Date:
March 25th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8234 39 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 1481)
---------------------------------------
Vector Time (GMT): 2008/082/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1959480
33 A = 6725476
47 meter
Y = -6407681
26 meter E =
0010084
Z = -515000
92 I = 51
97530
XDOT = 4417
554778 Wp = 144
58566
YDOT = 1831
060289 meter/sec RA = 103
55804 deg
ZDOT = -6040
698371 TA = 40
99698
MA = 40
92122
Ha = 186
015 n
mi
Hp = 180
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6428741
22 X = 2033488
15
Y = -21022576
31 feet Y = -6385355
49 meter
Z = -1689635
57 Z = -505301
36
XDOT = 14493
289955 XDOT = 4426
095801
YDOT = 6007
415647 feet/sec YDOT = 1880
507033 meter/sec
ZDOT = -19818
564210 ZDOT = -6019
217397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21941777
54 X = 6687853
79
Y = 1399169
15 feet Y = 426466
76 meter
Z = -1653185
07 Z = -503890
81
XDOT = -2362
891998 XDOT = -720
209481
YDOT = 13999
195547 feet/sec YDOT = 4266
954803 meter/sec
ZDOT = -19735
973053 ZDOT = -6015
524587
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
31957819
00020000 00000-0 20000-3 0 9000
2 25544 51
6391 104
2004 0001499 277
7934 82
3061 15
76319087 14822
Satellite: ISS
Catalog Number: 25544
Epoch time: 08082
31957819 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 104
2004 deg
Eccentricity:
0001499
Arg of perigee: 277
7934 deg
Mean anomaly: 82
3061 deg
Mean motion: 15
76319087 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1482
Checksum: 294
Coasting Arc #2 (Orbit 1497)
---------------------------------------
Vector Time (GMT): 2008/083/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3729247
69 A = 6714010
88 meter
Y = -2211057
11 meter E =
0003896
Z = 5125328
63 I = 51
94339
XDOT = 2240
587906 Wp = 35
66051
YDOT = -7222
810150 meter/sec RA = 98
40935 deg
ZDOT = -1481
970958 TA = 68
49673
MA = 68
45519
Ha = 186
015 n
mi
Hp = 180
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12235064
60 X = -3729144
11
Y = -7254124
37 feet Y = -2252758
63 meter
Z = 16815382
64 Z = 5107212
37
XDOT = 7351
010189 XDOT = 2328
387125
YDOT = -23696
883693 feet/sec YDOT = -7197
263842 meter/sec
ZDOT = -4862
109443 ZDOT = -1470
872230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3968406
97 X = 1209570
44
Y = -13744492
31 feet Y = -4189321
26 meter
Z = 16745653
07 Z = 5104075
06
XDOT = 23784
294676 XDOT = 7249
453017
YDOT = 979
560247 feet/sec YDOT = 298
569963 meter/sec
ZDOT = -4820
377914 ZDOT = -1469
251188
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
33390013
00020000 00000-0 20000-3 0 9011
2 25544 51
6396 98
9725 0001568 287
4981 72
6012 15
76389386 14987
Satellite: ISS
Catalog Number: 25544
Epoch time: 08083
33390013 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 98
9725 deg
Eccentricity:
0001568
Arg of perigee: 287
4981 deg
Mean anomaly: 72
6012 deg
Mean motion: 15
76389386 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1498
Checksum: 320
Coasting Arc #3 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2008/084/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1956521
64 A = 6723580
24 meter
Y = 6090511
97 meter E =
0013074
Z = 2048446
35 I = 51
97850
XDOT = -4195
617401 Wp = 64
61759
YDOT = -3237
357905 meter/sec RA = 93
30947 deg
ZDOT = 5596
068262 TA = 318
15767
MA = 318
25754
Ha = 185
978 n
mi
Hp = 180
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6419034
24 X = -2034432
30
Y = 19981994
66 feet Y = 6068197
56 meter
