[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 21st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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 1192)
---------------------------------------
Vector Time (GMT): 2013/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2929442
14 A = 6784105
73 meter
Y = -3244928
66 meter E =
0011485
Z = 5183246
82 I = 51
94489
XDOT = 4294
869436 Wp = 167
62837
YDOT = -6184
834481 meter/sec RA = 116
07676 deg
ZDOT = -1454
939368 TA = 296
25424
MA = 296
37223
Ha = 227
807 n
mi
Hp = 216
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9611030
64 X = -2918117
51
Y = -10646091
42 feet Y = -3277624
46 meter
Z = 17005402
96 Z = 5169043
33
XDOT = 14090
778990 XDOT = 4370
777994
YDOT = -20291
451710 feet/sec YDOT = -6136
382059 meter/sec
ZDOT = -4773
423122 ZDOT = -1433
891402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4311815
35 X = 1314241
32
Y = -13751823
79 feet Y = -4191555
89 meter
Z = 16946695
64 Z = 5165352
83
XDOT = 23637
641943 XDOT = 7204
753264
YDOT = 1679
754554 feet/sec YDOT = 511
989188 meter/sec
ZDOT = -4685
143521 ZDOT = -1428
031745
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 13021
54584001
00016717 00000-0 10270-3 0 9001
2 25544 51
6477 116
7938 0013855 185
1303 174
9708 15
52036715 11935
Satellite: ISS
Catalog Number: 25544
Epoch time: 13021
54584001 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 116
7938 deg
Eccentricity:
0013855
Arg of perigee: 185
1303 deg
Mean anomaly: 174
9708 deg
Mean motion: 15
52036715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1193
Checksum: 300
Coasting Arc #2 (Orbit 1207)
---------------------------------------
Vector Time (GMT): 2013/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2501268
28 A = 6785515
72 meter
Y = 4052006
60 meter E =
0019445
Z = -4848742
31 I = 51
96214
XDOT = -4357
795023 Wp = 152
48448
YDOT = 5752
201913 meter/sec RA = 111
12264 deg
ZDOT = 2546
308297 TA = 142
57395
MA = 142
43837
Ha = 227
547 n
mi
Hp = 216
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8206260
77 X = 2479325
59
Y = 13293984
91 feet Y = 4079854
93 meter
Z = -15907947
21 Z = -4836644
59
XDOT = -14297
227766 XDOT = -4434
162610
YDOT = 18872
053519 feet/sec YDOT = 5703
043181 meter/sec
ZDOT = 8354
029846 ZDOT = 2524
953597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7070825
86 X = -2155187
72
Y = 13987843
75 feet Y = 4263494
78 meter
Z = -15858095
22 Z = -4833547
42
XDOT = -22555
414590 XDOT = -6874
890367
YDOT = -1984
830856 feet/sec YDOT = -604
976445 meter/sec
ZDOT = 8264
508031 ZDOT = 2519
022048
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 13022
51168287
00016717 00000-0 10270-3 0 9014
2 25544 51
6476 111
9952 0013799 188
1588 171
9342 15
52055771 12083
Satellite: ISS
Catalog Number: 25544
Epoch time: 13022
51168287 = yrday
fracday
Element set: 901
Inclination: 51
6476 deg
RA of node: 111
9952 deg
Eccentricity:
0013799
Arg of perigee: 188
1588 deg
Mean anomaly: 171
9342 deg
Mean motion: 15
52055771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1208
Checksum: 321
Coasting Arc #3 (Orbit 1223)
---------------------------------------
Vector Time (GMT): 2013/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2143475
79 A = 6787413
74 meter
Y = -4758140
73 meter E =
0012186
Z = 4327927
92 I = 51
97919
XDOT = 4392
123158 Wp = 148
44882
YDOT = -5196
980440 meter/sec RA = 106
17165 deg
ZDOT = -3543
926881 TA = 337
42411
MA = 337
47767
Ha = 227
386 n
mi
Hp = 216
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7032400
87 X = -2111133
53
Y = -15610697
94 feet Y = -4781929
83 meter
Z = 14199238
60 Z = 4317593
55
XDOT = 14409
852882 XDOT = 4467
125642
