[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 16th 2013
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) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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 2497)
---------------------------------------
Vector Time (GMT): 2013/105/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4876881
37 A = 6785800
04 meter
Y = 1033651
66 meter E =
0019252
Z = -4622844
93 I = 51
93907
XDOT = 1422
588349 Wp = 127
57971
YDOT = 6875
959564 meter/sec RA = 58
52577 deg
ZDOT = 3035
444997 TA = 172
69792
MA = 172
66984
Ha = 227
100 n
mi
Hp = 215
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16000266
95 X = 4887417
16
Y = 3391245
60 feet Y = 1088246
77 meter
Z = -15166814
09 Z = -4599127
67
XDOT = 4667
284608 XDOT = 1330
848636
YDOT = 22558
922453 feet/sec YDOT = 6891
355000 meter/sec
ZDOT = 9958
809046 ZDOT = 3042
132810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14665315
58 X = 4469988
19
Y = -7444767
36 feet Y = -2269165
09 meter
Z = -15068022
32 Z = -4592733
20
XDOT = 17185
061101 XDOT = 5238
006624
YDOT = 13623
116640 feet/sec YDOT = 4152
325952 meter/sec
ZDOT = 9985
794164 ZDOT = 3043
670061
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 13105
55447960
00016717 00000-0 10270-3 0 9007
2 25544 51
6452 59
1629 0010150 145
3683 214
8132 15
52287759 24989
Satellite: ISS
Catalog Number: 25544
Epoch time: 13105
55447960 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 59
1629 deg
Eccentricity:
0010150
Arg of perigee: 145
3683 deg
Mean anomaly: 214
8132 deg
Mean motion: 15
52287759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2498
Checksum: 310
Coasting Arc #2 (Orbit 2513)
---------------------------------------
Vector Time (GMT): 2013/106/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5194688
66 A = 6788115
26 meter
Y = -1831051
64 meter E =
0017596
Z = 3948193
78 I = 51
93067
XDOT = -815
182581 Wp = 112
73433
YDOT = -6461
774095 meter/sec RA = 53
57204 deg
ZDOT = -4061
581698 TA = 19
53172
MA = 19
46439
Ha = 227
130 n
mi
Hp = 215
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17042941
79 X = -5193006
78
Y = -6007387
27 feet Y = -1889132
38 meter
Z = 12953391
65 Z = 3922962
38
XDOT = -2674
483534 XDOT = -723
134820
YDOT = -21200
046244 feet/sec YDOT = -6470
375449 meter/sec
ZDOT = -13325
399273 ZDOT = -4065
318017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17000264
19 X = -5181680
53
Y = 6344350
24 feet Y = 1933757
95 meter
Z = 12848391
32 Z = 3916189
67
XDOT = -15098
746943 XDOT = -4602
098068
YDOT = -13390
619943 feet/sec YDOT = -4081
460959 meter/sec
ZDOT = -13340
118662 ZDOT = -4066
068168
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 13106
58452396
00016717 00000-0 10270-3 0 9011
2 25544 51
6457 54
0427 0010156 149
1533 211
0218 15
52309160 25140
Satellite: ISS
Catalog Number: 25544
Epoch time: 13106
58452396 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 54
0427 deg
Eccentricity:
0010156
Arg of perigee: 149
1533 deg
Mean anomaly: 211
0218 deg
Mean motion: 15
52309160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2514
Checksum: 275
Coasting Arc #3 (Orbit 2528)
---------------------------------------
Vector Time (GMT): 2013/107/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5485282
95 A = 6790509
07 meter
Y = 2515357
60 meter E =
0011851
Z = -3130806
46 I = 51
91988
XDOT = 85
748756 Wp = 130
61699
YDOT = 5889
094211 meter/sec RA = 48
62054 deg
ZDOT = 4886
288339 TA = 193
57611
MA = 193
60801
Ha = 226
869 n
mi
Hp = 215
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17996335
13 X = 5471956
71
Y = 8252485
55 feet Y = 2576622
86 meter
Z = -10271674
72 Z = -3104191
74
XDOT = 281
327939 XDOT = -3
847152
YDOT = 19321
