[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 3rd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8880 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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 897)
---------------------------------------
Vector Time (GMT): 2013/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 914999
41 A = 6784552
68 meter
Y = -4257486
02 meter E =
0019787
Z = 5188673
29 I = 51
44416
XDOT = 6972
977576 Wp = 115
94692
YDOT = 2978
085074 meter/sec RA = 210
38494 deg
ZDOT = 1201
896848 TA = 322
43527
MA = 322
57334
Ha = 230
265 n
mi
Hp = 212
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3001966
56 X = 937334
48
Y = -13968130
00 feet Y = -4247129
24 meter
Z = 17023206
34 Z = 5193172
34
XDOT = 22877
223018 XDOT = 6933
319296
YDOT = 9770
620320 feet/sec YDOT = 3055
839489 meter/sec
ZDOT = 3943
231127 ZDOT = 1235
674537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14264105
69 X = 4347699
41
Y = 59925
44 feet Y = 18265
27 meter
Z = 17042350
51 Z = 5194508
43
XDOT = -5023
552680 XDOT = -1531
178857
YDOT = 23299
719981 feet/sec YDOT = 7101
754650 meter/sec
ZDOT = 4083
124633 ZDOT = 1244
536388
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 13002
55047226
00016717 00000-0 10270-3 0 9004
2 25544 51
6449 211
1706 0015722 113
4571 246
8235 15
51830596 8986
Satellite: ISS
Catalog Number: 25544
Epoch time: 13002
55047226 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 211
1706 deg
Eccentricity:
0015722
Arg of perigee: 113
4571 deg
Mean anomaly: 246
8235 deg
Mean motion: 15
51830596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 898
Checksum: 294
Coasting Arc #2 (Orbit 912)
---------------------------------------
Vector Time (GMT): 2013/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1712700
65 A = 6783953
69 meter
Y = 3877724
65 meter E =
0029589
Z = -5321245
35 I = 51
46820
XDOT = -6940
030665 Wp = 103
76107
YDOT = -3200
911266 meter/sec RA = 205
39455 deg
ZDOT = -106
235946 TA = 165
26410
MA = 165
17767
Ha = 230
156 n
mi
Hp = 212
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5619096
63 X = -1730085
80
Y = 12722193
74 feet Y = 3858475
12 meter
Z = -17458154
03 Z = -5329607
58
XDOT = -22769
129477 XDOT = -6903
205536
YDOT = -10501
677381 feet/sec YDOT = -3278
313131 meter/sec
ZDOT = -348
543129 ZDOT = -139
860547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13610674
80 X = -4148533
68
Y = -2636252
47 feet Y = -803529
75 meter
Z = -17493293
20 Z = -5331955
77
XDOT = 5148
394623 XDOT = 1569
230681
YDOT = -23504
017421 feet/sec YDOT = -7164
024510 meter/sec
ZDOT = -487
791800 ZDOT = -148
678941
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 13003
51641039
00016717 00000-0 10270-3 0 9014
2 25544 51
6438 206
3702 0015666 117
1343 243
1408 15
51871724 9139
Satellite: ISS
Catalog Number: 25544
Epoch time: 13003
51641039 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 206
3702 deg
Eccentricity:
0015666
Arg of perigee: 117
1343 deg
Mean anomaly: 243
1408 deg
Mean motion: 15
51871724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 913
Checksum: 277
Coasting Arc #3 (Orbit 928)
---------------------------------------
Vector Time (GMT): 2013/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2483178
16 A = 6784212
54 meter
Y = -3514816
39 meter E =
0017528
Z = 5229497
96 I = 51
49755
XDOT = 6828
338087 Wp = 111
21661
YDOT = 3371
986285 meter/sec RA = 200
40806 deg
ZDOT = -979
589280 TA = 348
14523
MA = 348
18644
Ha = 230
060 n
mi
Hp = 212
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8146909
96 X = 2496893
52
Y = -11531549
84 feet Y = -3486971
41 meter
Z = 17157145
55 Z = 5241594
23
XDOT = 22402
