[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 22nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 31215 34 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 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
126/05:17:59
941 -0
4 6
3 6
3
N/A -5
4 -0
0 216
4
000/00:15:59
882 -3
1 0
3 215
4
Coasting Arc #1 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2015/112/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6767445
43 A = 6783623
22 meter
Y = -308984
52 meter E =
0010750
Z = -167608
43 I = 51
68077
XDOT = 363
707237 Wp = 167
12655
YDOT = -4747
661986 meter/sec RA = 1
49380 deg
ZDOT = -6017
392923 TA = 14
68000
MA = 14
64881
Ha = 216
386 n
mi
Hp = 213
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22202904
95 X = -6762673
13
Y = -1013728
74 feet Y = -384635
84 meter
Z = -549896
42 Z = -200472
20
XDOT = 1193
265214 XDOT = 446
000317
YDOT = -15576
318853 feet/sec YDOT = -4743
134753 meter/sec
ZDOT = -19742
102765 ZDOT = -6015
426112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16900484
70 X = -5151267
74
Y = 14428982
55 feet Y = 4397953
88 meter
Z = -690724
20 Z = -210532
74
XDOT = -8630
071132 XDOT = -2630
445681
YDOT = -11042
354417 feet/sec YDOT = -3365
709626 meter/sec
ZDOT = -19732
729131 ZDOT = -6014
535839
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 15112
56970406
00016717 00000-0 10270-3 0 9004
2 25544 51
6471 1
8825 0006126 250
6069 109
4422 15
56087610 19385
Satellite: ISS
Catalog Number: 25544
Epoch time: 15112
56970406 = yrday
fracday
Element set: 900
Inclination: 51
6471 deg
RA of node: 1
8825 deg
Eccentricity:
0006126
Arg of perigee: 250
6069 deg
Mean anomaly: 109
4422 deg
Mean motion: 15
56087610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 293
Coasting Arc #2 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2015/113/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6111661
39 A = 6780678
04 meter
Y = 1581815
50 meter E =
0007556
Z = 2464714
90 I = 51
63979
XDOT = -3298
485355 Wp = 73
69426
YDOT = 4425
393954 meter/sec RA = 356
51192 deg
ZDOT = 5327
510844 TA = 313
93872
MA = 314
00105
Ha = 215
910 n
mi
Hp = 213
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20051382
52 X = 6081546
14
Y = 5189683
41 feet Y = 1649991
75 meter
Z = 8086334
97 Z = 2494331
29
XDOT = -10821
802347 XDOT = -3373
605321
YDOT = 14519
009036 feet/sec YDOT = 4388
088194 meter/sec
ZDOT = 17478
710117 ZDOT = 5311
304756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17976165
43 X = 5479135
22
Y = -10187439
45 feet Y = -3105131
54 meter
Z = 8212984
96 Z = 2503317
82
XDOT = 1508
032154 XDOT = 459
648201
YDOT = 16725
256336 feet/sec YDOT = 5097
858131 meter/sec
ZDOT = 17408
356163 ZDOT = 5306
066958
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 15113
59718927
00016717 00000-0 10270-3 0 9017
2 25544 51
6465 356
7437 0006163 257
2171 102
8294 15
56191082 19548
Satellite: ISS
Catalog Number: 25544
Epoch time: 15113
59718927 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 356
7437 deg
Eccentricity:
0006163
Arg of perigee: 257
2171 deg
Mean anomaly: 102
8294 deg
Mean motion: 15
56191082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 319
Coasting Arc #3 (Orbit 1968)
---------------------------------------
Vector Time (GMT): 2015/114/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4456484
62 A = 6775239
20 meter
Y = -2772043
78 meter E =
0002608
Z = -4287511
64 I = 51
58993
XDOT = 5708
854739 Wp = 41
26612
YDOT = -3693
812876 meter/sec RA = 351
51202 deg
ZDOT = -3544
960787 TA = 192
57578
MA = 192
58229
Ha = 215
548 n
mi
Hp = 213
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14621012
55 X = -4404328
48
Y = -9094631
84 feet Y = -2821587
57 meter
Z = -14066639
24 Z = -4309033
79
XDOT = 18729
838381 XDOT = 5766
955753
YDOT = -12118
808649 feet/sec YDOT = -3629
647943 meter/sec
ZDOT = -11630
448777 ZDOT = -3517
086880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16701970
