[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 17th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 123 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 362 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
053/10:36:18
424 -1
3 1
9 1
9
N/A -0
6 -0
2 223
8
000/00:04:36
848 -1
3 -0
0 219
5
Coasting Arc #1 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2013/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5554006
09 A = 6789043
12 meter
Y = -1947477
53 meter E =
0007878
Z = -3379296
36 I = 51
60675
XDOT = 4334
574840 Wp = 283
49987
YDOT = -4297
083002 meter/sec RA = 352
25987 deg
ZDOT = -4636
747277 TA = 295
94259
MA = 296
02375
Ha = 222
089 n
mi
Hp = 218
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18221804
75 X = -5515400
68
Y = -6389361
97 feet Y = -2009370
31 meter
Z = -11086930
30 Z = -3406182
98
XDOT = 14221
046064 XDOT = 4404
827378
YDOT = -14098
041346 feet/sec YDOT = -4248
218606 meter/sec
ZDOT = -15212
425451 ZDOT = -4615
519596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11162642
99 X = -3402373
58
Y = -15676936
09 feet Y = -4778330
12 meter
Z = -11198536
28 Z = -3413313
86
XDOT = 18678
434902 XDOT = 5693
186958
YDOT = -2471
324656 feet/sec YDOT = -753
259755 meter/sec
ZDOT = -15123
527099 ZDOT = -4609
651060
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 13046
52503624
00016717 00000-0 10270-3 0 9008
2 25544 51
6476 352
6416 0012658 278
7157 81
2561 15
52532453 15810
Satellite: ISS
Catalog Number: 25544
Epoch time: 13046
52503624 = yrday
fracday
Element set: 900
Inclination: 51
6476 deg
RA of node: 352
6416 deg
Eccentricity:
0012658
Arg of perigee: 278
7157 deg
Mean anomaly: 81
2561 deg
Mean motion: 15
52532453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 302
Coasting Arc #2 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2013/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4777671
36 A = 6786272
47 meter
Y = 2347724
46 meter E =
0002777
Z = 4211529
17 I = 51
56779
XDOT = -5279
140965 Wp = 265
44217
YDOT = 4172
465206 meter/sec RA = 347
28294 deg
ZDOT = 3664
722126 TA = 146
93571
MA = 146
91835
Ha = 222
236 n
mi
Hp = 218
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15674774
79 X = 4730605
28
Y = 7702508
08 feet Y = 2400888
48 meter
Z = 13817352
91 Z = 4234623
94
XDOT = -17320
016288 XDOT = -5343
208027
YDOT = 13689
190309 feet/sec YDOT = 4113
072537 meter/sec
ZDOT = 12023
366555 ZDOT = 3638
920962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8571784
74 X = 2612679
99
Y = 15129306
68 feet Y = 4611412
68 meter
Z = 13913124
12 Z = 4240720
23
XDOT = -20976
903360 XDOT = -6393
760144
YDOT = 932
829839 feet/sec YDOT = 284
326535 meter/sec
ZDOT = 11915
460045 ZDOT = 3631
832222
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 13047
55492527
00016717 00000-0 10270-3 0 9012
2 25544 51
6478 347
5204 0012694 281
9349 78
0379 15
52564429 15975
Satellite: ISS
Catalog Number: 25544
Epoch time: 13047
55492527 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 347
5204 deg
Eccentricity:
0012694
Arg of perigee: 281
9349 deg
Mean anomaly: 78
0379 deg
Mean motion: 15
52564429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1597
Checksum: 341
Coasting Arc #3 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2013/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3876508
14 A = 6783888
40 meter
Y = -2784940
89 meter E =
0007134
Z = -4822456
70 I = 51
53044
XDOT = 6022
498305 Wp = 351
28988
YDOT = -4018
357688 meter/sec RA = 342
29837 deg
ZDOT = -2513
184606 TA = 253
90920
MA = 253
98776
Ha = 222
555 n
mi
Hp = 218
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12718202
55 X = -3821652
32
Y = -9136945
17 feet Y = -2827983
95 meter
Z = -15821708
32 Z = -4841154
82
XDOT = 19758
852707 XDOT = 6079
193053
YDOT = -13183
588214 feet/sec YDOT = -3950
693452 meter/sec
ZDOT = -8245
356318 ZDOT = -2483
790305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5560872
