[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 14th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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 375)
---------------------------------------
Vector Time (GMT): 2013/226/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4358676
22 A = 6793663
27 meter
Y = 3330963
51 meter E =
0003765
Z = -4010106
03 I = 51
65220
XDOT = -5869
652096 Wp = 77
28048
YDOT = -2921
655411 meter/sec RA = 177
94375 deg
ZDOT = 3956
958656 TA = 233
91370
MA = 233
94858
Ha = 226
413 n
mi
Hp = 221
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14300118
83 X = -4376119
91
Y = 10928357
98 feet Y = 3282124
53 meter
Z = -13156515
85 Z = -4031322
34
XDOT = -19257
388768 XDOT = -5855
767013
YDOT = -9585
483632 feet/sec YDOT = -2987
215978 meter/sec
ZDOT = 12982
147823 ZDOT = 3928
478239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16285743
49 X = 4963894
61
Y = -7505915
50 feet Y = -2287803
04 meter
Z = -13245833
59 Z = -4037330
08
XDOT = 16186
377240 XDOT = 4933
607783
YDOT = 12442
783246 feet/sec YDOT = 3792
560333 meter/sec
ZDOT = 12863
153483 ZDOT = 3920
689182
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 13226
57792737
00016717 00000-0 10270-3 0 9008
2 25544 51
6476 179
0216 0004310 314
9108 45
1692 15
50279894 3764
Satellite: ISS
Catalog Number: 25544
Epoch time: 13226
57792737 = yrday
fracday
Element set: 900
Inclination: 51
6476 deg
RA of node: 179
0216 deg
Eccentricity:
0004310
Arg of perigee: 314
9108 deg
Mean anomaly: 45
1692 deg
Mean motion: 15
50279894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 376
Checksum: 316
Coasting Arc #2 (Orbit 391)
---------------------------------------
Vector Time (GMT): 2013/227/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4497464
13 A = 6794654
33 meter
Y = -3497486
73 meter E =
0009807
Z = 3698617
75 I = 51
68638
XDOT = 5699
258375 Wp = 63
98773
YDOT = 2741
779580 meter/sec RA = 172
98953 deg
ZDOT = -4324
407236 TA = 72
06726
MA = 71
96036
Ha = 226
515 n
mi
Hp = 221
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14755459
74 X = 4518272
76
Y = -11474693
98 feet Y = -3447076
97 meter
Z = 12134572
68 Z = 3720516
34
XDOT = 18698
354249 XDOT = 5689
182272
YDOT = 8995
339828 feet/sec YDOT = 2805
456060 meter/sec
ZDOT = -14187
687781 ZDOT = -4296
745350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16717980
45 X = -5095640
44
Y = 8225262
30 feet Y = 2507059
95 meter
Z = 12226783
62 Z = 3726723
65
XDOT = -15946
890866 XDOT = -4860
612336
YDOT = -11430
751171 feet/sec YDOT = -3484
092957 meter/sec
ZDOT = -14072
087595 ZDOT = -4289
172299
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 13227
60931305
00016717 00000-0 10270-3 0 9010
2 25544 51
6478 173
9103 0004291 318
8417 41
2410 15
50288959 3923
Satellite: ISS
Catalog Number: 25544
Epoch time: 13227
60931305 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 173
9103 deg
Eccentricity:
0004291
Arg of perigee: 318
8417 deg
Mean anomaly: 41
2410 deg
Mean motion: 15
50288959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 392
Checksum: 297
Coasting Arc #3 (Orbit 406)
---------------------------------------
Vector Time (GMT): 2013/228/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4589090
66 A = 6795527
67 meter
Y = 3699039
27 meter E =
0004103
Z = -3380094
93 I = 51
72033
XDOT = -5507
460912 Wp = 33
01460
YDOT = -2586
504411 meter/sec RA = 168
03717 deg
ZDOT = 4652
828279 TA = 287
66085
MA = 287
70564
Ha = 226
572 n
mi
Hp = 221
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15056071
72 X = -4613693
65
Y = 12135955
62 feet Y = 3647583
69 meter
Z = -11089550
28 Z = -3402447
72
XDOT = -18069
097480 XDOT = -5500
730662
YDOT = -8485