61 X = -5090760
64
Y = 3865482
44 feet Y = 1178199
05 meter
Z = -14158350
86 Z = -4315465
34
XDOT = 4978
992101 XDOT = 1517
596792
YDOT = -20654
236544 feet/sec YDOT = -6295
411299 meter/sec
ZDOT = -11510
224481 ZDOT = -3508
316422
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 15114
56041525
00016717 00000-0 10270-3 0 9029
2 25544 51
6458 351
9268 0006375 260
6621 99
3812 15
56255134 19693
Satellite: ISS
Catalog Number: 25544
Epoch time: 15114
56041525 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 351
9268 deg
Eccentricity:
0006375
Arg of perigee: 260
6621 deg
Mean anomaly: 99
3812 deg
Mean motion: 15
56255134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1969
Checksum: 316
Coasting Arc #4 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2015/115/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2090023
03 A = 6771311
88 meter
Y = 3767080
17 meter E =
0004106
Z = 5227296
87 I = 51
54623
XDOT = -7159
714339 Wp = 231
60344
YDOT = 2553
597784 meter/sec RA = 346
49024 deg
ZDOT = 1020
440404 TA = 208
60340
MA = 208
62593
Ha = 215
307 n
mi
Hp = 213
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6857030
94 X = 2022350
92
Y = 12359186
90 feet Y = 3790073
96 meter
Z = 17149924
12 Z = 5237285
37
XDOT = -23489
876441 XDOT = -7192
694095
YDOT = 8377
945484 feet/sec YDOT = 2473
348810 meter/sec
ZDOT = 3347
901588 ZDOT = 985
579525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13583106
86 X = 4140130
97
Y = 3717899
14 feet Y = 1133215
66 meter
Z = 17191995
38 Z = 5240120
19
XDOT = -10009
737183 XDOT = -3050
967893
YDOT = 21752
632510 feet/sec YDOT = 6630
202389 meter/sec
ZDOT = 3197
957984 ZDOT = 974
737594
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 15115
58781372
00016717 00000-0 10270-3 0 9034
2 25544 51
6461 346
7882 0006291 264
3308 95
7128 15
56312411 19851
Satellite: ISS
Catalog Number: 25544
Epoch time: 15115
58781372 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 346
7882 deg
Eccentricity:
0006291
Arg of perigee: 264
3308 deg
Mean anomaly: 95
7128 deg
Mean motion: 15
56312411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 319
Coasting Arc #5 (Orbit 1999)
---------------------------------------
Vector Time (GMT): 2015/116/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 580489
16 A = 6771779
23 meter
Y = -4451299
45 meter E =
0007211
Z = -5076529
99 I = 51
51672
XDOT = 7396
356076 Wp = 116
64904
YDOT = -1021
620691 meter/sec RA = 341
45787 deg
ZDOT = 1740
297431 TA = 170
21480
MA = 170
20075
Ha = 215
074 n
mi
Hp = 213
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1904491
98 X = 654881
51
Y = -14604000
81 feet Y = -4444392
31 meter
Z = -16655282
13 Z = -5073529
19
XDOT = 24266
260093 XDOT = 7398
776610
YDOT = -3351
773921 feet/sec YDOT = -938
896193 meter/sec
ZDOT = 5709
637240 ZDOT = 1776
233600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9320145
98 X = -2840780
49
Y = -11423500
75 feet Y = -3481883
03 meter
Z = -16641540
25 Z = -5072341
47
XDOT = 13224
237187 XDOT = 4030
747495
YDOT = -19337
714400 feet/sec YDOT = -5894
135349 meter/sec
ZDOT = 5863
879467 ZDOT = 1787
310461
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 15116
55095683
00016717 00000-0 10270-3 0 9046
2 25544 51
6449 341
9695 0006461 268
1417 91
8997 15
56408091 20008
Satellite: ISS
Catalog Number: 25544
Epoch time: 15116
55095683 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 341
9695 deg
Eccentricity:
0006461
Arg of perigee: 268
1417 deg
Mean anomaly: 91
8997 deg
Mean motion: 15
56408091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2000
Checksum: 328
Coasting Arc #6 (Orbit 2015)
---------------------------------------
Vector Time (GMT): 2015/117/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3079013
57 A = 6776277
23 meter
Y = 4664847
11 meter E =
0005010
Z = 3828515
38 I = 51
50332
XDOT = -6399
398010 Wp = 68
52531
YDOT = -811
428157 meter/sec RA = 336
43624 deg
ZDOT = -4151
