Date:
September 28th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6081 61 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 930)
---------------------------------------
Vector Time (GMT): 2006/270/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4235070
34 A = 6721499
84 meter
Y = -4167935
10 meter E =
0014517
Z = -3162237
23 I = 51
74811
XDOT = 5617
014305 Wp = 48
10187
YDOT = -2038
889007 meter/sec RA = 19
73495 deg
ZDOT = -4840
026758 TA = 168
64222
MA = 168
60943
Ha = 190
551 n
mi
Hp = 177
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13894587
74 X = -4172787
30
Y = -13674327
77 feet Y = -4214945
83 meter
Z = -10374794
06 Z = -3182660
21
XDOT = 18428
524623 XDOT = 5662
908383
YDOT = -6689
268395 feet/sec YDOT = -1975
819936 meter/sec
ZDOT = -15879
352879 ZDOT = -4812
627279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17743130
33 X = 5408106
13
Y = 7976987
11 feet Y = 2431385
67 meter
Z = -10451419
18 Z = -3185592
57
XDOT = -14429
484544 XDOT = -4398
106889
YDOT = 11443
654656 feet/sec YDOT = 3488
025939 meter/sec
ZDOT = -15777
556007 ZDOT = -4808
999071
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 06270
56687201
00020000 00000-0 20000-3 0 9009
2 25544 51
6371 20
0715 0012201 31
5505 328
6389 15
76203053 9319
Satellite: ISS
Catalog Number: 25544
Epoch time: 06270
56687201 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 20
0715 deg
Eccentricity:
0012201
Arg of perigee: 31
5505 deg
Mean anomaly: 328
6389 deg
Mean motion: 15
76203053 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 931
Checksum: 250
Coasting Arc #2 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2006/271/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5344574
31 A = 6719888
07 meter
Y = 1646824
77 meter E =
0022041
Z = 3719304
76 I = 51
71545
XDOT = -4425
991519 Wp = 58
71710
YDOT = -4635
847561 meter/sec RA = 14
53800 deg
ZDOT = -4277
624806 TA = 76
41410
MA = 76
16870
Ha = 190
714 n
mi
Hp = 177
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17534692
63 X = -5380660
12
Y = 5402968
40 feet Y = 1586857
02 meter
Z = 12202443
45 Z = 3693252
74
XDOT = -14520
969549 XDOT = -4353
043615
YDOT = -15209
473626 feet/sec YDOT = -4684
933588 meter/sec
ZDOT = -14034
202119 ZDOT = -4298
949415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14409133
92 X = 4391904
02
Y = -11462468
86 feet Y = -3493760
51 meter
Z = 12105610
54 Z = 3689790
09
XDOT = 18167
191939 XDOT = 5537
360103
YDOT = 7827
202847 feet/sec YDOT = 2385
731428 meter/sec
ZDOT = -14114
245412 ZDOT = -4302
022002
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 06271
58127367
00020000 00000-0 20000-3 0 9015
2 25544 51
6370 14
8446 0012403 35
3920 324
8065 15
76236964 9470
Satellite: ISS
Catalog Number: 25544
Epoch time: 06271
58127367 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 14
8446 deg
Eccentricity:
0012403
Arg of perigee: 35
3920 deg
Mean anomaly: 324
8065 deg
Mean motion: 15
76236964 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 947
Checksum: 287
Coasting Arc #3 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2006/272/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3415920
99 A = 6717837
61 meter
Y = 3943234
51 meter E =
0018506
Z = 4213151
52 I = 51
68153
XDOT = -6567
680101 Wp = 68
39135
YDOT = 1811
145642 meter/sec RA = 9
44031 deg
ZDOT = 3623
858151 TA = 344
81427
MA = 344
86975
Ha = 190
558 n
mi
Hp = 176
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11207089
87 X = 3351106
33
Y = 12937121
10 feet Y = 3981070
80 meter
Z = 13822675