175234 feet/sec YDOT = 5889
552333 meter/sec
ZDOT = 16031
129721 ZDOT = 4886
487054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19064554
38 X = 5810876
17
Y = -5547591
61 feet Y = -1690905
92 meter
Z = -10160998
54 Z = -3097072
36
XDOT = 12354
372819 XDOT = 3765
612835
YDOT = 13121
721339 feet/sec YDOT = 3999
500664 meter/sec
ZDOT = 16031
162605 ZDOT = 4886
298362
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 13107
55017797
00016717 00000-0 10270-3 0 9022
2 25544 51
6456 49
2418 0010110 152
8641 207
3041 15
52330131 25296
Satellite: ISS
Catalog Number: 25544
Epoch time: 13107
55017797 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 49
2418 deg
Eccentricity:
0010110
Arg of perigee: 152
8641 deg
Mean anomaly: 207
3041 deg
Mean motion: 15
52330131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2529
Checksum: 272
Coasting Arc #4 (Orbit 2544)
---------------------------------------
Vector Time (GMT): 2013/108/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5649073
51 A = 6792671
04 meter
Y = -3082235
36 meter E =
0022172
Z = 2132199
32 I = 51
90669
XDOT = 772
281651 Wp = 129
24848
YDOT = -5261
355423 meter/sec RA = 43
67202 deg
ZDOT = -5534
865116 TA = 27
19600
MA = 27
08005
Ha = 226
848 n
mi
Hp = 215
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18533705
74 X = -5624545
14
Y = -10112320
72 feet Y = -3145269
61 meter
Z = 6995404
60 Z = 2104816
21
XDOT = 2533
732451 XDOT = 857
944874
YDOT = -17261
664772 feet/sec YDOT = -5252
240563 meter/sec
ZDOT = -18159
006286 ZDOT = -5530
905111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20591018
49 X = -6276142
43
Y = 4831816
74 feet Y = 1472737
74 meter
Z = 6881603
67 Z = 2097512
80
XDOT = -9173
159335 XDOT = -2795
978965
YDOT = -13136
625188 feet/sec YDOT = -4004
043357 meter/sec
ZDOT = -18141
772074 ZDOT = -5529
612128
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 13108
58019627
00016717 00000-0 10270-3 0 9031
2 25544 51
6461 44
1209 0010136 156
5409 203
6207 15
52341834 25458
Satellite: ISS
Catalog Number: 25544
Epoch time: 13108
58019627 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 44
1209 deg
Eccentricity:
0010136
Arg of perigee: 156
5409 deg
Mean anomaly: 203
6207 deg
Mean motion: 15
52341834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2545
Checksum: 283
Coasting Arc #5 (Orbit 2559)
---------------------------------------
Vector Time (GMT): 2013/109/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5721533
67 A = 6793991
04 meter
Y = 3507381
50 meter E =
0009568
Z = -1074654
35 I = 51
88862
XDOT = -1701
250642 Wp = 101
26040
YDOT = 4570
680293 meter/sec RA = 38
72497 deg
ZDOT = 5902
602542 TA = 247
14644
MA = 247
24750
Ha = 226
623 n
mi
Hp = 215
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18771435
93 X = 5687108
55
Y = 11507157
15 feet Y = 3571170
75 meter
Z = -3525768
87 Z = -1046943
34
XDOT = -5581
530978 XDOT = -1780
907914
YDOT = 14995
670252 feet/sec YDOT = 4551
210778 meter/sec
ZDOT = 19365
493904 ZDOT = 5894
144239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21610723
44 X = 6586948
50
Y = -4307728
87 feet Y = -1312995
76 meter
Z = -3410663
14 Z = -1039570
13
XDOT = 5680
183161 XDOT = 1731
319828
YDOT = 13306
368583 feet/sec YDOT = 4055
781144 meter/sec
ZDOT = 19329
587561 ZDOT = 5891
658289
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 13109
54582553
00016717 00000-0 10270-3 0 9042
2 25544 51
6462 39
3199 0010041 160
3704 199
7836 15
52365593 25607
Satellite: ISS
Catalog Number: 25544
Epoch time: 13109
54582553 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 39
3199 deg
Eccentricity:
0010041
Arg of perigee: 160
3704 deg
Mean anomaly: 199
7836 deg
Mean motion: 15