684014 XDOT = 6794
882909
YDOT = 11062
947128 feet/sec YDOT = 3448
158010 meter/sec
ZDOT = -3213
875592 ZDOT = -946
498968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13084395
58 X = 3988123
77
Y = 5138905
59 feet Y = 1566338
42 meter
Z = 17207750
25 Z = 5244922
28
XDOT = -5169
496721 XDOT = -1575
662601
YDOT = 23426
037687 feet/sec YDOT = 7140
256287 meter/sec
ZDOT = -3076
849855 ZDOT = -937
823836
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 13004
54673683
00016717 00000-0 10270-3 0 9029
2 25544 51
6441 201
2516 0015636 121
0641 239
2047 15
51867625 9299
Satellite: ISS
Catalog Number: 25544
Epoch time: 13004
54673683 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 201
2516 deg
Eccentricity:
0015636
Arg of perigee: 121
0641 deg
Mean anomaly: 239
2047 deg
Mean motion: 15
51867625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 929
Checksum: 292
Coasting Arc #4 (Orbit 943)
---------------------------------------
Vector Time (GMT): 2013/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3295760
45 A = 6785200
33 meter
Y = 3218475
55 meter E =
0028069
Z = -5007556
21 I = 51
52913
XDOT = -6495
737835 Wp = 116
13084
YDOT = -3473
269907 meter/sec RA = 195
42241 deg
ZDOT = 2039
715972 TA = 173
81572
MA = 173
78100
Ha = 230
056 n
mi
Hp = 212
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10812862
35 X = -3307179
74
Y = 10559302
97 feet Y = 3181556
64 meter
Z = -16428990
20 Z = -5023594
38
XDOT = -21311
475837 XDOT = -6466
324638
YDOT = -11395
242477 feet/sec YDOT = -3545
744940 meter/sec
ZDOT = 6691
981536 ZDOT = 2008
231462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12895031
07 X = -3930405
47
Y = -7741503
18 feet Y = -2359610
17 meter
Z = -16495935
64 Z = -5027961
18
XDOT = 5147
764915 XDOT = 1569
038746
YDOT = -22578
355166 feet/sec YDOT = -6881
882654 meter/sec
ZDOT = 6561
621246 ZDOT = 1999
982156
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 13005
51265889
00016717 00000-0 10270-3 0 9033
2 25544 51
6432 196
4512 0015718 124
5247 235
7391 15
51897779 9444
Satellite: ISS
Catalog Number: 25544
Epoch time: 13005
51265889 = yrday
fracday
Element set: 903
Inclination: 51
6432 deg
RA of node: 196
4512 deg
Eccentricity:
0015718
Arg of perigee: 124
5247 deg
Mean anomaly: 235
7391 deg
Mean motion: 15
51897779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 944
Checksum: 331
Coasting Arc #5 (Orbit 959)
---------------------------------------
Vector Time (GMT): 2013/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4040446
82 A = 6786839
30 meter
Y = -2943241
47 meter E =
0020911
Z = 4570080
13 I = 51
56439
XDOT = 6068
116584 Wp = 107
71470
YDOT = 3581
882129 meter/sec RA = 190
44264 deg
ZDOT = -3052
789507 TA = 12
80987
MA = 12
75682
Ha = 229
879 n
mi
Hp = 213
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13256059
13 X = 4050858
16
Y = -9656304
04 feet Y = -2898000
72 meter
Z = 14993701
21 Z = 4589733
46
XDOT = 19908
518976 XDOT = 6042
441916
YDOT = 11751
581789 feet/sec YDOT = 3649
596231 meter/sec
ZDOT = -10015
713607 ZDOT = -3023
373163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12807885
24 X = 3903843
42
Y = 10122331
63 feet Y = 3085286
68 meter
Z = 15075638
14 Z = 4595054
51
XDOT = -5279
642445 XDOT = -1609
235017
YDOT = 21441
459432 feet/sec YDOT = 6535
356835 meter/sec
ZDOT = -9893
940550 ZDOT = -3015
673080
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 13006
54296652
00016717 00000-0 10270-3 0 9040
2 25544 51
6431 191
3324 0015622 128
4661 231
7894 15
51900524 9600
Satellite: ISS
Catalog Number: 25544
Epoch time: 13006
54296652 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 191
3324 deg
Eccentricity:
0015622
Arg of perigee: 128
