[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 18th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
265/11:30:45
000 0
0 0
0 0
0
N/A 0
0 0
0 227
3
000/00:00:00
000 0
0 0
0 219
8
Coasting Arc #1 (Orbit 2564)
---------------------------------------
Vector Time (GMT): 2014/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3778235
16 A = 6792124
79 meter
Y = -3569108
47 meter E =
0010374
Z = -4382765
64 I = 51
65345
XDOT = 6359
023195 Wp = 76
47288
YDOT = -2537
043017 meter/sec RA = 1
52808 deg
ZDOT = -3420
313596 TA = 158
80957
MA = 158
76657
Ha = 227
558 n
mi
Hp = 219
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12395784
65 X = -3716753
76
Y = -11709673
45 feet Y = -3611015
74 meter
Z = -14379152
36 Z = -4400970
08
XDOT = 20862
936991 XDOT = 6403
535112
YDOT = -8323
631944 feet/sec YDOT = -2465
683712 meter/sec
ZDOT = -11221
501300 ZDOT = -3389
314129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11351460
22 X = 3459925
07
Y = 12637325
51 feet Y = 3851856
81 meter
Z = -14455943
65 Z = -4406171
63
XDOT = -20598
571719 XDOT = -6278
444660
YDOT = 5834
291384 feet/sec YDOT = 1778
292014 meter/sec
ZDOT = -11089
157982 ZDOT = -3379
975353
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 14260
52228398
00016717 00000-0 10270-3 0 9009
2 25544 51
6472 1
9376 0001888 115
1223 245
0124 15
50361128 25651
Satellite: ISS
Catalog Number: 25544
Epoch time: 14260
52228398 = yrday
fracday
Element set: 900
Inclination: 51
6472 deg
RA of node: 1
9376 deg
Eccentricity:
0001888
Arg of perigee: 115
1223 deg
Mean anomaly: 245
0124 deg
Mean motion: 15
50361128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2565
Checksum: 284
Coasting Arc #2 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2014/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3582014
28 A = 6790994
00 meter
Y = 3449852
74 meter E =
0010180
Z = 4618504
49 I = 51
61939
XDOT = -6504
635838 Wp = 114
63674
YDOT = 2753
509977 meter/sec RA = 356
56906 deg
ZDOT = 2978
768409 TA = 305
60031
MA = 305
69512
Ha = 227
386 n
mi
Hp = 219
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11752015
36 X = 3520735
90
Y = 11318414
50 feet Y = 3489566
95 meter
Z = 15152573
79 Z = 4635756
16
XDOT = -21340
668759 XDOT = -6549
412617
YDOT = 9033
825383 feet/sec YDOT = 2680
520850 meter/sec
ZDOT = 9772
862233 ZDOT = 2947
060934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10943616
91 X = -3335614
43
Y = -12010136
50 feet Y = -3660689
60 meter
Z = 15225332
00 Z = 4640681
19
XDOT = 21037
597420 XDOT = 6412
259694
YDOT = -6913
360389 feet/sec YDOT = -2107
192247 meter/sec
ZDOT = 9637
473541 ZDOT = 2937
501935
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 14261
55359874
00016717 00000-0 10270-3 0 9018
2 25544 51
6474 356
8252 0001907 115
3403 244
7945 15
50431723 25816
Satellite: ISS
Catalog Number: 25544
Epoch time: 14261
55359874 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 356
8252 deg
Eccentricity:
0001907
Arg of perigee: 115
3403 deg
Mean anomaly: 244
7945 deg
Mean motion: 15
50431723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 308
Coasting Arc #3 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2014/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3343607
72 A = 6790148
84 meter
Y = -3394461
15 meter E =
0013122
Z = -4849994
37 I = 51
58511
XDOT = 6603
916558 Wp = 77
60662
YDOT = -2963
501705 meter/sec RA = 351
60774 deg
ZDOT = -2481
585212 TA = 167
95872
MA = 167
92732
Ha = 227
444 n
mi
Hp = 219
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10969841
61 X = -3281841
97
Y = -11136683
57 feet Y = -3431506
71 meter
Z = -15912055
01 Z = -4866086
67
XDOT = 21666
392906 XDOT = 6648
618985
YDOT = -9722
774624 feet/sec YDOT = -2889
402758 meter/sec
ZDOT = -8141
683768 ZDOT = -2449
395584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10370369
00 X = 3160888
47
Y = 11604102
53 feet Y = 3536930
45 meter
Z = -15979890