60 Z = 4229588
87
XDOT = -21547
506894 XDOT = -6605
048725
YDOT = 5942
078878 feet/sec YDOT = 1737
493239 meter/sec
ZDOT = 11889
298397 ZDOT = 3591
861207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15223958
68 X = -4640262
60
Y = -7712860
26 feet Y = -2350879
81 meter
Z = 13884422
76 Z = 4231972
06
XDOT = 17149
492161 XDOT = 5227
165211
YDOT = -12626
872905 feet/sec YDOT = -3848
670862 meter/sec
ZDOT = 11770
335664 ZDOT = 3587
598310
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 06272
59565438
00020000 00000-0 20000-3 0 9023
2 25544 51
6371 9
6172 0012338 38
8220 321
3828 15
76287691 9637
Satellite: ISS
Catalog Number: 25544
Epoch time: 06272
59565438 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 9
6172 deg
Eccentricity:
0012338
Arg of perigee: 38
8220 deg
Mean anomaly: 321
3828 deg
Mean motion: 15
76287691 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 963
Checksum: 302
Coasting Arc #4 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2006/273/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6034250
77 A = 6723019
34 meter
Y = -1548301
97 meter E =
0017784
Z = -2517842
32 I = 51
67001
XDOT = 3347
718983 Wp = 43
42268
YDOT = 4461
514115 meter/sec RA = 4
24397 deg
ZDOT = 5314
347802 TA = 288
04323
MA = 288
23692
Ha = 190
790 n
mi
Hp = 176
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19797410
67 X = 6063346
94
Y = -5079730
87 feet Y = -1480660
93 meter
Z = -8260637
53 Z = -2488457
03
XDOT = 10983
329998 XDOT = 3271
764553
YDOT = 14637
513501 feet/sec YDOT = 4498
525427 meter/sec
ZDOT = 17435
524285 ZDOT = 5330
426704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16191223
41 X = -4935084
89
Y = 12545070
86 feet Y = 3823737
60 meter
Z = -8151364
87 Z = -2484536
01
XDOT = -14891
499125 XDOT = -4538
928933
YDOT = -7926
375709 feet/sec YDOT = -2415
959316 meter/sec
ZDOT = 17496
005555 ZDOT = 5332
782493
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 06273
54662066
00020000 00000-0 20000-3 0 9035
2 25544 51
6366 4
7176 0012475 41
6205 318
5906 15
76271480 9788
Satellite: ISS
Catalog Number: 25544
Epoch time: 06273
54662066 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 4
7176 deg
Eccentricity:
0012475
Arg of perigee: 41
6205 deg
Mean anomaly: 318
5906 deg
Mean motion: 15
76271480 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 978
Checksum: 295
Coasting Arc #5 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2006/274/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2340367
56 A = 6714888
74 meter
Y = -3897371
57 meter E =
0024615
Z = -4964051
04 I = 51
61392
XDOT = 7206
956860 Wp = 60
26265
YDOT = -1725
044411 meter/sec RA = 359
12905 deg
ZDOT = -2039
014984 TA = 189
93053
MA = 189
97926
Ha = 190
755 n
mi
Hp = 176
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7678371
27 X = -2272498
11
Y = -12786652
15 feet Y = -3923163
38 meter
Z = -16286256
70 Z = -4975255
74
XDOT = 23644
871587 XDOT = 7235
616116
YDOT = -5659
594524 feet/sec YDOT = -1644
291985 meter/sec
ZDOT = -6689
681705 ZDOT = -2003
933829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12192088
31 X = 3716148
52
Y = 8510628
15 feet Y = 2594039
46 meter
Z = -16328509
01 Z = -4976929
55
XDOT = -18608
931671 XDOT = -5672
002373
YDOT = 14046
283848 feet/sec YDOT = 4281
307317 meter/sec
ZDOT = -6559
207385 ZDOT = -1999
246411
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 06274
56096531
00020000 00000-0 20000-3 0 9047
2 25544 51
6360 359
4898 0012488 45
7533 314
4654 15
76302069 9947
Satellite: ISS
Catalog Number: 25544
