[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
028/18:41:30
089 0
8 -1
3 1
3
N/A 0
6 0
2 220
6
000/00:02:56
179 -0
9 -0
0 216
5
Coasting Arc #1 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2015/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5199654
57 A = 6784193
53 meter
Y = 997578
18 meter E =
0005872
Z = 4241710
74 I = 51
91298
XDOT = 1745
186919 Wp = 140
93306
YDOT = -6504
016048 meter/sec RA = 130
24460 deg
ZDOT = 3661
756064 TA = 271
66472
MA = 271
73198
Ha = 220
670 n
mi
Hp = 218
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17059234
15 X = -5231027
89
Y = 3272894
30 feet Y = 939256
75 meter
Z = 13916373
80 Z = 4216375
67
XDOT = 5725
678869 XDOT = 1799
999226
YDOT = -21338
635327 feet/sec YDOT = -6484
193839 meter/sec
ZDOT = 12013
635380 ZDOT = 3670
366827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9663696
29 X = -2945494
63
Y = -14537917
34 feet Y = -4431157
21 meter
Z = 13807849
22 Z = 4208632
44
XDOT = 20799
311103 XDOT = 6339
630024
YDOT = -2356
822723 feet/sec YDOT = -718
359566 meter/sec
ZDOT = 12051
578438 ZDOT = 3673
321108
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 15014
55499029
00016717 00000-0 10270-3 0 9001
2 25544 51
6449 130
9674 0006346 253
3707 106
6749 15
53315256 4134
Satellite: ISS
Catalog Number: 25544
Epoch time: 15014
55499029 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 130
9674 deg
Eccentricity:
0006346
Arg of perigee: 253
3707 deg
Mean anomaly: 106
6749 deg
Mean motion: 15
53315256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 309
Coasting Arc #2 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2015/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4626065
15 A = 6781416
39 meter
Y = 189908
23 meter E =
0005940
Z = -4960414
61 I = 51
92347
XDOT = -2678
813836 Wp = 68
98087
YDOT = 6821
109008 meter/sec RA = 125
27868 deg
ZDOT = -2237
189691 TA = 179
24755
MA = 179
24666
Ha = 220
455 n
mi
Hp = 218
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15177379
10 X = 4647693
53
Y = 623058
50 feet Y = 241761
01 meter
Z = -16274326
14 Z = -4937889
57
XDOT = -8788
759305 XDOT = -2744
022567
YDOT = 22378
966563 feet/sec YDOT = 6790
788249 meter/sec
ZDOT = -7339
861192 ZDOT = -2250
360969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5594550
70 X = 1705219
05
Y = 14232623
77 feet Y = 4338103
73 meter
Z = -16178014
48 Z = -4931058
81
XDOT = -22965
432370 XDOT = -6999
863786
YDOT = 619
051239 feet/sec YDOT = 188
686818 meter/sec
ZDOT = -7397
380001 ZDOT = -2254
721424
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 15015
52003435
00016717 00000-0 10270-3 0 9012
2 25544 51
6451 126
1631 0006334 258
2072 101
8370 15
53310411 4284
Satellite: ISS
Catalog Number: 25544
Epoch time: 15015
52003435 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 126
1631 deg
Eccentricity:
0006334
Arg of perigee: 258
2072 deg
Mean anomaly: 101
8370 deg
Mean motion: 15
53310411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 250
Coasting Arc #3 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2015/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3953481
00 A = 6779642
81 meter
Y = -1475471
40 meter E =
0004096
Z = 5309495
99 I = 51
93638
XDOT = 3412
974402 Wp = 239
22161
YDOT = -6833
082205 meter/sec RA = 120
30787 deg
ZDOT = 640
780298 TA = 204
67333
MA = 204
69293
Ha = 220
156 n
mi
Hp = 218
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12970738
20 X = -3962479
56
Y = -4840785
42 feet Y = -1519732
38 meter
Z = 17419606
25 Z = 5290268
87
XDOT = 11197
422578 XDOT = 3486
017210
YDOT = -22418
248703 feet/sec YDOT = -6794
507734 meter/sec
ZDOT = 2102
297565 ZDOT = 657
536872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1087468
61 X = -331460
43
Y = -13904688
67 feet Y = -4238149
11 meter
Z = 17337617
48 Z = 5284505
81
XDOT = 24027
417215 XDOT = 7323
556767
YDOT = 839
929768 feet/sec YDOT = 256
010593 meter/sec
ZDOT = 2175