740502 TA = 65
25087
MA = 65
19874
Ha = 214
912 n
mi
Hp = 213
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10101750
55 X = -3149545
77
Y = 15304616
51 feet Y = 4630021
41 meter
Z = 12560746
01 Z = 3813386
48
XDOT = -20995
400294 XDOT = -6369
681085
YDOT = -2662
165870 feet/sec YDOT = -882
824475 meter/sec
ZDOT = -13621
195872 ZDOT = -4182
755498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4571798
61 X = 1393484
22
Y = 17805141
93 feet Y = 5427007
26 meter
Z = 12494981
76 Z = 3808470
44
XDOT = -14663
690159 XDOT = -4469
492761
YDOT = 13431
490656 feet/sec YDOT = 4093
918352 meter/sec
ZDOT = -13753
975427 ZDOT = -4192
211710
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 15117
57826559
00016717 00000-0 10270-3 0 9054
2 25544 51
6454 336
8310 0006694 272
9157 87
1231 15
56499491 20163
Satellite: ISS
Catalog Number: 25544
Epoch time: 15117
57826559 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 336
8310 deg
Eccentricity:
0006694
Arg of perigee: 272
9157 deg
Mean anomaly: 87
1231 deg
Mean motion: 15
56499491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 331
Coasting Arc #7 (Orbit 2030)
---------------------------------------
Vector Time (GMT): 2015/118/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4960514
33 A = 6781141
06 meter
Y = -4276596
23 meter E =
0006963
Z = -1738950
06 I = 51
48956
XDOT = 4367
692049 Wp = 343
51475
YDOT = 2760
424659 meter/sec RA = 331
43150 deg
ZDOT = 5671
500220 TA = 357
34097
MA = 357
34467
Ha = 214
999 n
mi
Hp = 213
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16274653
33 X = 5016414
81
Y = -14030827
54 feet Y = -4220812
07 meter
Z = -5705216
73 Z = -1714716
61
XDOT = 14329
698322 XDOT = 4308
949459
YDOT = 9056
511349 feet/sec YDOT = 2808
938942 meter/sec
ZDOT = 18607
284185 ZDOT = 5692
574940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 104384
99 X = 31816
54
Y = -21515141
44 feet Y = -6557815
11 meter
Z = -5600513
63 Z = -1707036
56
XDOT = 14589
338689 XDOT = 4446
830432
YDOT = -4795
331085 feet/sec YDOT = -1461
616915 meter/sec
ZDOT = 18697
070801 ZDOT = 5698
867180
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 15118
54132877
00016717 00000-0 10270-3 0 9066
2 25544 51
6438 332
0119 0006677 275
7249 84
3144 15
56521451 20315
Satellite: ISS
Catalog Number: 25544
Epoch time: 15118
54132877 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 332
0119 deg
Eccentricity:
0006677
Arg of perigee: 275
7249 deg
Mean anomaly: 84
3144 deg
Mean motion: 15
56521451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2031
Checksum: 305
Coasting Arc #8 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2015/119/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5924342
79 A = 6781864
57 meter
Y = 3202206
75 meter E =
0006751
Z = -761775
40 I = 51
46530
XDOT = -1696
753332 Wp = 179
86574
YDOT = -4550
306681 meter/sec RA = 326
43928 deg
ZDOT = -5938
753602 TA = 8
39581
MA = 8
38452
Ha = 215
100 n
mi
Hp = 213
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19436820
18 X = -5956009
86
Y = 10505927
67 feet Y = 3135779
77 meter
Z = -2499263
11 Z = -790632
13
XDOT = -5566
776022 XDOT = -1616
896060
YDOT = -14928
827695 feet/sec YDOT = -4568
834755 meter/sec
ZDOT = -19484
099743 ZDOT = -5946
801932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4434148
93 X = -1351528
59
Y = 21630211
72 feet Y = 6592888
53 meter
Z = -2623561
50 Z = -799661
55
XDOT = -13359
190760 XDOT = -4071
881344
YDOT = -5103
390216 feet/sec YDOT = -1555
513338 meter/sec
ZDOT = -19517
705904 ZDOT = -5948
996760
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 15119
56855109
00016717 00000-0 10270-3 0 9070
2 25544 51
6436 326
8729 0006694 280
3076 79
7323 15
56605789 20471
Satellite: ISS
Catalog Number: 25544
Epoch time: 15119
56855109 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 326
8729 deg
Eccentricity:
0006694
Arg of perigee: 280
3076 deg
Mean anomaly: 79
7323 deg
Mean motion: 15
