Date:
December 9th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16522 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 ET - UTC (sec) : 66 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 1090)
---------------------------------------
Vector Time (GMT): 2010/342/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -454199
70 A = 6729657
07 meter
Y = -5746824
72 meter E =
0006694
Z = -3478790
60 I = 51
93690
XDOT = 5739
379400 Wp =
35200
YDOT = 2315
602840 meter/sec RA = 57
28138 deg
ZDOT = -4568
134930 TA = 220
66107
MA = 220
71108
Ha = 191
884 n
mi
Hp = 186
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1490156
51 X = -373004
52
Y = -18854411
80 feet Y = -5751449
41 meter
Z = -11413355
00 Z = -3480800
64
XDOT = 18829
984908 XDOT = 5735
250539
YDOT = 7597
122178 feet/sec YDOT = 2379
761551 meter/sec
ZDOT = -14987
319324 ZDOT = -4540
262697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16748182
28 X = 5104845
96
Y = -8776514
88 feet Y = -2675081
74 meter
Z = -11421263
50 Z = -3481201
11
XDOT = -118
698302 XDOT = -36
179242
YDOT = 19159
056618 feet/sec YDOT = 5839
680457 meter/sec
ZDOT = -14875
274315 ZDOT = -4533
983611
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 10342
62695186
00016717 00000-0 10270-3 0 9000
2 25544 51
6462 57
7668 0008076 321
6339 38
4249 15
73038535 10914
Satellite: ISS
Catalog Number: 25544
Epoch time: 10342
62695186 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 57
7668 deg
Eccentricity:
0008076
Arg of perigee: 321
6339 deg
Mean anomaly: 38
4249 deg
Mean motion: 15
73038535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 318
Coasting Arc #2 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2010/343/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5123205
98 A = 6727264
86 meter
Y = -1253283
40 meter E =
0010887
Z = 4177616
12 I = 51
91073
XDOT = -1431
108136 Wp = 29
48757
YDOT = -6585
325325 meter/sec RA = 52
12271 deg
ZDOT = -3717
278824 TA = 98
43017
MA = 98
30675
Ha = 192
033 n
mi
Hp = 186
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16808418
58 X = -5129104
86
Y = -4111822
19 feet Y = -1310607
64 meter
Z = 13706089
62 Z = 4152713
12
XDOT = -4695
236667 XDOT = -1339
305578
YDOT = -21605
398047 feet/sec YDOT = -6600
815115 meter/sec
ZDOT = -12195
796666 ZDOT = -3724
008911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3211632
43 X = -978905
56
Y = -17083628
73 feet Y = -5207090
04 meter
Z = 13605952
96 Z = 4147094
46
XDOT = 16537
302648 XDOT = 5040
569847
YDOT = -12878
592021 feet/sec YDOT = -3925
394848 meter/sec
ZDOT = -12222
662508 ZDOT = -3725
467532
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 10343
64339650
00016717 00000-0 10270-3 0 9015
2 25544 51
6451 52
5548 0008201 325
9241 34
1394 15
73103412 11070
Satellite: ISS
Catalog Number: 25544
Epoch time: 10343
64339650 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 52
5548 deg
Eccentricity:
0008201
Arg of perigee: 325
9241 deg
Mean anomaly: 34
1394 deg
Mean motion: 15
73103412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 269
Coasting Arc #3 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2010/344/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2031467
13 A = 6730749
02 meter
Y = 5654164
98 meter E =
0012591
Z = 3015800
65 I = 51
90278
XDOT = -5852
128747 Wp = 46
85240
YDOT = -556
536780 meter/sec RA = 47
06181 deg
ZDOT = 4980
934614 TA = 347
90185
MA = 347
93207
Ha = 192
204 n
mi
Hp = 185
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6664918
42 X = 1953440
02
Y = 18550410
02 feet Y = 5676445
50 meter
Z = 9894359
08 Z = 3025480
52
XDOT = -19199
897463 XDOT = -5869
666957
YDOT = -1825
