[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 10th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 378 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 534)
---------------------------------------
Vector Time (GMT): 2014/129/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4225032
75 A = 6797225
53 meter
Y = -4313932
44 meter E =
0012232
Z = 3107071
69 I = 51
31750
XDOT = 2099
977089 Wp = 75
19397
YDOT = 5555
778095 meter/sec RA = 290
07400 deg
ZDOT = 4845
231273 TA = 320
68857
MA = 320
77731
Ha = 227
207 n
mi
Hp = 221
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13861655
99 X = 4257864
75
Y = -14153321
65 feet Y = -4266501
76 meter
Z = 10193804
75 Z = 3127676
41
XDOT = 6889
688612 XDOT = 2014
158168
YDOT = 18227
618423 feet/sec YDOT = 5578
781658 meter/sec
ZDOT = 15896
428062 ZDOT = 4855
224217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13778686
37 X = -4199743
60
Y = -14170784
25 feet Y = -4319255
04 meter
Z = 10281651
21 Z = 3133847
29
XDOT = 17370
560129 XDOT = 5294
546727
YDOT = -5295
652690 feet/sec YDOT = -1614
114940 meter/sec
ZDOT = 15937
729837 ZDOT = 4857
820054
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 14129
67456434
00016717 00000-0 10270-3 0 9003
2 25544 51
6470 290
4852 0002262 333
0466 27
0567 15
49995833 5358
Satellite: ISS
Catalog Number: 25544
Epoch time: 14129
67456434 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 290
4852 deg
Eccentricity:
0002262
Arg of perigee: 333
0466 deg
Mean anomaly: 27
0567 deg
Mean motion: 15
49995833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 535
Checksum: 315
Coasting Arc #2 (Orbit 549)
---------------------------------------
Vector Time (GMT): 2014/130/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3982836
29 A = 6796453
67 meter
Y = 4346718
63 meter E =
0004477
Z = -3387240
51 I = 51
30509
XDOT = -2284
937005 Wp = 60
88031
YDOT = -5676
231117 meter/sec RA = 285
09762 deg
ZDOT = -4599
875892 TA = 158
78404
MA = 158
76547
Ha = 227
348 n
mi
Hp = 221
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13067048
19 X = -4014691
88
Y = 14260887
89 feet Y = 4302001
80 meter
Z = -11112993
81 Z = -3406666
35
XDOT = -7496
512485 XDOT = -2198
949207
YDOT = -18622
805502 feet/sec YDOT = -5701
302070 meter/sec
ZDOT = -15091
456337 ZDOT = -4610
766978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14135508
95 X = 4308503
13
Y = 13132383
87 feet Y = 4002750
60 meter
Z = -11195855
66 Z = -3412496
81
XDOT = -17736
112501 XDOT = -5405
967090
YDOT = 6193
335323 feet/sec YDOT = 1887
728607 meter/sec
ZDOT = -15136
541103 ZDOT = -4613
617728
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 14130
64167643
00016717 00000-0 10270-3 0 9014
2 25544 51
6469 285
6945 0002387 336
9699 23
1344 15
49998233 5507
Satellite: ISS
Catalog Number: 25544
Epoch time: 14130
64167643 = yrday
fracday
Element set: 901
Inclination: 51
6469 deg
RA of node: 285
6945 deg
Eccentricity:
0002387
Arg of perigee: 336
9699 deg
Mean anomaly: 23
1344 deg
Mean motion: 15
49998233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 550
Checksum: 335
Coasting Arc #3 (Orbit 565)
---------------------------------------
Vector Time (GMT): 2014/131/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3737571
65 A = 6795493
92 meter
Y = -4345959
18 meter E =
0011105
Z = 3639014
66 I = 51
29577
XDOT = 2501
759129 Wp = 82
56599
YDOT = 5798
210922 meter/sec RA = 280
11942 deg
ZDOT = 4345
075690 TA = 320
81111
MA = 320
89147
Ha = 227
224 n
mi
Hp = 221
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12262374
19 X = 3768213
87
Y = -14258396
25 feet Y = -4303991
87 meter
Z = 11939024
48 Z = 3657246
10