23 Z = -4870670
54
XDOT = -21276
672652 XDOT = -6485
129824
YDOT = 8005
270013 feet/sec YDOT = 2440
006300 meter/sec
ZDOT = -8004
213833 ZDOT = -2439
684376
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 14262
52043972
00016717 00000-0 10270-3 0 9026
2 25544 51
6472 352
0332 0001819 116
9302 243
2034 15
50418238 25963
Satellite: ISS
Catalog Number: 25544
Epoch time: 14262
52043972 = yrday
fracday
Element set: 902
Inclination: 51
6472 deg
RA of node: 352
0332 deg
Eccentricity:
0001819
Arg of perigee: 116
9302 deg
Mean anomaly: 243
2034 deg
Mean motion: 15
50418238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 283
Coasting Arc #4 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2014/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3093889
82 A = 6789198
09 meter
Y = 3360507
97 meter E =
0007549
Z = 5018404
44 I = 51
55217
XDOT = -6682
413831 Wp = 121
94747
YDOT = 3196
753772 meter/sec RA = 346
64259 deg
ZDOT = 1973
009389 TA = 308
83331
MA = 308
90067
Ha = 227
255 n
mi
Hp = 219
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10150557
14 X = 3031704
20
Y = 11025288
60 feet Y = 3394758
75 meter
Z = 16464581
50 Z = 5033282
61
XDOT = -21923
929891 XDOT = -6727
248223
YDOT = 10488
037310 feet/sec YDOT = 3121
776251 meter/sec
ZDOT = 6473
127918 ZDOT = 1940
438022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9748952
43 X = -2971480
70
Y = -11290745
51 feet Y = -3441419
23 meter
Z = 16527257
34 Z = 5037508
04
XDOT = 21412
882963 XDOT = 6526
646727
YDOT = -9188
089163 feet/sec YDOT = -2800
529577 meter/sec
ZDOT = 6334
001833 ZDOT = 1930
603759
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 14263
55171466
00016717 00000-0 10270-3 0 9031
2 25544 51
6475 346
9206 0001828 117
5801 242
5536 15
50489304 26129
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
55171466 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 346
9206 deg
Eccentricity:
0001828
Arg of perigee: 117
5801 deg
Mean anomaly: 242
5536 deg
Mean motion: 15
50489304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 304
Coasting Arc #5 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2014/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2821629
47 A = 6788645
25 meter
Y = -3395212
68 meter E =
0015283
Z = -5170745
27 I = 51
51922
XDOT = 6700
897785 Wp = 83
15364
YDOT = -3408
602889 meter/sec RA = 341
67533 deg
ZDOT = -1420
304098 TA = 173
13910
MA = 173
11816
Ha = 227
338 n
mi
Hp = 219
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9257314
53 X = -2758335
95
Y = -11139149
20 feet Y = -3426412
76 meter
Z = -16964387
37 Z = -5184298
12
XDOT = 21984
572784 XDOT = 6745
414908
YDOT = -11183
080345 feet/sec YDOT = -3333
420393 meter/sec
ZDOT = -4659
790348 ZDOT = -1387
643582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9044312
23 X = 2756706
37
Y = 11226783
52 feet Y = 3421923
62 meter
Z = -17021418
98 Z = -5188128
51
XDOT = -21299
781709 XDOT = -6492
173465
YDOT = 10314
890895 feet/sec YDOT = 3143
978745 meter/sec
ZDOT = -4520
258451 ZDOT = -1377
774776
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 14264
51851830
00016717 00000-0 10270-3 0 9049
2 25544 51
6467 342
1284 0001762 117
8558 242
2772 15
50474306 26274
Satellite: ISS
Catalog Number: 25544
Epoch time: 14264
51851830 = yrday
fracday
Element set: 904
Inclination: 51
6467 deg
RA of node: 342
1284 deg
Eccentricity:
0001762
Arg of perigee: 117
8558 deg
Mean anomaly: 242
2772 deg
Mean motion: 15
50474306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 307
Coasting Arc #6 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2014/265/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4434992
45 A = 6796626
33 meter
Y = -4324605
20 meter E =
0005864
Z = -2799377
82 I = 51
51760
XDOT = 5296
819619 Wp = 72
99799
YDOT = 2138
073025 meter/sec RA = 336
77576 deg
ZDOT = 5099
188583 TA = 255
26094
MA = 255
32593
Ha = 227
299 n
mi
Hp = 219