4661 deg
Mean anomaly: 231
7894 deg
Mean motion: 15
51900524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 960
Checksum: 294
Coasting Arc #6 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2013/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4751579
81 A = 6788836
54 meter
Y = 2746984
12 meter E =
0022475
Z = -4021328
76 I = 51
60105
XDOT = -5441
120544 Wp = 124
94474
YDOT = -3654
433204 meter/sec RA = 185
46652 deg
ZDOT = 3935
940342 TA = 186
10493
MA = 186
13237
Ha = 229
939 n
mi
Hp = 213
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15589172
61 X = -4762409
42
Y = 9012415
09 feet Y = 2693788
75 meter
Z = -13193335
81 Z = -4044437
68
XDOT = -17851
445354 XDOT = -5418
971308
YDOT = -11989
610248 feet/sec YDOT = -3715
155690 meter/sec
ZDOT = 12913
190100 ZDOT = 3909
561274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13024653
73 X = -3969914
46
Y = -12331040
24 feet Y = -3758501
06 meter
Z = -13289615
50 Z = -4050674
80
XDOT = 5536
906290 XDOT = 1687
649037
YDOT = -19636
845870 feet/sec YDOT = -5985
310621 meter/sec
ZDOT = 12804
026129 ZDOT = 3902
667164
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 13007
50887166
00016717 00000-0 10270-3 0 9054
2 25544 51
6427 186
5323 0015787 131
8117 228
4385 15
51924815 9759
Satellite: ISS
Catalog Number: 25544
Epoch time: 13007
50887166 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 186
5323 deg
Eccentricity:
0015787
Arg of perigee: 131
8117 deg
Mean anomaly: 228
4385 deg
Mean motion: 15
51924815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 327
Coasting Arc #7 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2013/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5351278
75 A = 6791069
57 meter
Y = -2550104
78 meter E =
0026230
Z = 3280359
95 I = 51
63861
XDOT = 4716
175194 Wp = 116
59859
YDOT = 3786
536842 meter/sec RA = 180
49654 deg
ZDOT = -4732
221215 TA = 25
26758
MA = 25
13951
Ha = 229
740 n
mi
Hp = 213
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17556688
81 X = 5363461
73
Y = -8366485
49 feet Y = -2490195
64 meter
Z = 10762335
80 Z = 3306385
34
XDOT = 15473
015729 XDOT = 4696
470688
YDOT = 12423
021134 feet/sec YDOT = 3839
166363 meter/sec
ZDOT = -15525
660153 ZDOT = -4709
357924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13211163
86 X = 4026762
74
Y = 14189988
57 feet Y = 4325108
52 meter
Z = 10870724
32 Z = 3313396
77
XDOT = -6165
803043 XDOT = -1879
336768
YDOT = 17606
089427 feet/sec YDOT = 5366
336057 meter/sec
ZDOT = -15431
101038 ZDOT = -4703
399597
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 13008
53916011
00016717 00000-0 10270-3 0 9061
2 25544 51
6423 181
4128 0015668 135
7578 224
4829 15
51931206 9913
Satellite: ISS
Catalog Number: 25544
Epoch time: 13008
53916011 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 181
4128 deg
Eccentricity:
0015668
Arg of perigee: 135
7578 deg
Mean anomaly: 224
4829 deg
Mean motion: 15
51931206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 308
Coasting Arc #8 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2013/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5854703
73 A = 6792981
44 meter
Y = 2421427
06 meter E =
0016759
Z = -2477066
06 I = 51
67626
XDOT = -3861
128759 Wp = 121
00288
YDOT = -3914
442366 meter/sec RA = 175
53164 deg
ZDOT = 5317
845384 TA = 211
34229
MA = 211
44229
Ha = 229
789 n
mi
Hp = 213
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19208345
57 X = -5869312
64
Y = 7944314
50 feet Y = 2355874
69 meter
Z = -8126857
16 Z = -2505542
78
XDOT = -12667
745272 XDOT = -3842
902207
YDOT = -12842
658682 feet/sec YDOT = -3957
518610 meter/sec
ZDOT = 17446
999290 ZDOT = 5299