XDOT = 8207
871157 XDOT = 2415
628898
YDOT = 19023
001711 feet/sec YDOT = 5825
705680 meter/sec
ZDOT = 14255
497671 ZDOT = 4357
019823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14350530
50 X = -4374041
70
Y = -12077500
31 feet Y = -3681222
09 meter
Z = 12016831
96 Z = 3662730
38
XDOT = 18080
619285 XDOT = 5510
972758
YDOT = -7217
775930 feet/sec YDOT = -2199
978104 meter/sec
ZDOT = 14305
019405 ZDOT = 4360
169915
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 14131
67323537
00016717 00000-0 10270-3 0 9025
2 25544 51
6473 280
5836 0002468 341
8960 18
2103 15
50068110 5660
Satellite: ISS
Catalog Number: 25544
Epoch time: 14131
67323537 = yrday
fracday
Element set: 902
Inclination: 51
6473 deg
RA of node: 280
5836 deg
Eccentricity:
0002468
Arg of perigee: 341
8960 deg
Mean anomaly: 18
2103 deg
Mean motion: 15
50068110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 566
Checksum: 289
Coasting Arc #4 (Orbit 580)
---------------------------------------
Vector Time (GMT): 2014/132/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3530306
26 A = 6794652
30 meter
Y = 4302640
59 meter E =
0007082
Z = -3905981
32 I = 51
28851
XDOT = -2721
813808 Wp = 52
38072
YDOT = -5902
016400 meter/sec RA = 275
14088 deg
ZDOT = -4042
163688 TA = 175
02748
MA = 175
02044
Ha = 227
374 n
mi
Hp = 221
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11582369
61 X = -3559182
56
Y = 14116274
89 feet Y = 4263000
99 meter
Z = -12814899
35 Z = -3923201
56
XDOT = -8929
835327 XDOT = -2635
977868
YDOT = -19363
570865 feet/sec YDOT = -5931
973525 meter/sec
ZDOT = -13261
691891 ZDOT = -4055
177684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14396948
47 X = 4388189
89
Y = 11147134
47 feet Y = 3397646
59 meter
Z = -12888421
77 Z = -3928390
96
XDOT = -18325
768112 XDOT = -5585
694121
YDOT = 8275
748255 feet/sec YDOT = 2522
448068 meter/sec
ZDOT = -13315
724339 ZDOT = -4058
632779
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 14132
64030094
00016717 00000-0 10270-3 0 9037
2 25544 51
6474 275
7928 0002583 344
7230 15
3842 15
50069912 5815
Satellite: ISS
Catalog Number: 25544
Epoch time: 14132
64030094 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 275
7928 deg
Eccentricity:
0002583
Arg of perigee: 344
7230 deg
Mean anomaly: 15
3842 deg
Mean motion: 15
50069912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 581
Checksum: 296
Coasting Arc #5 (Orbit 596)
---------------------------------------
Vector Time (GMT): 2014/133/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3330759
89 A = 6793633
21 meter
Y = -4224668
38 meter E =
0009514
Z = 4140355
11 I = 51
28425
XDOT = 2971
292096 Wp = 89
50027
YDOT = 6003
061730 meter/sec RA = 270
16042 deg
ZDOT = 3727
643518 TA = 321
91330
MA = 321
98051
Ha = 227
251 n
mi
Hp = 221
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10927689
92 X = 3357640
55
Y = -13860460
58 feet Y = -4187271
49 meter
Z = 13583842
23 Z = 4156601
04
XDOT = 9748
333649 XDOT = 2885
835547
YDOT = 19695
084415 feet/sec YDOT = 6035
810720 meter/sec
ZDOT = 12229
801569 ZDOT = 3741
870548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14303162
29 X = -4359603
87
Y = -10249700
33 feet Y = -3124108
66 meter
Z = 13653231
70 Z = 4161505
02
XDOT = 18524
395642 XDOT = 5646
235792
YDOT = -9448
575351 feet/sec YDOT = -2879
925767 meter/sec
ZDOT = 12288
950793 ZDOT = 3745
672202
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 14133
67181061
00016717 00000-0 10270-3 0 9043
2 25544 51
6477 270
6814 0002686 349
6395 10
4700 15
50139676 5977
Satellite: ISS
Catalog Number: 25544
Epoch time: 14133
67181061 = yrday
fracday
Element set: 904
Inclination: 51