906861 feet/sec YDOT = -2648
054835 meter/sec
ZDOT = 15265
184644 ZDOT = 4626
090093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16999882
96 X = 5181564
33
Y = -9103492
82 feet Y = -2774744
61 meter
Z = -11183704
12 Z = -3408793
02
XDOT = 15582
247825 XDOT = 4749
469137
YDOT = 10506
296988 feet/sec YDOT = 3202
319322 meter/sec
ZDOT = 15153
421666 ZDOT = 4618
762924
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 13228
57622702
00016717 00000-0 10270-3 0 9026
2 25544 51
6481 169
1177 0004328 322
3725 37
7122 15
50316355 4077
Satellite: ISS
Catalog Number: 25544
Epoch time: 13228
57622702 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 169
1177 deg
Eccentricity:
0004328
Arg of perigee: 322
3725 deg
Mean anomaly: 37
7122 deg
Mean motion: 15
50316355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 407
Checksum: 287
Coasting Arc #4 (Orbit 422)
---------------------------------------
Vector Time (GMT): 2013/229/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4676747
59 A = 6796545
20 meter
Y = -3901604
61 meter E =
0010798
Z = 3009787
43 I = 51
75372
XDOT = 5279
445071 Wp = 79
07000
YDOT = 2485
123102 meter/sec RA = 163
08816 deg
ZDOT = -4964
838554 TA = 66
58918
MA = 66
47566
Ha = 226
708 n
mi
Hp = 221
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15343660
07 X = 4705408
09
Y = -12800540
08 feet Y = -3849146
08 meter
Z = 9874630
67 Z = 3032575
81
XDOT = 17321
014013 XDOT = 5275
380967
YDOT = 8153
291016 feet/sec YDOT = 2544
138595 meter/sec
ZDOT = -16288
840400 ZDOT = -4939
201698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17245171
15 X = -5256328
17
Y = 9999014
04 feet Y = 3047699
48 meter
Z = 9970649
51 Z = 3039053
97
XDOT = -15042
666407 XDOT = -4585
004721
YDOT = -9752
631135 feet/sec YDOT = -2972
601970 meter/sec
ZDOT = -16181
666124 ZDOT = -4932
171834
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 13229
60759228
00016717 00000-0 10270-3 0 9036
2 25544 51
6483 164
0061 0004307 326
2936 33
7941 15
50314049 4230
Satellite: ISS
Catalog Number: 25544
Epoch time: 13229
60759228 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 164
0061 deg
Eccentricity:
0004307
Arg of perigee: 326
2936 deg
Mean anomaly: 33
7941 deg
Mean motion: 15
50314049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 423
Checksum: 290
Coasting Arc #5 (Orbit 437)
---------------------------------------
Vector Time (GMT): 2013/230/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4707321
73 A = 6797321
69 meter
Y = 4127263
31 meter E =
0006871
Z = -2639281
54 I = 51
78681
XDOT = -5046
778375 Wp = 15
76477
YDOT = -2415
270651 meter/sec RA = 158
14116 deg
ZDOT = 5233
925269 TA = 314
60396
MA = 314
66000
Ha = 226
731 n
mi
Hp = 221
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15443968
93 X = -4740303
17
Y = 13540890
13 feet Y = 4074438
66 meter
Z = -8659060
17 Z = -2662228
91
XDOT = -16557
671835 XDOT = -5044
819695
YDOT = -7924
116309 feet/sec YDOT = -2471
696008 meter/sec
ZDOT = 17171
670831 ZDOT = 5209
413701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17291189
95 X = 5270354
70
Y = -11009185
53 feet Y = -3355599
75 meter
Z = -8755786
03 Z = -2668763
58
XDOT = 14442
550229 XDOT = 4402
089310
YDOT = 9133
159213 feet/sec YDOT = 2783
786928 meter/sec
ZDOT = 17069
191083 ZDOT = 5202
689442
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 13230
57448664
00016717 00000-0 10270-3 0 9044
2 25544 51
6493 159
2136 0004383 329
4835 30
6060 15
50351372 4381
Satellite: ISS
Catalog Number: 25544
Epoch time: 13230
57448664 = yrday
fracday
Element set: 904
Inclination: 51
6493 deg
RA of node: 159
2136 deg
Eccentricity:
0004383
Arg of perigee: 329
4835 deg
Mean anomaly: 30
6060 deg
Mean motion: 15