56 X = -1694953
96
Y = -14555321
34 feet Y = -4436461
94 meter
Z = -15899126
21 Z = -4846053
67
XDOT = 22733
416822 XDOT = 6929
145447
YDOT = 213
472632 feet/sec YDOT = 65
066458 meter/sec
ZDOT = -8122
525062 ZDOT = -2475
745639
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 13048
52043347
00016717 00000-0 10270-3 0 9023
2 25544 51
6479 342
7188 0012652 286
1797 73
7962 15
52582613 16125
Satellite: ISS
Catalog Number: 25544
Epoch time: 13048
52043347 = yrday
fracday
Element set: 902
Inclination: 51
6479 deg
RA of node: 342
7188 deg
Eccentricity:
0012652
Arg of perigee: 286
1797 deg
Mean anomaly: 73
7962 deg
Mean motion: 15
52582613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 322
Coasting Arc #4 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2013/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2864223
07 A = 6782193
73 meter
Y = 3287883
12 meter E =
0008999
Z = 5201901
76 I = 51
49632
XDOT = -6547
085605 Wp = 282
43585
YDOT = 3785
890537 meter/sec RA = 337
30809 deg
ZDOT = 1215
686290 TA = 155
88438
MA = 155
84222
Ha = 222
794 n
mi
Hp = 218
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9397057
32 X = 2801975
30
Y = 10787018
10 feet Y = 3319564
82 meter
Z = 17066606
83 Z = 5215664
38
XDOT = -21479
939649 XDOT = -6594
839038
YDOT = 12420
900713 feet/sec YDOT = 3712
409959 meter/sec
ZDOT = 3988
472081 ZDOT = 1183
765432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2114304
08 X = 644439
88
Y = 14080184
90 feet Y = 4291640
36 meter
Z = 17123423
31 Z = 5219219
43
XDOT = -23788
868436 XDOT = -7250
847099
YDOT = -1101
602493 feet/sec YDOT = -335
768440 meter/sec
ZDOT = 3855
164282 ZDOT = 1175
054073
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 13049
55029193
00016717 00000-0 10270-3 0 9031
2 25544 51
6480 337
5974 0012786 289
4358 70
5412 15
52622964 16285
Satellite: ISS
Catalog Number: 25544
Epoch time: 13049
55029193 = yrday
fracday
Element set: 903
Inclination: 51
6480 deg
RA of node: 337
5974 deg
Eccentricity:
0012786
Arg of perigee: 289
4358 deg
Mean anomaly: 70
5412 deg
Mean motion: 15
52622964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1628
Checksum: 330
Coasting Arc #5 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2013/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1826133
00 A = 6781749
37 meter
Y = -3813068
01 meter E =
0005682
Z = -5305285
90 I = 51
46727
XDOT = 6836
415102 Wp = 33
95713
YDOT = -3461
710586 meter/sec RA = 332
31296 deg
ZDOT = 139
562313 TA = 237
34933
MA = 237
40417
Ha = 223
086 n
mi
Hp = 218
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5991250
00 X = -1757587
51
Y = -12510065
67 feet Y = -3833105
93 meter
Z = -17405793
65 Z = -5313990
31
XDOT = 22429
183405 XDOT = 6873
938643
YDOT = -11357
318195 feet/sec YDOT = -3385
051686 meter/sec
ZDOT = 457
881603 ZDOT = 172
863746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1451287
81 X = 442352
52
Y = -13749414
16 feet Y = -4190821
44 meter
Z = -17441497
81 Z = -5316168
53
XDOT = 24062
686890 XDOT = 7334
306964
YDOT = 1802
196106 feet/sec YDOT = 549
309373 meter/sec
ZDOT = 596
885937 ZDOT = 181
930834
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 13050
51577255
00016717 00000-0 10270-3 0 9047
2 25544 51
6484 332
7953 0012694 293
5145 66
4672 15
52620975 16430
Satellite: ISS
Catalog Number: 25544
Epoch time: 13050
51577255 = yrday
fracday
Element set: 904
Inclination: 51
6484 deg
RA of node: 332
7953 deg
Eccentricity:
0012694
Arg of perigee: 293
5145 deg
Mean anomaly: 66
4672 deg
Mean motion: 15
52620975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 321
Coasting Arc #6 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2013/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 770593
59 A = 6782434
93 meter
Y = 4370623
21 meter E =
0011378
Z = 5137304
62 I = 51
44311
XDOT = -6887
374213 Wp = 318
75107
YDOT = 2992
383861 meter/sec RA = 327
31669 deg
ZDOT = -1506