YDOT = -17050
460761 feet/sec YDOT = -5147
445403 meter/sec
ZDOT = -11627
056697 ZDOT = -3522
408777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9420869
20 X = 2871480
93
Y = -14338721
26 feet Y = -4370442
24 meter
Z = 14156808
43 Z = 4314995
21
XDOT = 21098
432516 XDOT = 6430
802231
YDOT = 2489
861632 feet/sec YDOT = 758
909825 meter/sec
ZDOT = -11536
905612 ZDOT = -3516
448831
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 13023
54189916
00016717 00000-0 10270-3 0 9021
2 25544 51
6479 106
8760 0013649 192
2948 167
7872 15
52072765 12247
Satellite: ISS
Catalog Number: 25544
Epoch time: 13023
54189916 = yrday
fracday
Element set: 902
Inclination: 51
6479 deg
RA of node: 106
8760 deg
Eccentricity:
0013649
Arg of perigee: 192
2948 deg
Mean anomaly: 167
7872 deg
Mean motion: 15
52072765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1224
Checksum: 332
Coasting Arc #4 (Orbit 1238)
---------------------------------------
Vector Time (GMT): 2013/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1824523
65 A = 6789683
83 meter
Y = 5439580
75 meter E =
0014065
Z = -3645103
42 I = 51
99397
XDOT = -4398
931048 Wp = 173
11793
YDOT = 4441
914988 meter/sec RA = 101
22479 deg
ZDOT = 4415
002202 TA = 143
99418
MA = 143
89935
Ha = 227
132 n
mi
Hp = 216
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5985969
97 X = 1781268
11
Y = 17846393
53 feet Y = 5459742
05 meter
Z = -11959000
73 Z = -3636344
99
XDOT = -14432
188479 XDOT = -4469
721041
YDOT = 14573
211902 feet/sec YDOT = 4392
327344 meter/sec
ZDOT = 14484
915361 ZDOT = 4393
461265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11624465
10 X = -3543136
96
Y = 14834154
04 feet Y = 4521450
15 meter
Z = -11923211
90 Z = -3634194
99
XDOT = -19061
911214 XDOT = -5810
070538
YDOT = -3336
178923 feet/sec YDOT = -1016
867336 meter/sec
ZDOT = 14394
746700 ZDOT = 4387
518794
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 13024
50771323
00016717 00000-0 10270-3 0 9038
2 25544 51
6474 102
0770 0013657 195
6237 164
4495 15
52092469 12392
Satellite: ISS
Catalog Number: 25544
Epoch time: 13024
50771323 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 102
0770 deg
Eccentricity:
0013657
Arg of perigee: 195
6237 deg
Mean anomaly: 164
4495 deg
Mean motion: 15
52092469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1239
Checksum: 304
Coasting Arc #5 (Orbit 1254)
---------------------------------------
Vector Time (GMT): 2013/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1556687
86 A = 6791845
83 meter
Y = -5967509
16 meter E =
0017324
Z = 2816932
73 I = 52
00667
XDOT = 4432
817132 Wp = 149
91831
YDOT = -3581
859261 meter/sec RA = 96
28183 deg
ZDOT = -5139
273820 TA = 358
26570
MA = 358
27170
Ha = 226
912 n
mi
Hp = 217
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5107243
64 X = -1503525
82
Y = -19578442
14 feet Y = -5984619
89 meter
Z = 9241905
29 Z = 2809499
52
XDOT = 14543
363293 XDOT = 4497
505459
YDOT = -11751
506762 feet/sec YDOT = -3531
926817 meter/sec
ZDOT = -16861
134580 ZDOT = -5117
583071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13303805
46 X = 4054999
90
Y = -15263208
59 feet Y = -4652225
98 meter
Z = 9211697
52 Z = 2807725
41
XDOT = 16835
136228 XDOT = 5131
349522
YDOT = 4554
514675 feet/sec YDOT = 1388
216073 meter/sec
ZDOT = -16770
435919 ZDOT = -5111
628868
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 13025
53789952
00016717 00000-0 10270-3 0 9040
2 25544 51
6476 96
9578 0013436 199
6140 160
4496 15
52116126 12555
Satellite: ISS
Catalog Number: 25544
Epoch time: 13025
53789952 = yrday
fracday
Element set: 904
Inclination: 51
6476 deg
RA of node: 96
9578 deg
Eccentricity:
0013436
Arg of perigee: 199
