[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 26th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24218 8 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
119/08:10:59
330 3
6 3
6 3
7
N/A -0
9 0
0 227
4
000/00:19:58
659 0
3 0
6 223
3
Coasting Arc #1 (Orbit 315)
---------------------------------------
Vector Time (GMT): 2014/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924085
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4085228
26 A = 6792526
32 meter
Y = 3372180
75 meter E =
0006978
Z = 4245296
01 I = 51
64987
XDOT = -6123
325100 Wp = 83
89325
YDOT = 2848
345538 meter/sec RA =
18786 deg
ZDOT = 3625
507260 TA = 328
99185
MA = 329
03302
Ha = 226
493 n
mi
Hp = 221
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13402979
86 X = 4026593
65
Y = 11063585
15 feet Y = 3417536
88 meter
Z = 13928136
51 Z = 4264999
00
XDOT = -20089
649278 XDOT = -6172
332575
YDOT = 9344
965677 feet/sec YDOT = 2779
596842 meter/sec
ZDOT = 11894
708857 ZDOT = 3595
641453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17179077
01 X = 5236182
67
Y = 2147239
75 feet Y = 654478
67 meter
Z = 14010868
88 Z = 4270512
84
XDOT = -11794
775315 XDOT = -3595
047516
YDOT = 17484
630758 feet/sec YDOT = 5329
315455 meter/sec
ZDOT = 11767
895922 ZDOT = 3586
854677
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 14115
55491836
00016717 00000-0 10270-3 0 9000
2 25544 51
6505
4313 0004368 324
2453 35
8405 15
50385276 3166
Satellite: ISS
Catalog Number: 25544
Epoch time: 14115
55491836 = yrday
fracday
Element set: 900
Inclination: 51
6505 deg
RA of node:
4313 deg
Eccentricity:
0004368
Arg of perigee: 324
2453 deg
Mean anomaly: 35
8405 deg
Mean motion: 15
50385276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 316
Checksum: 280
Coasting Arc #2 (Orbit 330)
---------------------------------------
Vector Time (GMT): 2014/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924085
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3879580
02 A = 6791363
58 meter
Y = -3271398
71 meter E =
0009697
Z = -4522774
60 I = 51
61525
XDOT = 6266
320192 Wp = 42
17673
YDOT = -3043
459141 meter/sec RA = 355
22892 deg
ZDOT = -3170
726918 TA = 195
90465
MA = 195
93512
Ha = 226
538 n
mi
Hp = 221
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12728280
90 X = -3820739
65
Y = -10732935
41 feet Y = -3314454
00 meter
Z = -14838499
33 Z = -4541478
17
XDOT = 20558
793282 XDOT = 6315
289709
YDOT = -9985
102170 feet/sec YDOT = -2973
111547 meter/sec
ZDOT = -10402
647368 ZDOT = -3140
166414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16463801
86 X = -5018166
81
Y = -1952422
77 feet Y = -595098
46 meter
Z = -14917016
24 Z = -4546706
55
XDOT = 11513
883683 XDOT = 3509
431746
YDOT = -18527
114919 feet/sec YDOT = -5647
064627 meter/sec
ZDOT = -10272
870450 ZDOT = -3131
170913
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 14116
52176018
00016717 00000-0 10270-3 0 9011
2 25544 51
6502 355
6390 0004557 325
3017 34
7836 15
50440481 3314
Satellite: ISS
Catalog Number: 25544
Epoch time: 14116
52176018 = yrday
fracday
Element set: 901
Inclination: 51
6502 deg
RA of node: 355
6390 deg
Eccentricity:
0004557
Arg of perigee: 325
3017 deg
Mean anomaly: 34
7836 deg
Mean motion: 15
50440481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 331
Checksum: 279
Coasting Arc #3 (Orbit 346)
---------------------------------------
Vector Time (GMT): 2014/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924085