232490 TA = 145
85136
MA = 145
77811
Ha = 223
381 n
mi
Hp = 218
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2528194
20 X = 696707
91
Y = 14339315
00 feet Y = 4378827
57 meter
Z = 16854673
93 Z = 5140868
38
XDOT = -22596
372091 XDOT = -6913
007067
YDOT = 9817
532353 feet/sec YDOT = 2915
221532 meter/sec
ZDOT = -4941
707643 ZDOT = -1539
752499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5124662
91 X = -1561997
26
Y = 13611211
71 feet Y = 4148697
33 meter
Z = 16868921
13 Z = 5141647
16
XDOT = -23447
134415 XDOT = -7146
686570
YDOT = -2503
855519 feet/sec YDOT = -763
175162 meter/sec
ZDOT = -5081
555059 ZDOT = -1548
857982
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 13051
54560172
00016717 00000-0 10270-3 0 9052
2 25544 51
6483 327
6738 0012799 297
2752 62
7096 15
52658696 16591
Satellite: ISS
Catalog Number: 25544
Epoch time: 13051
54560172 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 327
6738 deg
Eccentricity:
0012799
Arg of perigee: 297
2752 deg
Mean anomaly: 62
7096 deg
Mean motion: 15
52658696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1659
Checksum: 347
Coasting Arc #7 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2013/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 212576
23 A = 6784269
10 meter
Y = -4893064
99 meter E =
0003116
Z = -4692461
14 I = 51
42470
XDOT = 6730
379025 Wp = 343
99800
YDOT = -2383
525430 meter/sec RA = 322
32031 deg
ZDOT = 2792
812501 TA = 313
76094
MA = 313
78673
Ha = 223
611 n
mi
Hp = 218
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 697428
59 X = 290069
96
Y = -16053362
83 feet Y = -4890254
77 meter
Z = -15395213
71 Z = -4691240
02
XDOT = 22081
296015 XDOT = 6742
965452
YDOT = -7819
965322 feet/sec YDOT = -2308
191591 meter/sec
ZDOT = 9162
770674 ZDOT = 2825
538083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8533700
58 X = 2601071
94
Y = -13621636
36 feet Y = -4151874
76 meter
Z = -15389491
46 Z = -4690717
00
XDOT = 22044
195831 XDOT = 6719
070889
YDOT = 3313
413179 feet/sec YDOT = 1009
928337 meter/sec
ZDOT = 9299
228807 ZDOT = 2834
404940
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 13052
51105381
00016717 00000-0 10270-3 0 9068
2 25544 51
6490 322
8716 0012764 300
9474 59
0423 15
52662970 16747
Satellite: ISS
Catalog Number: 25544
Epoch time: 13052
51105381 = yrday
fracday
Element set: 906
Inclination: 51
6490 deg
RA of node: 322
8716 deg
Eccentricity:
0012764
Arg of perigee: 300
9474 deg
Mean anomaly: 59
0423 deg
Mean motion: 15
52662970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 299
Coasting Arc #8 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2013/053/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4751211
48 A = 6794528
27 meter
Y = 4832630
46 meter E =
0002635
Z = 462126
92 I = 51
43228
XDOT = -3698
828532 Wp = 187
75610
YDOT = -3066
492400 meter/sec RA = 317
63011 deg
ZDOT = -5967
444969 TA = 347
25218
MA = 347
25884
Ha = 223
849 n
mi
Hp = 219
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15587964
17 X = -4807142
70
Y = 15855086
81 feet Y = 4779186
73 meter
Z = 1516164
43 Z = 438910
33
XDOT = -12135
264213 XDOT = -3635
275877
YDOT = -10060
670603 feet/sec YDOT = -3107
500051 meter/sec
ZDOT = -19578
231524 ZDOT = -5985
258585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22206407
01 X = -6768512
86
Y = -1236617
57 feet Y = -376921
03 meter
Z = 1418951
75 Z = 432496
49
XDOT = -471
999037 XDOT = -143
865306
YDOT = -14047
345108 feet/sec YDOT = -4281
630789 meter/sec
ZDOT = -19651
941293 ZDOT = -5989
911706
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 13053
47650126
00016717 00000-0 10270-3 0 9077
2 25544 51
6480 318
0699 0011647 299
3710 60
6278 15
52312913 16897
Satellite: ISS
Catalog Number: 25544
Epoch time: 13053
47650126 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 318
0699 deg
Eccentricity:
0011647
Arg of perigee: 299
3710 deg
Mean anomaly: 60
6278 deg