172817 ZDOT = 662
992675
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 15016
54938849
00016717 00000-0 10270-3 0 9022
2 25544 51
6456 121
0375 0006256 262
8368 97
2073 15
53391019 4449
Satellite: ISS
Catalog Number: 25544
Epoch time: 15016
54938849 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 121
0375 deg
Eccentricity:
0006256
Arg of perigee: 262
8368 deg
Mean anomaly: 97
2073 deg
Mean motion: 15
53391019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 444
Checksum: 315
Coasting Arc #4 (Orbit 458)
---------------------------------------
Vector Time (GMT): 2015/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3234047
01 A = 6779770
77 meter
Y = 2801220
90 meter E =
0008392
Z = -5266518
58 I = 51
95232
XDOT = -3952
917895 Wp = 105
21607
YDOT = 6482
936446 meter/sec RA = 115
33735 deg
ZDOT = 1020
037603 TA = 174
52231
MA = 174
51312
Ha = 219
894 n
mi
Hp = 218
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10610390
46 X = 3228065
35
Y = 9190357
28 feet Y = 2837353
00 meter
Z = -17278604
27 Z = -5250822
66
XDOT = -12968
890730 XDOT = -4030
072749
YDOT = 21269
476530 feet/sec YDOT = 6438
300887 meter/sec
ZDOT = 3346
580062 ZDOT = 1000
648230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3617019
41 X = -1102467
52
Y = 13647679
60 feet Y = 4159812
74 meter
Z = -17211950
22 Z = -5246202
43
XDOT = -23806
211640 XDOT = -7256
133308
YDOT = -2191
504728 feet/sec YDOT = -667
970641 meter/sec
ZDOT = 3262
484084 ZDOT = 994
405149
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 15017
51438757
00016717 00000-0 10270-3 0 9034
2 25544 51
6458 116
2335 0006134 267
6117 92
4333 15
53410282 4599
Satellite: ISS
Catalog Number: 25544
Epoch time: 15017
51438757 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 116
2335 deg
Eccentricity:
0006134
Arg of perigee: 267
6117 deg
Mean anomaly: 92
4333 deg
Mean motion: 15
53410282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 459
Checksum: 297
Coasting Arc #5 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2015/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2504946
59 A = 6781550
34 meter
Y = -4068979
10 meter E =
0003838
Z = 4813548
70 I = 51
97177
XDOT = 4323
668135 Wp = 5
51953
YDOT = -5763
202714 meter/sec RA = 110
36891 deg
ZDOT = -2617
832389 TA = 110
19359
MA = 110
15231
Ha = 219
913 n
mi
Hp = 217
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8218328
71 X = -2482642
29
Y = -13349668
96 feet Y = -4096866
65 meter
Z = 15792482
62 Z = 4801434
20
XDOT = 14185
262910 XDOT = 4400
508582
YDOT = -18908
145388 feet/sec YDOT = -5714
422835 meter/sec
ZDOT = -8588
688940 ZDOT = -2596
642827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8176872
83 X = 2492310
84
Y = -13435213
95 feet Y = -4095053
21 meter
Z = 15741374
54 Z = 4797970
96
XDOT = 22314
301202 XDOT = 6801
399006
YDOT = 3610
298436 feet/sec YDOT = 1100
418963 meter/sec
ZDOT = -8497
000285 ZDOT = -2589
885687
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 15018
54369517
00016717 00000-0 10270-3 0 9046
2 25544 51
6462 111
1078 0006115 272
4828 87
5624 15
53449315 4759
Satellite: ISS
Catalog Number: 25544
Epoch time: 15018
54369517 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 111
1078 deg
Eccentricity:
0006115
Arg of perigee: 272
4828 deg
Mean anomaly: 87
5624 deg
Mean motion: 15
53449315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 309
Coasting Arc #6 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2015/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1804168
27 A = 6784502
24 meter
Y = 5184636
37 meter E =
0001465
Z = -3988196
18 I = 51
99191
XDOT = -4548
817785 Wp = 161
42988
YDOT = 4676
966990 meter/sec RA = 105
40793 deg
ZDOT = 4021
309081 TA = 150
32798
MA = 150
31967
Ha = 219
920 n
mi
Hp = 217
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5919187
24 X = 1765431
21
Y = 17009961
85 feet Y = 5204595
39 meter
Z = -13084633