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3631464
45 A = 6790372
19 meter
Y = 3204114
93 meter E =
0004383
Z = 4755807
92 I = 51
58119
XDOT = -6396
103503 Wp = 85
07846
YDOT = 3259
020322 meter/sec RA = 350
26645 deg
ZDOT = 2686
511592 TA = 338
33789
MA = 338
35642
Ha = 226
571 n
mi
Hp = 221
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11914253
44 X = 3572262
80
Y = 10512188
10 feet Y = 3244393
57 meter
Z = 15603044
36 Z = 4773305
39
XDOT = -20984
591544 XDOT = -6445
121678
YDOT = 10692
323891 feet/sec YDOT = 3187
221071 meter/sec
ZDOT = 8814
014410 ZDOT = 2655
320398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15695516
23 X = 4783993
35
Y = 1951846
38 feet Y = 594922
78 meter
Z = 15676466
21 Z = 4778186
90
XDOT = -11114
034389 XDOT = -3387
557682
YDOT = 19598
917551 feet/sec YDOT = 5973
750070 meter/sec
ZDOT = 8681
539883 ZDOT = 2646
133356
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 14117
55303531
00016717 00000-0 10270-3 0 9028
2 25544 51
6502 350
5266 0004512 330
3046 29
7848 15
50457266 3472
Satellite: ISS
Catalog Number: 25544
Epoch time: 14117
55303531 = yrday
fracday
Element set: 902
Inclination: 51
6502 deg
RA of node: 350
5266 deg
Eccentricity:
0004512
Arg of perigee: 330
3046 deg
Mean anomaly: 29
7848 deg
Mean motion: 15
50457266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 347
Checksum: 284
Coasting Arc #4 (Orbit 361)
---------------------------------------
Vector Time (GMT): 2014/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924085
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3372001
37 A = 6789374
17 meter
Y = -3191367
83 meter E =
0012335
Z = -4964816
44 I = 51
54694
XDOT = 6470
070783 Wp = 52
23361
YDOT = -3470
476284 meter/sec RA = 345
30055 deg
ZDOT = -2159
826411 TA = 196
62312
MA = 196
66359
Ha = 226
607 n
mi
Hp = 220
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11062996
61 X = -3311946
17
Y = -10470366
88 feet Y = -3228740
14 meter
Z = -16288767
84 Z = -4981051
47
XDOT = 21227
266347 XDOT = 6518
889519
YDOT = -11386
077047 feet/sec YDOT = -3397
850933 meter/sec
ZDOT = -7086
044656 ZDOT = -2128
276338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15006480
07 X = -4573975
12
Y = -2145115
23 feet Y = -653831
12 meter
Z = -16356847
84 Z = -4985567
22
XDOT = 10526
726731 XDOT = 3208
546308
YDOT = -20538
816849 feet/sec YDOT = -6260
231376 meter/sec
ZDOT = -6952
021076 ZDOT = -2118
976024
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 14118
51983015
00016717 00000-0 10270-3 0 9037
2 25544 51
6491 345
7334 0004684 331
4908 28
5985 15
50519292 3624
Satellite: ISS
Catalog Number: 25544
Epoch time: 14118
51983015 = yrday
fracday
Element set: 903
Inclination: 51
6491 deg
RA of node: 345
7334 deg
Eccentricity:
0004684
Arg of perigee: 331
4908 deg
Mean anomaly: 28
5985 deg
Mean motion: 15
50519292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 315
Coasting Arc #5 (Orbit 374)
---------------------------------------
Vector Time (GMT): 2014/119/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2544406
33 A = 6794034
23 meter
Y = -4542348
37 meter E =
0003380
Z = -4366873
00 I = 51
52954
XDOT = 6828
064050 Wp = 69
20301
YDOT = 534
067269 meter/sec RA = 341
05011 deg
ZDOT = 3426
244113 TA = 235
63197
MA = 235
66395
Ha = 227
379 n
mi
Hp = 223
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8347789
81 X = 2616224
11