Mean motion: 15
52312913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 318
Coasting Arc #9 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2013/054/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4949556
55 A = 6794355
14 meter
Y = -4592721
88 meter E =
0014520
Z = 662254
78 I = 51
40959
XDOT = 2842
965330 Wp = 2
27674
YDOT = 3920
217155 meter/sec RA = 312
65245 deg
ZDOT = 5948
603501 TA = 4
89732
MA = 4
88313
Ha = 224
044 n
mi
Hp = 219
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16238702
60 X = 4997328
50
Y = -15067985
18 feet Y = -4537105
67 meter
Z = 2172751
89 Z = 686415
11
XDOT = 9327
314076 XDOT = 2770
021300
YDOT = 12861
604839 feet/sec YDOT = 3951
601606 meter/sec
ZDOT = 19516
415687 ZDOT = 5962
236558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22065167
04 X = 6725462
91
Y = 1848917
96 feet Y = 563550
19 meter
Z = 2273850
55 Z = 693069
65
XDOT = -3175
160857 XDOT = -967
789029
YDOT = 13859
219145 feet/sec YDOT = 4224
289995 meter/sec
ZDOT = 19572
628819 ZDOT = 5965
737264
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 13054
50652460
00016717 00000-0 10270-3 0 9086
2 25544 51
6477 312
9491 0011742 303
6052 56
3979 15
52333193 17052
Satellite: ISS
Catalog Number: 25544
Epoch time: 13054
50652460 = yrday
fracday
Element set: 908
Inclination: 51
6477 deg
RA of node: 312
9491 deg
Eccentricity:
0011742
Arg of perigee: 303
6052 deg
Mean anomaly: 56
3979 deg
Mean motion: 15
52333193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 302
Coasting Arc #10 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2013/055/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5027956
13 A = 6793129
27 meter
Y = 4216145
78 meter E =
0004975
Z = -1756683
29 I = 51
38640
XDOT = -2018
396570 Wp = 283
80577
YDOT = -4766
149939 meter/sec RA = 307
67252 deg
ZDOT = -5647
350335 TA = 275
52179
MA = 275
57853
Ha = 224
259 n
mi
Hp = 219
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16495919
07 X = -5066194
98
Y = 13832499
29 feet Y = 4159706
03 meter
Z = -5763396
62 Z = -1781201
40
XDOT = -6622
035992 XDOT = -1937
517776
YDOT = -15636
974866 feet/sec YDOT = -4788
269272 meter/sec
ZDOT = -18528
052279 ZDOT = -5656
958371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21355834
45 X = -6509258
34
Y = -2487845
08 feet Y = -758295
18 meter
Z = -5865925
73 Z = -1787934
16
XDOT = 6732
923226 XDOT = 2052
194999
YDOT = -13905
497721 feet/sec YDOT = -4238
395705 meter/sec
ZDOT = -18567
420486 ZDOT = -5659
349764
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 13055
47215737
00016717 00000-0 10270-3 0 9096
2 25544 51
6483 308
1489 0011740 306
6963 53
3109 15
52357011 17209
Satellite: ISS
Catalog Number: 25544
Epoch time: 13055
47215737 = yrday
fracday
Element set: 909
Inclination: 51
6483 deg
RA of node: 308
1489 deg
Eccentricity:
0011740
Arg of perigee: 306
6963 deg
Mean anomaly: 53
3109 deg
Mean motion: 15
52357011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 299
Coasting Arc #11 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2013/056/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4990472
40 A = 6791065
34 meter
Y = -3655075
10 meter E =
0010870
Z = 2784806
12 I = 51
36131
XDOT = 1253
051462 Wp = 22
92832
YDOT = 5591
996158 meter/sec RA = 302
68764 deg
ZDOT = 5097
111603 TA = 8
77726
MA = 8
75827
Ha = 224
374 n
mi
Hp = 218
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16372940
95 X = 5017445
77
Y = -11991716
20 feet Y = -3599117
35 meter
Z = 9136503
00 Z = 2809114
84
XDOT = 4111
061226 XDOT = 1165
667554
YDOT = 18346
444088 feet/sec YDOT = 5605
520587 meter/sec
ZDOT = 16722
807096 ZDOT = 5102
985773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19977440
48 X = 6089123
86
Y = 3303009
77 feet Y = 1006757
38 meter
Z = 9238080
88 Z = 2815767
05
XDOT = -10091
432731 XDOT = -3075
868697
YDOT = 14225
759964 feet/sec YDOT = 4336
011637 meter/sec
ZDOT = 16746
547653 ZDOT = 5104
347725
