[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 3rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
198/01:00:36
719 2
3 3
7 3
7
N/A -2
9 -0
0 225
3
000/00:01:13
438 -0
2 0
0 223
5
Coasting Arc #1 (Orbit 2824)
---------------------------------------
Vector Time (GMT): 2014/183/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6433953
59 A = 6799064
32 meter
Y = 1342371
60 meter E =
0004293
Z = -1735742
95 I = 51
81370
XDOT = 468
814351 Wp = 46
09941
YDOT = 5099
989342 meter/sec RA = 23
77369 deg
ZDOT = 5693
626290 TA = 294
94379
MA = 294
98839
Ha = 226
743 n
mi
Hp = 221
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21108771
63 X = 6426896
30
Y = 4404106
29 feet Y = 1414280
89 meter
Z = -5694694
73 Z = -1704505
05
XDOT = 1538
104825 XDOT = 384
092730
YDOT = 16732
248496 feet/sec YDOT = 5104
757743 meter/sec
ZDOT = 18679
876280 ZDOT = 5695
698348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17157945
86 X = 5229741
90
Y = -13117570
55 feet Y = -3998235
50 meter
Z = -5562389
49 Z = -1695416
32
XDOT = 12632
945845 XDOT = 3850
521894
YDOT = 8616
328124 feet/sec YDOT = 2626
256812 meter/sec
ZDOT = 18687
687681 ZDOT = 5696
007205
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 14183
36354415
00016717 00000-0 10270-3 0 9005
2 25544 51
6487 24
3405 0003488 207
8035 152
2929 15
50368131 28259
Satellite: ISS
Catalog Number: 25544
Epoch time: 14183
36354415 = yrday
fracday
Element set: 900
Inclination: 51
6487 deg
RA of node: 24
3405 deg
Eccentricity:
0003488
Arg of perigee: 207
8035 deg
Mean anomaly: 152
2929 deg
Mean motion: 15
50368131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2825
Checksum: 298
Coasting Arc #2 (Orbit 2840)
---------------------------------------
Vector Time (GMT): 2014/184/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6565648
01 A = 6799730
82 meter
Y = -1176615
80 meter E =
0014212
Z = 1277206
26 I = 51
78679
XDOT = -255
920951 Wp = 135
40130
YDOT = -4950
867286 meter/sec RA = 18
83040 deg
ZDOT = -5846
957511 TA = 30
75045
MA = 30
66726
Ha = 226
756 n
mi
Hp = 221
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21540839
93 X = -6558207
06
Y = -3860288
06 feet Y = -1249995
59 meter
Z = 4190309
25 Z = 1245329
49
XDOT = -839
635667 XDOT = -172
137782
YDOT = -16243
002906 feet/sec YDOT = -4953
260267 meter/sec
ZDOT = -19182
931468 ZDOT = -5847
997594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16783182
42 X = -5115514
00
Y = 14083603
68 feet Y = 4292682
40 meter
Z = 4055267
65 Z = 1236045
58
XDOT = -11905
064323 XDOT = -3628
663606
YDOT = -8633
600237 feet/sec YDOT = -2631
521352 meter/sec
ZDOT = -19186
390744 ZDOT = -5848
011899
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 14184
39487972
00016717 00000-0 10270-3 0 9015
2 25544 51
6488 19
2287 0003541 210
6186 149
4758 15
50337324 28416
Satellite: ISS
Catalog Number: 25544
Epoch time: 14184
39487972 = yrday
fracday
Element set: 901
Inclination: 51
6488 deg
RA of node: 19
2287 deg
Eccentricity:
0003541
Arg of perigee: 210
6186 deg
Mean anomaly: 149
4758 deg
Mean motion: 15
50337324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2841
Checksum: 325
Coasting Arc #3 (Orbit 2855)
---------------------------------------
Vector Time (GMT): 2014/185/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6674988
94 A = 6799908
87 meter
Y = 976412
60 meter E =
0006846