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14550500
17 X = 4496620
05
Y = -14188337
28 feet Y = -4274666
07 meter
Z = -9184310
43 Z = -2777682
94
XDOT = 17378
017124 XDOT = 5247
747293
YDOT = 7014
675279 feet/sec YDOT = 2197
031850 meter/sec
ZDOT = 16729
621335 ZDOT = 5124
800283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16204688
30 X = -4939188
99
Y = 12334282
62 feet Y = 3759489
34 meter
Z = -9091263
81 Z = -2771017
21
XDOT = -15406
487075 XDOT = -4695
897260
YDOT = -7855
738252 feet/sec YDOT = -2394
429019 meter/sec
ZDOT = 16838
164828 ZDOT = 5132
272640
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 14265
48530272
00016717 00000-0 10270-3 0 9051
2 25544 51
6471 337
3353 0001740 117
4695 242
6633 15
50509431 26421
Satellite: ISS
Catalog Number: 25544
Epoch time: 14265
48530272 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 337
3353 deg
Eccentricity:
0001740
Arg of perigee: 117
4695 deg
Mean anomaly: 242
6633 deg
Mean motion: 15
50509431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2642
Checksum: 296
Coasting Arc #7 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2014/266/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4511268
32 A = 6797501
38 meter
Y = 4513006
62 meter E =
0015633
Z = 2320885
41 I = 51
49225
XDOT = -4985
280598 Wp = 108
28128
YDOT = -2196
824423 meter/sec RA = 331
81035 deg
ZDOT = -5393
356221 TA = 45
81895
MA = 45
69059
Ha = 227
263 n
mi
Hp = 219
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14800749
09 X = -4572672
67
Y = 14806452
16 feet Y = 4462215
72 meter
Z = 7614453
44 Z = 2298820
40
XDOT = -16355
907473 XDOT = -4934
145392
YDOT = -7207
429208 feet/sec YDOT = -2252
287962 meter/sec
ZDOT = -17694
738258 ZDOT = -5417
449556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16292772
51 X = 4966037
06
Y = -13201179
09 feet Y = -4023719
39 meter
Z = 7519809
50 Z = 2292037
94
XDOT = 14453
763835 XDOT = 4405
507217
YDOT = 7653
544654 feet/sec YDOT = 2332
800411 meter/sec
ZDOT = -17796
808054 ZDOT = -5424
467095
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 14266
51652013
00016717 00000-0 10270-3 0 9065
2 25544 51
6466 332
2226 0001841 116
4851 243
6488 15
50562100 26581
Satellite: ISS
Catalog Number: 25544
Epoch time: 14266
51652013 = yrday
fracday
Element set: 906
Inclination: 51
6466 deg
RA of node: 332
2226 deg
Eccentricity:
0001841
Arg of perigee: 116
4851 deg
Mean anomaly: 243
6488 deg
Mean motion: 15
50562100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2658
Checksum: 290
Coasting Arc #8 (Orbit 2672)
---------------------------------------
Vector Time (GMT): 2014/267/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4529319
68 A = 6798339
29 meter
Y = -4718015
87 meter E =
0007818
Z = -1849149
70 I = 51
46736
XDOT = 4673
014642 Wp = 50
58130
YDOT = 2292
050053 meter/sec RA = 326
84335 deg
ZDOT = 5618
853788 TA = 289
06572
MA = 289
15037
Ha = 227
217 n
mi
Hp = 219
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14859972
71 X = 4590723
64
Y = -15479054
68 feet Y = -4667023
03 meter
Z = -6066764
11 Z = -1826996
88
XDOT = 15331
412868 XDOT = 4619
742310
YDOT = 7519
849255 feet/sec YDOT = 2344
009723 meter/sec
ZDOT = 18434
559671 ZDOT = 5641
425049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16170231
53 X = -4928686
57
Y = 14145236
52 feet Y = 4311468
09 meter
Z = -5971720
46 Z = -1820180
40
XDOT = -13482
592092 XDOT = -4109
494070
YDOT = -7619
084960 feet/sec YDOT = -2322
297096 meter/sec
ZDOT = 18530
134423 ZDOT = 5647
984972
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 14267
48326771
00016717 00000-0 10270-3 0 9072
2 25544 51
6460 327
4294 0001693 116
9516 243
1808 15
50552902 26731
Satellite: ISS
Catalog Number: 25544
Epoch time: 14267
48326771 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 327
4294 deg
Eccentricity:
0001693
Arg of perigee: 116
9516 deg
Mean anomaly: 243
1808 deg
Mean motion: 15