50351372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 438
Checksum: 299
Coasting Arc #6 (Orbit 453)
---------------------------------------
Vector Time (GMT): 2013/231/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4731072
02 A = 6798245
56 meter
Y = -4343789
92 meter E =
0011191
Z = 2217410
74 I = 51
81809
XDOT = 4786
970300 Wp = 92
86734
YDOT = 2406
450163 meter/sec RA = 153
19746 deg
ZDOT = -5476
067686 TA = 62
60287
MA = 62
48905
Ha = 226
887 n
mi
Hp = 221
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15521889
84 X = 4768522
26
Y = -14251279
27 feet Y = -4290674
64 meter
Z = 7274969
62 Z = 2240484
39
XDOT = 15705
283137 XDOT = 4786
305741
YDOT = 7895
177699 feet/sec YDOT = 2459
977287 meter/sec
ZDOT = -17966
101331 ZDOT = -5452
815185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17282253
49 X = -5267630
87
Y = 11996944
24 feet Y = 3656668
60 meter
Z = 7372262
27 Z = 2247065
54
XDOT = -13711
577137 XDOT = -4179
288711
YDOT = -8725
253328 feet/sec YDOT = -2659
457214 meter/sec
ZDOT = -17868
887232 ZDOT = -5446
436828
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 13231
60583162
00016717 00000-0 10270-3 0 9053
2 25544 51
6495 154
1021 0004331 333
3855 26
7073 15
50336582 4543
Satellite: ISS
Catalog Number: 25544
Epoch time: 13231
60583162 = yrday
fracday
Element set: 905
Inclination: 51
6495 deg
RA of node: 154
1021 deg
Eccentricity:
0004331
Arg of perigee: 333
3855 deg
Mean anomaly: 26
7073 deg
Mean motion: 15
50336582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 454
Checksum: 280
Coasting Arc #7 (Orbit 468)
---------------------------------------
Vector Time (GMT): 2013/232/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4692844
54 A = 6798814
58 meter
Y = 4568864
19 meter E =
0010127
Z = -1802951
81 I = 51
84835
XDOT = -4540
809332 Wp = 16
07723
YDOT = -2431
802583 meter/sec RA = 148
25553 deg
ZDOT = 5673
779923 TA = 324
19801
MA = 324
26586
Ha = 226
892 n
mi
Hp = 221
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15396471
59 X = -4734827
73
Y = 14989711
93 feet Y = 4516151
01 meter
Z = -5915196
23 Z = -1825850
90
XDOT = -14897
668411 XDOT = -4540
839993
YDOT = -7978
354932 feet/sec YDOT = -2482
580721 meter/sec
ZDOT = 18614
763527 ZDOT = 5651
721590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17045742
86 X = 5195542
42
Y = -13039683
28 feet Y = -3974495
46 meter
Z = -6011793
23 Z = -1832394
58
XDOT = 12997
405387 XDOT = 3961
609162
YDOT = 8476
308569 feet/sec YDOT = 2583
578852 meter/sec
ZDOT = 18522
550484 ZDOT = 5645
673388
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 13232
57270623
00016717 00000-0 10270-3 0 9066
2 25544 51
6504 149
3097 0004479 336
2074 23
8869 15
50384477 4694
Satellite: ISS
Catalog Number: 25544
Epoch time: 13232
57270623 = yrday
fracday
Element set: 906
Inclination: 51
6504 deg
RA of node: 149
3097 deg
Eccentricity:
0004479
Arg of perigee: 336
2074 deg
Mean anomaly: 23
8869 deg
Mean motion: 15
50384477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 469
Checksum: 324
Coasting Arc #8 (Orbit 484)
---------------------------------------
Vector Time (GMT): 2013/233/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4648111
24 A = 6799520
29 meter
Y = -4773338
13 meter E =
0010812
Z = 1339516
15 I = 51
87594
XDOT = 4279
374363 Wp = 105
10801
YDOT = 2520
047451 meter/sec RA = 143
31659 deg
ZDOT = -5832
750490 TA = 60
38152
MA = 60
27386
Ha = 227
046 n
mi
Hp = 220
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15249708
81 X = 4694635
41
Y = -15660558
17 feet Y = -4721099
79 meter
Z = 4394738
02 Z = 1362209
13
XDOT = 14039
942136 XDOT = 4279
209980
YDOT = 8267
872216 feet/sec YDOT = 2567
900839 meter/sec
ZDOT = -19136
320506 ZDOT = -5811