Y = -14902717
74 feet Y = -4513493
75 meter
Z = -14327011
15 Z = -4354337
79
XDOT = 22401
784941 XDOT = 6804
940558
YDOT = 1752
189203 feet/sec YDOT = 610
293872 meter/sec
ZDOT = 11240
958376 ZDOT = 3459
358413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12702806
38 X = 3871815
38
Y = -11487137
86 feet Y = -3501279
62 meter
Z = -14273199
12 Z = -4350471
09
XDOT = 19804
028819 XDOT = 6036
267984
YDOT = 7772
304771 feet/sec YDOT = 2368
998494 meter/sec
ZDOT = 11380
877597 ZDOT = 3468
891492
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 14119
35770536
00016717 00000-0 10270-3 0 9043
2 25544 51
6489 341
5793 0006496 310
3560 49
7023 15
49774608 3751
Satellite: ISS
Catalog Number: 25544
Epoch time: 14119
35770536 = yrday
fracday
Element set: 904
Inclination: 51
6489 deg
RA of node: 341
5793 deg
Eccentricity:
0006496
Arg of perigee: 310
3560 deg
Mean anomaly: 49
7023 deg
Mean motion: 15
49774608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 375
Checksum: 328
Coasting Arc #6 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2014/120/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2463203
71 A = 6794574
39 meter
Y = 4742877
19 meter E =
0008860
Z = 4196048
68 I = 51
50219
XDOT = -6714
315574 Wp = 35
86256
YDOT = -223
237350 meter/sec RA = 336
08872 deg
ZDOT = -3678
188616 TA = 92
04013
MA = 91
93867
Ha = 227
500 n
mi
Hp = 223
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8081377
01 X = -2536440
05
Y = 15560620
70 feet Y = 4714922
61 meter
Z = 13766563
92 Z = 4183904
60
XDOT = -22028
594402 XDOT = -6693
452425
YDOT = -732
406004 feet/sec YDOT = -298
204517 meter/sec
ZDOT = -12067
547952 ZDOT = -3710
755816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12442206
15 X = -3792384
43
Y = 12412389
94 feet Y = 3783296
45 meter
Z = 13714369
67 Z = 4180139
88
XDOT = -19826
572381 XDOT = -6043
139262
YDOT = -6348
785018 feet/sec YDOT = -1935
109673 meter/sec
ZDOT = -12205
204856 ZDOT = -3720
146440
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 14120
38942349
00016717 00000-0 10270-3 0 9052
2 25544 51
6486 336
4702 0006536 314
2010 45
8603 15
49800567 3912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14120
38942349 = yrday
fracday
Element set: 905
Inclination: 51
6486 deg
RA of node: 336
4702 deg
Eccentricity:
0006536
Arg of perigee: 314
2010 deg
Mean anomaly: 45
8603 deg
Mean motion: 15
49800567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 298
Coasting Arc #7 (Orbit 405)
---------------------------------------
Vector Time (GMT): 2014/121/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2343636
27 A = 6795031
96 meter
Y = -4949425
94 meter E =
0003522
Z = -4022508
32 I = 51
47687
XDOT = 6580
194641 Wp = 36
54875
YDOT = -65
724747 meter/sec RA = 331
12439 deg
ZDOT = 3919
236493 TA = 274
27889
MA = 274
31914
Ha = 227
583 n
mi
Hp = 222
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7689095
36 X = 2418348
10
Y = -16238274
07 feet Y = -4922800
12 meter
Z = -13197205
77 Z = -4010941
62
XDOT = 21588
565094 XDOT = 6561
401780
YDOT = -215
632373 feet/sec YDOT = 7
754101 meter/sec
ZDOT = 12858
387445 ZDOT = 3951
157109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12038320
56 X = 3669280
11
Y = -13386346
18 feet Y = -4080158
31 meter
Z = -13147415
95 Z = -4007332
38
XDOT = 19717
910377 XDOT = 6010
019083
YDOT = 4985
540658 feet/sec YDOT = 1519
592793 meter/sec
ZDOT = 12993
359691 ZDOT = 3960
376034