6140 deg
Mean anomaly: 160
4496 deg
Mean motion: 15
52116126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1255
Checksum: 329
Coasting Arc #6 (Orbit 1269)
---------------------------------------
Vector Time (GMT): 2013/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1316709
77 A = 6793751
80 meter
Y = 6399306
99 meter E =
0006762
Z = -1877672
30 I = 52
01454
XDOT = -4473
809209 Wp = 186
84165
YDOT = 2580
929856 meter/sec RA = 91
34209 deg
ZDOT = 5650
227208 TA = 152
64326
MA = 152
60763
Ha = 226
685 n
mi
Hp = 217
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4319913
95 X = 1254174
52
Y = 20995101
66 feet Y = 6413681
65 meter
Z = -6160342
20 Z = -1871427
73
XDOT = -14677
851735 XDOT = -4529
783850
YDOT = 8467
617638 feet/sec YDOT = 2530
587810 meter/sec
ZDOT = 18537
490841 ZDOT = 5628
358453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14662039
12 X = -4468989
52
Y = 15645781
43 feet Y = 4768834
18 meter
Z = -6135136
41 Z = -1869989
58
XDOT = -14297
420519 XDOT = -4357
853774
YDOT = -6154
083769 feet/sec YDOT = -1875
764733 meter/sec
ZDOT = 18446
165234 ZDOT = 5622
391163
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 13026
50368547
00016717 00000-0 10270-3 0 9052
2 25544 51
6469 92
1581 0013361 203
3775 156
6770 15
52098805 12705
Satellite: ISS
Catalog Number: 25544
Epoch time: 13026
50368547 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 92
1581 deg
Eccentricity:
0013361
Arg of perigee: 203
3775 deg
Mean anomaly: 156
6770 deg
Mean motion: 15
52098805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1270
Checksum: 311
Coasting Arc #7 (Orbit 1285)
---------------------------------------
Vector Time (GMT): 2013/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1084976
31 A = 6794772
10 meter
Y = -6639025
96 meter E =
0020266
Z = 853706
19 I = 52
01842
XDOT = 4576
155261 Wp = 165
93555
YDOT = -1517
057074 meter/sec RA = 86
40496 deg
ZDOT = -5971
397135 TA = 4
87357
MA = 4
85387
Ha = 226
433 n
mi
Hp = 217
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3559633
58 X = -1014803
66
Y = -21781581
23 feet Y = -6650766
49 meter
Z = 2800873
34 Z = 848606
03
XDOT = 15013
632746 XDOT = 4621
785945
YDOT = -4977
221370 feet/sec YDOT = -1465
628484 meter/sec
ZDOT = -19591
197949 ZDOT = -5949
056287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15486590
27 X = 4720312
71
Y = -15728563
58 feet Y = -4794066
18 meter
Z = 2780462
72 Z = 847485
04
XDOT = 11795
622090 XDOT = 3595
305613
YDOT = 8161
213030 feet/sec YDOT = 2487
537731 meter/sec
ZDOT = -19498
032300 ZDOT = -5943
000245
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 13027
53384226
00016717 00000-0 10270-3 0 9069
2 25544 51
6471 87
0384 0013221 206
7375 153
3097 15
52156575 12862
Satellite: ISS
Catalog Number: 25544
Epoch time: 13027
53384226 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 87
0384 deg
Eccentricity:
0013221
Arg of perigee: 206
7375 deg
Mean anomaly: 153
3097 deg
Mean motion: 15
52156575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1286
Checksum: 305
Coasting Arc #8 (Orbit 1301)
---------------------------------------
Vector Time (GMT): 2013/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 850014
53 A = 6795134
99 meter
Y = 6740519
04 meter E =
0003827
Z = 204116
42 I = 52
01571
XDOT = -4700
410450 Wp = 137
04742
YDOT = 408
033888 meter/sec RA = 81
46838 deg
ZDOT = 6030
564307 TA = 225
13614
MA = 225
16723
Ha = 226
208 n
mi
Hp = 217
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2788761
58 X = 773585
93
Y = 22114563
78 feet Y = 6749597
10 meter
Z = 669673
29 Z = 208059
86
XDOT = -15421
294126 XDOT = -4733
918000
YDOT = 1338
693857 feet/sec YDOT = 355