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 13056
50215230
00016717 00000-0 10270-3 0 9101
2 25544 51
6478 303
0277 0011770 311
0970 48
9165 15
52377945 17360
Satellite: ISS
Catalog Number: 25544
Epoch time: 13056
50215230 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 303
0277 deg
Eccentricity:
0011770
Arg of perigee: 311
0970 deg
Mean anomaly: 48
9165 deg
Mean motion: 15
52377945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 295
Coasting Arc #12 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2013/057/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4880199
59 A = 6788491
43 meter
Y = 2958995
60 meter E =
0009821
Z = -3681689
45 I = 51
33770
XDOT = -573
015960 Wp = 342
53177
YDOT = -6311
573089 meter/sec RA = 297
69786 deg
ZDOT = -4300
904418 TA = 241
43463
MA = 241
53351
Ha = 224
618 n
mi
Hp = 218
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16011153
50 X = -4895040
65
Y = 9707990
82 feet Y = 2904338
68 meter
Z = -12079033
63 Z = -3705433
05
XDOT = -1879
973622 XDOT = -481
503737
YDOT = -20707
260790 feet/sec YDOT = -6317
469806 meter/sec
ZDOT = -14110
578799 ZDOT = -4303
464925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18154392
15 X = -5533458
73
Y = -4314567
75 feet Y = -1315080
25 meter
Z = -12178165
96 Z = -3711904
98
XDOT = 12981
249149 XDOT = 3956
684741
YDOT = -14653
203486 feet/sec YDOT = -4466
296422 meter/sec
ZDOT = -14120
455698 ZDOT = -4303
914897
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 13057
46775796
00016717 00000-0 10270-3 0 9116
2 25544 51
6481 298
2273 0011882 314
2677 45
7499 15
52416048 17518
Satellite: ISS
Catalog Number: 25544
Epoch time: 13057
46775796 = yrday
fracday
Element set: 911
Inclination: 51
6481 deg
RA of node: 298
2273 deg
Eccentricity:
0011882
Arg of perigee: 314
2677 deg
Mean anomaly: 45
7499 deg
Mean motion: 15
52416048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 338
Coasting Arc #13 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2013/058/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4706543
21 A = 6785905
16 meter
Y = -2082243
62 meter E =
0005632
Z = 4419002
08 I = 51
31535
XDOT = -31
352089 Wp = 6
98810
YDOT = 6920
626460 meter/sec RA = 292
70107 deg
ZDOT = 3299
451225 TA = 49
57999
MA = 49
53087
Ha = 224
708 n
mi
Hp = 218
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15441414
73 X = 4708011
45
Y = -6831507
94 feet Y = -2029603
29 meter
Z = 14498038
33 Z = 4441869
60
XDOT = -102
861185 XDOT = -124
765321
YDOT = 22705
467388 feet/sec YDOT = 6919
754003 meter/sec
ZDOT = 10824
971212 ZDOT = 3299
071095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15814955
83 X = 4820398
54
Y = 5676211
92 feet Y = 1730109
39 meter
Z = 14593412
74 Z = 4448072
20
XDOT = -15404
431555 XDOT = -4695
270738
YDOT = 15137
276993 feet/sec YDOT = 4613
842027 meter/sec
ZDOT = 10822
551226 ZDOT = 3298
713614
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 13058
49772464
00016717 00000-0 10270-3 0 9120
2 25544 51
6477 293
1055 0011850 318
4340 41
5910 15
52424544 17672
Satellite: ISS
Catalog Number: 25544
Epoch time: 13058
49772464 = yrday
fracday
Element set: 912
Inclination: 51
6477 deg
RA of node: 293
1055 deg
Eccentricity:
0011850
Arg of perigee: 318
4340 deg
Mean anomaly: 41
5910 deg
Mean motion: 15
52424544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 306
Coasting Arc #14 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2013/059/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4516176
81 A = 6783694
80 meter
Y = 1120977
08 meter E =
0013598
Z = -4944423
18 I = 51
29746
XDOT = 537
913429 Wp = 19
44918
YDOT = -7333
036273 meter/sec RA = 287
69961 deg
ZDOT = -2142
955422 TA = 229
48077
MA = 229
59930
Ha = 224
921 n
mi
Hp = 217
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14816853
06 X = -4504357
69
Y = 3677746
32 feet Y = 1070539
79 meter
Z = -16221860
83 Z = -4966333
61
XDOT = 1764
807837 XDOT = 630