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 14121
35663642
00016717 00000-0 10270-3 0 9067
2 25544 51
6492 331
6794 0006647 317
5789 42
4847 15
49845957 4061
Satellite: ISS
Catalog Number: 25544
Epoch time: 14121
35663642 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 331
6794 deg
Eccentricity:
0006647
Arg of perigee: 317
5789 deg
Mean anomaly: 42
4847 deg
Mean motion: 15
49845957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 406
Checksum: 342
Coasting Arc #8 (Orbit 421)
---------------------------------------
Vector Time (GMT): 2014/122/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2241695
92 A = 6795649
62 meter
Y = 5159645
68 meter E =
0009801
Z = 3811687
40 I = 51
45219
XDOT = -6417
275509 Wp = 47
12556
YDOT = 302
327062 meter/sec RA = 326
15897 deg
ZDOT = -4169
948677 TA = 87
04896
MA = 86
93680
Ha = 227
702 n
mi
Hp = 222
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7354645
40 X = -2317741
89
Y = 16927971
39 feet Y = 5134152
32 meter
Z = 12505536
08 Z = 3800612
77
XDOT = -21054
053506 XDOT = -6399
922652
YDOT = 991
886685 feet/sec YDOT = 230
662082 meter/sec
ZDOT = -13680
933981 ZDOT = -4201
081245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11662876
58 X = -3554844
78
Y = 14346296
55 feet Y = 4372751
19 meter
Z = 12457790
43 Z = 3797134
52
XDOT = -19431
626717 XDOT = -5922
759823
YDOT = -3764
433614 feet/sec YDOT = -1147
399365 meter/sec
ZDOT = -13812
615521 ZDOT = -4210
085211
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 14122
38830778
00016717 00000-0 10270-3 0 9078
2 25544 51
6489 326
5697 0006690 321
5864 38
4809 15
49873574 4226
Satellite: ISS
Catalog Number: 25544
Epoch time: 14122
38830778 = yrday
fracday
Element set: 907
Inclination: 51
6489 deg
RA of node: 326
5697 deg
Eccentricity:
0006690
Arg of perigee: 321
5864 deg
Mean anomaly: 38
4809 deg
Mean motion: 15
49873574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 422
Checksum: 348
Coasting Arc #9 (Orbit 436)
---------------------------------------
Vector Time (GMT): 2014/123/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2094467
67 A = 6796179
34 meter
Y = -5368229
54 meter E =
0005110
Z = -3599652
03 I = 51
42988
XDOT = 6245
336710 Wp = 14
11894
YDOT = -513
799386 meter/sec RA = 321
19115 deg
ZDOT = 4406
284785 TA = 303
22190
MA = 303
27087
Ha = 227
782 n
mi
Hp = 222
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6871613
10 X = 2171826
95
Y = -17612301
65 feet Y = -5344375
23 meter
Z = -11809881
99 Z = -3589289
50
XDOT = 20489
949837 XDOT = 6229
213366
YDOT = -1685
693524 feet/sec YDOT = -444
050284 meter/sec
ZDOT = 14456
314912 ZDOT = 4436
584974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11112752
25 X = 3387166
89
Y = -15328875
04 feet Y = -4672241
11 meter
Z = -11765112
67 Z = -3586006
34
XDOT = 19058
054278 XDOT = 5808
894944
YDOT = 2638
054198 feet/sec YDOT = 804
078920 meter/sec
ZDOT = 14584
514378 ZDOT = 4445
359982
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 14123
35547671
00016717 00000-0 10270-3 0 9084
2 25544 51
6497 321
7788 0006858 324
5171 35
5523 15
49914232 4377
Satellite: ISS
Catalog Number: 25544
Epoch time: 14123
35547671 = yrday
fracday
Element set: 908
Inclination: 51
6497 deg
RA of node: 321
7788 deg
Eccentricity:
0006858
Arg of perigee: 324
5171 deg
Mean anomaly: 35
5523 deg
Mean motion: 15
49914232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 437
Checksum: 325
