[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 14th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
013/16:10:27
045 2
0 2
8 2
8
N/A 1
4 -0
2 215
7
000/00:00:54
090 -1
3 0
0 205
8
Coasting Arc #1 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2012/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3842093
55 A = 6766932
10 meter
Y = 3538822
22 meter E =
0016877
Z = -4292329
31 I = 51
61640
XDOT = -6323
439479 Wp = 291
96808
YDOT = 2569
025305 meter/sec RA = 182
03644 deg
ZDOT = -3524
835269 TA = 302
12097
MA = 302
28465
Ha = 215
638 n
mi
Hp = 204
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12605293
78 X = 3823087
05
Y = 11610309
13 feet Y = 3581680
70 meter
Z = -14082445
26 Z = -4273710
95
XDOT = -20746
192518 XDOT = -6334
574246
YDOT = 8428
560713 feet/sec YDOT = 2498
250534 meter/sec
ZDOT = -11564
420175 ZDOT = -3555
580815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6126549
23 X = -1867372
20
Y = 16071483
66 feet Y = 4898588
22 meter
Z = -14006454
98 Z = -4269167
48
XDOT = -14271
387690 XDOT = -4349
918968
YDOT = -15678
329741 feet/sec YDOT = -4778
754905 meter/sec
ZDOT = -11690
418393 ZDOT = -3563
239526
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 12013
52244303
00016717 00000-0 10270-3 0 9007
2 25544 51
6389 182
9687 0023785 278
0262 81
8194 15
59167041 33744
Satellite: ISS
Catalog Number: 25544
Epoch time: 12013
52244303 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 182
9687 deg
Eccentricity:
0023785
Arg of perigee: 278
0262 deg
Mean anomaly: 81
8194 deg
Mean motion: 15
59167041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 315
Coasting Arc #2 (Orbit 3376)
---------------------------------------
Vector Time (GMT): 2012/013/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4662605
15 A = 6769741
99 meter
Y = -2997221
90 meter E =
0011581
Z = 3899151
61 I = 51
62917
XDOT = 5558
928397 Wp = 289
05359
YDOT = 3342
395573 meter/sec RA = 181
11269 deg
ZDOT = -4084
331288 TA = 203
73496
MA = 203
78841
Ha = 215
699 n
mi
Hp = 205
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15297261
00 X = 4676833
20
Y = -9833405
19 feet Y = -2945002
31 meter
Z = 12792492
17 Z = 3921836
54
XDOT = 18237
954060 XDOT = 5540
980406
YDOT = 10965
864741 feet/sec YDOT = 3404
458658 meter/sec
ZDOT = -13400
037033 ZDOT = -4057
370152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16094271
18 X = 4905533
85
Y = -8323915
99 feet Y = -2537129
59 meter
Z = 12885525
42 Z = 3927508
15
XDOT = 16572
789920 XDOT = 5051
386368
YDOT = 11501
885844 feet/sec YDOT = 3505
774805 meter/sec
ZDOT = -13289
885722 ZDOT = -4050
757168
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 12013
71474515
00016717 00000-0 10270-3 0 9019
2 25544 51
6419 182
0045 0022017 274
8805 84
9836 15
58619286 33773
Satellite: ISS
Catalog Number: 25544
Epoch time: 12013
71474515 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 182
0045 deg
Eccentricity:
0022017
Arg of perigee: 274
8805 deg
Mean anomaly: 84
9836 deg
Mean motion: 15
58619286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3377
Checksum: 316
Coasting Arc #3 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2012/014/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6540500
98 A = 6775699
79 meter
Y = 1327239
63 meter E =
0019478
Z = -1113792
65 I = 51
68011
XDOT = -1933
826999 Wp = 304
41330
YDOT = -4534