6477 deg
RA of node: 270
6814 deg
Eccentricity:
0002686
Arg of perigee: 349
6395 deg
Mean anomaly: 10
4700 deg
Mean motion: 15
50139676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 597
Checksum: 314
Coasting Arc #6 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2014/134/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3178399
11 A = 6792788
59 meter
Y = 4114596
16 meter E =
0009939
Z = -4381958
08 I = 51
28207
XDOT = -3219
707740 Wp = 53
56717
YDOT = -6071
990465 meter/sec RA = 265
18042 deg
ZDOT = -3365
700315 TA = 182
11968
MA = 182
12390
Ha = 227
417 n
mi
Hp = 220
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10427818
59 X = -3202886
59
Y = 13499331
23 feet Y = 4078916
55 meter
Z = -14376502
89 Z = -4397457
94
XDOT = -10563
345604 XDOT = -3135
220202
YDOT = -19921
228560 feet/sec YDOT = -6107
522747 meter/sec
ZDOT = -11042
323868 ZDOT = -3381
136633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14086876
58 X = 4293679
98
Y = 9519606
65 feet Y = 2901576
11 meter
Z = -14442720
55 Z = -4402141
22
XDOT = -18571
233811 XDOT = -5660
512066
YDOT = 10628
677193 feet/sec YDOT = 3239
620808 meter/sec
ZDOT = -11106
580787 ZDOT = -3385
285824
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 14134
63882994
00016717 00000-0 10270-3 0 9054
2 25544 51
6475 265
8908 0002799 352
3425 7
7683 15
50140347 6129
Satellite: ISS
Catalog Number: 25544
Epoch time: 14134
63882994 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 265
8908 deg
Eccentricity:
0002799
Arg of perigee: 352
3425 deg
Mean anomaly: 7
7683 deg
Mean motion: 15
50140347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 327
Coasting Arc #7 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2014/135/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3044505
35 A = 6791780
76 meter
Y = -3971415
86 meter E =
0007541
Z = 4585818
79 I = 51
28325
XDOT = 3491
788050 Wp = 94
39220
YDOT = 6134
467645 meter/sec RA = 260
19859 deg
ZDOT = 2989
564104 TA = 325
59421
MA = 325
64302
Ha = 227
283 n
mi
Hp = 220
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9988534
60 X = 3066411
45
Y = -13029579
59 feet Y = -3937248
07 meter
Z = 15045337
23 Z = 4600661
82
XDOT = 11455
997541 XDOT = 3408
408881
YDOT = 20126
206183 feet/sec YDOT = 6173
048658 meter/sec
ZDOT = 9808
281181 ZDOT = 3006
324961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13746216
20 X = -4189846
70
Y = -8869609
77 feet Y = -2703457
06 meter
Z = 15108755
84 Z = 4605148
78
XDOT = 18550
761174 XDOT = 5654
272006
YDOT = -11896
570456 feet/sec YDOT = -3626
074675 meter/sec
ZDOT = 9878
136775 ZDOT = 3010
856089
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 14135
67029066
00016717 00000-0 10270-3 0 9063
2 25544 51
6479 260
7793 0002910 356
4600 3
6529 15
50210092 6280
Satellite: ISS
Catalog Number: 25544
Epoch time: 14135
67029066 = yrday
fracday
Element set: 906
Inclination: 51
6479 deg
RA of node: 260
7793 deg
Eccentricity:
0002910
Arg of perigee: 356
4600 deg
Mean anomaly: 3
6529 deg
Mean motion: 15
50210092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 297
Coasting Arc #8 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2014/136/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2964064
93 A = 6791020
91 meter
Y = 3810394
38 meter E =
0012628
Z = -4788435
04 I = 51
28599
XDOT = -3754
161213 Wp = 58
61201
YDOT = -6152
074713 meter/sec RA = 255
21748 deg
ZDOT = -2570
257834 TA = 185
88136
MA = 185
89620
Ha = 227
476 n
mi
Hp = 220
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9724622
47 X = -2983192
26
Y = 12501293
89 feet Y = 3777141
74 meter
Z = -15710088
72 Z = -4802880
44
XDOT = -12316