962630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16751297
00 X = -5105795
32
Y = 14012489
08 feet Y = 4271006
67 meter
Z = 4490503
54 Z = 1368705
48
XDOT = -12211
887650 XDOT = -3722
183356
YDOT = -8456
524723 feet/sec YDOT = -2577
548736 meter/sec
ZDOT = -19049
439739 ZDOT = -5806
269233
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 13233
60403077
00016717 00000-0 10270-3 0 9073
2 25544 51
6502 144
1982 0004373 339
9619 20
1360 15
50358372 4855
Satellite: ISS
Catalog Number: 25544
Epoch time: 13233
60403077 = yrday
fracday
Element set: 907
Inclination: 51
6502 deg
RA of node: 144
1982 deg
Eccentricity:
0004373
Arg of perigee: 339
9619 deg
Mean anomaly: 20
1360 deg
Mean motion: 15
50358372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 485
Checksum: 292
Coasting Arc #9 (Orbit 499)
---------------------------------------
Vector Time (GMT): 2013/234/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4542115
32 A = 6799781
01 meter
Y = 4970812
75 meter E =
0013047
Z = -891571
91 I = 51
90157
XDOT = -4049
418131 Wp = 22
37869
YDOT = -2640
564708 meter/sec RA = 138
37867 deg
ZDOT = 5948
042584 TA = 328
01953
MA = 328
09865
Ha = 227
051 n
mi
Hp = 220
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14901953
16 X = -4593031
51
Y = 16308440
79 feet Y = 4919735
18 meter
Z = -2925104
69 Z = -913760
83
XDOT = -13285
492557 XDOT = -4048
483360
YDOT = -8663
270039 feet/sec YDOT = -2685
842185 meter/sec
ZDOT = 19514
575406 ZDOT = 5928
373638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16225916
53 X = 4945659
36
Y = -14973183
89 feet Y = -4563826
45 meter
Z = -3018788
39 Z = -920126
70
XDOT = 11523
157549 XDOT = 3512
258421
YDOT = 8595
253328 feet/sec YDOT = 2619
833215 meter/sec
ZDOT = 19432
398354 ZDOT = 5922
995018
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 13234
57088555
00016717 00000-0 10270-3 0 9081
2 25544 51
6504 139
4055 0004585 342
5809 17
5184 15
50417314 5005
Satellite: ISS
Catalog Number: 25544
Epoch time: 13234
57088555 = yrday
fracday
Element set: 908
Inclination: 51
6504 deg
RA of node: 139
4055 deg
Eccentricity:
0004585
Arg of perigee: 342
5809 deg
Mean anomaly: 17
5184 deg
Mean motion: 15
50417314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 500
Checksum: 300
Coasting Arc #10 (Orbit 515)
---------------------------------------
Vector Time (GMT): 2013/235/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4433718
45 A = 6800158
13 meter
Y = -5136309
06 meter E =
0009552
Z = 399275
92 I = 51
92439
XDOT = 3817
345424 Wp = 114
95715
YDOT = 2819
341386 meter/sec RA = 133
44338 deg
ZDOT = -6012
517259 TA = 60
76329
MA = 60
66781
Ha = 227
179 n
mi
Hp = 220
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14546320
38 X = 4488884
70
Y = -16851407
68 feet Y = -5086419
92 meter
Z = 1309960
37 Z = 420948
72
XDOT = 12524
099161 XDOT = 3814
742109
YDOT = 9249
807697 feet/sec YDOT = 2862
014320 meter/sec
ZDOT = -19726
106493 ZDOT = -5993
979680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15658380
63 X = -4772674
42
Y = 15815570
23 feet Y = 4820585
81 meter
Z = 1401509
15 Z = 427179
99
XDOT = -10829
599252 XDOT = -3300
861852
YDOT = -8951
261220 feet/sec YDOT = -2728
344420 meter/sec
ZDOT = -19648
695168 ZDOT = -5988
922287
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 13235
60218923
00016717 00000-0 10270-3 0 9091
2 25544 51
6499 134
2938 0004443 345
9223 14
1803 15
50383378 5161
Satellite: ISS
Catalog Number: 25544
Epoch time: 13235
60218923 = yrday
fracday
Element set: 909
Inclination: 51
6499 deg
RA of node: 134
2938 deg
Eccentricity:
0004443
Arg of perigee: 345
9223 deg
Mean anomaly: 14
1803 deg
Mean motion: 15
50383378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 516