Epoch time: 06274
56096531 = yrday
fracday
Element set: 904
Inclination: 51
6360 deg
RA of node: 359
4898 deg
Eccentricity:
0012488
Arg of perigee: 45
7533 deg
Mean anomaly: 314
4654 deg
Mean motion: 15
76302069 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 994
Checksum: 316
Coasting Arc #6 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2006/275/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6481972
44 A = 6725042
96 meter
Y = 1479777
29 meter E =
0020931
Z = 995077
40 I = 51
62064
XDOT = -1956
433676 Wp = 88
21395
YDOT = -4512
497871 meter/sec RA = 353
94779 deg
ZDOT = -5926
261310 TA = 80
90239
MA = 80
66562
Ha = 190
806 n
mi
Hp = 176
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21266313
78 X = -6502871
67
Y = 4854912
36 feet Y = 1407175
45 meter
Z = 3264689
64 Z = 963537
14
XDOT = -6418
745655 XDOT = -1877
040146
YDOT = -14804
783040 feet/sec YDOT = -4533
931998 meter/sec
ZDOT = -19443
114533 ZDOT = -5935
572744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17148669
57 X = 5226914
49
Y = -13509317
15 feet Y = -4117639
87 meter
Z = 3147372
90 Z = 959319
26
XDOT = 11062
818826 XDOT = 3371
947178
YDOT = 9419
827949 feet/sec YDOT = 2871
163559 meter/sec
ZDOT = -19478
397693 ZDOT = -5937
015617
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 06275
57528997
00020000 00000-0 20000-3 0 9056
2 25544 51
6363 354
2619 0012745 49
3870 310
8400 15
76369842 10105
Satellite: ISS
Catalog Number: 25544
Epoch time: 06275
57528997 = yrday
fracday
Element set: 905
Inclination: 51
6363 deg
RA of node: 354
2619 deg
Eccentricity:
0012745
Arg of perigee: 49
3870 deg
Mean anomaly: 310
8400 deg
Mean motion: 15
76369842 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1010
Checksum: 303
Coasting Arc #7 (Orbit 1025)
---------------------------------------
Vector Time (GMT): 2006/276/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1068341
97 A = 6713246
91 meter
Y = 4035018
07 meter E =
0014393
Z = 5246974
40 I = 51
55328
XDOT = -7524
958560 Wp = 59
46024
YDOT = 1685
896977 meter/sec RA = 348
80191 deg
ZDOT = 242
393882 TA = 28
27976
MA = 28
20169
Ha = 190
738 n
mi
Hp = 176
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3505058
95 X = 997653
56
Y = 13238248
25 feet Y = 4046569
87 meter
Z = 17214482
95 Z = 5251992
52
XDOT = -24688
184251 XDOT = -7544
428729
YDOT = 5531
158061 feet/sec YDOT = 1601
639869 meter/sec
ZDOT = 795
255518 ZDOT = 205
790234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8934459
76 X = -2723223
34
Y = -10346481
45 feet Y = -3153607
54 meter
Z = 17233711
98 Z = 5252835
41
XDOT = 18912
581959 XDOT = 5764
554981
YDOT = -15270
327584 feet/sec YDOT = -4654
395848 meter/sec
ZDOT = 659
100973 ZDOT = 200
893977
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 06276
58959424
00020000 00000-0 20000-3 0 9062
2 25544 51
6363 349
0343 0012626 52
9791 307
2527 15
76407584 10264
Satellite: ISS
Catalog Number: 25544
Epoch time: 06276
58959424 = yrday
fracday
Element set: 906
Inclination: 51
6363 deg
RA of node: 349
0343 deg
Eccentricity:
0012626
Arg of perigee: 52
9791 deg
Mean anomaly: 307
2527 deg
Mean motion: 15
76407584 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1026
Checksum: 308
Coasting Arc #8 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2006/277/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6531868
61 A = 6725301
13 meter
Y = -1437410
18 meter E =
0026307
Z = 579490
61 I = 51
56542
XDOT = 511
711320 Wp = 53
35132
YDOT = 4814
719017 meter/sec RA = 343
64655 deg
ZDOT = 6003
236278 TA = 312
97546