282835
YDOT = -24058
517957 feet/sec YDOT = -7326
504798 meter/sec
ZDOT = -7030
693642 ZDOT = -2140
117001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13303171
29 X = -4054806
61
Y = -7288416
44 feet Y = -2221509
33 meter
Z = -16313133
99 Z = -4972243
24
XDOT = 17125
802012 XDOT = 5219
944453
YDOT = -15471
494723 feet/sec YDOT = -4715
711592 meter/sec
ZDOT = -7018
007132 ZDOT = -2139
088574
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 13059
46330361
00016717 00000-0 10270-3 0 9135
2 25544 51
6476 288
3044 0012013 321
7584 38
2714 15
52475647 17826
Satellite: ISS
Catalog Number: 25544
Epoch time: 13059
46330361 = yrday
fracday
Element set: 913
Inclination: 51
6476 deg
RA of node: 288
3044 deg
Eccentricity:
0012013
Arg of perigee: 321
7584 deg
Mean anomaly: 38
2714 deg
Mean motion: 15
52475647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 305
Coasting Arc #15 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2013/060/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4310544
38 A = 6782384
85 meter
Y = -26761
60 meter E =
0009094
Z = 5238752
05 I = 51
28477
XDOT = -991
511758 Wp = 334
11315
YDOT = 7550
483903 meter/sec RA = 282
69310 deg
ZDOT = 863
009773 TA = 107
63883
MA = 107
53949
Ha = 225
032 n
mi
Hp = 217
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14142205
97 X = 4285074
95
Y = -87800
52 feet Y = 21299
82 meter
Z = 17187506
71 Z = 5259630
31
XDOT = -3252
991333 XDOT = -1080
061433
YDOT = 24771
928815 feet/sec YDOT = 7538
901186 meter/sec
ZDOT = 2831
396892 ZDOT = 857
977163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10527966
04 X = 3208924
05
Y = 9283248
40 feet Y = 2829534
11 meter
Z = 17274354
28 Z = 5265223
19
XDOT = -18260
634052 XDOT = -5565
841259
YDOT = 15533
259636 feet/sec YDOT = 4734
537537 meter/sec
ZDOT = 2809
564870 ZDOT = 856
355372
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 13060
49324156
00016717 00000-0 10270-3 0 9146
2 25544 51
6476 283
1824 0011989 325
4293 34
6079 15
52481878 17988
Satellite: ISS
Catalog Number: 25544
Epoch time: 13060
49324156 = yrday
fracday
Element set: 914
Inclination: 51
6476 deg
RA of node: 283
1824 deg
Eccentricity:
0011989
Arg of perigee: 325
4293 deg
Mean anomaly: 34
6079 deg
Mean motion: 15
52481878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 338
Coasting Arc #16 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2013/061/10:38:36
848
Vector Time (MET): N/A
Weight (LBS) : 906332
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4129450
92 A = 6782111
95 meter
Y = -1061088
45 meter E =
0012688
Z = -5281062
69 I = 51
27802
XDOT = 1375
687733 Wp = 41
63416
YDOT = -7522
681859 meter/sec RA = 277
68488 deg
ZDOT = 445
712264 TA = 232
58494
MA = 232
70049
Ha = 225
201 n
mi
Hp = 217
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13548067
33 X = -4091624
81
Y = -3481261
30 feet Y = -1107055
58 meter
Z = -17326321
15 Z = -5301031
13
XDOT = 4513
411196 XDOT = 1457
540576
YDOT = -24680
714760 feet/sec YDOT = -7506
840345 meter/sec
ZDOT = 1462
310576 ZDOT = 452
594756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7904684
86 X = -2409347
95
Y = -11415097
96 feet Y = -3479321
86 meter
Z = -17409256
42 Z = -5306341
36
XDOT = 18696
675025 XDOT = 5698
746548
YDOT = -15172
756174 feet/sec YDOT = -4624
656082 meter/sec
ZDOT = 1491
828120 ZDOT = 454
709211
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 13061
45879466
00016717 00000-0 10270-3 0 9153
2 25544 51
6472 278
3806 0012135 328
7976 31
2454 15
52517126 18132
Satellite: ISS
Catalog Number: 25544
Epoch time: 13061
45879466 = yrday
fracday
Element set: 915
Inclination: 51
6472 deg
RA of node: 278
3806 deg
Eccentricity:
0012135
Arg of perigee: 328
7976 deg
Mean anomaly: 31
2454 deg
Mean motion: 15
52517126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 319
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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