean motion: 15
76320625 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1497
Checksum: 310
Coasting Arc #5 (Orbit 1512)
---------------------------------------
Vector Time (GMT): 2008/084/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2393685
55 A = 6720350
73 meter
Y = -5233502
50 meter E =
0011693
Z = 3461094
10 I = 51
96624
XDOT = 3888
175993 Wp = 86
84440
YDOT = -4820
897396 meter/sec RA = 93
48500 deg
ZDOT = -4586
777066 TA = 52
28631
MA = 52
18037
Ha = 186
297 n
mi
Hp = 180
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7853299
06 X = -2351799
26
Y = -17170283
81 feet Y = -5260035
60 meter
Z = 11355295
59 Z = 3449567
66
XDOT = 12756
482916 XDOT = 3964
076877
YDOT = -15816
592506 feet/sec YDOT = -4776
993555 meter/sec
ZDOT = -15048
481189 ZDOT = -4567
703493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17188154
27 X = 5238949
42
Y = -7878813
34 feet Y = -2401462
31 meter
Z = 11310497
04 Z = 3447439
50
XDOT = 15212
973422 XDOT = 4636
914299
YDOT = 11623
998790 feet/sec YDOT = 3542
994831 meter/sec
ZDOT = -14975
881428 ZDOT = -4564
648659
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
28486659
00020000 00000-0 20000-3 0 9041
2 25544 51
6387 94
0713 0000829 297
0618 63
0462 15
76337649 15130
Satellite: ISS
Catalog Number: 25544
Epoch time: 08084
28486659 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 94
0713 deg
Eccentricity:
0000829
Arg of perigee: 297
0618 deg
Mean anomaly: 63
0462 deg
Mean motion: 15
76337649 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1513
Checksum: 313
Coasting Arc #6 (Orbit 1528)
---------------------------------------
Vector Time (GMT): 2008/085/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3396562
37 A = 6716680
99 meter
Y = 3681464
22 meter E =
0008130
Z = 4469922
10 I = 51
95562
XDOT = -2714
772899 Wp = 111
09945
YDOT = -6445
637460 meter/sec RA = 88
40265 deg
ZDOT = 3238
253674 TA = 306
62053
MA = 306
69528
Ha = 186
208 n
mi
Hp = 180
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11143577
34 X = -3459190
84
Y = 12078294
70 feet Y = 3643132
00 meter
Z = 14665098
74 Z = 4453269
17
XDOT = -8906
735232 XDOT = -2658
225958
YDOT = -21147
104529 feet/sec YDOT = -6475
679253 meter/sec
ZDOT = 10624
191843 ZDOT = 3225
202937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12244668
41 X = -3732174
93
Y = -11044894
84 feet Y = -3366483
95 meter
Z = 14601644
88 Z = 4450581
36
XDOT = 20205
371986 XDOT = 6158
597381
YDOT = -8388
990344 feet/sec YDOT = -2556
964257 meter/sec
ZDOT = 10573
419637 ZDOT = 3222
778305
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
29916947
00020000 00000-0 20000-3 0 9052
2 25544 51
6393 88
8433 0000949 300
0067 60
1003 15
76410379 15291
Satellite: ISS
Catalog Number: 25544
Epoch time: 08085
29916947 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 88
8433 deg
Eccentricity:
0000949
Arg of perigee: 300
0067 deg
Mean anomaly: 60
1003 deg
Mean motion: 15
76410379 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1529
Checksum: 295
Coasting Arc #7 (Orbit 1543)
---------------------------------------
Vector Time (GMT): 2008/086/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2364539
32 A = 6723499
09 meter
Y = 5927119
82 meter E =
0006573
Z = -2109278
71 I = 51
97634
XDOT = -3961
271838 Wp = 30
95376
YDOT = 3556
655594 meter/sec RA = 83
23012 deg
ZDOT = 5566
741836 TA = 305
56842
MA = 305
62967
Ha = 186
189 n
mi
Hp = 180
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7757674
94 X = 2308332
16
Y = 19445931
16 feet Y = 5953247
10 meter
Z = -6920205
75 Z = -2097928
45
XDOT = -12996
298680 XDOT = -4027
790892
YDOT = 11668
817566 feet/sec YDOT = 3511
986659 meter/sec
ZDOT = 18263
588701 ZDOT = 5547
336162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19185309
92 X = -5847682
46
Y = 8417791
66 feet Y = 2565742
90 meter
Z = -6876021
63 Z = -2095811
39
XDOT = -11469
940696 XDOT = -3496
037924
YDOT = -11318
933258 feet/sec YDOT = -3450