908071 feet/sec YDOT = -622
077342 meter/sec
ZDOT = 16341
648995 ZDOT = 4952
462344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13945114
61 X = -4250470
93
Y = 13903385
83 feet Y = 4237752
00 meter
Z = 9933117
94 Z = 3027614
35
XDOT = -5586
904428 XDOT = -1702
888470
YDOT = -17207
533473 feet/sec YDOT = -5244
856202 meter/sec
ZDOT = 16227
130795 ZDOT = 4946
029466
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 10344
65981300
00016717 00000-0 10270-3 0 9023
2 25544 51
6449 47
3419 0008159 331
6679 28
4039 15
73101951 11233
Satellite: ISS
Catalog Number: 25544
Epoch time: 10344
65981300 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 47
3419 deg
Eccentricity:
0008159
Arg of perigee: 331
6679 deg
Mean anomaly: 28
4039 deg
Mean motion: 15
73101951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 300
Coasting Arc #4 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2010/345/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4995989
11 A = 6725906
08 meter
Y = -261318
34 meter E =
0006843
Z = -4498034
17 I = 51
86635
XDOT = 3193
412921 Wp = 53
32163
YDOT = 6232
647082 meter/sec RA = 41
90308 deg
ZDOT = 3192
176718 TA = 248
46556
MA = 248
53852
Ha = 192
361 n
mi
Hp = 185
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16391040
40 X = 5020390
55
Y = -857343
64 feet Y = -205313
39 meter
Z = -14757329
94 Z = -4473704
40
XDOT = 10477
076511 XDOT = 3107
973935
YDOT = 20448
317198 feet/sec YDOT = 6267
879781 meter/sec
ZDOT = 10473
020727 ZDOT = 3207
483280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8070085
82 X = 2459762
16
Y = 14392855
12 feet Y = 4386942
24 meter
Z = -14659449
75 Z = -4468200
28
XDOT = -12668
388993 XDOT = -3861
324965
YDOT = 17808
038006 feet/sec YDOT = 5427
889984 meter/sec
ZDOT = 10534
392479 ZDOT = 3210
882828
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 10345
61267269
00016717 00000-0 10270-3 0 9032
2 25544 51
6461 42
4555 0008274 334
4904 25
5849 15
73155198 11389
Satellite: ISS
Catalog Number: 25544
Epoch time: 10345
61267269 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 42
4555 deg
Eccentricity:
0008274
Arg of perigee: 334
4904 deg
Mean anomaly: 25
5849 deg
Mean motion: 15
73155198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 315
Coasting Arc #5 (Orbit 1153)
---------------------------------------
Vector Time (GMT): 2010/346/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3490958
94 A = 6731483
49 meter
Y = -5147836
59 meter E =
0004688
Z = -2581961
56 I = 51
86153
XDOT = 5487
854699 Wp = 12
32338
YDOT = -1071
006425 meter/sec RA = 36
83460 deg
ZDOT = -5281
824085 TA = 196
85003
MA = 196
86561
Ha = 192
316 n
mi
Hp = 185
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11453277
36 X = -3420592
68
Y = -16889227
65 feet Y = -5186480
98 meter
Z = -8471002
48 Z = -2598750
11
XDOT = 18004
772634 XDOT = 5525
081228
YDOT = -3513
800607 feet/sec YDOT = -1009
429427 meter/sec
ZDOT = -17328
819175 ZDOT = -5255
073670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9783325
23 X = 2981957
53
Y = -17876361
25 feet Y = -5448714
91 meter
Z = -8538367
06 Z = -2602494
28
XDOT = 10120
653516 XDOT = 3084
775192
YDOT = 13768
471681 feet/sec YDOT = 4196
630169 meter/sec
ZDOT = -17221
176070 ZDOT = -5249
014466
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 10346
62902786
00016717 00000-0 10270-3 0 9045
2 25544 51
6452 37
2423 0008209 338
6873 21
3947 15
73210116 11547
Satellite: ISS
Catalog Number: 25544
Epoch time: 10346
62902786 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 37
2423 deg
Eccentricity:
0008209
Arg of perigee: 338
6873 deg
Mean anomaly: 21
3947 deg
Mean motion: 15