132282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13578665
80 X = -4138777
34
Y = -15676451
39 feet Y = -4778182
38 meter
Z = -8245434
29 Z = -2513208
37
XDOT = 7015
717612 XDOT = 2138
390728
YDOT = -15181
733159 feet/sec YDOT = -4627
392267 meter/sec
ZDOT = 17369
682915 ZDOT = 5294
279352
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 13009
50504752
00016717 00000-0 10270-3 0 9075
2 25544 51
6427 176
6131 0015843 139
0001 221
2344 15
51954697 10064
Satellite: ISS
Catalog Number: 25544
Epoch time: 13009
50504752 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 176
6131 deg
Eccentricity:
0015843
Arg of perigee: 139
0001 deg
Mean anomaly: 221
2344 deg
Mean motion: 15
51954697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 283
Coasting Arc #9 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2013/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6210473
50 A = 6794571
87 meter
Y = -2248666
04 meter E =
0028828
Z = 1521280
99 I = 51
71163
XDOT = 2923
433995 Wp = 131
28625
YDOT = 4133
661453 meter/sec RA = 170
57172 deg
ZDOT = -5772
214595 TA = 32
09792
MA = 31
92271
Ha = 229
579 n
mi
Hp = 213
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20375569
23 X = 6227767
09
Y = -7377513
27 feet Y = -2179120
12 meter
Z = 4991079
38 Z = 1551492
35
XDOT = 9591
318880 XDOT = 2905
032797
YDOT = 13561
881406 feet/sec YDOT = 4166
250880 meter/sec
ZDOT = -18937
711925 ZDOT = -5758
057199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13705172
53 X = 4177336
59
Y = 16747785
82 feet Y = 5104725
12 meter
Z = 5116865
53 Z = 1559620
61
XDOT = -8353
587755 XDOT = -2546
173548
YDOT = 12655
188794 feet/sec YDOT = 3857
301544 meter/sec
ZDOT = -18879
337555 ZDOT = -5754
422087
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 13010
53531623
00016717 00000-0 10270-3 0 9088
2 25544 51
6423 171
4931 0015652 142
8482 217
3756 15
51977314 10226
Satellite: ISS
Catalog Number: 25544
Epoch time: 13010
53531623 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 171
4931 deg
Eccentricity:
0015652
Arg of perigee: 142
8482 deg
Mean anomaly: 217
3756 deg
Mean motion: 15
51977314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 288
Coasting Arc #10 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2013/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6436714
48 A = 6795379
44 meter
Y = 2116807
98 meter E =
0016637
Z = -572596
57 I = 51
74597
XDOT = -1954
367122 Wp = 108
06859
YDOT = -4363
456203 meter/sec RA = 165
61615 deg
ZDOT = 5976
498718 TA = 245
77571
MA = 245
94966
Ha = 229
599 n
mi
Hp = 213
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21117829
66 X = -6457125
21
Y = 6944908
06 feet Y = 2044714
54 meter
Z = -1878597
68 Z = -603914
41
XDOT = -6411
965624 XDOT = -1934
460515
YDOT = -14315
801192 feet/sec YDOT = -4385
200446 meter/sec
ZDOT = 19607
935427 ZDOT = 5967
052654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13850595
73 X = -4221661
58
Y = -17373789
83 feet Y = -5295531
14 meter
Z = -2008987
76 Z = -612339
47
XDOT = 9882
582077 XDOT = 3012
211017
YDOT = -10092
403506 feet/sec YDOT = -3076
164589 meter/sec
ZDOT = 19569
156340 ZDOT = 5964
678853
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 13011
50118581
00016717 00000-0 10270-3 0 9091
2 25544 51
6438 166
6938 0015858 146
1794 214
0372 15
51990272 10378
Satellite: ISS
Catalog Number: 25544
Epoch time: 13011
50118581 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 166
6938 deg
Eccentricity:
0015858
Arg of perigee: 146
1794 deg
Mean anomaly: 214
0372 deg
Mean motion: 15
51990272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 313
Coasting Arc #11 (Orbit 1052)
---------------------------------------