13 Z = -3979525
81
XDOT = -14923
942864 XDOT = -4620
312346
YDOT = 15344
379887 feet/sec YDOT = 4625
699172 meter/sec
ZDOT = 13193
271264 ZDOT = 3999
038783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12262445
89 X = -3737593
51
Y = 13226989
97 feet Y = 4031586
54 meter
Z = -13048462
01 Z = -3977171
22
XDOT = -19601
597425 XDOT = -5974
566895
YDOT = -5248
771559 feet/sec YDOT = -1599
825571 meter/sec
ZDOT = 13097
136568 ZDOT = 3992
007226
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 15019
50864932
00016717 00000-0 10270-3 0 9055
2 25544 51
6460 106
3034 0006079 275
9752 84
0708 15
53484292 4903
Satellite: ISS
Catalog Number: 25544
Epoch time: 15019
50864932 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 106
3034 deg
Eccentricity:
0006079
Arg of perigee: 275
9752 deg
Mean anomaly: 84
0708 deg
Mean motion: 15
53484292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 312
Coasting Arc #7 (Orbit 505)
---------------------------------------
Vector Time (GMT): 2015/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1130491
22 A = 6787751
33 meter
Y = -6060813
66 meter E =
0007357
Z = 2831633
10 I = 52
01029
XDOT = 4672
573690 Wp = 98
41591
YDOT = -3270
178925 meter/sec RA = 100
45458 deg
ZDOT = -5123
725172 TA = 49
60754
MA = 49
54335
Ha = 220
068 n
mi
Hp = 217
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3708960
69 X = -1076388
49
Y = -19884559
26 feet Y = -6073153
15 meter
Z = 9290134
85 Z = 2826272
68
XDOT = 15329
966176 XDOT = 4733
682955
YDOT = -10728
933482 feet/sec YDOT = -3217
585287 meter/sec
ZDOT = -16810
121954 ZDOT = -5100
878879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15627935
19 X = 4763394
65
Y = -12857883
93 feet Y = -3919083
02 meter
Z = 9268287
56 Z = 2824974
05
XDOT = 15889
715831 XDOT = 4843
185385
YDOT = 7242
284463 feet/sec YDOT = 2207
448304 meter/sec
ZDOT = -16711
762920 ZDOT = -5093
745338
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 15020
53791033
00016717 00000-0 10270-3 0 9062
2 25544 51
6459 101
1778 0006022 281
5684 78
4792 15
53508651 5068
Satellite: ISS
Catalog Number: 25544
Epoch time: 15020
53791033 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 101
1778 deg
Eccentricity:
0006022
Arg of perigee: 281
5684 deg
Mean anomaly: 78
4792 deg
Mean motion: 15
53508651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 506
Checksum: 304
Coasting Arc #8 (Orbit 520)
---------------------------------------
Vector Time (GMT): 2015/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 498504
30 A = 6790272
75 meter
Y = 6609440
07 meter E =
0008497
Z = -1448337
03 I = 52
02308
XDOT = -4720
642109 Wp = 355
16962
YDOT = 1629
873642 meter/sec RA = 95
50816 deg
ZDOT = 5818
832744 TA = 349
11748
MA = 349
13585
Ha = 220
379 n
mi
Hp = 217
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1635512
79 X = 431594
26
Y = 21684514
66 feet Y = 6614640
57 meter
Z = -4751761
92 Z = -1446077
86
XDOT = -15487
670961 XDOT = -4766
781970
YDOT = 5347
354469 feet/sec YDOT = 1576
826283 meter/sec
ZDOT = 19090
658610 ZDOT = 5795
789251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18009859
48 X = -5489405
17
Y = 12190918
24 feet Y = 3715791
88 meter
Z = -4743289
29 Z = -1445754
58
XDOT = -11490
992661 XDOT = -3502
454563
YDOT = -9593
829682 feet/sec YDOT = -2924
199287 meter/sec
ZDOT = 18991
743143 ZDOT = 5788
683310
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 15021
50282005
00016717 00000-0 10270-3 0 9075
2 25544 51
6455 96
3722 0006142 286
8194 73
2284 15
53498966 5218
Satellite: ISS
Catalog Number: 25544
Epoch time: 15021
50282005 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 96
3722 deg
Eccentricity:
0006142
Arg of perigee: 286
8194 deg
Mean anomaly: 73
2284 deg
Mean motion: 15
53498966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 521
Checksum: 307
Coasting Arc #9 (Orbit 536)
---------------------------------------