50552902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2673
Checksum: 317
Coasting Arc #9 (Orbit 2688)
---------------------------------------
Vector Time (GMT): 2014/268/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4533303
64 A = 6798833
94 meter
Y = 4884489
89 meter E =
0015536
Z = 1309466
85 I = 51
44392
XDOT = -4350
947674 Wp = 120
01785
YDOT = -2469
377351 meter/sec RA = 321
87498 deg
ZDOT = -5807
470837 TA = 45
70799
MA = 45
58066
Ha = 227
117 n
mi
Hp = 219
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14873043
44 X = -4593947
25
Y = 16025229
30 feet Y = 4833456
67 meter
Z = 4296151
08 Z = 1287296
45
XDOT = -14274
762710 XDOT = -4294
800017
YDOT = -8101
631730 feet/sec YDOT = -2517
719380 meter/sec
ZDOT = -19053
382012 ZDOT = -5828
470608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15963885
04 X = 4865792
16
Y = -14965900
51 feet Y = -4561606
48 meter
Z = 4201012
46 Z = 1280468
60
XDOT = 12474
005238 XDOT = 3802
076796
YDOT = 7890
895163 feet/sec YDOT = 2405
144846 meter/sec
ZDOT = -19142
238333 ZDOT = -5834
554244
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 14268
51444594
00016717 00000-0 10270-3 0 9082
2 25544 51
6458 322
3161 0001800 116
7487 243
3848 15
50628384 26891
Satellite: ISS
Catalog Number: 25544
Epoch time: 14268
51444594 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 322
3161 deg
Eccentricity:
0001800
Arg of perigee: 116
7487 deg
Mean anomaly: 243
3848 deg
Mean motion: 15
50628384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2689
Checksum: 327
Coasting Arc #10 (Orbit 2703)
---------------------------------------
Vector Time (GMT): 2014/269/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4477883
37 A = 6799359
17 meter
Y = -5050149
48 meter E =
0010931
Z = -787747
92 I = 51
42074
XDOT = 4052
905090 Wp = 48
34879
YDOT = 2679
069013 meter/sec RA = 316
90491 deg
ZDOT = 5923
680206 TA = 303
12334
MA = 303
22819
Ha = 227
151 n
mi
Hp = 219
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14691218
42 X = 4537849
18
Y = -16568731
89 feet Y = -4999739
71 meter
Z = -2584474
81 Z = -765848
36
XDOT = 13296
932710 XDOT = 3993
870168
YDOT = 8789
596499 feet/sec YDOT = 2724
061944 meter/sec
ZDOT = 19434
646346 ZDOT = 5943
225154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15539678
37 X = -4736493
97
Y = 15790828
28 feet Y = 4813044
46 meter
Z = -2490466
50 Z = -759094
19
XDOT = -11553
310072 XDOT = -3521
448910
YDOT = -8323
836883 feet/sec YDOT = -2537
105482 meter/sec
ZDOT = 19517
276310 ZDOT = 5948
865819
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 14269
48115718
00016717 00000-0 10270-3 0 9093
2 25544 51
6451 317
5223 0001720 115
3579 244
7750 15
50599680 27048
Satellite: ISS
Catalog Number: 25544
Epoch time: 14269
48115718 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 317
5223 deg
Eccentricity:
0001720
Arg of perigee: 115
3579 deg
Mean anomaly: 244
7750 deg
Mean motion: 15
50599680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2704
Checksum: 315
Coasting Arc #11 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2014/270/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4413970
55 A = 6799340
33 meter
Y = 5159118
64 meter E =
0014195
Z = 205450
12 I = 51
39972
XDOT = -3757
743178 Wp = 130
54966
YDOT = -2966
163890 meter/sec RA = 311
93336 deg
ZDOT = -5984
806818 TA = 47
23239
MA = 47
11306
Ha = 227
011 n
mi
Hp = 219
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14481530
68 X = -4472330
98
Y = 16926242
25 feet Y = 5109432
47 meter
Z = 674048
94 Z = 183864
96
XDOT = -12328
553733 XDOT = -3695
222841
YDOT = -9731
508824 feet/sec YDOT = -3007
836559 meter/sec
ZDOT = -19635
192974 ZDOT = -6002
909465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15056399
98 X = 4589190
71
Y = -16420523
26 feet Y = -5004975
49 meter
Z = 581364
70 Z = 177199
96
XDOT = 10666
885505 XDOT = 3251
266702
YDOT = 9047
328727 feet/sec YDOT = 2757