Z = -829712
53 I = 51
75866
XDOT = 27
945152 Wp = 40
14430
YDOT = 4831
819683 meter/sec RA = 13
88455 deg
ZDOT = 5943
389944 TA = 310
91422
MA = 310
97348
Ha = 226
448 n
mi
Hp = 221
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21899570
01 X = 6667604
83
Y = 3203453
43 feet Y = 1051015
40 meter
Z = -2722153
98 Z = -797304
40
XDOT = 91
683571 XDOT = -54
958370
YDOT = 15852
426782 feet/sec YDOT = 4831
668234 meter/sec
ZDOT = 19499
310841 ZDOT = 5943
324665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16246429
67 X = 4951911
76
Y = -15054421
20 feet Y = -4588587
58 meter
Z = -2584826
55 Z = -787855
13
XDOT = 11227
253522 XDOT = 3422
066874
YDOT = 8787
674986 feet/sec YDOT = 2678
483336 meter/sec
ZDOT = 19498
100983 ZDOT = 5943
021180
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 14185
36174367
00016717 00000-0 10270-3 0 9025
2 25544 51
6491 14
4357 0003450 218
1452 141
9455 15
50404681 28561
Satellite: ISS
Catalog Number: 25544
Epoch time: 14185
36174367 = yrday
fracday
Element set: 902
Inclination: 51
6491 deg
RA of node: 14
4357 deg
Eccentricity:
0003450
Arg of perigee: 218
1452 deg
Mean anomaly: 141
9455 deg
Mean motion: 15
50404681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2856
Checksum: 300
Coasting Arc #4 (Orbit 2871)
---------------------------------------
Vector Time (GMT): 2014/186/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6738163
23 A = 6800251
89 meter
Y = -785267
54 meter E =
0013158
Z = 343677
40 I = 51
72894
XDOT = 243
142939 Wp = 146
73406
YDOT = -4757
397728 meter/sec RA = 8
93793 deg
ZDOT = -6004
830056 TA = 29
57082
MA = 29
49647
Ha = 226
432 n
mi
Hp = 221
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22106834
73 X = -6730550
86
Y = -2576337
07 feet Y = -860575
48 meter
Z = 1127550
51 Z = 310962
85
XDOT = 797
713053 XDOT = 325
492648
YDOT = -15608
260262 feet/sec YDOT = -4754
217883 meter/sec
ZDOT = -19700
886010 ZDOT = -6003
449216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15611308
88 X = -4758326
95
Y = 15872307
61 feet Y = 4837879
36 meter
Z = 988893
80 Z = 301414
83
XDOT = -10597
754558 XDOT = -3230
195589
YDOT = -9173
584495 feet/sec YDOT = -2796
108554 meter/sec
ZDOT = -19694
106698 ZDOT = -6002
763721
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 14186
39305626
00016717 00000-0 10270-3 0 9034
2 25544 51
6490 9
3240 0003544 220
7927 139
2959 15
50366205 28720
Satellite: ISS
Catalog Number: 25544
Epoch time: 14186
39305626 = yrday
fracday
Element set: 903
Inclination: 51
6490 deg
RA of node: 9
3240 deg
Eccentricity:
0003544
Arg of perigee: 220
7927 deg
Mean anomaly: 139
2959 deg
Mean motion: 15
50366205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2872
Checksum: 308
Coasting Arc #5 (Orbit 2887)
---------------------------------------
Vector Time (GMT): 2014/187/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6770592
98 A = 6800050
30 meter
Y = 570732
82 meter E =
0008927
Z = 124686
98 I = 51
69781
XDOT = -513
635202 Wp = 46
26158
YDOT = 4722
725069 meter/sec RA = 3
98794 deg
ZDOT = 6010
286778 TA = 315
07813
MA = 315
15033
Ha = 226
152 n
mi
Hp = 221
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22213231
56 X = 6763102
02
Y = 1872482
99 feet Y = 646404
05 meter
Z = 409078
00 Z = 157559
43
XDOT = -1685
154862 XDOT = -595
603666
YDOT = 15494
504819 feet/sec YDOT = 4716
522488 meter/sec
ZDOT = 19718