283710 meter/sec
ZDOT = 19785
315967 ZDOT = 6007
649271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15957434
33 X = -4863825
98
Y = 15561821
94 feet Y = 4743243
33 meter
Z = 685253
51 Z = 208865
27
XDOT = -9310
460283 XDOT = -2837
828294
YDOT = -10423
947293 feet/sec YDOT = -3177
219135 meter/sec
ZDOT = 19689
893875 ZDOT = 6001
479653
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 13028
56398543
00016717 00000-0 10270-3 0 9071
2 25544 51
6463 81
9181 0013020 210
6727 149
3665 15
52124412 13023
Satellite: ISS
Catalog Number: 25544
Epoch time: 13028
56398543 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 81
9181 deg
Eccentricity:
0013020
Arg of perigee: 210
6727 deg
Mean anomaly: 149
3665 deg
Mean motion: 15
52124412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1302
Checksum: 288
Coasting Arc #9 (Orbit 1316)
---------------------------------------
Vector Time (GMT): 2013/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -569633
71 A = 6794280
25 meter
Y = -6637761
56 meter E =
0018020
Z = -1270187
26 I = 52
00864
XDOT = 4886
189141 Wp = 185
49712
YDOT = 702
760348 meter/sec RA = 76
53122 deg
ZDOT = -5874
351282 TA = 8
25007
MA = 8
22048
Ha = 225
973 n
mi
Hp = 217
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1868877
01 X = -489196
42
Y = -21777432
95 feet Y = -6643681
86 meter
Z = -4167281
05 Z = -1272758
82
XDOT = 16030
804268 XDOT = 4906
502985
YDOT = 2305
644186 feet/sec YDOT = 757
514152 meter/sec
ZDOT = -19272
806043 ZDOT = -5850
565800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16002995
58 X = 4877713
05
Y = -14885260
80 feet Y = -4537027
49 meter
Z = -4177159
53 Z = -1273198
22
XDOT = 7063
336016 XDOT = 2152
904818
YDOT = 12964
662231 feet/sec YDOT = 3951
629048 meter/sec
ZDOT = -19173
897771 ZDOT = -5844
204041
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 13029
52972764
00016717 00000-0 10270-3 0 9082
2 25544 51
6470 77
1179 0013056 213
8224 146
2096 15
52193055 13170
Satellite: ISS
Catalog Number: 25544
Epoch time: 13029
52972764 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 77
1179 deg
Eccentricity:
0013056
Arg of perigee: 213
8224 deg
Mean anomaly: 146
2096 deg
Mean motion: 15
52193055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1317
Checksum: 306
Coasting Arc #10 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2013/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 249926
47 A = 6792786
37 meter
Y = 6395661
01 meter E =
0008068
Z = 2281126
78 I = 51
99453
XDOT = -5078
134253 Wp = 137
79294
YDOT = -1753
989422 meter/sec RA = 71
59136 deg
ZDOT = 5457
086344 TA = 247
42463
MA = 247
51002
Ha = 225
721 n
mi
Hp = 218
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 819968
73 X = 167309
36
Y = 20983139
78 feet Y = 6397994
01 meter
Z = 7484011
75 Z = 2282139
91
XDOT = -16660
545448 XDOT = -5084
651930
YDOT = -5754
558472 feet/sec YDOT = -1810
812497 meter/sec
ZDOT = 17903
826587 ZDOT = 5432
401917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15802173
46 X = -4816502
47
Y = 13827677
62 feet Y = 4214676
14 meter
Z = 7487428
21 Z = 2282168
12
XDOT = -5096
438745 XDOT = -1553
394530
YDOT = -15493
434568 feet/sec YDOT = -4722
398856 meter/sec
ZDOT = 17801
309478 ZDOT = 5425
839129
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 13030
55984070
00016717 00000-0 10270-3 0 9091
2 25544 51
6459 71
9973 0012836 217
4212 142
6047 15
52183945 13334
Satellite: ISS
Catalog Number: 25544
Epoch time: 13030
55984070 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 71
9973 deg
Eccentricity:
0012836
Arg of perigee: 217
4212 deg
Mean anomaly: 142
6047 deg
Mean motion: 15
52183945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 309