73210116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1154
Checksum: 296
Coasting Arc #6 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2010/347/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4525995
63 A = 6724664
04 meter
Y = 1570103
82 meter E =
0012412
Z = 4720439
40 I = 51
81317
XDOT = -4731
582988 Wp = 20
90151
YDOT = -5430
512854 meter/sec RA = 31
67575 deg
ZDOT = -2716
849278 TA = 95
84996
MA = 95
70846
Ha = 192
466 n
mi
Hp = 185
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14849067
02 X = -4566147
60
Y = 5151259
26 feet Y = 1519266
61 meter
Z = 15487005
91 Z = 4698354
57
XDOT = -15523
566235 XDOT = -4657
308282
YDOT = -17816
643223 feet/sec YDOT = -5483
008800 meter/sec
ZDOT = -8913
547499 ZDOT = -2739
655361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11613911
35 X = -3539920
18
Y = -10718802
09 feet Y = -3267090
88 meter
Z = 15398115
48 Z = 4693345
60
XDOT = 7583
031083 XDOT = 2311
307874
YDOT = -21216
776744 feet/sec YDOT = -6466
873552 meter/sec
ZDOT = -9005
102990 ZDOT = -2744
755391
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 10347
64535204
00016717 00000-0 10270-3 0 9056
2 25544 51
6445 32
0290 0008302 343
0846 17
0039 15
73277683 11702
Satellite: ISS
Catalog Number: 25544
Epoch time: 10347
64535204 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 32
0290 deg
Eccentricity:
0008302
Arg of perigee: 343
0846 deg
Mean anomaly: 17
0039 deg
Mean motion: 15
73277683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 282
Coasting Arc #7 (Orbit 1185)
---------------------------------------
Vector Time (GMT): 2010/348/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4717782
35 A = 6732016
28 meter
Y = 4268550
75 meter E =
0016979
Z = 2166854
27 I = 51
81201
XDOT = -4775
256610 Wp = 41
57804
YDOT = 2467
773542 meter/sec RA = 26
59909 deg
ZDOT = 5523
491613 TA = 342
63807
MA = 342
69605
Ha = 192
417 n
mi
Hp = 184
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15478288
56 X = 4659173
71
Y = 14004431
58 feet Y = 4320979
99 meter
Z = 7109101
92 Z = 2189631
37
XDOT = -15666
852395 XDOT = -4829
329154
YDOT = 8096
369890 feet/sec YDOT = 2414
071051 meter/sec
ZDOT = 18121
691645 ZDOT = 5500
162037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4674763
98 X = -1424868
06
Y = 20311060
33 feet Y = 6190811
19 meter
Z = 7200573
64 Z = 2194734
84
XDOT = -13292
328291 XDOT = -4051
501663
YDOT = -9464
340622 feet/sec YDOT = -2884
731022 meter/sec
ZDOT = 18027
764368 ZDOT = 5494
862579
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 10348
66164613
00016717 00000-0 10270-3 0 9062
2 25544 51
6445 26
8164 0008319 346
8093 13
2851 15
73322580 11860
Satellite: ISS
Catalog Number: 25544
Epoch time: 10348
66164613 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 26
8164 deg
Eccentricity:
0008319
Arg of perigee: 346
8093 deg
Mean anomaly: 13
2851 deg
Mean motion: 15
73322580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1186
Checksum: 306
Coasting Arc #8 (Orbit 1200)
---------------------------------------
Vector Time (GMT): 2010/349/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3753018
88 A = 6723743
93 meter
Y = -2676850
27 meter E =
0011458
Z = -4901908
05 I = 51
75607
XDOT = 5987
969717 Wp = 64
96920
YDOT = 4267
765586 meter/sec RA = 21
44155 deg
ZDOT = 2262
831337 TA = 226
97592
MA = 227
07196
Ha = 192
653 n
mi
Hp = 184
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12313054
07 X = 3806485
83
Y = -8782317
16 feet Y = -2634582
44 meter
Z = -16082375
50 Z = -4883546
01
XDOT = 19645
569939 XDOT = 5928
809173
YDOT = 14001
855598 feet/sec YDOT = 4334
395718 meter/sec
ZDOT = 7423
987326 ZDOT = 2291