342297 meter/sec RA = 176
10811 deg
ZDOT = 5890
226365 TA = 43
47513
MA = 43
32173
Ha = 215
826 n
mi
Hp = 205
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21458336
55 X = -6549445
83
Y = 4354460
72 feet Y = 1254049
73 meter
Z = -3654175
37 Z = -1145587
52
XDOT = -6344
576767 XDOT = -1911
592474
YDOT = -14876
451105 feet/sec YDOT = -4555
843323 meter/sec
ZDOT = 19324
889650 ZDOT = 5880
885936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21712798
98 X = -6618061
13
Y = 2647104
84 feet Y = 806837
56 meter
Z = -3784406
16 Z = -1153487
00
XDOT = -5073
129207 XDOT = -1546
289782
YDOT = -13756
029334 feet/sec YDOT = -4192
837741 meter/sec
ZDOT = 19286
930059 ZDOT = 5878
656282
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 12014
67647452
00016717 00000-0 10270-3 0 9028
2 25544 51
6425 177
1767 0022171 279
1698 80
6949 15
58634597 33922
Satellite: ISS
Catalog Number: 25544
Epoch time: 12014
67647452 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 177
1767 deg
Eccentricity:
0022171
Arg of perigee: 279
1698 deg
Mean anomaly: 80
6949 deg
Mean motion: 15
58634597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 344
Coasting Arc #4 (Orbit 3407)
---------------------------------------
Vector Time (GMT): 2012/015/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6426168
44 A = 6774432
44 meter
Y = 623354
58 meter E =
0017263
Z = -2036172
06 I = 51
70571
XDOT = -2239
788852 Wp = 269
29629
YDOT = 4793
854425 meter/sec RA = 171
12109 deg
ZDOT = -5560
735675 TA = 293
23756
MA = 293
41924
Ha = 215
902 n
mi
Hp = 205
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21083229
79 X = 6428611
56
Y = 2045126
56 feet Y = 695229
66 meter
Z = -6680354
52 Z = -2004948
25
XDOT = -7348
388622 XDOT = -2266
215581
YDOT = 15727
868850 feet/sec YDOT = 4768
660118 meter/sec
ZDOT = -18243
883447 ZDOT = -5571
680466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20956436
01 X = 6387521
70
Y = 3347221
94 feet Y = 1020233
25 meter
Z = -6552568
40 Z = -1997222
85
XDOT = -7952
377675 XDOT = -2423
884715
YDOT = 13720
935080 feet/sec YDOT = 4182
141012 meter/sec
ZDOT = -18288
981852 ZDOT = -5574
481669
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 12015
70230604
00016717 00000-0 10270-3 0 9031
2 25544 51
6418 172
0288 0022125 282
7090 77
1592 15
58680420 34080
Satellite: ISS
Catalog Number: 25544
Epoch time: 12015
70230604 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 172
0288 deg
Eccentricity:
0022125
Arg of perigee: 282
7090 deg
Mean anomaly: 77
1592 deg
Mean motion: 15
58680420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3408
Checksum: 285
Coasting Arc #5 (Orbit 3423)
---------------------------------------
Vector Time (GMT): 2012/016/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4350754
33 A = 6767467
76 meter
Y = -2585189
85 meter E =
0013145
Z = 4502259
77 I = 51
71299
XDOT = 5691
814972 Wp = 283
60272
YDOT = -4014
513030 meter/sec RA = 166
11028 deg
ZDOT = 3206
022730 TA = 134
26300
MA = 134
15506
Ha = 216
025 n
mi
Hp = 205
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14274128
38 X = -4343393
74
Y = -8481594
01 feet Y = -2633801
72 meter
Z = 14771193
47 Z = 4481141
84
XDOT = 18673
933634 XDOT = 5720
708954
YDOT = -13170
974509 feet/sec YDOT = -3950
702246 meter/sec
ZDOT = 10518
447276 ZDOT = 3233
743205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13970239
62 X = -4258129