801880 XDOT = -3672
602603
YDOT = -20183
972155 feet/sec YDOT = -6193
599924 meter/sec
ZDOT = -8432
604443 ZDOT = -2588
297727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13345643
16 X = 4067752
04
Y = 8414368
84 feet Y = 2564699
62 meter
Z = -15771801
56 Z = -4807245
11
XDOT = -18335
299991 XDOT = -5588
599437
YDOT = 13125
079884 feet/sec YDOT = 4000
524349 meter/sec
ZDOT = -8507
877280 ZDOT = -2593
200995
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 14136
63726429
00016717 00000-0 10270-3 0 9078
2 25544 51
6470 255
9884 0003031 359
8978
2172 15
50209201 6432
Satellite: ISS
Catalog Number: 25544
Epoch time: 14136
63726429 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 255
9884 deg
Eccentricity:
0003031
Arg of perigee: 359
8978 deg
Mean anomaly:
2172 deg
Mean motion: 15
50209201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 304
Coasting Arc #9 (Orbit 658)
---------------------------------------
Vector Time (GMT): 2014/137/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2911741
24 A = 6790118
16 meter
Y = -3620322
30 meter E =
0005480
Z = 4947168
27 I = 51
29272
XDOT = 4030
964384 Wp = 92
80416
YDOT = 6161
151373 meter/sec RA = 250
23505 deg
ZDOT = 2133
900916 TA = 336
28389
MA = 336
30914
Ha = 227
333 n
mi
Hp = 220
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9552956
82 X = 2927976
05
Y = -11877697
84 feet Y = -3587671
00 meter
Z = 16230867
02 Z = 4961352
39
XDOT = 13224
948768 XDOT = 3951
403471
YDOT = 20213
751223 feet/sec YDOT = 6205
783169 meter/sec
ZDOT = 7000
987257 ZDOT = 2153
290296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12849235
83 X = -3916447
08
Y = -8078717
35 feet Y = -2462393
05 meter
Z = 16291445
57 Z = 4965632
61
XDOT = 18042
448022 XDOT = 5499
338157
YDOT = -14399
884738 feet/sec YDOT = -4389
084868 meter/sec
ZDOT = 7081
980461 ZDOT = 2158
587644
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 14137
66867654
00016717 00000-0 10270-3 0 9089
2 25544 51
6472 250
8768 0003141 3
4303 356
6869 15
50278996 6590
Satellite: ISS
Catalog Number: 25544
Epoch time: 14137
66867654 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 250
8768 deg
Eccentricity:
0003141
Arg of perigee: 3
4303 deg
Mean anomaly: 356
6869 deg
Mean motion: 15
50278996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 659
Checksum: 343
Coasting Arc #10 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2014/138/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2914735
66 A = 6789539
09 meter
Y = 3429887
61 meter E =
0014819
Z = -5096401
57 I = 51
30091
XDOT = -4285
774158 Wp = 65
49420
YDOT = -6115
864915 meter/sec RA = 245
25296 deg
ZDOT = -1662
673434 TA = 188
32546
MA = 188
35008
Ha = 227
549 n
mi
Hp = 220
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9562781
05 X = -2928115
94
Y = 11252912
12 feet Y = 3397218
77 meter
Z = -16720477
58 Z = -5110593
27
XDOT = -14060
938837 XDOT = -4208
989844
YDOT = -20065
173605 feet/sec YDOT = -6163
361730 meter/sec
ZDOT = -5454
965334 ZDOT = -1683
307283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12367452
11 X = 3769599
40
Y = 7943008
92 feet Y = 2421029
12 meter
Z = -16781058
39 Z = -5114866
60
XDOT = -17530
252550 XDOT = -5343
220977
YDOT = 15572
970363 feet/sec YDOT = 4746
641367 meter/sec
ZDOT = -5541
246803 ZDOT = -1688
972026
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 14138
63560509
00016717 00000-0 10270-3 0 9097
2 25544 51
6460 246
0850 0003274 7
6819 352
4381 15
50277812 6747
Satellite: ISS
Catalog Number: 25544
Epoch time: 14138
63560509 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 246
0850 deg
Eccentricity:
0003274
Arg of perigee: 7
6819 deg