Coasting Arc #10 (Orbit 452)
---------------------------------------
Vector Time (GMT): 2014/124/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1964286
32 A = 6796829
26 meter
Y = 5579832
90 meter E =
0010554
Z = 3345448
85 I = 51
40866
XDOT = -6052
570713 Wp = 57
91616
YDOT = 664
597975 meter/sec RA = 316
22252 deg
ZDOT = -4645
955057 TA = 83
04755
MA = 82
92751
Ha = 227
895 n
mi
Hp = 222
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6444508
92 X = -2042786
57
Y = 18306538
39 feet Y = 5557428
00 meter
Z = 10975882
07 Z = 3335715
97
XDOT = -19857
515461 XDOT = -6036
983762
YDOT = 2180
439550 feet/sec YDOT = 597
001496 meter/sec
ZDOT = -15242
634702 ZDOT = -4675
320028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10588216
87 X = -3227288
50
Y = 16293372
27 feet Y = 4966219
87 meter
Z = 10933741
97 Z = 3332604
55
XDOT = -18539
067558 XDOT = -5650
707792
YDOT = -1699
525656 feet/sec YDOT = -518
015420 meter/sec
ZDOT = -15366
906333 ZDOT = -4683
833050
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 14124
38710136
00016717 00000-0 10270-3 0 9097
2 25544 51
6496 316
6689 0006885 328
7694 31
3047 15
49947789 4531
Satellite: ISS
Catalog Number: 25544
Epoch time: 14124
38710136 = yrday
fracday
Element set: 909
Inclination: 51
6496 deg
RA of node: 316
6689 deg
Eccentricity:
0006885
Arg of perigee: 328
7694 deg
Mean anomaly: 31
3047 deg
Mean motion: 15
49947789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 453
Checksum: 352
Coasting Arc #11 (Orbit 467)
---------------------------------------
Vector Time (GMT): 2014/125/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1784485
62 A = 6797406
79 meter
Y = -5779846
54 meter E =
0007562
Z = -3092244
22 I = 51
38945
XDOT = 5863
642610 Wp = 6
60348
YDOT = -789
614463 meter/sec RA = 311
25174 deg
ZDOT = 4868
268793 TA = 317
76981
MA = 317
82802
Ha = 227
975 n
mi
Hp = 222
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5854611
61 X = 1864005
80
Y = -18962751
10 feet Y = -5759446
61 meter
Z = -10145158
21 Z = -3083382
29
XDOT = 19237
672604 XDOT = 5848
387764
YDOT = -2590
598632 feet/sec YDOT = -724
128806 meter/sec
ZDOT = 15972
010477 ZDOT = 4896
716730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9866725
11 X = 3007377
81
Y = -17242087
07 feet Y = -5255388
14 meter
Z = -10106671
59 Z = -3080513
50
XDOT = 17988
158688 XDOT = 5482
790768
YDOT = 877
384920 feet/sec YDOT = 267
426924 meter/sec
ZDOT = 16092
425975 ZDOT = 4904
971437
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 14125
35422630
00016717 00000-0 10270-3 0 9106
2 25544 51
6498 311
8778 0007096 331
2281 28
8477 15
49980226 4682
Satellite: ISS
Catalog Number: 25544
Epoch time: 14125
35422630 = yrday
fracday
Element set: 910
Inclination: 51
6498 deg
RA of node: 311
8778 deg
Eccentricity:
0007096
Arg of perigee: 331
2281 deg
Mean anomaly: 28
8477 deg
Mean motion: 15
49980226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 468
Checksum: 322
Coasting Arc #12 (Orbit 483)
---------------------------------------
Vector Time (GMT): 2014/126/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1621933
85 A = 6798031
05 meter
Y = 5980543
47 meter E =
0011007
Z = 2792478
87 I = 51
37209
XDOT = -5663
555572 Wp = 68
23916
YDOT = 848
021293 meter/sec RA = 306
28054 deg
ZDOT = -5085
489586 TA = 80
03073
MA = 79
90653
Ha = 228
075 n
mi
Hp = 221
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5321305
27 X = -1702254
