[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 9th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 ET - UTC (sec) : 67 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 3562)
---------------------------------------
Vector Time (GMT): 2012/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2514252
47 A = 6797662
67 meter
Y = -5946041
99 meter E =
0025323
Z = 2127544
50 I = 51
31110
XDOT = 3932
217307 Wp = 112
58788
YDOT = 3641
988704 meter/sec RA = 277
61800 deg
ZDOT = 5469
706527 TA = 271
05261
MA = 271
34273
Ha = 232
508 n
mi
Hp = 215
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8248859
81 X = 2570220
25
Y = -19508011
76 feet Y = -5917612
97 meter
Z = 6980132
89 Z = 2139895
07
XDOT = 12900
975417 XDOT = 3864
628731
YDOT = 11948
781837 feet/sec YDOT = 3685
583660 meter/sec
ZDOT = 17945
231387 ZDOT = 5488
644825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2248402
57 X = -685313
10
Y = 21043458
15 feet Y = 6414046
04 meter
Z = 7031786
49 Z = 2143288
52
XDOT = -14152
877412 XDOT = -4313
797035
YDOT = -7602
116338 feet/sec YDOT = -2317
125060 meter/sec
ZDOT = 18023
145627 ZDOT = 5493
454787
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 12282
56019740
00016717 00000-0 10270-3 0 9004
2 25544 51
6450 278
0650 0017748 144
7209 215
5120 15
50603505 35638
Satellite: ISS
Catalog Number: 25544
Epoch time: 12282
56019740 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 278
0650 deg
Eccentricity:
0017748
Arg of perigee: 144
7209 deg
Mean anomaly: 215
5120 deg
Mean motion: 15
50603505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 286
Coasting Arc #2 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2012/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2392403
04 A = 6796618
78 meter
Y = 5775714
88 meter E =
0022364
Z = -2651678
61 I = 51
30385
XDOT = -3973
764184 Wp = 142
73916
YDOT = -4008
247358 meter/sec RA = 272
63737 deg
ZDOT = -5185
744561 TA = 67
28199
MA = 67
04575
Ha = 232
390 n
mi
Hp = 215
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7849091
35 X = -2443929
12
Y = 18949195
81 feet Y = 5748673
24 meter
Z = -8699732
97 Z = -2663426
49
XDOT = -13037
284069 XDOT = -3903
456409
YDOT = -13150
417842 feet/sec YDOT = -4052
291756 meter/sec
ZDOT = -17013
597641 ZDOT = -5204
877993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1665167
40 X = 507543
02
Y = -20421804
36 feet Y = -6224565
97 meter
Z = -8748870
48 Z = -2666655
72
XDOT = 14830
103137 XDOT = 4520
215436
YDOT = 8475
161696 feet/sec YDOT = 2583
229285 meter/sec
ZDOT = -17092
290677 ZDOT = -5209
730198
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 12283
52693116
00016717 00000-0 10270-3 0 9017
2 25544 51
6444 273
2702 0017705 147
7083 212
5155 15
50591658 35788
Satellite: ISS
Catalog Number: 25544
Epoch time: 12283
52693116 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 273
2702 deg
Eccentricity:
0017705
Arg of perigee: 147
7083 deg
Mean anomaly: 212
5155 deg
Mean motion: 15
50591658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3578
Checksum: 309
Coasting Arc #3 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2012/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2236147
69 A = 6795386
03 meter
Y = -5630967
60 meter E =
0025617
Z = 3076098
67 I = 51
29966
XDOT = 4072
825961 Wp = 123
97119
YDOT = 4296
102198 meter/sec RA = 267
65733 deg
ZDOT = 4860
215365 TA = 271
48477
MA = 271
77821
Ha = 232
198 n
mi
Hp = 215
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7336442
56 X = 2284005
04
Y = -18474303
14 feet Y = -5605693
73 meter
Z = 10092187
25 Z = 3087078
63
XDOT = 13362
289898 XDOT = 4000
873331
YDOT = 14094