56605789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 345
Coasting Arc #9 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2015/120/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5835417
48 A = 6777730
03 meter
Y = -1489512
55 meter E =
0006732
Z = 3100709
30 I = 51
42534
XDOT = -1097
398034 Wp = 67
78769
YDOT = 5834
029032 meter/sec RA = 321
43646 deg
ZDOT = 4861
832280 TA = 328
05106
MA = 328
09186
Ha = 214
971 n
mi
Hp = 213
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19145070
47 X = 5836577
56
Y = -4886852
19 feet Y = -1424250
41 meter
Z = 10172930
76 Z = 3129059
92
XDOT = -3600
387251 XDOT = -1186
171265
YDOT = 19140
515196 feet/sec YDOT = 5821
261149 meter/sec
ZDOT = 15950
893308 ZDOT = 4856
285275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8213820
04 X = 2503572
35
Y = -17901271
22 feet Y = -5456307
47 meter
Z = 10294717
92 Z = 3137830
02
XDOT = 11238
387330 XDOT = 3425
460458
YDOT = 14326
516126 feet/sec YDOT = 4366
722115 meter/sec
ZDOT = 15925
988261 ZDOT = 4854
241222
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 15120
59572755
00016717 00000-0 10270-3 0 9089
2 25544 51
6426 321
7316 0006811 282
6425 77
3967 15
56681386 20633
Satellite: ISS
Catalog Number: 25544
Epoch time: 15120
59572755 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 321
7316 deg
Eccentricity:
0006811
Arg of perigee: 282
6425 deg
Mean anomaly: 77
3967 deg
Mean motion: 15
56681386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 326
Coasting Arc #10 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2015/121/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4788883
15 A = 6772053
67 meter
Y = -676018
75 meter E =
0007078
Z = -4746442
67 I = 51
38214
XDOT = 3518
266409 Wp = 37
80357
YDOT = -6274
538896 meter/sec RA = 316
41151 deg
ZDOT = -2652
679428 TA = 205
89522
MA = 205
93065
Ha = 215
282 n
mi
Hp = 212
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15711558
89 X = -4757910
99
Y = -2217909
29 feet Y = -729398
26 meter
Z = -15572318
47 Z = -4769631
27
XDOT = 11542
868797 XDOT = 3601
054255
YDOT = -20585
757533 feet/sec YDOT = -6234
732591 meter/sec
ZDOT = -8703
016495 ZDOT = -2635
386651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11365610
86 X = -3464238
19
Y = 10931352
30 feet Y = 3331876
18 meter
Z = -15671558
11 Z = -4776690
91
XDOT = -8275
284944 XDOT = -2522
306851
YDOT = -20988
812235 feet/sec YDOT = -6397
389969 meter/sec
ZDOT = -8627
697120 ZDOT = -2629
722082
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 15121
55866597
00016717 00000-0 10270-3 0 9097
2 25544 51
6421 316
9125 0006649 287
3982 72
6445 15
56739281 20784
Satellite: ISS
Catalog Number: 25544
Epoch time: 15121
55866597 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 316
9125 deg
Eccentricity:
0006649
Arg of perigee: 287
3982 deg
Mean anomaly: 72
6445 deg
Mean motion: 15
56739281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 345
Coasting Arc #11 (Orbit 2093)
---------------------------------------
Vector Time (GMT): 2015/122/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3028007
99 A = 6769744
10 meter
Y = 2958047
49 meter E =
0004757
Z = 5286433
46 I = 51
35172
XDOT = -5181
656342 Wp = 306
62249
YDOT = 5652
192552 meter/sec RA = 311
36547 deg
ZDOT = -192
049728 TA = 145
23023
MA = 145
19913
Ha = 215
461 n
mi
Hp = 213
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9934409
42 X = 2969025
32
Y = 9704880
22 feet Y = 2991579
09 meter
Z = 17343941
80 Z = 5300999
84
XDOT = -17000
184848 XDOT = -5243
542465
YDOT = 18543
938819 feet/sec YDOT = 5593
901849 meter/sec
ZDOT = -630
084411 ZDOT = -217
372262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13665587
93 X = 4165271
20
Y = -1994916
89 feet Y = -608050
67 meter
Z = 17405789
87 Z = 5305284
75
XDOT = 4418
846187 XDOT = 1346
864318
YDOT = 23740
118844 feet/sec YDOT = 7235
988224 meter/sec
ZDOT = -739
685236 ZDOT = -225
456060