Z = 6720624
50 Z = 2038751
82
XDOT = -13765
148953 XDOT = -4186
289752
YDOT = -10621
252970 feet/sec YDOT = -3284
223123 meter/sec
ZDOT = 18359
804010 ZDOT = 5575
708759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20978436
83 X = -6394227
55
Y = -937230
77 feet Y = -285667
94 meter
Z = 6684137
29 Z = 2037325
05
XDOT = 6502
717996 XDOT = 1982
028445
YDOT = -14656
205481 feet/sec YDOT = -4467
211431 meter/sec
ZDOT = 18281
357417 ZDOT = 5572
157741
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
34820442
00020000 00000-0 20000-3 0 9028
2 25544 51
6395 93
7453 0001469 291
7631 68
3377 15
76391282 15140
Satellite: ISS
Catalog Number: 25544
Epoch time: 08084
34820442 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 93
7453 deg
Eccentricity:
0001469
Arg of perigee: 291
7631 deg
Mean anomaly: 68
3377 deg
Mean motion: 15
76391282 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1514
Checksum: 300
Coasting Arc #4 (Orbit 1528)
---------------------------------------
Vector Time (GMT): 2008/085/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3639023
02 A = 6716471
48 meter
Y = 3411487
92 meter E =
0008425
Z = -4506052
67 I = 51
95496
XDOT = -2276
177728 Wp = 109
24444
YDOT = 6628
747883 meter/sec RA = 88
13747 deg
ZDOT = 3182
432376 TA = 192
41290
MA = 192
43366
Ha = 185
928 n
mi
Hp = 180
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11939051
90 X = 3622494
49
Y = 11192545
66 feet Y = 3452088
89 meter
Z = -14783637
36 Z = -4488414
52
XDOT = -7467
774698 XDOT = -2365
592023
YDOT = 21747
860507 feet/sec YDOT = 6602
794595 meter/sec
ZDOT = 10441
051104 ZDOT = 3171
157090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7359198
90 X = -2243083
83
Y = 14685466
90 feet Y = 4476130
31 meter
Z = -14715611
62 Z = -4485318
42
XDOT = -21916
051621 XDOT = -6680
012534
YDOT = -569
576521 feet/sec YDOT = -173
606923 meter/sec
ZDOT = 10398
550258 ZDOT = 3169
478118
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
29909626
00020000 00000-0 20000-3 0 9036
2 25544 51
6391 88
8452 0001424 298
0272 62
0748 15
76442085 15299
Satellite: ISS
Catalog Number: 25544
Epoch time: 08085
29909626 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 88
8452 deg
Eccentricity:
0001424
Arg of perigee: 298
0272 deg
Mean anomaly: 62
0748 deg
Mean motion: 15
76442085 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1529
Checksum: 307
Coasting Arc #5 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2008/086/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2064533
17 A = 6720101
06 meter
Y = -5385935
04 meter E =
0003885
Z = -3452264
99 I = 51
96451
XDOT = 4177
882705 Wp = 75
04051
YDOT = 4546
957390 meter/sec RA = 83
05481 deg
ZDOT = -4598
600173 TA = 145
65428
MA = 145
62916
Ha = 185
940 n
mi
Hp = 180
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6773402
77 X = 2141376
67
Y = -17670390
56 feet Y = -5362418
72 meter
Z = -11326328
69 Z = -3442048
59
XDOT = 13706
964256 XDOT = 4149
066714
YDOT = 14917
839206 feet/sec YDOT = 4593
515584 meter/sec
ZDOT = -15087
270908 ZDOT = -4578
374050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18904766
65 X = 5762172
88
Y = 1266549
54 feet Y = 386044
30 meter
Z = -11287739
33 Z = -3440502
95
XDOT = -10042
632996 XDOT = -3060
994537
YDOT = 16229
806265 feet/sec YDOT = 4946
844949 meter/sec
ZDOT = -15009
197923 ZDOT = -4574
803527
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
31336191
00020000 00000-0 20000-3 0 9042
2 25544 51
6387 83
6173 0001468 301
4360 58
6660 15
76433550 15451