823485 feet/sec YDOT = 4341
245224 meter/sec
ZDOT = 15945
588467 ZDOT = 4879
825948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -972124
28 X = -296303
48
Y = 19830503
01 feet Y = 6044337
32 meter
Z = 10138127
74 Z = 3090101
34
XDOT = -15635
302031 XDOT = -4765
640059
YDOT = -9032
044260 feet/sec YDOT = -2752
967090 meter/sec
ZDOT = 16026
235158 ZDOT = 4884
796476
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 12284
55808974
00016717 00000-0 10270-3 0 9022
2 25544 51
6440 268
1578 0017646 152
1108 208
0992 15
50668300 35946
Satellite: ISS
Catalog Number: 25544
Epoch time: 12284
55808974 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 268
1578 deg
Eccentricity:
0017646
Arg of perigee: 152
1108 deg
Mean anomaly: 208
0992 deg
Mean motion: 15
50668300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3594
Checksum: 322
Coasting Arc #4 (Orbit 3608)
---------------------------------------
Vector Time (GMT): 2012/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2178395
21 A = 6794060
55 meter
Y = 5364782
78 meter E =
0019912
Z = -3550440
84 I = 51
29725
XDOT = -4187
467695 Wp = 140
49183
YDOT = -4624
684512 meter/sec RA = 262
67379 deg
ZDOT = -4447
599746 TA = 81
56204
MA = 81
33638
Ha = 232
068 n
mi
Hp = 215
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7146965
91 X = -2220976
02
Y = 17600993
37 feet Y = 5340184
13 meter
Z = -11648427
95 Z = -3561127
50
XDOT = -13738
411073 XDOT = -4113
836646
YDOT = -15172
849448 feet/sec YDOT = -4671
100190 meter/sec
ZDOT = -14591
862684 ZDOT = -4467
763098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 737504
15 X = 224791
27
Y = -18954866
11 feet Y = -5777443
19 meter
Z = -11693121
97 Z = -3564063
58
XDOT = 16578
057716 XDOT = 5052
991992
YDOT = 9639
598245 feet/sec YDOT = 2938
149545 meter/sec
ZDOT = -14674
772246 ZDOT = -4472
870581
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 12285
52478431
00016717 00000-0 10270-3 0 9032
2 25544 51
6438 263
3624 0017578 154
9366 205
2642 15
50659129 36099
Satellite: ISS
Catalog Number: 25544
Epoch time: 12285
52478431 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 263
3624 deg
Eccentricity:
0017578
Arg of perigee: 154
9366 deg
Mean anomaly: 205
2642 deg
Mean motion: 15
50659129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3609
Checksum: 325
Coasting Arc #5 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2012/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2096763
81 A = 6792690
82 meter
Y = -5133481
12 meter E =
0025049
Z = 3922720
31 I = 51
29815
XDOT = 4350
185811 Wp = 136
91766
YDOT = 4866
400844 meter/sec RA = 257
69149 deg
ZDOT = 4009
957676 TA = 270
81507
MA = 271
10207
Ha = 231
866 n
mi
Hp = 215
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6879146
37 X = 2134955
70
Y = -16842129
65 feet Y = -5109819
76 meter
Z = 12869817
29 Z = 3932999
83
XDOT = 14272
263159 XDOT = 4275
965670
YDOT = 15965
882035 feet/sec YDOT = 4914
632852 meter/sec
ZDOT = 13156
029121 ZDOT = 4030
910052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -421496
93 X = -128472
26
Y = 18157481
87 feet Y = 5534400
47 meter
Z = 12912798
90 Z = 3935821
10
XDOT = -17587
773730 XDOT = -5360
753433
YDOT = -9902
786110 feet/sec YDOT = -3018
369206 meter/sec
ZDOT = 13242
186377 ZDOT = 4036
218408
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 12286
55590057
00016717 00000-0 10270-3 0 9046
2 25544 51
6438 258
2496 0017543 159
4680 200
7179 15
50732031 36257
Satellite: ISS
Catalog Number: 25544
Epoch time: 12286
55590057 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 258
2496 deg
Eccentricity:
0017543
Arg of perigee: 159
4680 deg