010857 meter/sec
ZDOT = 18189
555063 ZDOT = 5544
176383
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
25006451
00020000 00000-0 20000-3 0 9060
2 25544 51
6395 83
9433 0001131 311
8168 48
2900 15
76377305 15446
Satellite: ISS
Catalog Number: 25544
Epoch time: 08086
25006451 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 83
9433 deg
Eccentricity:
0001131
Arg of perigee: 311
8168 deg
Mean anomaly: 48
2900 deg
Mean motion: 15
76377305 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1544
Checksum: 278
Coasting Arc #8 (Orbit 1559)
---------------------------------------
Vector Time (GMT): 2008/087/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3582149
69 A = 6713960
70 meter
Y = -2468507
50 meter E =
0013281
Z = -5125597
14 I = 51
93941
XDOT = 2691
892493 Wp = 74
95371
YDOT = 7048
126128 meter/sec RA = 78
13041 deg
ZDOT = -1512
972708 TA = 180
58450
MA = 180
58605
Ha = 186
115 n
mi
Hp = 180
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11752459
60 X = 3634386
03
Y = -8098777
90 feet Y = -2428157
89 meter
Z = -16816263
59 Z = -5108068
05
XDOT = 8831
668285 XDOT = 2620
228965
YDOT = 23123
773385 feet/sec YDOT = 7077
827687 meter/sec
ZDOT = -4963
821222 ZDOT = -1500
069642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8673306
60 X = 2643623
85
Y = 11433805
95 feet Y = 3485024
05 meter
Z = -16749300
44 Z = -5105186
77
XDOT = -21824
838657 XDOT = -6652
210823
YDOT = 9357
090149 feet/sec YDOT = 2852
041077 meter/sec
ZDOT = -4913
567022 ZDOT = -1497
655228
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
26433380
00020000 00000-0 20000-3 0 9078
2 25544 51
6391 78
7160 0001045 310
6852 49
4221 15
76418664 15603
Satellite: ISS
Catalog Number: 25544
Epoch time: 08087
26433380 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 78
7160 deg
Eccentricity:
0001045
Arg of perigee: 310
6852 deg
Mean anomaly: 49
4221 deg
Mean motion: 15
76418664 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1560
Checksum: 283
Coasting Arc #9 (Orbit 1575)
---------------------------------------
Vector Time (GMT): 2008/088/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2326690
05 A = 6725075
92 meter
Y = -6284379
38 meter E =
0012191
Z = 492859
22 I = 51
96983
XDOT = 4307
117022 Wp = 128
79438
YDOT = -2075
731128 meter/sec RA = 72
98143 deg
ZDOT = -6042
490767 TA = 45
86252
MA = 45
76233
Ha = 186
141 n
mi
Hp = 180
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7633497
54 X = -2258638
44
Y = -20618042
59 feet Y = -6310017
26 meter
Z = 1616992
18 Z = 481721
49
XDOT = 14130
961357 XDOT = 4359
361447
YDOT = -6810
141497 feet/sec YDOT = -2027
274427 meter/sec
ZDOT = -19824
444774 ZDOT = -6021
439828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20064169
34 X = 6115558
81
Y = -8996750
92 feet Y = -2742209
68 meter
Z = 1573597
98 Z = 479632
67
XDOT = 7086
165182 XDOT = 2159
863147
YDOT = 12295
756894 feet/sec YDOT = 3747
746701 meter/sec
ZDOT = -19743
924391 ZDOT = -6017
948155
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
27858460
00020000 00000-0 20000-3 0 9081
2 25544 51
6389 73
4885 0000954 324
1006 36
0095 15
76464624 15760
Satellite: ISS
Catalog Number: 25544
Epoch time: 08088
27858460 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 73
4885 deg
Eccentricity:
0000954
Arg of perigee: 324
1006 deg
Mean anomaly: 36
0095 deg
Mean motion: 15
76464624 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1576
Checksum: 313
Coasting Arc #10 (Orbit 1591)
---------------------------------------
Vector Time (GMT): 2008/089/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3990163
04 A = 6712953
16 meter
Y = 1154150
16 meter E =
0002447
Z = 5272115
93 I = 51
92039
XDOT = -2614
884044 Wp = 46
81474
YDOT = -7239
199061 meter/sec RA = 67
84966 deg
ZDOT = -392
527181 TA = 46
90530
MA = 46
88483
Ha = 186
127 n
mi
Hp = 180
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13091086
10 X = -4028383
34
Y = 3786581
89 feet Y = 1109316
21 meter