Coasting Arc #11 (Orbit 1347)
---------------------------------------
Vector Time (GMT): 2013/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 161238
89 A = 6790447
81 meter
Y = -5970203
48 meter E =
0011206
Z = -3215872
03 I = 51
97793
XDOT = 5293
657123 Wp = 200
46050
YDOT = 2740
042424 meter/sec RA = 66
64783 deg
ZDOT = -4826
574605 TA = 16
53978
MA = 16
50325
Ha = 225
485 n
mi
Hp = 218
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 528999
00 X = 243608
61
Y = -19587281
74 feet Y = -5967940
00 meter
Z = -10550761
25 Z = -3214888
40
XDOT = 17367
641481 XDOT = 5286
069815
YDOT = 8989
640500 feet/sec YDOT = 2799
196764 meter/sec
ZDOT = -15835
218520 ZDOT = -4800
877424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15374151
75 X = 4686041
45
Y = -12152332
10 feet Y = -3704030
82 meter
Z = -10545913
50 Z = -3214394
43
XDOT = 3474
803375 XDOT = 1059
120069
YDOT = 18030
803076 feet/sec YDOT = 5495
788778 meter/sec
ZDOT = -15728
614343 ZDOT = -4794
081652
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 13031
52555581
00016717 00000-0 10270-3 0 9102
2 25544 51
6472 67
1968 0012897 221
1123 138
9058 15
52239419 13484
Satellite: ISS
Catalog Number: 25544
Epoch time: 13031
52555581 = yrday
fracday
Element set: 910
Inclination: 51
6472 deg
RA of node: 67
1968 deg
Eccentricity:
0012897
Arg of perigee: 221
1123 deg
Mean anomaly: 138
9058 deg
Mean motion: 15
52239419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1348
Checksum: 310
Coasting Arc #12 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2013/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -634513
10 A = 6788035
05 meter
Y = 5443715
61 meter E =
0011324
Z = 4012044
78 I = 51
95574
XDOT = -5470
968930 Wp = 170
91855
YDOT = -3583
510175 meter/sec RA = 61
69909 deg
ZDOT = 3984
602837 TA = 237
67603
MA = 237
78573
Ha = 225
209 n
mi
Hp = 218
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2081735
90 X = -714827
94
Y = 17859959
34 feet Y = 5436171
19 meter
Z = 13162876
59 Z = 4008767
10
XDOT = -17949
373130 XDOT = -5449
846661
YDOT = -11756
923145 feet/sec YDOT = -3644
571713 meter/sec
ZDOT = 13072
843955 ZDOT = 3958
077106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14890461
37 X = -4538612
63
Y = 10097680
20 feet Y = 3077772
92 meter
Z = 13148540
11 Z = 4007675
03
XDOT = -2237
092094 XDOT = -681
865670
YDOT = -20231
447901 feet/sec YDOT = -6166
545320 meter/sec
ZDOT = 12962
904828 ZDOT = 3951
093392
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 13032
55563916
00016717 00000-0 10270-3 0 9118
2 25544 51
6460 62
0760 0012734 224
6592 135
3534 15
52243032 13647
Satellite: ISS
Catalog Number: 25544
Epoch time: 13032
55563916 = yrday
fracday
Element set: 911
Inclination: 51
6460 deg
RA of node: 62
0760 deg
Eccentricity:
0012734
Arg of perigee: 224
6592 deg
Mean anomaly: 135
3534 deg
Mean motion: 15
52243032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 279
Coasting Arc #13 (Orbit 1378)
---------------------------------------
Vector Time (GMT): 2013/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1218773
37 A = 6785578
84 meter
Y = -4785145
94 meter E =
0004979
Z = -4651942
03 I = 51
93379
XDOT = 5604
016557 Wp = 177
08642
YDOT = 4307
648634 meter/sec RA = 56
74564 deg
ZDOT = -2967
764261 TA = 63
48543
MA = 63
43438
Ha = 224
998 n
mi
Hp = 218
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3998600
31 X = 1294788
99
Y = -15699297
71 feet Y = -4771091
96 meter
Z = -15262277
00 Z = -4645836
61
XDOT = 18385
881093 XDOT = 5569
847488
YDOT = 14132
705493 feet/sec YDOT = 4370
125130 meter/sec
ZDOT = -9736
759386 ZDOT = -2940
623803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14401873