Mean anomaly: 200
7179 deg
Mean motion: 15
50732031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3625
Checksum: 317
Coasting Arc #6 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2012/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2131812
20 A = 6791309
55 meter
Y = 4790964
84 meter E =
0019088
Z = -4318625
33 I = 51
30135
XDOT = -4511
307489 Wp = 135
74613
YDOT = -5120
638627 meter/sec RA = 252
70551 deg
ZDOT = -3476
502826 TA = 98
79799
MA = 98
58178
Ha = 231
721 n
mi
Hp = 215
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6994134
52 X = -2164248
06
Y = 15718388
58 feet Y = 4766943
67 meter
Z = -14168718
26 Z = -4329061
15
XDOT = -14800
877589 XDOT = -4436
823794
YDOT = -16799
995495 feet/sec YDOT = -5170
670873 meter/sec
ZDOT = -11405
849166 ZDOT = -3498
237335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 623088
70 X = 189917
43
Y = -17156930
97 feet Y = -5229432
56 meter
Z = -14212308
55 Z = -4331911
65
XDOT = 18637
715195 XDOT = 5680
775592
YDOT = 10137
586874 feet/sec YDOT = 3089
936479 meter/sec
ZDOT = -11495
223516 ZDOT = -3503
744128
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 12287
52255469
00016717 00000-0 10270-3 0 9050
2 25544 51
6441 253
4538 0017464 162
3728 197
8032 15
50726716 36407
Satellite: ISS
Catalog Number: 25544
Epoch time: 12287
52255469 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 253
4538 deg
Eccentricity:
0017464
Arg of perigee: 162
3728 deg
Mean anomaly: 197
8032 deg
Mean motion: 15
50726716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 321
Coasting Arc #7 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2012/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2149611
68 A = 6790002
91 meter
Y = -4496083
73 meter E =
0023539
Z = 4611761
02 I = 51
30812
XDOT = 4705
677792 Wp = 150
56272
YDOT = 5286
850750 meter/sec RA = 247
72165 deg
ZDOT = 2934
298294 TA = 269
91806
MA = 270
18780
Ha = 231
508 n
mi
Hp = 215
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7052531
76 X = 2177324
68
Y = -14750930
88 feet Y = -4471889
92 meter
Z = 15130449
55 Z = 4622271
82
XDOT = 15438
575434 XDOT = 4631
954914
YDOT = 17345
310861 feet/sec YDOT = 5339
060726 meter/sec
ZDOT = 9626
962907 ZDOT = 2956
979043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -748607
50 X = -228175
57
Y = 16292276
75 feet Y = 4965885
95 meter
Z = 15174319
58 Z = 4625132
61
XDOT = -19681
412773 XDOT = -5998
894613
YDOT = -10038
488986 feet/sec YDOT = -3059
731443 meter/sec
ZDOT = 9720
239862 ZDOT = 2962
729110
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 12288
55362772
00016717 00000-0 10270-3 0 9061
2 25544 51
6446 248
3409 0017450 166
8609 193
3000 15
50797190 36561
Satellite: ISS
Catalog Number: 25544
Epoch time: 12288
55362772 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 248
3409 deg
Eccentricity:
0017450
Arg of perigee: 166
8609 deg
Mean anomaly: 193
3000 deg
Mean motion: 15
50797190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3656
Checksum: 326
Coasting Arc #8 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2296262
13 A = 6788850
93 meter
Y = 4108523
83 meter E =
0019961
Z = -4900119
23 I = 51
31726
XDOT = -4872
910893 Wp = 133
19451
YDOT = -5440
196850 meter/sec RA = 242
73434 deg
ZDOT = -2297
170343 TA = 114
30576
MA = 114
09717
Ha = 231
352 n
mi
Hp = 216
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7533668
40 X = -2318229
55
Y = 13479408
90 feet Y = 4082722
28 meter
Z = -16076506
67 Z = -4911328
43
XDOT = -15987
240463 XDOT = -4800
555883
YDOT = -17848
414862 feet/sec YDOT = -5494
284454 meter/sec
ZDOT = -7536
648106 ZDOT = -2320