777835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13837228
93 X = 4217587
38
Y = 6296405
23 feet Y = 1919144
31 meter
Z = -16008421
96 Z = -4879367
01
XDOT = -1765
488347 XDOT = -538
120848
YDOT = 22976
622324 feet/sec YDOT = 7003
274484 meter/sec
ZDOT = 7540
267400 ZDOT = 2298
273504
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 10349
61439472
00016717 00000-0 10270-3 0 9077
2 25544 51
6444 21
9289 0008423 350
7122 9
3884 15
73331009 12012
Satellite: ISS
Catalog Number: 25544
Epoch time: 10349
61439472 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 21
9289 deg
Eccentricity:
0008423
Arg of perigee: 350
7122 deg
Mean anomaly: 9
3884 deg
Mean motion: 15
73331009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1201
Checksum: 293
Coasting Arc #9 (Orbit 1216)
---------------------------------------
Vector Time (GMT): 2010/350/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5667218
47 A = 6732397
58 meter
Y = -3154039
44 meter E =
0004704
Z = -1815306
11 I = 51
75661
XDOT = 3790
279071 Wp = 53
74702
YDOT = -3548
735407 meter/sec RA = 16
35373 deg
ZDOT = -5674
528522 TA = 146
32390
MA = 146
29400
Ha = 192
655 n
mi
Hp = 184
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18593236
44 X = -5622709
66
Y = -10347898
43 feet Y = -3217164
67 meter
Z = -5955728
70 Z = -1842729
98
XDOT = 12435
298791 XDOT = 3857
246184
YDOT = -11642
832700 feet/sec YDOT = -3505
975288 meter/sec
ZDOT = -18617
219562 ZDOT = -5655
952753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -771879
96 X = -235269
01
Y = -21233628
67 feet Y = -6472010
02 meter
Z = -6065918
09 Z = -1848891
83
XDOT = 14912
480277 XDOT = 4545
323988
YDOT = 4748
145639 feet/sec YDOT = 1447
234791 meter/sec
ZDOT = -18542
372762 ZDOT = -5651
715218
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 10350
63063011
00016717 00000-0 10270-3 0 9084
2 25544 51
6437 16
7147 0008447 355
4318 4
6766 15
73398872 12179
Satellite: ISS
Catalog Number: 25544
Epoch time: 10350
63063011 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 16
7147 deg
Eccentricity:
0008447
Arg of perigee: 355
4318 deg
Mean anomaly: 4
6766 deg
Mean motion: 15
73398872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1217
Checksum: 307
Coasting Arc #10 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2010/351/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2838761
15 A = 6722909
68 meter
Y = 3471121
82 meter E =
0012595
Z = 5008579
97 I = 51
69485
XDOT = -6884
910451 Wp = 20
43664
YDOT = -2884
697936 meter/sec RA = 11
19646 deg
ZDOT = -1890
022305 TA = 87
86238
MA = 87
71816
Ha = 192
759 n
mi
Hp = 183
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9313520
82 X = -2901696
00
Y = 11388194
94 feet Y = 3439024
65 meter
Z = 16432348
99 Z = 4994636
59
XDOT = -22588
288882 XDOT = -6842
960002
YDOT = -9464
232075 feet/sec YDOT = -2961
454386 meter/sec
ZDOT = -6200
860581 ZDOT = -1923
368074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14652606
50 X = -4466114
46
Y = -1891585
95 feet Y = -576555
40 meter
Z = 16376134
25 Z = 4991445
72
XDOT = -4151
389964 XDOT = -1265
343661
YDOT = -23056
496175 feet/sec YDOT = -7027
620034 meter/sec
ZDOT = -6334
874421 ZDOT = -1930
869724
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 10351
64683409
00016717 00000-0 10270-3 0 9096
2 25544 51
6433 11
5007 0008515 358
3854 1
7280 15
73449100 12334
Satellite: ISS
Catalog Number: 25544
Epoch time: 10351
64683409 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 11
5007 deg
Eccentricity:
0008515
Arg of perigee: 358
3854 deg
Mean anomaly: 1
7280 deg
Mean motion: 15
73449100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 284