23 X = 4389690
96
Y = -7472391
13 feet Y = -2277584
82 meter
Z = -15236248
57 Z = -4644008
56
XDOT = 1308
451270 XDOT = 398
815947
YDOT = 22112
597026 feet/sec YDOT = 6739
919573 meter/sec
ZDOT = -9624
362681 ZDOT = -2933
505745
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 13033
52132744
00016717 00000-0 10270-3 0 9128
2 25544 51
6473 57
2759 0012804 228
5131 131
4923 15
52278153 13792
Satellite: ISS
Catalog Number: 25544
Epoch time: 13033
52132744 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 57
2759 deg
Eccentricity:
0012804
Arg of perigee: 228
5131 deg
Mean anomaly: 131
4923 deg
Mean motion: 15
52278153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1379
Checksum: 294
Coasting Arc #14 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2013/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1859822
77 A = 6783773
65 meter
Y = 4088932
96 meter E =
0012190
Z = 5091155
24 I = 51
90916
XDOT = -5639
607002 Wp = 206
81005
YDOT = -4849
612894 meter/sec RA = 51
78678 deg
ZDOT = 1825
875891 TA = 225
50755
MA = 225
60726
Ha = 224
677 n
mi
Hp = 218
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6101780
73 X = -1930139
11
Y = 13415134
39 feet Y = 4067742
15 meter
Z = 16703265
22 Z = 5081949
63
XDOT = -18502
647644 XDOT = -5593
827993
YDOT = -15910
803457 feet/sec YDOT = -4912
422535 meter/sec
ZDOT = 5990
406468 ZDOT = 1798
590657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14042112
58 X = -4280035
91
Y = 4616588
32 feet Y = 1407136
12 meter
Z = 16664417
62 Z = 5079314
49
XDOT = -678
544233 XDOT = -206
820282
YDOT = -23385
276176 feet/sec YDOT = -7127
832178 meter/sec
ZDOT = 5877
485834 ZDOT = 1791
457682
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 13034
55138122
00016717 00000-0 10270-3 0 9139
2 25544 51
6462 52
1549 0012674 232
2936 127
7067 15
52292847 13952
Satellite: ISS
Catalog Number: 25544
Epoch time: 13034
55138122 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 52
1549 deg
Eccentricity:
0012674
Arg of perigee: 232
2936 deg
Mean anomaly: 127
7067 deg
Mean motion: 15
52292847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 305
Coasting Arc #15 (Orbit 1409)
---------------------------------------
Vector Time (GMT): 2013/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2592170
25 A = 6782752
00 meter
Y = -3329289
30 meter E =
0007263
Z = -5313615
19 I = 51
88678
XDOT = 5553
505135 Wp = 145
53627
YDOT = 5248
016371 meter/sec RA = 46
82454 deg
ZDOT = -585
213072 TA = 118
93027
MA = 118
85741
Ha = 224
470 n
mi
Hp = 219
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8504495
59 X = 2655018
26
Y = -10922865
14 feet Y = -3299950
58 meter
Z = -17433120
71 Z = -5300870
16
XDOT = 18220
161204 XDOT = 5497
250733
YDOT = 17217
901480 feet/sec YDOT = 5309
804619 meter/sec
ZDOT = -1919
990393 ZDOT = -558
371513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13840244
52 X = 4218506
53
Y = -1394629
33 feet Y = -425083
02 meter
Z = -17379636
54 Z = -5297313
22
XDOT = 179
160659 XDOT = 54
608169
YDOT = 24065
950218 feet/sec YDOT = 7335
301627 meter/sec
ZDOT = -1808
975782 ZDOT = -551
375818
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 13035
51704216
00016717 00000-0 10270-3 0 9140
2 25544 51
6468 47
3548 0012754 236
2325 123
7612 15
52307877 14108
Satellite: ISS
Catalog Number: 25544
Epoch time: 13035
51704216 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 47
3548 deg
Eccentricity:
0012754
Arg of perigee: 236
2325 deg
Mean anomaly: 123
7612 deg
Mean motion: 15
52307877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 292
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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