04
Y = -9113873
25 feet Y = -2777908
57 meter
Z = 14684892
03 Z = 4475955
09
XDOT = 18514
963274 XDOT = 5643
360806
YDOT = -11307
231722 feet/sec YDOT = -3446
444229 meter/sec
ZDOT = 10632
189096 ZDOT = 3240
691236
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 12016
72812105
00016717 00000-0 10270-3 0 9047
2 25544 51
6421 166
8786 0022154 286
7917 73
0808 15
58725594 34247
Satellite: ISS
Catalog Number: 25544
Epoch time: 12016
72812105 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 166
8786 deg
Eccentricity:
0022154
Arg of perigee: 286
7917 deg
Mean anomaly: 73
0808 deg
Mean motion: 15
58725594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3424
Checksum: 318
Coasting Arc #6 (Orbit 3438)
---------------------------------------
Vector Time (GMT): 2012/017/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1047442
42 A = 6764014
83 meter
Y = 4061797
74 meter E =
0009421
Z = -5300942
89 I = 51
72993
XDOT = -7332
928318 Wp = 321
78950
YDOT = 2267
866226 meter/sec RA = 161
07280 deg
ZDOT = 295
740169 TA = 310
98069
MA = 311
06215
Ha = 216
281 n
mi
Hp = 205
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3436490
87 X = 1027695
41
Y = 13326108
06 feet Y = 4073400
84 meter
Z = -17391544
90 Z = -5295902
16
XDOT = -24058
163773 XDOT = -7359
179683
YDOT = 7440
505991 feet/sec YDOT = 2185
718113 meter/sec
ZDOT = 970
276146 ZDOT = 260
053673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3174368
78 X = 967547
60
Y = 13417400
55 feet Y = 4089623
69 meter
Z = -17371160
15 Z = -5294729
61
XDOT = -23280
550451 XDOT = -7095
911777
YDOT = 6545
065166 feet/sec YDOT = 1994
935863 meter/sec
ZDOT = 824
008458 ZDOT = 251
157778
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 12017
68981018
00016717 00000-0 10270-3 0 9054
2 25544 51
6412 162
0522 0022206 290
7865 69
0911 15
58722897 34397
Satellite: ISS
Catalog Number: 25544
Epoch time: 12017
68981018 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 162
0522 deg
Eccentricity:
0022206
Arg of perigee: 290
7865 deg
Mean anomaly: 69
0911 deg
Mean motion: 15
58722897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3439
Checksum: 315
Coasting Arc #7 (Orbit 3454)
---------------------------------------
Vector Time (GMT): 2012/018/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2478081
49 A = 6768316
08 meter
Y = -4715204
32 meter E =
0015891
Z = 4192709
12 I = 51
77377
XDOT = 6700
728574 Wp = 319
61876
YDOT = 219
531500 meter/sec RA = 156
03864 deg
ZDOT = -3709
595959 TA = 168
44542
MA = 168
40891
Ha = 216
382 n
mi
Hp = 205
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8130188
60 X = 2510256
58
Y = -15469830
46 feet Y = -4687313
36 meter
Z = 13755607
37 Z = 4204825
18
XDOT = 21984
017630 XDOT = 6715
795966
YDOT = 720
247705 feet/sec YDOT = 294
547741 meter/sec
ZDOT = -12170
590416 ZDOT = -3677
007729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8205227
31 X = 2500953
28
Y = -15385513
47 feet Y = -4689504
51 meter
Z = 13805526
98 Z = 4207924
62
XDOT = 20926
897644 XDOT = 6378
518402
YDOT = 347
894887 feet/sec YDOT = 106
038361 meter/sec
ZDOT = -12037
148188 ZDOT = -3668
922768
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 12018
71559558
00016717 00000-0 10270-3 0 9060
2 25544 51
6415 156
9024 0022240 294
9036 64
9808 15
58780133 34557
Satellite: ISS
Catalog Number: 25544
Epoch time: 12018