Checksum: 306
Coasting Arc #11 (Orbit 531)
---------------------------------------
Vector Time (GMT): 2013/236/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4270350
92 A = 6800040
80 meter
Y = 5280050
26 meter E =
0015191
Z = 69145
78 I = 51
94453
XDOT = -3632
158130 Wp = 31
30574
YDOT = -3024
235289 meter/sec RA = 128
50820 deg
ZDOT = 6035
928910 TA = 329
43515
MA = 329
52359
Ha = 227
194 n
mi
Hp = 220
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14010337
65 X = -4329412
10
Y = 17322999
55 feet Y = 5231966
26 meter
Z = 226856
23 Z = 48257
07
XDOT = -11916
529298 XDOT = -3627
391244
YDOT = -9922
031788 feet/sec YDOT = -3064
825270 meter/sec
ZDOT = 19802
916371 ZDOT = 6018
296137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14882497
54 X = 4536185
25
Y = -16580693
72 feet Y = -5053795
45 meter
Z = 138567
20 Z = 42235
28
XDOT = 10304
850639 XDOT = 3140
918475
YDOT = 9440
382433 feet/sec YDOT = 2877
428565 meter/sec
ZDOT = 19729
325731 ZDOT = 6013
498483
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 13236
63347917
00016717 00000-0 10270-3 0 9103
2 25544 51
6494 129
1809 0004661 348
8415 11
2632 15
50452182 5329
Satellite: ISS
Catalog Number: 25544
Epoch time: 13236
63347917 = yrday
fracday
Element set: 910
Inclination: 51
6494 deg
RA of node: 129
1809 deg
Eccentricity:
0004661
Arg of perigee: 348
8415 deg
Mean anomaly: 11
2632 deg
Mean motion: 15
50452182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 532
Checksum: 296
Coasting Arc #12 (Orbit 546)
---------------------------------------
Vector Time (GMT): 2013/237/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4112530
01 A = 6800008
01 meter
Y = -5382275
32 meter E =
0007481
Z = -574941
51 I = 51
96199
XDOT = 3457
346957 Wp = 119
78669
YDOT = 3275
741321 meter/sec RA = 123
57541 deg
ZDOT = -5997
428642 TA = 66
37782
MA = 66
29930
Ha = 227
292 n
mi
Hp = 220
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13492552
51 X = 4175203
03
Y = -17658383
59 feet Y = -5335936
01 meter
Z = -1886291
05 Z = -554810
71
XDOT = 11343
001827 XDOT = 3449
593711
YDOT = 10747
182811 feet/sec YDOT = 3314
359824 meter/sec
ZDOT = -19676
603155 ZDOT = -5980
652279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14099368
72 X = -4297487
59
Y = 17186890
92 feet Y = 5238564
35 meter
Z = -1801155
34 Z = -548992
15
XDOT = -9837
845080 XDOT = -2998
575180
YDOT = -10102
934537 feet/sec YDOT = -3079
374447 meter/sec
ZDOT = -19606
637675 ZDOT = -5976
103163
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 13237
60030699
00016717 00000-0 10270-3 0 9118
2 25544 51
6489 124
3884 0004550 351
6029 8
5044 15
50416815 5478
Satellite: ISS
Catalog Number: 25544
Epoch time: 13237
60030699 = yrday
fracday
Element set: 911
Inclination: 51
6489 deg
RA of node: 124
3884 deg
Eccentricity:
0004550
Arg of perigee: 351
6029 deg
Mean anomaly: 8
5044 deg
Mean motion: 15
50416815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 547
Checksum: 300
Coasting Arc #13 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2013/238/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3910991
65 A = 6799500
98 meter
Y = 5450526
27 meter E =
0016299
Z = 1048390
81 I = 51
97646
XDOT = -3340
609174 Wp = 41
67680
YDOT = -3543
938523 meter/sec RA = 118
64195 deg
ZDOT = 5921
828638 TA = 329
62658
MA = 329
72092
Ha = 227
317 n
mi
Hp = 220
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12831337
43 X = -3976742
73
Y = 17882304
04 feet Y = 5406423
50 meter
Z = 3439602
40 Z = 1029231
65
XDOT = -10960
003851 XDOT = -3329
498341
YDOT = -11627
094891 feet/sec YDOT = -3581
232904 meter/sec
ZDOT = 19428
571648 ZDOT = 5905
627487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13153979