Vector Time (GMT): 2013/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6496766
85 A = 6795409
40 meter
Y = -1886273
97 meter E =
0026694
Z = -471490
15 I = 51
77543
XDOT = 937
848558 Wp = 145
20399
YDOT = 4684
373157 meter/sec RA = 160
66314 deg
ZDOT = -6006
296703 TA = 39
87343
MA = 39
67763
Ha = 229
442 n
mi
Hp = 213
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21314851
86 X = 6519667
03
Y = -6188562
89 feet Y = -1813494
97 meter
Z = -1546883
71 Z = -439874
60
XDOT = 3076
930963 XDOT = 914
573582
YDOT = 15368
678338 feet/sec YDOT = 4694
731087 meter/sec
ZDOT = -19705
697844 ZDOT = -6001
796986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13522459
82 X = 4121645
75
Y = 17611194
74 feet Y = 5367892
16 meter
Z = -1415263
16 Z = -431372
21
XDOT = -11866
442778 XDOT = -3616
891759
YDOT = 7583
654207 feet/sec YDOT = 2311
497802 meter/sec
ZDOT = -19687
506638 ZDOT = -6000
752023
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 13012
53143531
00016717 00000-0 10270-3 0 9100
2 25544 51
6437 161
5737 0015647 149
7807 210
4250 15
52014981 10536
Satellite: ISS
Catalog Number: 25544
Epoch time: 13012
53143531 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 161
5737 deg
Eccentricity:
0015647
Arg of perigee: 149
7807 deg
Mean anomaly: 210
4250 deg
Mean motion: 15
52014981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1053
Checksum: 280
Coasting Arc #12 (Orbit 1068)
---------------------------------------
Vector Time (GMT): 2013/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6431143
16 A = 6794592
56 meter
Y = 1665514
99 meter E =
0020440
Z = 1432525
16 I = 51
80312
XDOT = 10
528342 Wp = 111
50788
YDOT = -5006
606951 meter/sec RA = 155
71218 deg
ZDOT = 5794
290251 TA = 264
05032
MA = 264
28332
Ha = 229
363 n
mi
Hp = 213
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21099551
05 X = -6456248
00
Y = 5464288
01 feet Y = 1593457
47 meter
Z = 4699885
70 Z = 1401223
00
XDOT = 34
541806 XDOT = 38
365991
YDOT = -16425
875823 feet/sec YDOT = -5006
333857 meter/sec
ZDOT = 19010
138618 ZDOT = 5794
408760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13079198
21 X = -3986539
62
Y = -17469744
39 feet Y = -5324778
09 meter
Z = 4569576
41 Z = 1392806
89
XDOT = 13888
713191 XDOT = 4233
279781
YDOT = -5360
190136 feet/sec YDOT = -1633
785954 meter/sec
ZDOT = 19011
177183 ZDOT = 5794
606805
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 13013
56167502
00016717 00000-0 10270-3 0 9119
2 25544 51
6454 156
4550 0015821 153
7910 206
4045 15
52037842 10690
Satellite: ISS
Catalog Number: 25544
Epoch time: 13013
56167502 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 156
4550 deg
Eccentricity:
0015821
Arg of perigee: 153
7910 deg
Mean anomaly: 206
4045 deg
Mean motion: 15
52037842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1069
Checksum: 283
Coasting Arc #13 (Orbit 1083)
---------------------------------------
Vector Time (GMT): 2013/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6205904
55 A = 6793042
87 meter
Y = -1295885
11 meter E =
0020949
Z = -2417357
32 I = 51
82535
XDOT = -956
895086 Wp = 151
27995
YDOT = 5382
158114 meter/sec RA = 150
76080 deg
ZDOT = -5379
002013 TA = 55
66968
MA = 55
47162
Ha = 229
303 n
mi
Hp = 214
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20360579
22 X = 6231676
81
Y = -4251591
58 feet Y = -1226342
63 meter
Z = -7930962
35 Z = -2387147
62
XDOT = -3139
419573 XDOT = -990
879166
YDOT = 17657
999062 feet/sec YDOT = 5371
267640 meter/sec
ZDOT = -17647
644401 ZDOT = -5383
732836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11979737
74 X = 3651424
06
Y = 17061470
42 feet Y = 5200336
18 meter
Z = -7805222
08 Z = -2379031