788641 ZDOT = 6007
592882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14831258
43 X = 4520567
57
Y = -16638334
70 feet Y = -5071364
42 meter
Z = 548438
93 Z = 167164
19
XDOT = 10093
735332 XDOT = 3076
570529
YDOT = 9668
250849 feet/sec YDOT = 2946
882859 meter/sec
ZDOT = 19706
443054 ZDOT = 6006
523843
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 14187
42435371
00016717 00000-0 10270-3 0 9041
2 25544 51
6487 4
2111 0003464 228
5116 131
5738 15
50443311 28885
Satellite: ISS
Catalog Number: 25544
Epoch time: 14187
42435371 = yrday
fracday
Element set: 904
Inclination: 51
6487 deg
RA of node: 4
2111 deg
Eccentricity:
0003464
Arg of perigee: 228
5116 deg
Mean anomaly: 131
5738 deg
Mean motion: 15
50443311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2888
Checksum: 290
Coasting Arc #6 (Orbit 2902)
---------------------------------------
Vector Time (GMT): 2014/188/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6754070
53 A = 6799988
02 meter
Y = -379543
37 meter E =
0011071
Z = -623487
08 I = 51
66577
XDOT = 813
129938 Wp = 157
77930
YDOT = -4735
347036 meter/sec RA = 359
03698 deg
ZDOT = -5970
500511 TA = 28
93991
MA = 28
87857
Ha = 226
083 n
mi
Hp = 221
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22159024
06 X = -6746295
71
Y = -1245221
03 feet Y = -455028
20 meter
Z = -2045561
29 Z = -656278
61
XDOT = 2667
749139 XDOT = 895
024050
YDOT = -15535
915471 feet/sec YDOT = -4725
795645 meter/sec
ZDOT = -19588
256270 ZDOT = -5966
351956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13997106
62 X = -4266318
10
Y = 17206560
63 feet Y = 5244559
68 meter
Z = -2184610
08 Z = -665869
15
XDOT = -9693
271947 XDOT = -2954
509289
YDOT = -10352
451858 feet/sec YDOT = -3155
427326 meter/sec
ZDOT = -19569
734734 ZDOT = -5964
855147
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 14188
39118773
00016717 00000-0 10270-3 0 9053
2 25544 51
6483 359
4188 0003555 231
5491 128
5341 15
50404853 29033
Satellite: ISS
Catalog Number: 25544
Epoch time: 14188
39118773 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 359
4188 deg
Eccentricity:
0003555
Arg of perigee: 231
5491 deg
Mean anomaly: 128
5341 deg
Mean motion: 15
50404853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2903
Checksum: 320
Coasting Arc #7 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2014/189/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6702924
65 A = 6799405
42 meter
Y = 178728
90 meter E =
0010113
Z = 1097562
16 I = 51
63270
XDOT = -1095
742580 Wp = 56
90363
YDOT = 4791
614365 meter/sec RA = 354
08186 deg
ZDOT = 5877
634649 TA = 314
98606
MA = 315
06798
Ha = 225
863 n
mi
Hp = 221
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21991222
62 X = 6695096
28
Y = 586380
92 feet Y = 253641
43 meter
Z = 3600925
73 Z = 1130105
08
XDOT = -3594
955970 XDOT = -1177
793759
YDOT = 15720
519570 feet/sec YDOT = 4778
901641 meter/sec
ZDOT = 19283
578246 ZDOT = 5872
112913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13057321
86 X = 3979871
70
Y = -17676281
94 feet Y = -5387730
73 meter
Z = 3738954
90 Z = 1139633
45
XDOT = 9474
671498 XDOT = 2887
879873
YDOT = 11095
303651 feet/sec YDOT = 3381
848553 meter/sec
ZDOT = 19259
218390 ZDOT = 5870
209765
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 14189
42246219
00016717 00000-0 10270-3 0 9066
2 25544 51
6475 354
3053 0003525 237