71559558 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 156
9024 deg
Eccentricity:
0022240
Arg of perigee: 294
9036 deg
Mean anomaly: 64
9808 deg
Mean motion: 15
58780133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3455
Checksum: 321
Coasting Arc #8 (Orbit 3469)
---------------------------------------
Vector Time (GMT): 2012/019/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5091930
53 A = 6774949
79 meter
Y = 4181047
95 meter E =
0022569
Z = -1516824
19 I = 51
82224
XDOT = -4129
255577 Wp = 320
19637
YDOT = -2917
530571 meter/sec RA = 151
03943 deg
ZDOT = 5789
334328 TA = 23
22083
MA = 23
11902
Ha = 216
713 n
mi
Hp = 205
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16705808
82 X = -5130937
10
Y = 13717348
91 feet Y = 4123888
90 meter
Z = -4976457
32 Z = -1541654
60
XDOT = -13547
426435 XDOT = -4124
447220
YDOT = -9571
950691 feet/sec YDOT = -2963
680134 meter/sec
ZDOT = 18993
879029 ZDOT = 5769
286214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16579961
91 X = -5053572
39
Y = 13832181
84 feet Y = 4216049
02 meter
Z = -5078429
46 Z = -1547905
30
XDOT = -12719
600635 XDOT = -3876
934274
YDOT = -8267
008510 feet/sec YDOT = -2519
784194 meter/sec
ZDOT = 18911
954871 ZDOT = 5764
363845
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 12019
67725639
00016717 00000-0 10270-3 0 9072
2 25544 51
6409 152
0746 0022309 298
9168 60
9749 15
58737376 34702
Satellite: ISS
Catalog Number: 25544
Epoch time: 12019
67725639 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 152
0746 deg
Eccentricity:
0022309
Arg of perigee: 298
9168 deg
Mean anomaly: 60
9749 deg
Mean motion: 15
58737376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3470
Checksum: 348
Coasting Arc #9 (Orbit 3485)
---------------------------------------
Vector Time (GMT): 2012/020/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6072327
64 A = 6774597
20 meter
Y = -2483306
67 meter E =
0014972
Z = -1692994
65 I = 51
84772
XDOT = 475
994147 Wp = 293
21951
YDOT = 5091
866546 meter/sec RA = 146
06131 deg
ZDOT = -5715
742865 TA = 265
30768
MA = 265
47869
Ha = 216
840 n
mi
Hp = 205
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19922334
79 X = 6107869
21
Y = -8147331
61 feet Y = -2415203
28 meter
Z = -5554444
40 Z = -1663409
98
XDOT = 1561
660587 XDOT = 446
785811
YDOT = 16705
598903 feet/sec YDOT = 5097
026654 meter/sec
ZDOT = -18752
437221 ZDOT = -5713
500991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19753285
91 X = 6020801
55
Y = -8626674
59 feet Y = -2629410
42 meter
Z = -5433090
24 Z = -1656005
91
XDOT = 1448
739515 XDOT = 441
575804
YDOT = 15218
810558 feet/sec YDOT = 4638
693458 meter/sec
ZDOT = -18743
587323 ZDOT = -5713
045416
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 12020
70301276
00016717 00000-0 10270-3 0 9086
2 25544 51
6409 146
9253 0022116 302
9371 56
9657 15
58805768 34866
Satellite: ISS
Catalog Number: 25544
Epoch time: 12020
70301276 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 146
9253 deg
Eccentricity:
0022116
Arg of perigee: 302
9371 deg
Mean anomaly: 56
9657 deg
Mean motion: 15
58805768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3486
Checksum: 316
Coasting Arc #10 (Orbit 3501)
---------------------------------------
Vector Time (GMT): 2012/021/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5205838
72 A = 6767831
90 meter
Y = -158996
51 meter E =
0013276
Z = 4322537