667031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1413155
99 X = 430729
94
Y = -15328052
57 feet Y = -4671990
42 meter
Z = -16123228
13 Z = -4914359
93
XDOT = 20638
177737 XDOT = 6290
516574
YDOT = 9865
491633 feet/sec YDOT = 3007
001850 meter/sec
ZDOT = -7633
289601 ZDOT = -2326
626670
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 12289
52024056
00016717 00000-0 10270-3 0 9070
2 25544 51
6452 243
5451 0017374 169
9634 190
1867 15
50793988 36713
Satellite: ISS
Catalog Number: 25544
Epoch time: 12289
52024056 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 243
5451 deg
Eccentricity:
0017374
Arg of perigee: 169
9634 deg
Mean anomaly: 190
1867 deg
Mean motion: 15
50793988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 337
Coasting Arc #9 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2012/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2426713
97 A = 6787845
16 meter
Y = -3782825
05 meter E =
0021121
Z = 5086787
57 I = 51
33005
XDOT = 5055
218798 Wp = 163
61366
YDOT = 5512
845016 meter/sec RA = 237
75008 deg
ZDOT = 1666
414486 TA = 270
09329
MA = 270
33532
Ha = 231
122 n
mi
Hp = 216
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7961660
00 X = 2444122
80
Y = -12410843
35 feet Y = -3755590
31 meter
Z = 16688935
60 Z = 5098619
33
XDOT = 16585
363511 XDOT = 4985
102006
YDOT = 18086
761863 feet/sec YDOT = 5568
983706 meter/sec
ZDOT = 5467
239126 ZDOT = 1690
802466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1979857
99 X = -603460
71
Y = 14555079
73 feet Y = 4436388
30 meter
Z = 16738203
32 Z = 5101804
37
XDOT = -21517
311792 XDOT = -6558
476634
YDOT = -9410
789849 feet/sec YDOT = -2868
408746 meter/sec
ZDOT = 5567
564929 ZDOT = 1696
993790
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 12290
55126965
00016717 00000-0 10270-3 0 9088
2 25544 51
6459 238
4323 0017371 174
3021 185
8330 15
50862108 36872
Satellite: ISS
Catalog Number: 25544
Epoch time: 12290
55126965 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 238
4323 deg
Eccentricity:
0017371
Arg of perigee: 174
3021 deg
Mean anomaly: 185
8330 deg
Mean motion: 15
50862108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 314
Coasting Arc #10 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2012/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2688775
71 A = 6787196
09 meter
Y = 3389350
63 meter E =
0021500
Z = -5240402
36 I = 51
34510
XDOT = -5179
100069 Wp = 136
07057
YDOT = -5554
607204 meter/sec RA = 232
76279 deg
ZDOT = -952
779799 TA = 124
85846
MA = 124
65611
Ha = 230
964 n
mi
Hp = 216
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8821442
61 X = -2701018
92
Y = 11119916
75 feet Y = 3359214
36 meter
Z = -17192921
12 Z = -5253494
55
XDOT = -16991
798128 XDOT = -5111
973853
YDOT = -18223
776916 feet/sec YDOT = -5612
147854 meter/sec
ZDOT = -3125
917975 ZDOT = -977
776995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3059390
90 X = 932502
35
Y = -13792582
95 feet Y = -4203979
28 meter
Z = -17247368
44 Z = -5256997
90
XDOT = 22172
549536 XDOT = 6758
193099
YDOT = 8883
998042 feet/sec YDOT = 2707
842603 meter/sec
ZDOT = -3228
767034 ZDOT = -984
128192
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 12291
51784050
00016717 00000-0 10270-3 0 9091
2 25544 51
6460 233
6367 0017313 177
5750 182
5488 15
50861322 37022
Satellite: ISS
Catalog Number: 25544
Epoch time: 12291
51784050 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 233
6367 deg
Eccentricity:
0017313
Arg of perigee: 177
5750 deg
Mean anomaly: 182
5488 deg
Mean motion: 15
50861322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 307