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 15122
58575626
00016717 00000-0 10270-3 0 9103
2 25544 51
6417 311
7709 0006686 291
2398 68
8042 15
56749987 20948
Satellite: ISS
Catalog Number: 25544
Epoch time: 15122
58575626 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 311
7709 deg
Eccentricity:
0006686
Arg of perigee: 291
2398 deg
Mean anomaly: 68
8042 deg
Mean motion: 15
56749987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2094
Checksum: 345
Coasting Arc #12 (Orbit 2108)
---------------------------------------
Vector Time (GMT): 2015/123/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -934010
46 A = 6772458
76 meter
Y = -4908482
19 meter E =
0003441
Z = -4574989
07 I = 51
34193
XDOT = 5866
573100 Wp = 101
44956
YDOT = -3918
514755 meter/sec RA = 306
31905 deg
ZDOT = 3007
712038 TA = 198
69105
MA = 198
70369
Ha = 215
447 n
mi
Hp = 212
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3064338
79 X = -856829
16
Y = -16103944
18 feet Y = -4918495
47 meter
Z = -15009806
67 Z = -4579338
82
XDOT = 19247
287075 XDOT = 5895
344190
YDOT = -12856
019536 feet/sec YDOT = -3852
749958 meter/sec
ZDOT = 9867
821646 ZDOT = 3036
281306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14767914
99 X = -4501260
49
Y = -7078445
45 feet Y = -2157510
17 meter
Z = -15027500
91 Z = -4580382
28
XDOT = 381
812480 XDOT = 116
376444
YDOT = -21998
696686 feet/sec YDOT = -6705
202750 meter/sec
ZDOT = 9990
994756 ZDOT = 3045
255202
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 15123
54860933
00016717 00000-0 10270-3 0 9119
2 25544 51
6421 306
9505 0006715 294
4363 65
6091 15
56865837 21092
Satellite: ISS
Catalog Number: 25544
Epoch time: 15123
54860933 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 306
9505 deg
Eccentricity:
0006715
Arg of perigee: 294
4363 deg
Mean anomaly: 65
6091 deg
Mean motion: 15
56865837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2109
Checksum: 315
Coasting Arc #13 (Orbit 2124)
---------------------------------------
Vector Time (GMT): 2015/124/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1139049
65 A = 6778027
15 meter
Y = 6092172
57 meter E =
0007170
Z = 2738843
41 I = 51
34273
XDOT = -5566
652739 Wp = 84
32154
YDOT = 1268
014925 meter/sec RA = 301
29157 deg
ZDOT = -5123
342396 TA = 64
50622
MA = 64
43208
Ha = 215
643 n
mi
Hp = 212
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3737039
54 X = -1220393
69
Y = 19987442
82 feet Y = 6078980
17 meter
Z = 8985706
72 Z = 2733112
40
XDOT = -18263
296387 XDOT = -5555
530426
YDOT = 4160
153955 feet/sec YDOT = 1205
827141 meter/sec
ZDOT = -16808
866130 ZDOT = -5150
357703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14179844
29 X = 4322016
54
Y = 14589620
29 feet Y = 4446916
26 meter
Z = 8959980
81 Z = 2731002
15
XDOT = -5964
148044 XDOT = -1817
872324
YDOT = 16215
579211 feet/sec YDOT = 4942
508544 meter/sec
ZDOT = -16924
868186 ZDOT = -5158
699823
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 15124
57560871
00016717 00000-0 10270-3 0 9122
2 25544 51
6417 301
8089 0006941 298
4035 61
6419 15
56929596 21250
Satellite: ISS
Catalog Number: 25544
Epoch time: 15124
57560871 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 301
8089 deg
Eccentricity:
0006941
Arg of perigee: 298
4035 deg
Mean anomaly: 61
6419 deg
Mean motion: 15
56929596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2125
Checksum: 326
Coasting Arc #14 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2015/125/12:54:41
801
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2836396
17 A = 6780961
11 meter
Y = -6146234
17 meter E =
0012329
Z = -223040
50 I = 51
33879
XDOT = 4438
274056 Wp = 10
72608
YDOT = 1833
242334 meter/sec RA = 296
28317 deg
ZDOT = 5988
705339 TA = 346
85681
MA = 346
88890
Ha = 215
644 n
mi
Hp = 212
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9305761
70 X = 2905997
48
Y = -20164810
25 feet Y = -6114126
56 meter
Z = -731760
18 Z = -209092
57
XDOT = 14561