MA = 313
19573
Ha = 190
982 n
mi
Hp = 175
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21430015
13 X = 6544641
40
Y = -4715912
66 feet Y = -1364295
74 meter
Z = 1901215
92 Z = 611253
66
XDOT = 1678
842915 XDOT = 428
671704
YDOT = 15796
322234 feet/sec YDOT = 4819
977409 meter/sec
ZDOT = 19695
657080 ZDOT = 6005
520114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16857754
33 X = -5138243
52
Y = 14029906
79 feet Y = 4276315
59 meter
Z = 2019365
59 Z = 615502
63
XDOT = -7629
164550 XDOT = -2325
369355
YDOT = -12079
377430 feet/sec YDOT = -3681
794241 meter/sec
ZDOT = 19704
806248 ZDOT = 6006
024944
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 06277
60388314
00020000 00000-0 20000-3 0 9071
2 25544 51
6359 343
8066 0013013 56
3161 303
9242 15
76367275 10420
Satellite: ISS
Catalog Number: 25544
Epoch time: 06277
60388314 = yrday
fracday
Element set: 907
Inclination: 51
6359 deg
RA of node: 343
8066 deg
Eccentricity:
0013013
Arg of perigee: 56
3161 deg
Mean anomaly: 303
9242 deg
Mean motion: 15
76367275 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1042
Checksum: 283
Coasting Arc #9 (Orbit 1056)
---------------------------------------
Vector Time (GMT): 2006/278/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 180454
96 A = 6714108
92 meter
Y = -4412714
54 meter E =
0024761
Z = -5077281
80 I = 51
50143
XDOT = 7360
485736 Wp = 81
44780
YDOT = -1532
884585 meter/sec RA = 338
46519 deg
ZDOT = 1604
116152 TA = 203
95761
MA = 204
07302
Ha = 190
904 n
mi
Hp = 175
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 592043
82 X = 254449
86
Y = -14477409
92 feet Y = -4410283
35 meter
Z = -16657748
68 Z = -5076224
99
XDOT = 24148
575248 XDOT = 7369
287043
YDOT = -5029
148900 feet/sec YDOT = -1450
526191 meter/sec
ZDOT = 5262
848268 ZDOT = 1639
895209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6269885
79 X = 1911061
19
Y = 13066979
56 feet Y = 3982815
37 meter
Z = -16654401
29 Z = -5076261
51
XDOT = -17888
786021 XDOT = -5452
501979
YDOT = 15417
924345 feet/sec YDOT = 4699
383340 meter/sec
ZDOT = 5395
942747 ZDOT = 1644
683349
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 06278
55475658
00020000 00000-0 20000-3 0 9085
2 25544 51
6361 338
9052 0012903 60
0085 300
2358 15
76420203 10572
Satellite: ISS
Catalog Number: 25544
Epoch time: 06278
55475658 = yrday
fracday
Element set: 908
Inclination: 51
6361 deg
RA of node: 338
9052 deg
Eccentricity:
0012903
Arg of perigee: 60
0085 deg
Mean anomaly: 300
2358 deg
Mean motion: 15
76420203 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1057
Checksum: 279
Coasting Arc #10 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2006/279/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6246316
70 A = 6722909
41 meter
Y = 1170352
02 meter E =
0015922
Z = -2209817
29 I = 51
50634
XDOT = 924
580625 Wp = 84
73996
YDOT = -5331
601959 meter/sec RA = 333
33435 deg
ZDOT = -5469
439264 TA = 120
07154
MA = 119
91355
Ha = 190
891 n
mi
Hp = 175
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20493165
02 X = -6248204
44
Y = 3839737
59 feet Y = 1100491
47 meter
Z = -7250056
72 Z = -2240167
05
XDOT = 3033
401002 XDOT = 1010
700575
YDOT = -17492
132411 feet/sec YDOT = -5320
781791 meter/sec
ZDOT = -17944
354540 ZDOT = -5464
737882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15951719
30 X = 4862084
04
Y = -13364358
60 feet Y = -4073456
50 meter
Z = -7362967
51 Z = -2244232
50
XDOT = 4860
896180 XDOT = 1481
601156
YDOT = 15621
493641 feet/sec YDOT = 4761
431262 meter/sec
ZDOT = -17927
553506 ZDOT = -5464