69
XDOT = -16171
009487 XDOT = -4928
923692
YDOT = 3328
574636 feet/sec YDOT = 1014
549549 meter/sec
ZDOT = -17667
899226 ZDOT = -5385
175684
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 13014
52751674
00016717 00000-0 10270-3 0 9126
2 25544 51
6455 151
6553 0015658 157
0900 203
0954 15
52027597 10840
Satellite: ISS
Catalog Number: 25544
Epoch time: 13014
52751674 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 151
6553 deg
Eccentricity:
0015658
Arg of perigee: 157
0900 deg
Mean anomaly: 203
0954 deg
Mean motion: 15
52027597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1084
Checksum: 300
Coasting Arc #14 (Orbit 1099)
---------------------------------------
Vector Time (GMT): 2013/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5891893
16 A = 6790942
71 meter
Y = 915213
13 meter E =
0022746
Z = 3250858
48 I = 51
84603
XDOT = 1762
648280 Wp = 128
50251
YDOT = -5728
987032 meter/sec RA = 145
80886 deg
ZDOT = 4771
124600 TA = 268
99627
MA = 269
25689
Ha = 229
096 n
mi
Hp = 214
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19330358
14 X = -5917480
90
Y = 3002667
75 feet Y = 849183
19 meter
Z = 10665546
18 Z = 3222174
52
XDOT = 5782
966798 XDOT = 1803
403568
YDOT = -18795
889211 feet/sec YDOT = -5709
048165 meter/sec
ZDOT = 15653
295932 ZDOT = 4779
786182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10716395
60 X = -3266357
38
Y = -16442918
91 feet Y = -5011801
68 meter
Z = 10546180
24 Z = 3214475
74
XDOT = 18271
051833 XDOT = 5569
016599
YDOT = -1767
159188 feet/sec YDOT = -538
630120 meter/sec
ZDOT = 15689
935258 ZDOT = 4782
292267
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 13015
55773566
00016717 00000-0 10270-3 0 9135
2 25544 51
6466 146
5366 0015675 161
1493 199
0242 15
52076107 11003
Satellite: ISS
Catalog Number: 25544
Epoch time: 13015
55773566 = yrday
fracday
Element set: 913
Inclination: 51
6466 deg
RA of node: 146
5366 deg
Eccentricity:
0015675
Arg of perigee: 161
1493 deg
Mean anomaly: 199
0242 deg
Mean motion: 15
52076107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1100
Checksum: 302
Coasting Arc #15 (Orbit 1114)
---------------------------------------
Vector Time (GMT): 2013/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5450841
42 A = 6788630
75 meter
Y = -356949
36 meter E =
0016798
Z = -4030123
81 I = 51
86278
XDOT = -2515
940712 Wp = 140
58756
YDOT = 6058
157220 meter/sec RA = 140
85438 deg
ZDOT = -3961
117212 TA = 88
42157
MA = 88
22916
Ha = 229
044 n
mi
Hp = 214
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17883337
99 X = 5474004
78
Y = -1171093
71 feet Y = -295865
11 meter
Z = -13222190
97 Z = -4003588
20
XDOT = -8254
398663 XDOT = -2564
255533
YDOT = 19875
843899 feet/sec YDOT = 6029
752262 meter/sec
ZDOT = -12995
791379 ZDOT = -3973
456602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8730469
05 X = 2661046
97
Y = 15743917
06 feet Y = 4798745
92 meter
Z = -13111809
87 Z = -3996479
65
XDOT = -20314
275517 XDOT = -6191
791178
YDOT = 458
175682 feet/sec YDOT = 139
651948 meter/sec
ZDOT = -13047
766386 ZDOT = -3976
959194
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 13016
52355902
00016717 00000-0 10270-3 0 9144
2 25544 51
6466 141
7371 0015554 164
5634 195
5995 15
52044869 11158
Satellite: ISS
Catalog Number: 25544
Epoch time: 13016
52355902 = yrday
fracday
Element set: 914
Inclination: 51
6466 deg
RA of node: 141
7371 deg
Eccentricity:
0015554
Arg of perigee: 164
5634 deg
Mean anomaly: 195
5995 deg
Mean motion: 15
52044869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1115
Checksum: 316
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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