Satellite: ISS
Catalog Number: 25544
Epoch time: 08086
31336191 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 83
6173 deg
Eccentricity:
0001468
Arg of perigee: 301
4360 deg
Mean anomaly: 58
6660 deg
Mean motion: 15
76433550 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1545
Checksum: 285
Coasting Arc #6 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2008/087/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3689273
96 A = 6720027
24 meter
Y = -4453355
20 meter E =
0011360
Z = 3414302
68 I = 51
96099
XDOT = 2496
759852 Wp = 84
30446
YDOT = -5630
512615 meter/sec RA = 77
87192 deg
ZDOT = -4631
992281 TA = 55
49083
MA = 55
38361
Ha = 185
907 n
mi
Hp = 180
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12103917
19 X = -3655787
79
Y = -14610745
42 feet Y = -4494423
48 meter
Z = 11201780
43 Z = 3396461
52
XDOT = 8191
469331 XDOT = 2582
037038
YDOT = -18472
810417 feet/sec YDOT = -5602
115697 meter/sec
ZDOT = -15196
825070 ZDOT = -4619
655725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10049485
69 X = 3063083
24
Y = -16140807
00 feet Y = -4919717
97 meter
Z = 11132868
66 Z = 3393298
37
XDOT = 18960
868581 XDOT = 5779
272743
YDOT = 1323
447511 feet/sec YDOT = 403
386801 meter/sec
ZDOT = -15150
120408 ZDOT = -4617
756700
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
32760564
00020000 00000-0 20000-3 0 9050
2 25544 51
6396 78
3895 0001619 310
6281 49
4742 15
76508521 15613
Satellite: ISS
Catalog Number: 25544
Epoch time: 08087
32760564 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 78
3895 deg
Eccentricity:
0001619
Arg of perigee: 310
6281 deg
Mean anomaly: 49
4742 deg
Mean motion: 15
76508521 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1561
Checksum: 305
Coasting Arc #7 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2008/088/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2355211
14 A = 6716121
32 meter
Y = 4365493
36 meter E =
0007362
Z = 4523225
84 I = 51
94040
XDOT = -4298
382792 Wp = 109
45574
YDOT = -5575
839868 meter/sec RA = 72
78812 deg
ZDOT = 3136
758970 TA = 309
38849
MA = 309
45366
Ha = 185
941 n
mi
Hp = 180
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7727070
68 X = -2425824
78
Y = 14322484
79 feet Y = 4338761
27 meter
Z = 14839979
78 Z = 4511612
64
XDOT = -14102
305748 XDOT = -4250
951257
YDOT = -18293
437886 feet/sec YDOT = -5623
641608 meter/sec
ZDOT = 10291
203970 ZDOT = 3115
992645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16098907
52 X = -4906947
01
Y = -2640565
39 feet Y = -804844
33 meter
Z = 14795904
26 Z = 4509791
62
XDOT = 12395
161630 XDOT = 3778
045265
YDOT = -18235
315601 feet/sec YDOT = -5558
124195 meter/sec
ZDOT = 10210
954404 ZDOT = 3112
298902
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
34182989
00020000 00000-0 20000-3 0 9063
2 25544 51
6394 73
1616 0001520 312
7049 47
3987 15
76525236 15778
Satellite: ISS
Catalog Number: 25544
Epoch time: 08088
34182989 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 73
1616 deg
Eccentricity:
0001520
Arg of perigee: 312
7049 deg
Mean anomaly: 47
3987 deg
Mean motion: 15
76525236 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1577
Checksum: 313
Coasting Arc #8 (Orbit 1591)
---------------------------------------
Vector Time (GMT): 2008/089/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3802781
87 A = 6723326
76 meter
Y = 5177128
74 meter E =
0007400
Z = -1973686
36 I = 51
95444
XDOT = -2981
380706 Wp = 27
14332
YDOT = 4330
769923 meter/sec RA = 67
61420 deg
ZDOT = 5630