9606 122
1203 15
50481163 29197
Satellite: ISS
Catalog Number: 25544
Epoch time: 14189
42246219 = yrday
fracday
Element set: 906
Inclination: 51
6475 deg
RA of node: 354
3053 deg
Eccentricity:
0003525
Arg of perigee: 237
9606 deg
Mean anomaly: 122
1203 deg
Mean motion: 15
50481163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 297
Coasting Arc #8 (Orbit 2933)
---------------------------------------
Vector Time (GMT): 2014/190/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6604991
28 A = 6798902
60 meter
Y = -16055
68 meter E =
0008050
Z = -1592015
98 I = 51
59929
XDOT = 1390
014304 Wp = 167
31813
YDOT = -4892
354785 meter/sec RA = 349
12555 deg
ZDOT = -5730
766424 TA = 30
07935
MA = 30
03314
Ha = 225
754 n
mi
Hp = 221
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21669918
90 X = -6596587
35
Y = -52676
12 feet Y = -89869
75 meter
Z = -5223149
54 Z = -1624081
66
XDOT = 4560
414383 XDOT = 1472
456615
YDOT = -16051
032758 feet/sec YDOT = -4876
349054 meter/sec
ZDOT = -18801
727114 ZDOT = -5723
814317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12123600
37 X = -3695273
39
Y = 17921130
29 feet Y = 5462360
51 meter
Z = -5359184
10 Z = -1633479
31
XDOT = -9399
324382 XDOT = -2864
914072
YDOT = -11959
427623 feet/sec YDOT = -3645
233540 meter/sec
ZDOT = -18771
278403 ZDOT = -5721
485657
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 14190
38927405
00016717 00000-0 10270-3 0 9077
2 25544 51
6469 349
5125 0003544 242
1315 117
9477 15
50454307 29344
Satellite: ISS
Catalog Number: 25544
Epoch time: 14190
38927405 = yrday
fracday
Element set: 907
Inclination: 51
6469 deg
RA of node: 349
5125 deg
Eccentricity:
0003544
Arg of perigee: 242
1315 deg
Mean anomaly: 117
9477 deg
Mean motion: 15
50454307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2934
Checksum: 315
Coasting Arc #9 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2014/191/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6473624
97 A = 6797999
12 meter
Y = -141547
76 meter E =
0010308
Z = 2054405
82 I = 51
56589
XDOT = -1652
634773 Wp = 70
24579
YDOT = 5034
554769 meter/sec RA = 344
16477 deg
ZDOT = 5535
231458 TA = 312
46442
MA = 312
55151
Ha = 225
596 n
mi
Hp = 221
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21238927
08 X = 6464747
07
Y = -464395
52 feet Y = -69205
44 meter
Z = 6740176
58 Z = 2085832
05
XDOT = -5422
030094 XDOT = -1735
697723
YDOT = 16517
568141 feet/sec YDOT = 5015
608740 meter/sec
ZDOT = 18160
208194 ZDOT = 5527
002179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11140150
97 X = 3395518
02
Y = -18038550
33 feet Y = -5498150
14 meter
Z = 6873529
32 Z = 2095051
74
XDOT = 9535
072998 XDOT = 2906
290250
YDOT = 12818
432034 feet/sec YDOT = 3907
058084 meter/sec
ZDOT = 18124
313805 ZDOT = 5524
290848
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 14191
42052566
00016717 00000-0 10270-3 0 9081
2 25544 51
6463 344
3984 0003589 246
5828 113
4946 15
50516387 29507
Satellite: ISS
Catalog Number: 25544
Epoch time: 14191
42052566 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 344
3984 deg
Eccentricity:
0003589
Arg of perigee: 246
5828 deg
Mean anomaly: 113
4946 deg
Mean motion: 15
50516387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 332
Coasting Arc #10 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2014/192/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6303107