Coasting Arc #11 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2012/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2929036
96 A = 6786721
58 meter
Y = -3070802
63 meter E =
0018009
Z = 5295285
53 I = 51
36364
XDOT = 5299
045428 Wp = 173
90655
YDOT = 5531
614234 meter/sec RA = 227
77930 deg
ZDOT = 259
081917 TA = 273
51026
MA = 273
71623
Ha = 230
715 n
mi
Hp = 216
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9609701
32 X = 2937433
72
Y = -10074811
77 feet Y = -3038001
22 meter
Z = 17372984
03 Z = 5309535
47
XDOT = 17385
319647 XDOT = 5235
537332
YDOT = 18148
340662 feet/sec YDOT = 5590
516380 meter/sec
ZDOT = 850
006288 ZDOT = 284
670636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3993183
00 X = -1217122
18
Y = 13260536
64 feet Y = 4041811
57 meter
Z = 17432195
02 Z = 5313333
04
XDOT = -22695
180669 XDOT = -6917
491068
YDOT = -8165
995694 feet/sec YDOT = -2488
995487 meter/sec
ZDOT = 955
314821 ZDOT = 291
179958
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 12292
54882499
00016717 00000-0 10270-3 0 9103
2 25544 51
6463 228
5238 0017306 181
7165 178
3930 15
50924252 37188
Satellite: ISS
Catalog Number: 25544
Epoch time: 12292
54882499 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 228
5238 deg
Eccentricity:
0017306
Arg of perigee: 181
7165 deg
Mean anomaly: 178
3930 deg
Mean motion: 15
50924252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 325
Coasting Arc #12 (Orbit 3732)
---------------------------------------
Vector Time (GMT): 2012/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3291859
17 A = 6786760
72 meter
Y = 2712206
86 meter E =
0022426
Z = -5291675
62 I = 51
38481
XDOT = -5328
272179 Wp = 144
29451
YDOT = -5470
554975 meter/sec RA = 222
79342 deg
ZDOT = 493
960134 TA = 130
54193
MA = 130
34643
Ha = 230
559 n
mi
Hp = 216
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10800062
91 X = -3296236
72
Y = 8898316
48 feet Y = 2675370
68 meter
Z = -17361140
49 Z = -5307678
30
XDOT = -17481
207936 XDOT = -5269
102871
YDOT = -17948
015011 feet/sec YDOT = -5529
808199 meter/sec
ZDOT = 1620
604115 ZDOT = 468
218952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5364135
31 X = 1634988
44
Y = -12834964
90 feet Y = -3912097
30 meter
Z = -17427573
63 Z = -5311924
44
XDOT = 22873
862717 XDOT = 6971
953356
YDOT = 7428
646501 feet/sec YDOT = 2264
251454 meter/sec
ZDOT = 1514
644905 ZDOT = 461
663767
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 12293
51535314
00016717 00000-0 10270-3 0 9113
2 25544 51
6462 223
7279 0017269 185
0874 175
0104 15
50929781 37337
Satellite: ISS
Catalog Number: 25544
Epoch time: 12293
51535314 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 223
7279 deg
Eccentricity:
0017269
Arg of perigee: 185
0874 deg
Mean anomaly: 175
0104 deg
Mean motion: 15
50929781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3733
Checksum: 314
Coasting Arc #13 (Orbit 3748)
---------------------------------------
Vector Time (GMT): 2012/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3620391
26 A = 6786969
15 meter
Y = -2437542
85 meter E =
0014849
Z = 5194372
77 I = 51
40895
XDOT = 5336
491125 Wp = 177
90970
YDOT = 5368
250734 meter/sec RA = 217
81196 deg
ZDOT = -1214
747593 TA = 283
70402
MA = 283
86928
Ha = 230
288 n
mi
Hp = 217
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11877924
08 X = 3622145
83
Y = -7997187
83 feet Y = -2397047
47 meter
Z = 17041905
43 Z = 5211965
03
XDOT = 17508
172983 XDOT = 5281
966658
YDOT = 17612
371173 feet/sec YDOT = 5427
621823 meter/sec
ZDOT = -3985
392365 ZDOT = -1188
955321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6521680
46 X = -1987808
20
Y = 12649691
13 feet Y = 3855625
86 meter