240310 TA = 310
95943
MA = 311
02344
Ha = 185
961 n
mi
Hp = 180
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12476318
48 X = 3754195
58
Y = 16985330
52 feet Y = 5219381
95 meter
Z = -6475348
95 Z = -1955330
51
XDOT = -9781
432762 XDOT = -3056
937128
YDOT = 14208
562739 feet/sec YDOT = 4297
007998 meter/sec
ZDOT = 18471
917027 ZDOT = 5615
573225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11595970
95 X = -3534451
94
Y = 17624056
65 feet Y = 5371812
47 meter
Z = -6404389
51 Z = -1952057
92
XDOT = -15469
041204 XDOT = -4714
963759
YDOT = -3503
495935 feet/sec YDOT = -1067
865561 meter/sec
ZDOT = 18416
116929 ZDOT = 5613
232440
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
29264683
00020000 00000-0 20000-3 0 9071
2 25544 51
6391 68
2605 0001570 321
3772 38
7280 15
76527353 15921
Satellite: ISS
Catalog Number: 25544
Epoch time: 08089
29264683 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 68
2605 deg
Eccentricity:
0001570
Arg of perigee: 321
3772 deg
Mean anomaly: 38
7280 deg
Mean motion: 15
76527353 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1592
Checksum: 304
Coasting Arc #9 (Orbit 1607)
---------------------------------------
Vector Time (GMT): 2008/090/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2926397
47 A = 6713366
31 meter
Y = -3150725
71 meter E =
0013678
Z = -5167357
84 I = 51
90924
XDOT = 4373
525826 Wp = 74
34770
YDOT = 6196
234268 meter/sec RA = 62
50831 deg
ZDOT = -1300
460627 TA = 183
24803
MA = 183
25692
Ha = 185
931 n
mi
Hp = 180
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9601041
56 X = 2986513
86
Y = -10337026
61 feet Y = -3117664
99 meter
Z = -16953273
75 Z = -5152995
40
XDOT = 14348
838011 XDOT = 4310
230897
YDOT = 20328
852585 feet/sec YDOT = 6244
787618 meter/sec
ZDOT = -4266
603108 ZDOT = -1279
367936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13150028
44 X = 4008128
67
Y = 5288161
07 feet Y = 1611831
49 meter
Z = -16898512
17 Z = -5150666
51
XDOT = -13346
847672 XDOT = -4068
119170
YDOT = 19807
888208 feet/sec YDOT = 6037
444326 meter/sec
ZDOT = -4185
037885 ZDOT = -1275
599547
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
30683041
00020000 00000-0 20000-3 0 9089
2 25544 51
6395 63
0319 0001485 325
9525 34
1544 15
76556115 16080
Satellite: ISS
Catalog Number: 25544
Epoch time: 08090
30683041 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 63
0319 deg
Eccentricity:
0001485
Arg of perigee: 325
9525 deg
Mean anomaly: 34
1544 deg
Mean motion: 15
76556115 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1608
Checksum: 281
Coasting Arc #10 (Orbit 1623)
---------------------------------------
Vector Time (GMT): 2008/091/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3788947
48 A = 6724692
29 meter
Y = -5543580
23 meter E =
0011320
Z = 256080
87 I = 51
93373
XDOT = 3790
819706 Wp = 129
19426
YDOT = -2878
691397 meter/sec RA = 57
35954 deg
ZDOT = -6058
621864 TA = 48
03122
MA = 47
93483
Ha = 185
913 n
mi
Hp = 179
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12430930
04 X = -3727920
68
Y = -18187599
17 feet Y = -5585609
18 meter
Z = 840160
33 Z = 237822
64
XDOT = 12437
072527 XDOT = 3852
159433
YDOT = -9444
525581 feet/sec YDOT = -2835
957450 meter/sec
ZDOT = -19877
368319 ZDOT = -6040
057130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12124927
28 X = 3695677
83
Y = -18396103
04 feet Y = -5607132
21 meter
Z = 769536
50 Z = 234554
73
XDOT = 12151
618367 XDOT = 3703
813278
YDOT = 7155
157174 feet/sec YDOT = 2180
891906 meter/sec