91 I = 51
85041
XDOT = 3101
329862 Wp = 321
01077
YDOT = -6068
277395 meter/sec RA = 141
06323 deg
ZDOT = 3527
796456 TA = 93
29149
MA = 93
13960
Ha = 217
154 n
mi
Hp = 205
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17079523
37 X = -5224671
33
Y = -521642
09 feet Y = -217317
08 meter
Z = 14181554
82 Z = 4297202
98
XDOT = 10174
966740 XDOT = 3151
819198
YDOT = -19909
046570 feet/sec YDOT = -6033
314425 meter/sec
ZDOT = 11574
135354 ZDOT = 3542
984347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17172056
53 X = -5234042
83
Y = 188814
90 feet Y = 57550
78 meter
Z = 14077767
93 Z = 4290903
66
XDOT = 9287
203470 XDOT = 2830
739618
YDOT = -19056
656574 feet/sec YDOT = -5808
468924 meter/sec
ZDOT = 11636
760454 ZDOT = 3546
884586
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 12021
72875205
00016717 00000-0 10270-3 0 9098
2 25544 51
6414 141
7748 0022173 306
8080 53
1040 15
58832461 35021
Satellite: ISS
Catalog Number: 25544
Epoch time: 12021
72875205 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 141
7748 deg
Eccentricity:
0022173
Arg of perigee: 306
8080 deg
Mean anomaly: 53
1040 deg
Mean motion: 15
58832461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3502
Checksum: 283
Coasting Arc #11 (Orbit 3516)
---------------------------------------
Vector Time (GMT): 2012/022/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2943208
64 A = 6763687
14 meter
Y = 2963519
00 meter E =
0014764
Z = -5318524
09 I = 51
85993
XDOT = -5501
335191 Wp = 352
83051
YDOT = 5355
939320 meter/sec RA = 136
03498 deg
ZDOT = -45
692809 TA = 276
65195
MA = 276
81998
Ha = 217
443 n
mi
Hp = 205
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9656196
31 X = 2935686
75
Y = 9722831
38 feet Y = 2996390
09 meter
Z = -17449226
01 Z = -5304244
54
XDOT = -18048
999970 XDOT = -5560
595545
YDOT = 17571
979395 feet/sec YDOT = 5294
088666 meter/sec
ZDOT = -149
910792 ZDOT = -72
560929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10313804
79 X = 3143647
70
Y = 9134150
63 feet Y = 2784089
11 meter
Z = -17390911
10 Z = -5300749
70
XDOT = -16322
876918 XDOT = -4975
212885
YDOT = 17845
516477 feet/sec YDOT = 5439
313422 meter/sec
ZDOT = -260
358046 ZDOT = -79
357132
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 12022
69037005
00016717 00000-0 10270-3 0 9105
2 25544 51
6417 136
9473 0022205 310
7128 49
2098 15
58831234 35170
Satellite: ISS
Catalog Number: 25544
Epoch time: 12022
69037005 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 136
9473 deg
Eccentricity:
0022205
Arg of perigee: 310
7128 deg
Mean anomaly: 49
2098 deg
Mean motion: 15
58831234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3517
Checksum: 289
Coasting Arc #12 (Orbit 3532)
---------------------------------------
Vector Time (GMT): 2012/023/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 297
48 A = 6767459
91 meter
Y = -5198985
68 meter E =
0019897
Z = 4349487
18 I = 51
89459
XDOT = 6165
053766 Wp = 340
53793
YDOT = -2925
965704 meter/sec RA = 131
00701 deg
ZDOT = -3484
150271 TA = 144
82961
MA = 144
69812
Ha = 217
542 n
mi
Hp = 204
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 975
99 X = 37305
31
Y = -17057039
64 feet Y = -5198775
64 meter
Z = 14269971
07 Z = 4349578
27
XDOT = 20226
554349 XDOT = 6214
239054
YDOT = -9599
625013 feet/sec YDOT = -2856
749105 meter/sec
ZDOT = -11430
939209 ZDOT = -3454