32 A = 6797095
47 meter
Y = 247615
47 meter E =
0004398
Z = -2525499
58 I = 51
53256
XDOT = 1908
460240 Wp = 170
02543
YDOT = -5212
037713 meter/sec RA = 339
20258 deg
ZDOT = -5279
746480 TA = 38
31538
MA = 38
28415
Ha = 225
512 n
mi
Hp = 221
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20679485
96 X = -6293139
82
Y = 812386
72 feet Y = 177186
16 meter
Z = -8285759
78 Z = -2556094
63
XDOT = 6261
352492 XDOT = 1992
247637
YDOT = -17099
861262 feet/sec YDOT = -5190
226860 meter/sec
ZDOT = -17322
002887 ZDOT = -5270
272762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10231793
24 X = -3118650
58
Y = 17928827
90 feet Y = 5464706
74 meter
Z = -8415608
35 Z = -2565077
43
XDOT = -9828
304771 XDOT = -2995
667294
YDOT = -13711
822017 feet/sec YDOT = -4179
363351 meter/sec
ZDOT = -17280
796882 ZDOT = -5267
186890
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 14192
38731549
00016717 00000-0 10270-3 0 9093
2 25544 51
6457 339
6051 0003482 251
6160 108
4613 15
50507749 29653
Satellite: ISS
Catalog Number: 25544
Epoch time: 14192
38731549 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 339
6051 deg
Eccentricity:
0003482
Arg of perigee: 251
6160 deg
Mean anomaly: 108
4613 deg
Mean motion: 15
50507749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2965
Checksum: 320
Coasting Arc #11 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2014/193/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6105286
54 A = 6795969
82 meter
Y = -334933
57 meter E =
0009586
Z = 2957014
36 I = 51
50027
XDOT = -2121
397225 Wp = 85
78668
YDOT = 5423
212989 meter/sec RA = 334
23625 deg
ZDOT = 4980
993554 TA = 308
01395
MA = 308
10046
Ha = 225
375 n
mi
Hp = 221
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20030467
66 X = 6094214
09
Y = -1098863
41 feet Y = -266722
61 meter
Z = 9701490
68 Z = 2986645
58
XDOT = -6959
964649 XDOT = -2206
078849
YDOT = 17792
693532 feet/sec YDOT = 5399
016038 meter/sec
ZDOT = 16341
842368 ZDOT = 4970
483279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9337721
74 X = 2846137
59
Y = -17685525
31 feet Y = -5390548
12 meter
Z = 9827268
40 Z = 2995351
41
XDOT = 10330
575149 XDOT = 3148
759305
YDOT = 14533
583091 feet/sec YDOT = 4429
836126 meter/sec
ZDOT = 16296
202960 ZDOT = 4967
082662
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 14193
41854430
00016717 00000-0 10270-3 0 9105
2 25544 51
6456 334
4910 0003602 254
4350 105
6403 15
50548627 29819
Satellite: ISS
Catalog Number: 25544
Epoch time: 14193
41854430 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 334
4910 deg
Eccentricity:
0003602
Arg of perigee: 254
4350 deg
Mean anomaly: 105
6403 deg
Mean motion: 15
50548627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 288
Coasting Arc #12 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2014/194/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5881199
80 A = 6794793
86 meter
Y = 360809
21 meter E =
0001667
Z = -3384602
26 I = 51
46857
XDOT = 2310
705388 Wp = 110
57621
YDOT = -5654
152527 meter/sec RA = 329
26825 deg
ZDOT = -4620
335161 TA = 108
97195
MA = 108
95389
Ha = 225
387 n
mi
Hp = 221
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19295274
94 X = -5868356
36
Y = 1183757
24 feet Y = 295114
02 meter
Z = -11104338
13 Z = -3413140
52
XDOT = 7581
054422 XDOT = 2396
203345
YDOT = -18550