625796 meter/sec
ZDOT = -19711
638095 ZDOT = -6008
107292
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 14270
51229619
00016717 00000-0 10270-3 0 9107
2 25544 51
6455 312
4082 0001838 118
0822 242
0515 15
50686696 27202
Satellite: ISS
Catalog Number: 25544
Epoch time: 14270
51229619 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 312
4082 deg
Eccentricity:
0001838
Arg of perigee: 118
0822 deg
Mean anomaly: 242
0515 deg
Mean motion: 15
50686696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 293
Coasting Arc #12 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2014/271/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4296928
22 A = 6799378
07 meter
Y = -5250831
55 meter E =
0013579
Z = 345917
13 I = 51
37878
XDOT = 3508
262573 Wp = 55
91811
YDOT = 3275
100728 meter/sec RA = 306
96026 deg
ZDOT = 5973
838630 TA = 307
81855
MA = 307
94139
Ha = 227
082 n
mi
Hp = 219
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14097533
52 X = 4353644
49
Y = -17227137
62 feet Y = -5202463
36 meter
Z = 1134898
73 Z = 366929
64
XDOT = 11510
047813 XDOT = 3442
359444
YDOT = 10745
081129 feet/sec YDOT = 3313
964530 meter/sec
ZDOT = 19599
208105 ZDOT = 5990
721125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14381512
44 X = -4383484
99
Y = 16984516
53 feet Y = 5176880
64 meter
Z = 1225159
20 Z = 373428
52
XDOT = -9963
101862 XDOT = -3036
753448
YDOT = -9890
446309 feet/sec YDOT = -3014
608035 meter/sec
ZDOT = 19670
411232 ZDOT = 5995
541343
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 14271
54341685
00016717 00000-0 10270-3 0 9110
2 25544 51
6448 307
2944 0001823 115
4434 244
6905 15
50658262 27363
Satellite: ISS
Catalog Number: 25544
Epoch time: 14271
54341685 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 307
2944 deg
Eccentricity:
0001823
Arg of perigee: 115
4434 deg
Mean anomaly: 244
6905 deg
Mean motion: 15
50658262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 307
Coasting Arc #13 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2014/272/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4182671
29 A = 6798800
30 meter
Y = 5269569
97 meter E =
0011613
Z = -946130
02 I = 51
36044
XDOT = -3273
817247 Wp = 137
77232
YDOT = -3647
000370 meter/sec RA = 301
98546 deg
ZDOT = -5890
046985 TA = 52
49781
MA = 52
39229
Ha = 226
923 n
mi
Hp = 219
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13722674
85 X = -4236689
91
Y = 17288615
37 feet Y = 5222494
51 meter
Z = -3104101
11 Z = -966580
82
XDOT = -10740
870234 XDOT = -3204
179948
YDOT = -11965
224311 feet/sec YDOT = -3683
221476 meter/sec
ZDOT = -19324
301132 ZDOT = -5905
781487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13699960
67 X = 4175748
01
Y = -17290629
28 feet Y = -5270183
81 meter
Z = -3191972
27 Z = -972913
15
XDOT = 9360
059256 XDOT = 2852
946061
YDOT = 10966
094876 feet/sec YDOT = 3342
465718 meter/sec
ZDOT = -19390
560380 ZDOT = -5910
242804
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 14272
51007014
00016717 00000-0 10270-3 0 9124
2 25544 51
6456 302
4997 0001904 121
6947 238
4390 15
50738180 27519
Satellite: ISS
Catalog Number: 25544
Epoch time: 14272
51007014 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 302
4997 deg
Eccentricity:
0001904
Arg of perigee: 121
6947 deg
Mean anomaly: 238
4390 deg
Mean motion: 15
50738180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 297
Coasting Arc #14 (Orbit 2766)
---------------------------------------
Vector Time (GMT): 2014/273/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4028362
03 A = 6798247
16 meter
Y = -5258106
83 meter E =
0015017
Z = 1501495
31 I = 51
34201
XDOT = 3100
290519 Wp = 68
05611
YDOT = 4025
430395 meter/sec RA = 297
00922 deg
ZDOT = 5738
169402 TA = 308
38935
MA = 308
52414
Ha = 226
972 n
mi
Hp = 219
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13216410
87 X = 4079566
13
Y = -17251006
68 feet Y = -5212772