082204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1375786
80 X = -419339
82
Y = -17000862
66 feet Y = -5181862
94 meter
Z = 14270688
70 Z = 4349705
92
XDOT = 18271
246493 XDOT = 5569
075931
YDOT = -11007
987979 feet/sec YDOT = -3355
234736 meter/sec
ZDOT = -11307
527053 ZDOT = -3446
534246
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 12023
71607848
00016717 00000-0 10270-3 0 9118
2 25544 51
6418 131
7976 0022281 314
7989 45
1354 15
58898921 35339
Satellite: ISS
Catalog Number: 25544
Epoch time: 12023
71607848 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 131
7976 deg
Eccentricity:
0022281
Arg of perigee: 314
7989 deg
Mean anomaly: 45
1354 deg
Mean motion: 15
58898921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3533
Checksum: 331
Coasting Arc #13 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2012/024/16:10:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2655840
86 A = 6774192
64 meter
Y = 5966211
49 meter E =
0024711
Z = -1736296
06 I = 51
93672
XDOT = -5101
033109 Wp = 336
36929
YDOT = -603
629821 meter/sec RA = 126
01259 deg
ZDOT = 5722
476410 TA = 4
58347
MA = 4
56088
Ha = 217
786 n
mi
Hp = 204
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8713388
66 X = -2713924
54
Y = 19574184
67 feet Y = 5936187
52 meter
Z = -5696509
40 Z = -1749338
61
XDOT = -16735
672929 XDOT = -5121
701832
YDOT = -1980
412800 feet/sec YDOT = -660
788413 meter/sec
ZDOT = 18774
528903 ZDOT = 5697
646270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6824760
60 X = -2080187
03
Y = 20294779
84 feet Y = 6185848
90 meter
Z = -5750358
30 Z = -1752709
21
XDOT = -15480
276134 XDOT = -4718
388166
YDOT = 90
482707 feet/sec YDOT = 27
579129 meter/sec
ZDOT = 18672
806657 ZDOT = 5691
471469
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 12024
67766812
00016717 00000-0 10270-3 0 9122
2 25544 51
6423 126
9693 0022211 318
7390 41
2086 15
58898901 35483
Satellite: ISS
Catalog Number: 25544
Epoch time: 12024
67766812 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 126
9693 deg
Eccentricity:
0022211
Arg of perigee: 318
7390 deg
Mean anomaly: 41
2086 deg
Mean motion: 15
58898901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 319
Coasting Arc #14 (Orbit 3563)
---------------------------------------
Vector Time (GMT): 2012/025/16:14:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4863396
00 A = 6772047
09 meter
Y = -3770368
48 meter E =
0017988
Z = -2840167
68 I = 51
94714
XDOT = 1315
547105 Wp = 328
97036
YDOT = 5564
922108 meter/sec RA = 121
03651 deg
ZDOT = -5105
440261 TA = 243
18213
MA = 243
36620
Ha = 218
022 n
mi
Hp = 204
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15956023
63 X = 4918992
11
Y = -12369975
31 feet Y = -3715672
13 meter
Z = -9318135
43 Z = -2816407
08
XDOT = 4316
099425 XDOT = 1278
021718
YDOT = 18257
618466 feet/sec YDOT = 5579
423560 meter/sec
ZDOT = -16750
132090 ZDOT = -5099
140686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14307325
30 X = 4360872
75
Y = -14308091
51 feet Y = -4361106
29 meter
Z = -9220498
20 Z = -2810407
85
XDOT = 5662
222912 XDOT = 1725
845544
YDOT = 16502
528702 feet/sec YDOT = 5029
970748 meter/sec
ZDOT = -16724
684087 ZDOT = -5097
683710
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 12025
70334693
00016717 00000-0 10270-3 0 9136
2 25544 51
6426 121
8195 0022206 322
9023 37
0596 15
58929908 35640
Satellite: ISS