369182 feet/sec YDOT = -5627
834190 meter/sec
ZDOT = -15158
579923 ZDOT = -4608
903236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8586763
69 X = -2617245
57
Y = 17241555
72 feet Y = 5255226
18 meter
Z = -11225483
85 Z = -3421527
48
XDOT = -10972
267166 XDOT = -3344
347032
YDOT = -15296
398051 feet/sec YDOT = -4662
342126 meter/sec
ZDOT = -15108
993980 ZDOT = -4605
221365
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 14194
38531237
00016717 00000-0 10270-3 0 9110
2 25544 51
6453 329
6977 0003376 259
6217 100
4553 15
50555733 29963
Satellite: ISS
Catalog Number: 25544
Epoch time: 14194
38531237 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 329
6977 deg
Eccentricity:
0003376
Arg of perigee: 259
6217 deg
Mean anomaly: 100
4553 deg
Mean motion: 15
50555733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 327
Coasting Arc #13 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2014/195/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5640024
91 A = 6793567
50 meter
Y = -357077
50 meter E =
0008103
Z = 3765066
21 I = 51
43820
XDOT = -2451
052534 Wp = 103
35858
YDOT = 5906
593351 meter/sec RA = 324
29647 deg
ZDOT = 4222
312762 TA = 301
80072
MA = 301
87961
Ha = 225
221 n
mi
Hp = 221
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18504018
73 X = 5625309
55
Y = -1171514
10 feet Y = -294089
70 meter
Z = 12352579
44 Z = 3792428
33
XDOT = -8041
510938 XDOT = -2537
429464
YDOT = 19378
587109 feet/sec YDOT = 5878
700795 meter/sec
ZDOT = 13852
732160 ZDOT = 4210
196822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7912195
11 X = 2411637
07
Y = -16681883
70 feet Y = -5084638
15 meter
Z = 12468732
81 Z = 3800469
76
XDOT = 11790
045965 XDOT = 3593
606010
YDOT = 15929
964535 feet/sec YDOT = 4855
453190 meter/sec
ZDOT = 13800
206623 ZDOT = 4206
302979
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 14195
41651828
00016717 00000-0 10270-3 0 9125
2 25544 51
6451 324
5839 0003548 261
8895 98
1854 15
50579525 30122
Satellite: ISS
Catalog Number: 25544
Epoch time: 14195
41651828 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 324
5839 deg
Eccentricity:
0003548
Arg of perigee: 261
8895 deg
Mean anomaly: 98
1854 deg
Mean motion: 15
50579525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 331
Coasting Arc #14 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2014/196/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5389602
11 A = 6792312
43 meter
Y = 287506
61 meter E =
0004627
Z = -4128842
06 I = 51
40960
XDOT = 2555
365031 Wp = 58
92822
YDOT = -6158
175040 meter/sec RA = 319
32284 deg
ZDOT = -3765
276469 TA = 172
08980
MA = 172
08250
Ha = 225
342 n
mi
Hp = 221
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17682421
63 X = -5372360
30
Y = 943263
16 feet Y = 227333
26 meter
Z = -13546069
74 Z = -4154981
60
XDOT = 8383
743541 XDOT = 2642
327392
YDOT = -20203
986351 feet/sec YDOT = -6129
112840 meter/sec
ZDOT = -12353
269255 ZDOT = -3752
652248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7436116
82 X = -2266528
41
Y = 15976350
04 feet Y = 4869591
49 meter
Z = -13657019
87 Z = -4162659
66
XDOT = -12695
650039 XDOT = -3869
634132
YDOT = -16420
034535 feet/sec YDOT = -5004
826526 meter/sec
ZDOT = -12298
551738 ZDOT = -3748
598570
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 14196
38326465
00016717 00000-0 10270-3 0 9139
2 25544 51
6453 319