Z = 17296968
26 Z = 5252638
89
XDOT = -8579
015893 XDOT = -2531
833026
YDOT = -23750
653087 feet/sec YDOT = -7267
975828 meter/sec
ZDOT = -1287
818835 ZDOT = -405
028501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4876599
69 X = -1486387
59
Y = -12826075
76 feet Y = -3909387
89 meter
Z = 17222380
92 Z = 5249381
71
XDOT = 22015
061666 XDOT = 6710
190796
YDOT = -10172
755808 feet/sec YDOT = -3100
655970 meter/sec
ZDOT = -1336
540664 ZDOT = -407
377594
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 08089
29281412
00020000 00000-0 20000-3 0 9092
2 25544 51
6396 68
2604 0001089 320
9980 39
1106 15
76528592 15924
Satellite: ISS
Catalog Number: 25544
Epoch time: 08089
29281412 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 68
2604 deg
Eccentricity:
0001089
Arg of perigee: 320
9980 deg
Mean anomaly: 39
1106 deg
Mean motion: 15
76528592 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1592
Checksum: 308
Coasting Arc #11 (Orbit 1607)
---------------------------------------
Vector Time (GMT): 2008/090/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2181595
50 A = 6724459
60 meter
Y = 6243107
10 meter E =
0014178
Z = 1176908
94 I = 51
94618
XDOT = -4905
046037 Wp = 53
37339
YDOT = 591
208271 meter/sec RA = 62
73072 deg
ZDOT = 5915
677896 TA = 319
48285
MA = 319
58832
Ha = 186
170 n
mi
Hp = 180
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7157465
55 X = 2105904
78
Y = 20482634
83 feet Y = 6267079
75 meter
Z = 3861249
81 Z = 1187323
18
XDOT = -16092
670724 XDOT = -4940
029645
YDOT = 1939
659682 feet/sec YDOT = 536
161702 meter/sec
ZDOT = 19408
392047 ZDOT = 5891
764298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19659210
93 X = -5992127
49
Y = 9163395
96 feet Y = 2793003
09 meter
Z = 3901857
62 Z = 1189286
20
XDOT = -2894
487841 XDOT = -882
239894
YDOT = -14491
045999 feet/sec YDOT = -4416
870820 meter/sec
ZDOT = 19316
722332 ZDOT = 5887
736967
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 08090
30702820
00020000 00000-0 20000-3 0 9109
2 25544 51
6390 63
0325 0001115 339
8240 20
2880 15
76502401 16088
Satellite: ISS
Catalog Number: 25544
Epoch time: 08090
30702820 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 63
0325 deg
Eccentricity:
0001115
Arg of perigee: 339
8240 deg
Mean anomaly: 20
2880 deg
Mean motion: 15
76502401 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1608
Checksum: 239
Coasting Arc #12 (Orbit 1622)
---------------------------------------
Vector Time (GMT): 2008/091/05:54:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4606164
49 A = 6714601
99 meter
Y = 91307
78 meter E =
0011683
Z = -4895354
74 I = 51
89836
XDOT = 2299
686237 Wp = 101
97511
YDOT = 6976
104618 meter/sec RA = 57
56596 deg
ZDOT = 2296
160239 TA = 190
29409
MA = 190
31803
Ha = 186
115 n
mi
Hp = 180
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15112088
21 X = 4628581
72
Y = 299566
21 feet Y = 142941
78 meter
Z = -16060875
13 Z = -4872923
69
XDOT = 7544
902351 XDOT = 2210
353174
YDOT = 22887
482344 feet/sec YDOT = 7001
321585 meter/sec
ZDOT = 7533
334117 ZDOT = 2307
114904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1494651
41 X = 455569
75
Y = 15132345
85 feet Y = 4612339
01 meter
Z = -15974817
25 Z = -4869124
30
XDOT = -20740
071333 XDOT = -6321
573742
YDOT = 10038
724840 feet/sec YDOT = 3059
803331 meter/sec
ZDOT = 7576
091156 ZDOT = 2309
192584
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 08091
25783298
00020000 00000-0 20000-3 0 9113
2 25544 51
6386 58
1310 0001133 342
5905 17
5220 15
76551440 16232
Satellite: ISS
Catalog Number: 25544
Epoch time: 08091
25783298 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 58
1310 deg
Eccentricity:
0001133
Arg of perigee: 342
5905 deg
Mean anomaly: 17
5220 deg
Mean motion: 15
76551440 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1623
Checksum: 267
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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