Catalog Number: 25544
Epoch time: 12025
70334693 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 121
8195 deg
Eccentricity:
0022206
Arg of perigee: 322
9023 deg
Mean anomaly: 37
0596 deg
Mean motion: 15
58929908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3564
Checksum: 310
Coasting Arc #15 (Orbit 3579)
---------------------------------------
Vector Time (GMT): 2012/026/16:14:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4578192
02 A = 6765025
99 meter
Y = 538397
37 meter E =
0016492
Z = 4951815
23 I = 51
93714
XDOT = 1555
947805 Wp = 336
53339
YDOT = -7175
927533 meter/sec RA = 116
02979 deg
ZDOT = 2236
054276 TA = 91
84498
MA = 91
65609
Ha = 218
337 n
mi
Hp = 204
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15020315
04 X = -4607926
50
Y = 1766395
57 feet Y = 487035
02 meter
Z = 16246112
97 Z = 4929502
84
XDOT = 5104
815632 XDOT = 1625
212811
YDOT = -23543
069335 feet/sec YDOT = -7158
140655 meter/sec
ZDOT = 7336
136076 ZDOT = 2243
781170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14705175
51 X = -4482137
50
Y = 3930928
87 feet Y = 1198147
12 meter
Z = 16154622
10 Z = 4923928
82
XDOT = 1895
884375 XDOT = 577
865558
YDOT = -22954
183552 feet/sec YDOT = -6996
435147 meter/sec
ZDOT = 7368
291119 ZDOT = 2245
855133
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 12026
72901025
00016717 00000-0 10270-3 0 9149
2 25544 51
6412 116
6683 0022177 327
0723 32
9049 15
58939646 35804
Satellite: ISS
Catalog Number: 25544
Epoch time: 12026
72901025 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 116
6683 deg
Eccentricity:
0022177
Arg of perigee: 327
0723 deg
Mean anomaly: 32
9049 deg
Mean motion: 15
58939646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3580
Checksum: 307
Coasting Arc #16 (Orbit 3594)
---------------------------------------
Vector Time (GMT): 2012/027/16:14:54
090
Vector Time (MET): N/A
Weight (LBS) : 884857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3194963
15 A = 6764012
40 meter
Y = 2967904
97 meter E =
0016978
Z = -5169317
33 I = 51
94715
XDOT = -3739
103221 Wp = 8
91962
YDOT = 6544
116590 meter/sec RA = 111
00144 deg
ZDOT = 1463
216567 TA = 274
98948
MA = 275
18328
Ha = 218
572 n
mi
Hp = 204
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10482162
56 X = 3186648
90
Y = 9737221
02 feet Y = 3003586
42 meter
Z = -16959702
52 Z = -5153816
88
XDOT = -12267
399020 XDOT = -3819
110789
YDOT = 21470
198786 feet/sec YDOT = 6501
856317 meter/sec
ZDOT = 4800
579288 ZDOT = 1444
858047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12016953
80 X = 3662767
52
Y = 7901027
82 feet Y = 2408233
28 meter
Z = -16896369
31 Z = -5150013
37
XDOT = -8095
135982 XDOT = -2467
397447
YDOT = 22296
718948 feet/sec YDOT = 6796
039935 meter/sec
ZDOT = 4724
880036 ZDOT = 1440
143435
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 12027
69055473
00016717 00000-0 10270-3 0 9154
2 25544 51
6420 111
8407 0022317 330
4317 29
5575 15
58950674 35953
Satellite: ISS
Catalog Number: 25544
Epoch time: 12027
69055473 = yrday
fracday
Element set: 915
Inclination: 51
6420 deg
RA of node: 111
8407 deg
Eccentricity:
0022317
Arg of perigee: 330
4317 deg
Mean anomaly: 29
5575 deg
Mean motion: 15
58950674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
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
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