318309
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 06279
56900423
00020000 00000-0 20000-3 0 9091
2 25544 51
6363 333
6766 0013075 64
0762 296
1748 15
76486243 10735
Satellite: ISS
Catalog Number: 25544
Epoch time: 06279
56900423 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node: 333
6766 deg
Eccentricity:
0013075
Arg of perigee: 64
0762 deg
Mean anomaly: 296
1748 deg
Mean motion: 15
76486243 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1073
Checksum: 308
Coasting Arc #11 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2006/280/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1360324
95 A = 6716739
35 meter
Y = 4924177
57 meter E =
0022611
Z = 4347579
96 I = 51
45962
XDOT = -6851
188246 Wp = 68
31685
YDOT = 1100
832662 meter/sec RA = 328
12422 deg
ZDOT = -3368
305768 TA = 55
72830
MA = 55
51438
Ha = 190
890 n
mi
Hp = 175
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4463008
38 X = -1436406
90
Y = 16155438
23 feet Y = 4908540
61 meter
Z = 14263713
78 Z = 4340786
16
XDOT = -22477
651727 XDOT = -6846
625736
YDOT = 3611
655716 feet/sec YDOT = 1024
244121 meter/sec
ZDOT = -11050
871941 ZDOT = -3401
578560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4232086
52 X = -1289939
97
Y = -16239110
37 feet Y = -4949680
84 meter
Z = 14239062
36 Z = 4340066
21
XDOT = 16345
492463 XDOT = 4982
106103
YDOT = -14122
191703 feet/sec YDOT = -4304
444031 meter/sec
ZDOT = -11174
678005 ZDOT = -3406
041856
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 06280
58323131
00020000 00000-0 20000-3 0 9102
2 25544 51
6350 328
4483 0013071 67
4790 292
7757 15
76534722 10898
Satellite: ISS
Catalog Number: 25544
Epoch time: 06280
58323131 = yrday
fracday
Element set: 910
Inclination: 51
6350 deg
RA of node: 328
4483 deg
Eccentricity:
0013071
Arg of perigee: 67
4790 deg
Mean anomaly: 292
7757 deg
Mean motion: 15
76534722 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1089
Checksum: 292
Coasting Arc #12 (Orbit 1104)
---------------------------------------
Vector Time (GMT): 2006/281/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5631978
83 A = 6719322
42 meter
Y = -672378
06 meter E =
0024810
Z = 3578217
13 I = 51
44452
XDOT = -2099
548647 Wp = 81
93197
YDOT = 5977
918609 meter/sec RA = 323
00609 deg
ZDOT = 4405
419188 TA = 321
09125
MA = 321
26955
Ha = 190
899 n
mi
Hp = 175
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18477620
84 X = 5621696
10
Y = -2205964
75 feet Y = -609455
46 meter
Z = 11739557
52 Z = 3605553
03
XDOT = -6888
282962 XDOT = -2187
639790
YDOT = 19612
593862 feet/sec YDOT = 5953
947968 meter/sec
ZDOT = 14453
475027 ZDOT = 4395
005049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14587756
46 X = -4446348
17
Y = 11449317
42 feet Y = 3489751
95 meter
Z = 11841302
95 Z = 3609229
14
XDOT = -3398
394820 XDOT = -1035
830741
YDOT = -19314
628971 feet/sec YDOT = -5887
098910 meter/sec
ZDOT = 14415
473751 ZDOT = 4393
836399
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 06281
59744112
00020000 00000-0 20000-3 0 9111
2 25544 51
6345 323
2194 0013299 71
5600 288
7009 15
76520869 11053
Satellite: ISS
Catalog Number: 25544
Epoch time: 06281
59744112 = yrday
fracday
Element set: 911
Inclination: 51
6345 deg
RA of node: 323
2194 deg
Eccentricity:
0013299
Arg of perigee: 71
5600 deg
Mean anomaly: 288
7009 deg
Mean motion: 15
76520869 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1105
Checksum: 286
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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