Z = 17114895
06 Z = 5216620
01
XDOT = -22894
327295 XDOT = -6978
190959
YDOT = -6618
725168 feet/sec YDOT = -2017
387431 meter/sec
ZDOT = -3879
195772 ZDOT = -1182
378871
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 12294
54629260
00016717 00000-0 10270-3 0 9122
2 25544 51
6460 218
6145 0017256 189
0502 171
0341 15
50983644 37492
Satellite: ISS
Catalog Number: 25544
Epoch time: 12294
54629260 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 218
6145 deg
Eccentricity:
0017256
Arg of perigee: 189
0502 deg
Mean anomaly: 171
0341 deg
Mean motion: 15
50983644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3749
Checksum: 308
Coasting Arc #14 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2012/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4050097
27 A = 6787726
58 meter
Y = 2148737
64 meter E =
0021871
Z = -5018850
35 I = 51
43641
XDOT = -5227
036882 Wp = 156
73612
YDOT = -5232
921687 meter/sec RA = 212
82939 deg
ZDOT = 1960
970311 TA = 132
48875
MA = 132
30373
Ha = 230
130 n
mi
Hp = 217
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13287720
69 X = -4049443
16
Y = 7049664
18 feet Y = 2103450
43 meter
Z = -16466044
45 Z = -5038524
24
XDOT = -17149
071134 XDOT = -5177
658831
YDOT = -17168
378239 feet/sec YDOT = -5291
097531 meter/sec
ZDOT = 6433
629629 ZDOT = 1935
697410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7999819
89 X = 2438345
10
Y = -12632136
14 feet Y = -3850275
10 meter
Z = -16547625
94 Z = -5043716
39
XDOT = 22495
812970 XDOT = 6856
723793
YDOT = 5883
332772 feet/sec YDOT = 1793
239829 meter/sec
ZDOT = 6329
551879 ZDOT = 1929
247413
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 12295
51277768
00016717 00000-0 10270-3 0 9133
2 25544 51
6462 213
8182 0017235 192
5149 167
5576 15
51001194 37644
Satellite: ISS
Catalog Number: 25544
Epoch time: 12295
51277768 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 213
8182 deg
Eccentricity:
0017235
Arg of perigee: 192
5149 deg
Mean anomaly: 167
5576 deg
Mean motion: 15
51001194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 321
Coasting Arc #15 (Orbit 3779)
---------------------------------------
Vector Time (GMT): 2012/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4427126
32 A = 6788620
98 meter
Y = -1945945
49 meter E =
0013081
Z = 4757357
74 I = 51
46576
XDOT = 5084
191810 Wp = 172
71504
YDOT = 5085
275909 meter/sec RA = 207
85180 deg
ZDOT = -2663
103739 TA = 303
58026
MA = 303
70507
Ha = 229
838 n
mi
Hp = 217
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14524692
66 X = 4425446
86
Y = -6384335
61 feet Y = -1896447
77 meter
Z = 15608129
06 Z = 4778860
73
XDOT = 16680
419324 XDOT = 5039
886205
YDOT = 16683
976078 feet/sec YDOT = 5141
882667 meter/sec
ZDOT = -8737
216992 ZDOT = -2638
512579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9189300
35 X = -2800898
75
Y = 12825470
96 feet Y = 3909203
55 meter
Z = 15697266
78 Z = 4784526
92
XDOT = -21951
878584 XDOT = -6690
932592
YDOT = -5206
175694 feet/sec YDOT = -1586
842351 meter/sec
ZDOT = -8635
930133 ZDOT = -2632
231505
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 12296
54367216
00016717 00000-0 10270-3 0 9146
2 25544 51
6460 208
7040 0017221 196
3754 163
6843 15
51042151 37807
Satellite: ISS
Catalog Number: 25544
Epoch time: 12296
54367216 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 208
7040 deg
Eccentricity:
0017221
Arg of perigee: 196
3754 deg
Mean anomaly: 163
6843 deg
Mean motion: 15
51042151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 297
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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