Mean anomaly: 352
4381 deg
Mean motion: 15
50277812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 308
Coasting Arc #11 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2014/139/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2953159
29 A = 6788851
67 meter
Y = -3216623
38 meter E =
0004130
Z = 5194487
22 I = 51
31327
XDOT = 4542
657704 Wp = 75
27609
YDOT = 6062
476716 meter/sec RA = 240
27057 deg
ZDOT = 1171
780383 TA = 3
43205
MA = 3
42922
Ha = 227
410 n
mi
Hp = 220
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9688842
81 X = 2963675
54
Y = -10553226
33 feet Y = -3183540
82 meter
Z = 17042280
89 Z = 5208858
64
XDOT = 14903
732626 XDOT = 4468
835933
YDOT = 19890
015471 feet/sec YDOT = 6112
862789 meter/sec
ZDOT = 3844
423829 ZDOT = 1193
669193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11827871
07 X = -3605135
10
Y = -7953133
98 feet Y = -2424115
24 meter
Z = 17103588
06 Z = 5213173
64
XDOT = 16946
512809 XDOT = 5165
297104
YDOT = -16739
889321 feet/sec YDOT = -5102
318265 meter/sec
ZDOT = 3936
041036 ZDOT = 1199
705308
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 14139
66696967
00016717 00000-0 10270-3 0 9101
2 25544 51
6461 240
9731 0003379 11
3690 348
7536 15
50347065 6900
Satellite: ISS
Catalog Number: 25544
Epoch time: 14139
66696967 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 240
9731 deg
Eccentricity:
0003379
Arg of perigee: 11
3690 deg
Mean anomaly: 348
7536 deg
Mean motion: 15
50347065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 325
Coasting Arc #12 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2014/140/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3043163
13 A = 6788547
70 meter
Y = 3022341
71 meter E =
0016186
Z = -5275965
36 I = 51
32789
XDOT = -4763
204565 Wp = 73
21921
YDOT = -5950
490734 meter/sec RA = 235
28825 deg
ZDOT = -658
445224 TA = 190
43499
MA = 190
46863
Ha = 227
626 n
mi
Hp = 220
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9984131
01 X = -3051104
42
Y = 9915819
27 feet Y = 2988266
98 meter
Z = -17309597
64 Z = -5290767
81
XDOT = -15627
311565 XDOT = -4693
112286
YDOT = -19522
607396 feet/sec YDOT = -6003
364005 meter/sec
ZDOT = -2160
253360 ZDOT = -681
414349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11381393
92 X = 3469048
87
Y = 8141361
64 feet Y = 2481487
03 meter
Z = -17372697
47 Z = -5295198
19
XDOT = -16145
928961 XDOT = -4921
279147
YDOT = 17736
305916 feet/sec YDOT = 5406
026043 meter/sec
ZDOT = -2256
477036 ZDOT = -687
774201
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 14140
63385399
00016717 00000-0 10270-3 0 9115
2 25544 51
6456 236
1803 0003513 15
5945 344
5313 15
50347251 7051
Satellite: ISS
Catalog Number: 25544
Epoch time: 14140
63385399 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 236
1803 deg
Eccentricity:
0003513
Arg of perigee: 15
5945 deg
Mean anomaly: 344
5313 deg
Mean motion: 15
50347251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 290
Coasting Arc #13 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2014/141/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3172318
08 A = 6788184
09 meter
Y = -2812929
35 meter E =
0004784
Z = 5298014
10 I = 51
34572
XDOT = 4971
122003 Wp = 49
92953
YDOT = 5834
048709 meter/sec RA = 230
30689 deg
ZDOT = 123
897325 TA = 38
90177
MA = 38
86735
Ha = 227
500 n
mi
Hp = 219
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10407867
72 X = 3177800
93
Y = -9228770
84 feet Y = -2777423
98 meter
Z = 17381936
02 Z = 5313438
08
XDOT = 16309
455392 XDOT = 4904
913024
YDOT = 19140
579753 feet/sec YDOT = 5889
268788 meter/sec
ZDOT = 406
487288 ZDOT = 147