266587 XDOT = 4388
352936
YDOT = 6014
574585 feet/sec YDOT = 1882
594808 meter/sec
ZDOT = 19647
983395 ZDOT = 6010
144839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11483755
52 X = -3500248
68
Y = -19011196
91 feet Y = -5794612
82 meter
Z = -670818
65 Z = -204465
52
XDOT = 11686
533140 XDOT = 3562
055301
YDOT = -7747
551332 feet/sec YDOT = -2361
453646 meter/sec
ZDOT = 19739
499959 ZDOT = 6016
599587
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 15125
53837985
00016717 00000-0 10270-3 0 9133
2 25544 51
6429 296
9884 0006819 302
2869 57
7625 15
57006154 21402
Satellite: ISS
Catalog Number: 25544
Epoch time: 15125
53837985 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 296
9884 deg
Eccentricity:
0006819
Arg of perigee: 302
2869 deg
Mean anomaly: 57
7625 deg
Mean motion: 15
57006154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2140
Checksum: 339
Coasting Arc #15 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2015/126/05:25:59
882
Vector Time (MET): N/A
Weight (LBS) : 923014
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4339616
81 A = 6773016
74 meter
Y = -407765
63 meter E =
0005463
Z = -5188518
18 I = 51
29389
XDOT = 2067
797566 Wp = 54
09487
YDOT = -7292
826512 meter/sec RA = 292
83739 deg
ZDOT = -1154
045633 TA = 204
77173
MA = 204
79796
Ha = 216
360 n
mi
Hp = 215
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14237587
97 X = -4309530
17
Y = -1337813
75 feet Y = -456125
71 meter
Z = -17022697
43 Z = -5209526
54
XDOT = 6784
112748 XDOT = 2154
800036
YDOT = -23926
596168 feet/sec YDOT = -7269
216561 meter/sec
ZDOT = -3786
238953 ZDOT = -1143
789326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6881950
43 X = -2097618
49
Y = -12412379
77 feet Y = -3783293
35 meter
Z = -17112640
70 Z = -5215932
88
XDOT = 22680
721697 XDOT = 6913
083973
YDOT = -7407
350924 feet/sec YDOT = -2257
760562 meter/sec
ZDOT = -3740
899977 ZDOT = -1140
226313
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 15126
24439713
00016717 00000-0 10270-3 0 9140
2 25544 51
6459 293
4586 0009675 276
1499 83
8552 15
55765691 21514
Satellite: ISS
Catalog Number: 25544
Epoch time: 15126
24439713 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 293
4586 deg
Eccentricity:
0009675
Arg of perigee: 276
1499 deg
Mean anomaly: 83
8552 deg
Mean motion: 15
55765691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 348
Coasting Arc #16 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2015/127/05:25:59
882
Vector Time (MET): N/A
Weight (LBS) : 923014
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3443165
08 A = 6773019
87 meter
Y = 2762669
49 meter E =
0007465
Z = 5142910
30 I = 51
28310
XDOT = -3340
494415 Wp = 305
59700
YDOT = 6758
377076 meter/sec RA = 287
79514 deg
ZDOT = -1391
170650 TA = 157
86810
MA = 157
83586
Ha = 216
612 n
mi
Hp = 214
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11296473
35 X = 3387033
59
Y = 9063876
28 feet Y = 2800859
18 meter
Z = 16873065
28 Z = 5159500
56
XDOT = -10959
627347 XDOT = -3409
062024
YDOT = 22173
153136 feet/sec YDOT = 6720
638149 meter/sec
ZDOT = -4564
208169 ZDOT = -1407
564706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -906187
26 X = -276205
88
Y = 14372077
87 feet Y = 4380609
33 meter
Z = 16943632
96 Z = 5164419
33
XDOT = -23356
912472 XDOT = -7119
186922
YDOT = 4003
453951 feet/sec YDOT = 1220
252764 meter/sec
ZDOT = -4635
740894 ZDOT = -1412
973824
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 15127
27213661
00016717 00000-0 10270-3 0 9157
2 25544 51
6458 288
3226 0009908 280
4837 79
5200 15
55845176 21676
Satellite: ISS
Catalog Number: 25544
Epoch time: 15127
27213661 = yrday
fracday
Element set: 915
Inclination: 51
6458 deg
RA of node: 288
3226 deg
Eccentricity:
0009908
Arg of perigee: 280
4837 deg
Mean anomaly: 79
5200 deg
Mean motion: 15
55845176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 327
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