52365593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2560
Checksum: 313
Coasting Arc #6 (Orbit 2575)
---------------------------------------
Vector Time (GMT): 2013/110/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5600342
13 A = 6794466
99 meter
Y = -3824662
56 meter E =
0021329
Z = -83275
51 I = 51
86642
XDOT = 2726
281719 Wp = 148
34595
YDOT = -3876
202504 meter/sec RA = 33
77815 deg
ZDOT = -6034
848975 TA = 32
54847
MA = 32
41715
Ha = 226
553 n
mi
Hp = 215
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18373825
88 X = -5556753
17
Y = -12548105
50 feet Y = -3887045
40 meter
Z = -273213
61 Z = -110375
48
XDOT = 8944
493830 XDOT = 2798
739458
YDOT = -12717
199817 feet/sec YDOT = -3845
310785 meter/sec
ZDOT = -19799
373277 ZDOT = -6021
428604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21949075
66 X = -6690078
26
Y = 3635432
81 feet Y = 1108079
92 meter
Z = -385720
72 Z = -117567
68
XDOT = -1977
427540 XDOT = -602
719914
YDOT = -13857
026076 feet/sec YDOT = -4223
621548 meter/sec
ZDOT = -19742
863970 ZDOT = -6017
624938
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 13110
57581791
00016717 00000-0 10270-3 0 9051
2 25544 51
6470 34
1986 0010153 164
4123 195
7343 15
52363222 25760
Satellite: ISS
Catalog Number: 25544
Epoch time: 13110
57581791 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 34
1986 deg
Eccentricity:
0010153
Arg of perigee: 164
4123 deg
Mean anomaly: 195
7343 deg
Mean motion: 15
52363222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2576
Checksum: 295
Coasting Arc #7 (Orbit 2591)
---------------------------------------
Vector Time (GMT): 2013/111/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5347499
79 A = 6793718
66 meter
Y = 4015457
65 meter E =
0014030
Z = 1195173
08 I = 51
83847
XDOT = -3734
533083 Wp = 100
12423
YDOT = 3208
516883 meter/sec RA = 28
82929 deg
ZDOT = 5868
467406 TA = 272
80570
MA = 272
96627
Ha = 226
342 n
mi
Hp = 215
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17544290
65 X = 5296394
77
Y = 13174073
67 feet Y = 4074971
12 meter
Z = 3921171
51 Z = 1221026
50
XDOT = -12252
405128 XDOT = -3798
641509
YDOT = 10526
630194 feet/sec YDOT = 3166
397000 meter/sec
ZDOT = 19253
501987 ZDOT = 5850
169259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21718584
71 X = 6619824
62
Y = -2967936
13 feet Y = -904626
93 meter
Z = 4028445
19 Z = 1227870
09
XDOT = -1597
708683 XDOT = -486
981607
YDOT = 14601
847358 feet/sec YDOT = 4450
643075 meter/sec
ZDOT = 19176
741002 ZDOT = 5845
070657
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 13111
60579622
00016717 00000-0 10270-3 0 9067
2 25544 51
6471 29
0774 0009955 168
0783 192
0606 15
52400316 25925
Satellite: ISS
Catalog Number: 25544
Epoch time: 13111
60579622 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 29
0774 deg
Eccentricity:
0009955
Arg of perigee: 168
0783 deg
Mean anomaly: 192
0606 deg
Mean motion: 15
52400316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2592
Checksum: 306
Coasting Arc #8 (Orbit 2606)
---------------------------------------
Vector Time (GMT): 2013/112/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4860414
61 A = 6792036
66 meter
Y = -4135044
15 meter E =
0015008
Z = -2305455
21 I = 51
80643
XDOT = 4756
250377 Wp = 158
57127
YDOT = -2572
822687 meter/sec RA = 23
87686 deg
ZDOT = -5437
410395 TA = 47
04453
MA = 46
91876
Ha = 226
188 n
mi
Hp = 215
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15946242
16 X = -4802615
01
Y = -13566417
82 feet Y = -4189073
39 meter
Z = -7563829
44 Z = -2328926
20
XDOT = 15604
495987 XDOT = 4811
080517
YDOT = -8441
019315 feet/sec YDOT = -2519
329190 meter/sec
ZDOT = -17839
272951 ZDOT = -5414
171287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20813751