67 meter
Z = 4926165
73 Z = 1521189
55
XDOT = 10171
556820 XDOT = 3027
172281
YDOT = 13206
792636 feet/sec YDOT = 4059
691474 meter/sec
ZDOT = 18826
015100 ZDOT = 5753
052440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12883511
52 X = -3926894
31
Y = 17476977
20 feet Y = 5326982
65 meter
Z = 5010813
83 Z = 1527296
05
XDOT = -9006
195146 XDOT = -2745
088281
YDOT = -12092
340760 feet/sec YDOT = -3685
745464 meter/sec
ZDOT = 18888
592679 ZDOT = 5757
243049
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 14273
54115052
00016717 00000-0 10270-3 0 9131
2 25544 51
6449 297
3859 0001925 118
7520 241
3824 15
50729346 27673
Satellite: ISS
Catalog Number: 25544
Epoch time: 14273
54115052 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 297
3859 deg
Eccentricity:
0001925
Arg of perigee: 118
7520 deg
Mean anomaly: 241
3824 deg
Mean motion: 15
50729346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2767
Checksum: 318
Coasting Arc #15 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2014/274/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3893059
15 A = 6797158
96 meter
Y = 5162438
17 meter E =
0008291
Z = -2089365
51 I = 51
32635
XDOT = -2950
265810 Wp = 135
59547
YDOT = -4442
654613 meter/sec RA = 292
03099 deg
ZDOT = -5498
920821 TA = 67
59877
MA = 67
51096
Ha = 226
820 n
mi
Hp = 219
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12772503
77 X = -3940347
83
Y = 16937133
11 feet Y = 5118638
90 meter
Z = -6854873
71 Z = -2108392
85
XDOT = -9679
349769 XDOT = -2873
655524
YDOT = -14575
638493 feet/sec YDOT = -4475
218457 meter/sec
ZDOT = -18041
078808 ZDOT = -5513
066501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12136053
28 X = 3699069
04
Y = -17366390
46 feet Y = -5293275
81 meter
Z = -6936664
70 Z = -2114295
40
XDOT = 8797
247308 XDOT = 2681
400979
YDOT = 13352
880533 feet/sec YDOT = 4069
957986 meter/sec
ZDOT = -18100
455971 ZDOT = -5517
018980
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 14274
50776646
00016717 00000-0 10270-3 0 9141
2 25544 51
6456 292
5912 0001929 126
8054 233
3274 15
50790284 27820
Satellite: ISS
Catalog Number: 25544
Epoch time: 14274
50776646 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 292
5912 deg
Eccentricity:
0001929
Arg of perigee: 126
8054 deg
Mean anomaly: 233
3274 deg
Mean motion: 15
50790284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 325
Coasting Arc #16 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2014/275/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3735758
85 A = 6796057
55 meter
Y = -5029098
80 meter E =
0014938
Z = 2618379
29 I = 51
31091
XDOT = 2867
349664 Wp = 82
80216
YDOT = 4848
864041 meter/sec RA = 287
05105 deg
ZDOT = 5198
442648 TA = 306
80449
MA = 306
94146
Ha = 226
803 n
mi
Hp = 219
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12256426
68 X = 3778998
43
Y = -16499667
97 feet Y = -4987081
14 meter
Z = 8590483
23 Z = 2636632
61
XDOT = 9407
315171 XDOT = 2787
662935
YDOT = 15908
346591 feet/sec YDOT = 4880
483472 meter/sec
ZDOT = 17055
258033 ZDOT = 5212
177951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11331880
55 X = -3453957
19
Y = 17108277
54 feet Y = 5214602
99 meter
Z = 8668953
99 Z = 2642297
17
XDOT = -8862
986861 XDOT = -2701
438395
YDOT = -14580
901121 feet/sec YDOT = -4444
258662 meter/sec
ZDOT = 17112
829882 ZDOT = 5215
990548
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 14275
53880541
00016717 00000-0 10270-3 0 9156
2 25544 51
6445 287
4771 0001942 125
0927 235
0406 15
50806716 27979
Satellite: ISS
Catalog Number: 25544
Epoch time: 14275
53880541 = yrday
fracday
Element set: 915
Inclination: 51
6445 deg
RA of node: 287
4771 deg
Eccentricity:
0001942
Arg of perigee: 125
0927 deg
Mean anomaly: 235
0406 deg
Mean motion: 15
50806716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2797
Checksum: 319
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