17
Y = 19621205
62 feet Y = 5961956
86 meter
Z = 9161676
08 Z = 2784404
60
XDOT = -18581
219067 XDOT = -5647
913535
YDOT = 2782
222090 feet/sec YDOT = 784
775254 meter/sec
ZDOT = -16684
677120 ZDOT = -5112
964567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9170823
48 X = -2795267
00
Y = 18161702
58 feet Y = 5535686
95 meter
Z = 9126492
46 Z = 2781754
90
XDOT = -17336
063204 XDOT = -5284
032065
YDOT = -277
760606 feet/sec YDOT = -84
661433 meter/sec
ZDOT = -16800
987585 ZDOT = -5120
941016
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 14126
38580397
00016717 00000-0 10270-3 0 9116
2 25544 51
6497 306
7678 0007102 335
6753 24
4061 15
50022326 4842
Satellite: ISS
Catalog Number: 25544
Epoch time: 14126
38580397 = yrday
fracday
Element set: 911
Inclination: 51
6497 deg
RA of node: 306
7678 deg
Eccentricity:
0007102
Arg of perigee: 335
6753 deg
Mean anomaly: 24
4061 deg
Mean motion: 15
50022326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 484
Checksum: 302
Coasting Arc #13 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2014/127/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1408825
41 A = 6798608
97 meter
Y = -6158235
44 meter E =
0010360
Z = -2496782
45 I = 51
35617
XDOT = 5480
863255 Wp = 6
86285
YDOT = -883
045204 meter/sec RA = 301
30714 deg
ZDOT = 5282
974158 TA = 325
06369
MA = 325
13163
Ha = 228
151 n
mi
Hp = 221
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4622130
63 X = 1489712
16
Y = -20204184
52 feet Y = -6142028
80 meter
Z = -8191543
47 Z = -2489742
01
XDOT = 17981
834825 XDOT = 5464
667109
YDOT = -2897
129936 feet/sec YDOT = -821
845196 meter/sec
ZDOT = 17332
592381 ZDOT = 5309
560308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8269579
08 X = 2520567
70
Y = -19018187
11 feet Y = -5796743
43 meter
Z = -8160708
87 Z = -2487384
06
XDOT = 16714
638963 XDOT = 5094
621956
YDOT = -200
313779 feet/sec YDOT = -61
055640 meter/sec
ZDOT = 17445
148785 ZDOT = 5317
281350
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 14127
35288475
00016717 00000-0 10270-3 0 9127
2 25544 51
6492 301
9762 0007311 337
8420 22
2413 15
50045758 4992
Satellite: ISS
Catalog Number: 25544
Epoch time: 14127
35288475 = yrday
fracday
Element set: 912
Inclination: 51
6492 deg
RA of node: 301
9762 deg
Eccentricity:
0007311
Arg of perigee: 337
8420 deg
Mean anomaly: 22
2413 deg
Mean motion: 15
50045758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 303
Coasting Arc #14 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2014/128/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1214623
70 A = 6799137
22 meter
Y = 6332840
65 meter E =
0011046
Z = 2151052
31 I = 51
34296
XDOT = -5297
816642 Wp = 77
93458
YDOT = 848
990948 meter/sec RA = 296
33380 deg
ZDOT = -5464
819195 TA = 78
15990
MA = 78
03604
Ha = 228
238 n
mi
Hp = 221
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3984985
90 X = -1295797
91
Y = 20777036
24 feet Y = 6318804
11 meter
Z = 7057258
22 Z = 2144954
51
XDOT = -17381
288194 XDOT = -5280
369910
YDOT = 2785
403372 feet/sec YDOT = 789
844827 meter/sec
ZDOT = -17929
196833 ZDOT = -5490
513126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7400249
07 X = -2255595
92
Y = 19828771
88 feet Y = 6043809
67 meter
Z = 7030388
36 Z = 2142862
37
XDOT = -16045
344264 XDOT = -4890
620932
YDOT = 437
750344 feet/sec YDOT = 133
426305 meter/sec
ZDOT = -18037
972555 ZDOT = -5497
974035