74 X = -6344031
53
Y = 1906962
00 feet Y = 581242
02 meter
Z = -7661141
02 Z = -2335115
78
XDOT = 5069
312311 XDOT = 1545
126393
YDOT = -15625
892995 feet/sec YDOT = -4762
772185 meter/sec
ZDOT = -17741
995956 ZDOT = -5407
760367
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 13112
57138862
00016717 00000-0 10270-3 0 9072
2 25544 51
6479 24
2764 0010049 172
7012 187
4288 15
52403469 26075
Satellite: ISS
Catalog Number: 25544
Epoch time: 13112
57138862 = yrday
fracday
Element set: 907
Inclination: 51
6479 deg
RA of node: 24
2764 deg
Eccentricity:
0010049
Arg of perigee: 172
7012 deg
Mean anomaly: 187
4288 deg
Mean motion: 15
52403469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2607
Checksum: 311
Coasting Arc #9 (Orbit 2622)
---------------------------------------
Vector Time (GMT): 2013/113/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4242341
89 A = 6789672
60 meter
Y = 4174148
77 meter E =
0016367
Z = 3266480
82 I = 51
77051
XDOT = -5662
997952 Wp = 124
53034
YDOT = 2016
366103 meter/sec RA = 18
91860 deg
ZDOT = 4752
136257 TA = 273
24005
MA = 273
42729
Ha = 226
016 n
mi
Hp = 216
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13918444
53 X = 4179482
42
Y = 13694713
80 feet Y = 4221238
11 meter
Z = 10716800
59 Z = 3286937
04
XDOT = -18579
389606 XDOT = -5708
209467
YDOT = 6615
374355 feet/sec YDOT = 1952
786486 meter/sec
ZDOT = 15590
998220 ZDOT = 4724
515499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19467242
53 X = 5933615
52
Y = -686763
80 feet Y = -209325
61 meter
Z = 10801524
10 Z = 3292304
55
XDOT = -8044
244070 XDOT = -2451
885593
YDOT = 16708
785769 feet/sec YDOT = 5092
837902 meter/sec
ZDOT = 15475
530282 ZDOT = 4716
941630
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 13113
60134178
00016717 00000-0 10270-3 0 9084
2 25544 51
6480 19
1552 0009874 175
7458 184
3779 15
52436789 26236
Satellite: ISS
Catalog Number: 25544
Epoch time: 13113
60134178 = yrday
fracday
Element set: 908
Inclination: 51
6480 deg
RA of node: 19
1552 deg
Eccentricity:
0009874
Arg of perigee: 175
7458 deg
Mean anomaly: 184
3779 deg
Mean motion: 15
52436789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2623
Checksum: 334
Coasting Arc #10 (Orbit 2637)
---------------------------------------
Vector Time (GMT): 2013/114/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3396674
94 A = 6786917
12 meter
Y = -4191640
39 meter E =
0010192
Z = -4118598
26 I = 51
73252
XDOT = 6469
928752 Wp = 135
75269
YDOT = -1499
487024 meter/sec RA = 13
95375 deg
ZDOT = -3822
601171 TA = 94
85849
MA = 94
74211
Ha = 225
796 n
mi
Hp = 216
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11143946
67 X = -3329543
23
Y = -13752101
02 feet Y = -4229249
07 meter
Z = -13512461
49 Z = -4134935
99
XDOT = 21226
800368 XDOT = 6504
785013
YDOT = -4919
576850 feet/sec YDOT = -1426
941564 meter/sec
ZDOT = -12541
342426 ZDOT = -3791
085440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17615577
75 X = -5369228
10
Y = -1081440
63 feet Y = -329623
10 meter
Z = -13579998
23 Z = -4139183
46
XDOT = 10626
027061 XDOT = 3238
813048
YDOT = -17780
315997 feet/sec YDOT = -5419
440316 meter/sec
ZDOT = -12409
710229 ZDOT = -3782
479678
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 13114
56690964
00016717 00000-0 10270-3 0 9091
2 25544 51
6482 14
3542 0009861 180
7270 179
3869 15
52464719 26382
Satellite: ISS
Catalog Number: 25544
Epoch time: 13114
56690964 = yrday
fracday
Element set: 909
Inclination: 51
6482 deg
RA of node: 14
3542 deg
Eccentricity:
0009861
Arg of perigee: 180
7270 deg
Mean anomaly: 179
3869 deg
Mean motion: 15
52464719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2638
Checksum: 337
Coasting Arc #11 (Orbit 2653)