82 X = 4009333
05
Y = -17661937
66 feet Y = -5383358
60 meter
Z = 3358519
84 Z = 1023676
85
XDOT = 9593
632179 XDOT = 2924
139088
YDOT = 10852
722503 feet/sec YDOT = 3307
909819 meter/sec
ZDOT = 19361
055080 ZDOT = 5901
249588
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 13238
63157647
00016717 00000-0 10270-3 0 9126
2 25544 51
6482 119
2750 0004689 354
7034 5
4067 15
50486262 5631
Satellite: ISS
Catalog Number: 25544
Epoch time: 13238
63157647 = yrday
fracday
Element set: 912
Inclination: 51
6482 deg
RA of node: 119
2750 deg
Eccentricity:
0004689
Arg of perigee: 354
7034 deg
Mean anomaly: 5
4067 deg
Mean motion: 15
50486262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 311
Coasting Arc #14 (Orbit 577)
---------------------------------------
Vector Time (GMT): 2013/239/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3726265
10 A = 6799024
02 meter
Y = -5471329
54 meter E =
0005154
Z = -1550129
87 I = 51
98806
XDOT = 3243
778689 Wp = 110
79480
YDOT = 3840
634370 meter/sec RA = 113
71055 deg
ZDOT = -5775
621357 TA = 86
02633
MA = 85
96741
Ha = 227
398 n
mi
Hp = 220
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12225279
20 X = 3794699
84
Y = -17950556
23 feet Y = -5429277
50 meter
Z = -5085727
91 Z = -1531861
64
XDOT = 10642
318533 XDOT = 3228
647081
YDOT = 12600
506462 feet/sec YDOT = 3876
823528 meter/sec
ZDOT = -18948
888967 ZDOT = -5759
900343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12252381
19 X = -3734525
79
Y = 17953828
98 feet Y = 5472327
07 meter
Z = -5008365
90 Z = -1526549
93
XDOT = -9453
494797 XDOT = -2881
425214
YDOT = -11703
064877 feet/sec YDOT = -3567
094174 meter/sec
ZDOT = -18883
427117 ZDOT = -5755
668585
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 13239
59838481
00016717 00000-0 10270-3 0 9135
2 25544 51
6477 114
4823 0004671 357
7572 2
3558 15
50460443 5784
Satellite: ISS
Catalog Number: 25544
Epoch time: 13239
59838481 = yrday
fracday
Element set: 913
Inclination: 51
6477 deg
RA of node: 114
4823 deg
Eccentricity:
0004671
Arg of perigee: 357
7572 deg
Mean anomaly: 2
3558 deg
Mean motion: 15
50460443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 578
Checksum: 323
Coasting Arc #15 (Orbit 593)
---------------------------------------
Vector Time (GMT): 2013/240/13:39:30
481
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3512803
49 A = 6798179
98 meter
Y = 5449887
72 meter E =
0016284
Z = 2011207
79 I = 51
99680
XDOT = -3210
623271 Wp = 52
90507
YDOT = -4142
896595 meter/sec RA = 108
77789 deg
ZDOT = 5596
966973 TA = 329
17952
MA = 329
27503
Ha = 227
431 n
mi
Hp = 220
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11524945
84 X = -3583254
09
Y = 17880209
04 feet Y = 5410211
47 meter
Z = 6598450
77 Z = 1993971
72
XDOT = -10533
540916 XDOT = -3191
246267
YDOT = -13592
180429 feet/sec YDOT = -4178
691300 meter/sec
ZDOT = 18362
752537 ZDOT = 5581
417344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11252140
36 X = 3429652
38
Y = -18079662
37 feet Y = -5510681
09 meter
Z = 6525408
06 Z = 1988944
38
XDOT = 9564
303931 XDOT = 2915
199838
YDOT = 12582
533795 feet/sec YDOT = 3835
156301 meter/sec
ZDOT = 18298
051423 ZDOT = 5577
246074
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 13240
62963435
00016717 00000-0 10270-3 0 9140
2 25544 51
6472 109
3686 0004676
8386 359
2772 15
50517738 5943
Satellite: ISS
Catalog Number: 25544
Epoch time: 13240
62963435 = yrday
fracday
Element set: 914
Inclination: 51
6472 deg
RA of node: 109
3686 deg
Eccentricity:
0004676
Arg of perigee:
8386 deg
Mean anomaly: 359
2772 deg
Mean motion: 15
50517738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 594
Checksum: 327
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