ZDOT = -19806
454230 ZDOT = -6037
007249
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
32099137
00020000 00000-0 20000-3 0 9090
2 25544 51
6398 57
8034 0001539 335
8981 24
2112 15
76626290 16245
Satellite: ISS
Catalog Number: 25544
Epoch time: 08091
32099137 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 57
8034 deg
Eccentricity:
0001539
Arg of perigee: 335
8981 deg
Mean anomaly: 24
2112 deg
Mean motion: 15
76626290 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1624
Checksum: 297
Coasting Arc #11 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2008/092/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739901
81 A = 6712717
80 meter
Y = 1890575
82 meter E =
0003627
Z = 5242402
33 I = 51
87601
XDOT = -4243
152977 Wp = 37
43551
YDOT = -6393
889543 meter/sec RA = 52
21905 deg
ZDOT = -718
124539 TA = 59
38453
MA = 59
34876
Ha = 186
029 n
mi
Hp = 179
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12270019
07 X = -3786231
01
Y = 6202676
57 feet Y = 1848495
26 meter
Z = 17199482
71 Z = 5224121
43
XDOT = -13921
105568 XDOT = -4167
851658
YDOT = -20977
327897 feet/sec YDOT = -6440
917901 meter/sec
ZDOT = -2356
051636 ZDOT = -738
554457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10578557
56 X = -3224344
34
Y = -8917474
26 feet Y = -2718046
15 meter
Z = 17129551
75 Z = 5221087
37
XDOT = 13139
180682 XDOT = 4004
822272
YDOT = -20283
711165 feet/sec YDOT = -6182
475163 meter/sec
ZDOT = -2435
096524 ZDOT = -742
217421
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 08092
33513074
00020000 00000-0 20000-3 0 9105
2 25544 51
6391 52
5750 0001484 339
9379 20
1727 15
76656470 16408
Satellite: ISS
Catalog Number: 25544
Epoch time: 08092
33513074 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 52
5750 deg
Eccentricity:
0001484
Arg of perigee: 339
9379 deg
Mean anomaly: 20
1727 deg
Mean motion: 15
76656470 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1640
Checksum: 285
Coasting Arc #12 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2008/093/06:55:53
577
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3522702
46 A = 6723654
77 meter
Y = 5518014
57 meter E =
0014654
Z = 1498987
62 I = 51
89417
XDOT = -4833
662914 Wp = 55
70648
YDOT = 1497
531762 meter/sec RA = 47
10084 deg
ZDOT = 5814
746287 TA = 320
77166
MA = 320
87777
Ha = 186
018 n
mi
Hp = 179
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11557422
76 X = 3453455
59
Y = 18103722
35 feet Y = 5557020
35 meter
Z = 4917938
39 Z = 1515932
26
XDOT = -15858
474128 XDOT = -4878
296078
YDOT = 4913
161948 feet/sec YDOT = 1443
229766 meter/sec
ZDOT = 19077
251599 ZDOT = 5791
156029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11780227
96 X = -3590613
48
Y = 17941450
57 feet Y = 5468554
13 meter
Z = 4983521
07 Z = 1518977
22
XDOT = -9722
573534 XDOT = -2963
440413
YDOT = -11686
436683 feet/sec YDOT = -3562
025901 meter/sec
ZDOT = 18986
911097 ZDOT = 5787
210502
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 08093
34924992
00020000 00000-0 20000-3 0 9113
2 25544 51
6393 47
3459 0001624 349
4493 10
6637 15
76648743 16562
Satellite: ISS
Catalog Number: 25544
Epoch time: 08093
34924992 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 47
3459 deg
Eccentricity:
0001624
Arg of perigee: 349
4493 deg
Mean anomaly: 10
6637 deg
Mean motion: 15
76648743 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1656
Checksum: 317
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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