---------------------------------------
Vector Time (GMT): 2013/115/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2465157
73 A = 6784570
66 meter
Y = 4181037
92 meter E =
0014719
Z = 4740947
28 I = 51
69473
XDOT = -7082
849257 Wp = 154
81655
YDOT = 1063
039768 meter/sec RA = 8
98226 deg
ZDOT = 2729
249146 TA = 268
11298
MA = 268
28156
Ha = 225
671 n
mi
Hp = 216
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8087787
84 X = 2395190
48
Y = 13717316
01 feet Y = 4208213
86 meter
Z = 15554288
98 Z = 4752752
94
XDOT = -23237
694412 XDOT = -7107
468236
YDOT = 3487
663282 feet/sec YDOT = 983
697348 meter/sec
ZDOT = 8954
229483 ZDOT = 2694
780669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15578852
96 X = 4748434
38
Y = 3059606
72 feet Y = 932568
13 meter
Z = 15602920
35 Z = 4755770
12
XDOT = -12541
070089 XDOT = -3822
518163
YDOT = 18657
553522 feet/sec YDOT = 5686
822313 meter/sec
ZDOT = 8810
352011 ZDOT = 2685
395293
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 13115
59683804
00016717 00000-0 10270-3 0 9102
2 25544 51
6482 9
2331 0009814 183
7014 176
4066 15
52475134 26546
Satellite: ISS
Catalog Number: 25544
Epoch time: 13115
59683804 = yrday
fracday
Element set: 910
Inclination: 51
6482 deg
RA of node: 9
2331 deg
Eccentricity:
0009814
Arg of perigee: 183
7014 deg
Mean anomaly: 176
4066 deg
Mean motion: 15
52475134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2654
Checksum: 302
Coasting Arc #12 (Orbit 2668)
---------------------------------------
Vector Time (GMT): 2013/116/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1366773
21 A = 6782694
94 meter
Y = -4190412
69 meter E =
0014062
Z = -5164362
53 I = 51
65768
XDOT = 7488
205370 Wp = 119
70198
YDOT = -642
002978 meter/sec RA = 4
00343 deg
ZDOT = -1470
674945 TA = 136
18101
MA = 136
06935
Ha = 225
453 n
mi
Hp = 216
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4484164
08 X = -1294725
88
Y = -13748073
15 feet Y = -4205294
05 meter
Z = -16943446
62 Z = -5170827
28
XDOT = 24567
602919 XDOT = 7501
972146
YDOT = -2106
308982 feet/sec YDOT = -558
188194 meter/sec
ZDOT = -4825
049031 ZDOT = -1434
263622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13314085
83 X = -4058133
36
Y = -5564049
23 feet Y = -1695922
20 meter
Z = -16969799
67 Z = -5172394
94
XDOT = 13913
576006 XDOT = 4240
857967
YDOT = -19138
916119 feet/sec YDOT = -5833
541633 meter/sec
ZDOT = -4673
134821 ZDOT = -1424
371494
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 13116
56238219
00016717 00000-0 10270-3 0 9117
2 25544 51
6475 4
4311 0009761 188
4169 171
6820 15
52523269 26691
Satellite: ISS
Catalog Number: 25544
Epoch time: 13116
56238219 = yrday
fracday
Element set: 911
Inclination: 51
6475 deg
RA of node: 4
4311 deg
Eccentricity:
0009761
Arg of perigee: 188
4169 deg
Mean anomaly: 171
6820 deg
Mean motion: 15
52523269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2669
Checksum: 312
Coasting Arc #13 (Orbit 2684)
---------------------------------------
Vector Time (GMT): 2013/117/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 261261
09 A = 6782022
09 meter
Y = 4204769
06 meter E =
0009835
Z = 5314668
88 I = 51
62475
XDOT = -7660
419598 Wp = 177
32991
YDOT = 259
117554 meter/sec RA = 359
02139 deg
ZDOT = 161
950301 TA = 271
06969
MA = 271
18237
Ha = 225
321 n
mi
Hp = 216
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 857155
82 X = 188405
28
Y = 13795174
09 feet Y = 4207283
23 meter
Z = 17436577
70 Z = 5315761
17
XDOT = -25132
610229 XDOT = -7663
534488
YDOT = 850
123210 feet/sec YDOT = 173
436498 meter/sec
ZDOT = 531
333008 ZDOT = 124
728328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11142034
91 X = 3396092
24
Y = 8170619
08 feet Y = 2490404
70 meter
Z = 17440522