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 14128
38441491
00016717 00000-0 10270-3 0 9131
2 25544 51
6491 296
8658 0007317 342
2804 17
8091 15
50097314 5155
Satellite: ISS
Catalog Number: 25544
Epoch time: 14128
38441491 = yrday
fracday
Element set: 913
Inclination: 51
6491 deg
RA of node: 296
8658 deg
Eccentricity:
0007317
Arg of perigee: 342
2804 deg
Mean anomaly: 17
8091 deg
Mean motion: 15
50097314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 310
Coasting Arc #15 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2014/129/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 972908
22 A = 6799648
65 meter
Y = -6472697
76 meter E =
0013176
Z = -1813439
55 I = 51
33076
XDOT = 5145
369879 Wp = 11
12183
YDOT = -797
131578 meter/sec RA = 291
35813 deg
ZDOT = 5625
208811 TA = 328
88132
MA = 328
95928
Ha = 228
302 n
mi
Hp = 221
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3191956
11 X = 1054024
30
Y = -21235885
05 feet Y = -6461364
57 meter
Z = -5949604
82 Z = -1808516
07
XDOT = 16881
134773 XDOT = 5126
575384
YDOT = -2615
261082 feet/sec YDOT = -739
697710 meter/sec
ZDOT = 18455
409486 ZDOT = 5650
158957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6334774
86 X = 1930839
38
Y = -20525164
36 feet Y = -6256070
10 meter
Z = -5927685
09 Z = -1806758
42
XDOT = 15470
649516 XDOT = 4715
453972
YDOT = -567
093423 feet/sec YDOT = -172
850075 meter/sec
ZDOT = 18561
029125 ZDOT = 5657
401677
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
35145132
00016717 00000-0 10270-3 0 9143
2 25544 51
6480 292
0734 0007470 344
4830 15
6091 15
50112657 5300
Satellite: ISS
Catalog Number: 25544
Epoch time: 14129
35145132 = yrday
fracday
Element set: 914
Inclination: 51
6480 deg
RA of node: 292
0734 deg
Eccentricity:
0007470
Arg of perigee: 344
4830 deg
Mean anomaly: 15
6091 deg
Mean motion: 15
50112657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 277
Coasting Arc #16 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2014/130/08:20:58
659
Vector Time (MET): N/A
Weight (LBS) : 923654
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -753791
42 A = 6799997
19 meter
Y = 6604850
81 meter E =
0010589
Z = 1423784
46 I = 51
32204
XDOT = -5003
472339 Wp = 86
49142
YDOT = 678
258136 meter/sec RA = 286
38309 deg
ZDOT = -5757
520973 TA = 77
94753
MA = 77
82888
Ha = 228
381 n
mi
Hp = 220
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2473068
95 X = -834508
72
Y = 21669458
03 feet Y = 6595970
14 meter
Z = 4671208
87 Z = 1419926
38
XDOT = -16415
591662 XDOT = -4982
716299
YDOT = 2225
256352 feet/sec YDOT = 622
422013 meter/sec
ZDOT = -18889
504506 ZDOT = -5781
777100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5316879
33 X = -1620584
82
Y = 21155963
83 feet Y = 6448337
78 meter
Z = 4653779
36 Z = 1418471
95
XDOT = -14905
055840 XDOT = -4543
061020
YDOT = 459
309843 feet/sec YDOT = 139
997640 meter/sec
ZDOT = -18992
167607 ZDOT = -5788
812687
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
38293348
00016717 00000-0 10270-3 0 9152
2 25544 51
6479 286
9625 0007513 348
7221 11
3760 15
50174538 5467
Satellite: ISS
Catalog Number: 25544
Epoch time: 14130
38293348 = yrday
fracday
Element set: 915
Inclination: 51
6479 deg
RA of node: 286
9625 deg
Eccentricity:
0007513
Arg of perigee: 348
7221 deg
Mean anomaly: 11
3760 deg
Mean motion: 15
50174538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 313
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