Coasting Arc #11 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2010/352/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6285300
91 A = 6732482
02 meter
Y = 1854767
75 meter E =
0019624
Z = 1489465
66 I = 51
69794
XDOT = -2657
412188 Wp = 40
24134
YDOT = 4324
225433 meter/sec RA = 6
09972 deg
ZDOT = 5801
538080 TA = 336
16362
MA = 336
25437
Ha = 192
569 n
mi
Hp = 183
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20621065
99 X = 6256857
77
Y = 6085196
02 feet Y = 1924894
53 meter
Z = 4886698
35 Z = 1519931
18
XDOT = -8718
543925 XDOT = -2733
752143
YDOT = 14187
091315 feet/sec YDOT = 4294
081046 meter/sec
ZDOT = 19033
917586 ZDOT = 5788
443351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6182566
41 X = 1884446
24
Y = 20562634
39 feet Y = 6267490
96 meter
Z = 5009164
95 Z = 1526793
48
XDOT = -15208
397449 XDOT = -4635
519542
YDOT = -72
648892 feet/sec YDOT = -22
143382 meter/sec
ZDOT = 18981
078984 ZDOT = 5785
432874
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 10352
66300609
00016717 00000-0 10270-3 0 9109
2 25544 51
6433 6
2872 0008323 2
6373 357
4833 15
73539930 12490
Satellite: ISS
Catalog Number: 25544
Epoch time: 10352
66300609 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 6
2872 deg
Eccentricity:
0008323
Arg of perigee: 2
6373 deg
Mean anomaly: 357
4833 deg
Mean motion: 15
73539930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1249
Checksum: 293
Coasting Arc #12 (Orbit 1263)
---------------------------------------
Vector Time (GMT): 2010/353/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1791617
67 A = 6722301
66 meter
Y = -4009164
86 meter E =
0015457
Z = -5100781
03 I = 51
63275
XDOT = 7410
777101 Wp = 68
10164
YDOT = 1350
089229 meter/sec RA =
94219 deg
ZDOT = 1551
230062 TA = 216
75244
MA = 216
85852
Ha = 192
839 n
mi
Hp = 183
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5878010
74 X = 1861094
63
Y = -13153428
03 feet Y = -3988740
68 meter
Z = -16734845
89 Z = -5091909
12
XDOT = 24313
573165 XDOT = 7387
593700
YDOT = 4429
426604 feet/sec YDOT = 1432
831139 meter/sec
ZDOT = 5089
337474 ZDOT = 1587
175832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14240092
37 X = 4340380
16
Y = -2445790
38 feet Y = -745476
91 meter
Z = -16699000
71 Z = -5089855
42
XDOT = 9800
639232 XDOT = 2987
234838
YDOT = 21538
075345 feet/sec YDOT = 6564
805365 meter/sec
ZDOT = 5233
868199 ZDOT = 1595
283027
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 10353
61564244
00016717 00000-0 10270-3 0 9113
2 25544 51
6432 1
3984 0008578 6
4660 353
6612 15
73520892 12649
Satellite: ISS
Catalog Number: 25544
Epoch time: 10353
61564244 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 1
3984 deg
Eccentricity:
0008578
Arg of perigee: 6
4660 deg
Mean anomaly: 353
6612 deg
Mean motion: 15
73520892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1264
Checksum: 296
Coasting Arc #13 (Orbit 1279)
---------------------------------------
Vector Time (GMT): 2010/354/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6597209
52 A = 6732589
27 meter
Y = -513487
65 meter E =
0007124
Z = -1252460
63 I = 51
63824
XDOT = 1477
861695 Wp = 78
24583
YDOT = -4758
333333 meter/sec RA = 355
83458 deg
ZDOT = -5860
258274 TA = 115
47417
MA = 115
40046
Ha = 192
842 n
mi
Hp = 183
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21644388
18 X = -6584893
03
Y = -1684670
77 feet Y = -587192
55 meter
Z = -4109122
81 Z = -1284480
17
XDOT = 4848
627609 XDOT = 1559
428611
YDOT = -15611
329833 feet/sec YDOT = -4741
349980 meter/sec
ZDOT = -19226
569140 ZDOT = -5852
881436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11075536
27 X = -3375823