58 Z = 5315871
28
XDOT = -14688
452051 XDOT = -4477
040185
YDOT = 19160
065589 feet/sec YDOT = 5839
987992 meter/sec
ZDOT = 376
096056 ZDOT = 114
634078
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 13117
59228514
00016717 00000-0 10270-3 0 9129
2 25544 51
6475 359
3100 0009803 192
1596 167
9321 15
52525212 26854
Satellite: ISS
Catalog Number: 25544
Epoch time: 13117
59228514 = yrday
fracday
Element set: 912
Inclination: 51
6475 deg
RA of node: 359
3100 deg
Eccentricity:
0009803
Arg of perigee: 192
1596 deg
Mean anomaly: 167
9321 deg
Mean motion: 15
52525212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2685
Checksum: 307
Coasting Arc #14 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2013/118/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 908781
01 A = 6782442
25 meter
Y = -4252822
57 meter E =
0016136
Z = -5216461
37 I = 51
59444
XDOT = 7562
363266 Wp = 135
94247
YDOT = 153
100998 meter/sec RA = 354
03440 deg
ZDOT = 1183
526959 TA = 145
48748
MA = 145
38262
Ha = 225
143 n
mi
Hp = 217
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2981564
99 X = 981610
02
Y = -13952829
96 feet Y = -4242252
65 meter
Z = -17114374
56 Z = -5211869
73
XDOT = 24810
903103 XDOT = 7554
339851
YDOT = 502
299862 feet/sec YDOT = 237
623213 meter/sec
ZDOT = 3882
962464 ZDOT = 1220
245370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9022576
25 X = -2750081
24
Y = -11083340
83 feet Y = -3378202
28 meter
Z = -17094609
80 Z = -5210437
07
XDOT = 14974
070149 XDOT = 4564
096581
YDOT = -18461
180320 feet/sec YDOT = -5626
967762 meter/sec
ZDOT = 4036
039620 ZDOT = 1230
184876
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 13118
55780677
00016717 00000-0 10270-3 0 9130
2 25544 51
6462 354
5069 0009770 196
4121 163
6716 15
52556778 27005
Satellite: ISS
Catalog Number: 25544
Epoch time: 13118
55780677 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 354
5069 deg
Eccentricity:
0009770
Arg of perigee: 196
4121 deg
Mean anomaly: 163
6716 deg
Mean motion: 15
52556778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 329
Coasting Arc #15 (Orbit 2715)
---------------------------------------
Vector Time (GMT): 2013/119/13:03:04
910
Vector Time (MET): N/A
Weight (LBS) : 889591
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1994621
82 A = 6783919
80 meter
Y = 4302577
69 meter E =
0006224
Z = 4846286
69 I = 51
56947
XDOT = -7239
396895 Wp = 153
38586
YDOT = -588
465519 meter/sec RA = 349
04931 deg
ZDOT = -2461
347365 TA = 320
77795
MA = 320
82303
Ha = 224
949 n
mi
Hp = 217
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6544034
84 X = -2066128
15
Y = 14116068
52 feet Y = 4279872
59 meter
Z = 15899890
71 Z = 4836423
34
XDOT = -23751
302148 XDOT = -7220
321794
YDOT = -1930
661153 feet/sec YDOT = -669
314277 meter/sec
ZDOT = -8075
286630 ZDOT = -2496
469809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7182767
71 X = 2189307
60
Y = 13849969
63 feet Y = 4221470
74 meter
Z = 15858136
60 Z = 4833560
03
XDOT = -14917
043280 XDOT = -4546
714792
YDOT = 17134
007085 feet/sec YDOT = 5222
445359 meter/sec
ZDOT = -8221
646441 ZDOT = -2505
957835
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 13119
58768414
00016717 00000-0 10270-3 0 9140
2 25544 51
6465 349
3855 0009779 200
9288 159
1465 15
52582778 27164
Satellite: ISS
Catalog Number: 25544
Epoch time: 13119
58768414 = yrday
fracday
Element set: 914
Inclination: 51
6465 deg
RA of node: 349
3855 deg
Eccentricity:
0009779
Arg of perigee: 200
9288 deg
Mean anomaly: 159
1465 deg
Mean motion: 15
52582778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2716
Checksum: 358
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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