885852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10919415
02 X = -3328237
70
Y = -8483637
58 feet Y = -2585812
74 meter
Z = 17447632
81 Z = 5318038
48
XDOT = 15299
218858 XDOT = 4663
201908
YDOT = -18668
843952 feet/sec YDOT = -5690
263636 meter/sec
ZDOT = 507
059052 ZDOT = 154
551599
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 14141
66517224
00016717 00000-0 10270-3 0 9124
2 25544 51
6455 231
0681 0003619 19
9038 340
2254 15
50415296 7216
Satellite: ISS
Catalog Number: 25544
Epoch time: 14141
66517224 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 231
0681 deg
Eccentricity:
0003619
Arg of perigee: 19
9038 deg
Mean anomaly: 340
2254 deg
Mean motion: 15
50415296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 284
Coasting Arc #14 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2014/142/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3343163
55 A = 6788235
19 meter
Y = 2641621
88 meter E =
0016432
Z = -5298386
24 I = 51
36705
XDOT = -5128
761908 Wp = 80
98720
YDOT = -5661
578111 meter/sec RA = 225
32604 deg
ZDOT = 417
068557 TA = 192
99333
MA = 193
03571
Ha = 227
689 n
mi
Hp = 219
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10968384
35 X = -3346716
22
Y = 8666738
46 feet Y = 2604216
75 meter
Z = -17383156
96 Z = -5314635
56
XDOT = -16826
646680 XDOT = -5067
097676
YDOT = -18574
731335 feet/sec YDOT = -5718
586448 meter/sec
ZDOT = 1368
335160 ZDOT = 392
303173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10622207
76 X = 3237648
93
Y = 8954170
71 feet Y = 2729231
23 meter
Z = -17452320
36 Z = -5319467
25
XDOT = -14269
307478 XDOT = -4349
284919
YDOT = 19368
814966 feet/sec YDOT = 5903
614802 meter/sec
ZDOT = 1264
434856 ZDOT = 385
399744
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 14142
63201352
00016717 00000-0 10270-3 0 9135
2 25544 51
6461 226
2747 0003731 23
1734 336
9585 15
50416685 7365
Satellite: ISS
Catalog Number: 25544
Epoch time: 14142
63201352 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 226
2747 deg
Eccentricity:
0003731
Arg of perigee: 23
1734 deg
Mean anomaly: 336
9585 deg
Mean motion: 15
50416685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 294
Coasting Arc #15 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2014/143/14:47:49
039
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3552342
05 A = 6788275
32 meter
Y = -2463074
92 meter E =
0007089
Z = 5230565
22 I = 51
38973
XDOT = 5257
840296 Wp = 42
84429
YDOT = 5491
988866 meter/sec RA = 220
34692 deg
ZDOT = -978
803354 TA = 56
59404
MA = 56
52624
Ha = 227
579 n
mi
Hp = 219
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11654665
53 X = 3554211
98
Y = -8080954
46 feet Y = -2423340
04 meter
Z = 17160647
06 Z = 5247826
69
XDOT = 17250
132205 XDOT = 5200
791624
YDOT = 18018
336174 feet/sec YDOT = 5550
466463 meter/sec
ZDOT = -3211
297094 ZDOT = -953
399607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10348377
23 X = -3154185
38
Y = -9566548
06 feet Y = -2915883
85 meter
Z = 17234068
24 Z = 5252944
00
XDOT = 13239
672489 XDOT = 4035
452175
YDOT = -19949
330095 feet/sec YDOT = -6080
555813 meter/sec
ZDOT = -3104
656884 ZDOT = -946
299418
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 14143
66328702
00016717 00000-0 10270-3 0 9149
2 25544 51
6454 221
1622 0003846 28
0128 332
1229 15
50483794 7527
Satellite: ISS
Catalog Number: 25544
Epoch time: 14143
66328702 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 221
1622 deg
Eccentricity:
0003846
Arg of perigee: 28
0128 deg
Mean anomaly: 332
1229 deg
Mean motion: 15
50483794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 290
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