45
Y = -18643370
39 feet Y = -5682499
29 meter
Z = -4237898
38 Z = -1291711
43
XDOT = 14261
359675 XDOT = 4346
862429
YDOT = -4127
860387 feet/sec YDOT = -1258
171846 meter/sec
ZDOT = -19196
704510 ZDOT = -5851
155535
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 10354
63175530
00016717 00000-0 10270-3 0 9123
2 25544 51
6436 356
1833 0008674 10
2883 349
8456 15
73597603 12809
Satellite: ISS
Catalog Number: 25544
Epoch time: 10354
63175530 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 356
1833 deg
Eccentricity:
0008674
Arg of perigee: 10
2883 deg
Mean anomaly: 349
8456 deg
Mean motion: 15
73597603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1280
Checksum: 316
Coasting Arc #14 (Orbit 1295)
---------------------------------------
Vector Time (GMT): 2010/355/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -786451
28 A = 6721756
41 meter
Y = 4259600
27 meter E =
0012279
Z = 5137295
49 I = 51
57159
XDOT = -7588
404804 Wp = 26
88895
YDOT = 192
872207 meter/sec RA = 350
67661 deg
ZDOT = -1309
618277 TA = 75
71356
MA = 75
57723
Ha = 192
906 n
mi
Hp = 182
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2580220
73 X = -858980
48
Y = 13975066
49 feet Y = 4250399
34 meter
Z = 16854643
99 Z = 5133299
43
XDOT = -24896
341221 XDOT = -7583
635671
YDOT = 632
782830 feet/sec YDOT = 108
040973 meter/sec
ZDOT = -4296
647892 ZDOT = -1346
471073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12865806
81 X = -3921497
92
Y = 6080988
20 feet Y = 1853485
20 meter
Z = 16838397
91 Z = 5132343
68
XDOT = -14740
186197 XDOT = -4492
808753
YDOT = -18769
423131 feet/sec YDOT = -5720
920170 meter/sec
ZDOT = -4444
899123 ZDOT = -1354
805253
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 10355
64783716
00016717 00000-0 10270-3 0 9137
2 25544 51
6437 350
9687 0008627 14
0177 346
1224 15
73631555 12960
Satellite: ISS
Catalog Number: 25544
Epoch time: 10355
64783716 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 350
9687 deg
Eccentricity:
0008627
Arg of perigee: 14
0177 deg
Mean anomaly: 346
1224 deg
Mean motion: 15
73631555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1296
Checksum: 321
Coasting Arc #15 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2010/356/14:27:32
605
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6585456
61 A = 6732531
56 meter
Y = -844500
05 meter E =
0021148
Z = 1039197
24 I = 51
57893
XDOT = -310
454045 Wp = 41
59409
YDOT = 4928
222776 meter/sec RA = 345
56076 deg
ZDOT = 5919
319390 TA = 329
78948
MA = 329
91126
Ha = 192
799 n
mi
Hp = 182
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21605828
79 X = 6589362
33
Y = -2770669
44 feet Y = -770835
82 meter
Z = 3409439
76 Z = 1071198
53
XDOT = -1018
550018 XDOT = -394
294059
YDOT = 16168
709895 feet/sec YDOT = 4924
281442 meter/sec
ZDOT = 19420
339207 ZDOT = 5917
608298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15241117
62 X = 4645492
65
Y = 15533903
49 feet Y = 4734733
78 meter
Z = 3538206
07 Z = 1078445
21
XDOT = -12441
659509 XDOT = -3792
217818
YDOT = 7747
208626 feet/sec YDOT = 2361
349189 meter/sec
ZDOT = 19413
259840 ZDOT = 5917
161599
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 10356
66388593
00016717 00000-0 10270-3 0 9145
2 25544 51
6439 345
7537 0008545 18
1207 342
0259 15
73701524 13122
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
66388593 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 345
7537 deg
Eccentricity:
0008545
Arg of perigee: 18
1207 deg
Mean anomaly: 342
0259 deg
Mean motion: 15
73701524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 311
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list