7908 0003267 266
7754 93
3023 15
50594910 30279
Satellite: ISS
Catalog Number: 25544
Epoch time: 14196
38326465 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 319
7908 deg
Eccentricity:
0003267
Arg of perigee: 266
7754 deg
Mean anomaly: 93
3023 deg
Mean motion: 15
50594910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 322
Coasting Arc #15 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2014/197/08:38:42
814
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5134906
93 A = 6791136
68 meter
Y = -181723
04 meter E =
0006032
Z = 4438106
78 I = 51
38216
XDOT = -2610
848909 Wp = 123
01211
YDOT = 6416
190448 meter/sec RA = 314
34532 deg
ZDOT = 3277
010630 TA = 293
77286
MA = 293
83611
Ha = 225
142 n
mi
Hp = 221
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16846807
50 X = 5114998
80
Y = -596204
20 feet Y = -124412
72 meter
Z = 14560717
80 Z = 4463002
69
XDOT = -8565
777262 XDOT = -2698
320591
YDOT = 21050
493596 feet/sec YDOT = 6386
505019 meter/sec
ZDOT = 10751
347210 ZDOT = 3264
115530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7086656
20 X = 2160012
81
Y = -15194138
17 feet Y = -4631173
31 meter
Z = 14666368
14 Z = 4470309
01
XDOT = 13718
100567 XDOT = 4181
277053
YDOT = 16742
499143 feet/sec YDOT = 5103
113739 meter/sec
ZDOT = 10695
444204 ZDOT = 3259
971393
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 14197
41444763
00016717 00000-0 10270-3 0 9147
2 25544 51
6447 314
6769 0003452 269
5499 90
5257 15
50609798 30431
Satellite: ISS
Catalog Number: 25544
Epoch time: 14197
41444763 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 314
6769 deg
Eccentricity:
0003452
Arg of perigee: 269
5499 deg
Mean anomaly: 90
5257 deg
Mean motion: 15
50609798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 342
Coasting Arc #16 (Orbit 3052)
---------------------------------------
Vector Time (GMT): 2014/198/01:01:13
438
Vector Time (MET): N/A
Weight (LBS) : 887919
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3353986
47 A = 6789630
52 meter
Y = -2605501
88 meter E =
0008566
Z = -5304728
11 I = 51
35903
XDOT = 4891
230232 Wp = 85
40863
YDOT = -5885
766154 meter/sec RA = 310
93226 deg
ZDOT = -201
268615 TA = 182
66017
MA = 182
66473
Ha = 225
331 n
mi
Hp = 223
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11003892
61 X = -3298833
55
Y = -8548234
52 feet Y = -2642699
71 meter
Z = -17403963
63 Z = -5320887
25
XDOT = 16047
343282 XDOT = 4957
660375
YDOT = -19310
256411 feet/sec YDOT = -5830
697826 meter/sec
ZDOT = -660
330102 ZDOT = -177
346917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -274860
12 X = -83777
36
Y = -13845884
65 feet Y = -4220225
64 meter
Z = -17472030
40 Z = -5325474
86
XDOT = 24099
809139 XDOT = 7345
621826
YDOT = 227
022927 feet/sec YDOT = 69
196588 meter/sec
ZDOT = -557
755949 ZDOT = -170
004013
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 14198
05893405
00016717 00000-0 10270-3 0 9150
2 25544 51
6480 311
4855 0006292 272
7710 87
2720 15
49924002 30531
Satellite: ISS
Catalog Number: 25544
Epoch time: 14198
05893405 = yrday
fracday
Element set: 915
Inclination: 51
6480 deg
RA of node: 311
4855 deg
Eccentricity:
0006292
Arg of perigee: 272
7710 deg
Mean anomaly: 87
2720 deg
Mean motion: 15
49924002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3053
Checksum: 305
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