Vector Time (GMT): 2015/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 126308
81 A = 6790934
36 meter
Y = -6785045
44 meter E =
0006975
Z = -75911
07 I = 52
02749
XDOT = 4715
128622 Wp = 155
67610
YDOT = 153
110975 meter/sec RA = 90
56623 deg
ZDOT = -6042
706188 TA = 25
13691
MA = 25
10297
Ha = 220
402 n
mi
Hp = 217
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 414398
98 X = 202540
13
Y = -22260647
78 feet Y = -6783206
74 meter
Z = -249052
08 Z = -75112
29
XDOT = 15469
582092 XDOT = 4742
418627
YDOT = 502
332595 feet/sec YDOT = 205
991144 meter/sec
ZDOT = -19825
151537 ZDOT = -6019
735225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19355658
38 X = 5899604
68
Y = -11003133
65 feet Y = -3353755
14 meter
Z = -244400
46 Z = -74493
26
XDOT = 6726
071877 XDOT = 2050
106708
YDOT = 12254
961481 feet/sec YDOT = 3735
312260 meter/sec
ZDOT = -19726
864747 ZDOT = -6012
748375
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 15022
53203463
00016717 00000-0 10270-3 0 9081
2 25544 51
6449 91
2461 0005956 290
8949 69
1566 15
53575083 5370
Satellite: ISS
Catalog Number: 25544
Epoch time: 15022
53203463 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 91
2461 deg
Eccentricity:
0005956
Arg of perigee: 290
8949 deg
Mean anomaly: 69
1566 deg
Mean motion: 15
53575083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 537
Checksum: 325
Coasting Arc #10 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2015/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -746043
92 A = 6789849
32 meter
Y = 6550483
55 meter E =
0011389
Z = 1593281
26 I = 52
02308
XDOT = -4666
261830 Wp = 38
20013
YDOT = -1938
251010 meter/sec RA = 85
62316 deg
ZDOT = 5770
586232 TA = 339
13780
MA = 339
18424
Ha = 220
693 n
mi
Hp = 217
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2447650
64 X = -826976
93
Y = 21491087
75 feet Y = 6541688
32 meter
Z = 5227300
73 Z = 1589460
45
XDOT = -15309
257971 XDOT = -4672
271858
YDOT = -6359
091241 feet/sec YDOT = -1990
465637 meter/sec
ZDOT = 18932
369529 ZDOT = 5747
904326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19593100
88 X = -5971977
15
Y = 9173407
81 feet Y = 2796054
70 meter
Z = 5209751
08 Z = 1587932
13
XDOT = -2021
806582 XDOT = -616
246646
YDOT = -15040
142404 feet/sec YDOT = -4584
235405 meter/sec
ZDOT = 18835
643833 ZDOT = 5741
104240
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 15023
56122529
00016717 00000-0 10270-3 0 9099
2 25544 51
6446 86
1191 0005940 296
3141 63
7401 15
53583222 5538
Satellite: ISS
Catalog Number: 25544
Epoch time: 15023
56122529 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 86
1191 deg
Eccentricity:
0005940
Arg of perigee: 296
3141 deg
Mean anomaly: 63
7401 deg
Mean motion: 15
53583222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 553
Checksum: 291
Coasting Arc #11 (Orbit 567)
---------------------------------------
Vector Time (GMT): 2015/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1399853
41 A = 6786955
69 meter
Y = -5926167
15 meter E =
0001571
Z = -2998221
01 I = 52
01063
XDOT = 4550
327063 Wp = 326
89576
YDOT = 3606
374505 meter/sec RA = 80
67527 deg
ZDOT = -5001
183772 TA = 247
19386
MA = 247
21046
Ha = 220
716 n
mi
Hp = 217
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4592694
92 X = 1480581
17
Y = -19442805
61 feet Y = -5910061
81 meter
Z = -9836683
09 Z = -2991224
62
XDOT = 14928
894565 XDOT = 4533
955048
YDOT = 11831
937353 feet/sec YDOT = 3657
167511 meter/sec
ZDOT = -16408
083243 ZDOT = -4979
119400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18881572
52 X = 5755103
30
Y = -6573534
23 feet Y = -2003613
23 meter
Z = -9805648
26 Z = -2988761
59
XDOT = -2327
376666 XDOT = -709
384408
YDOT = 17663
090520 feet/sec YDOT = 5383
709990 meter/sec
ZDOT = -16314
309112 ZDOT = -4972
601417
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 15024
52606890
00016717 00000-0 10270-3 0 9106
2 25544 51
6445 81
3127 0005879 300
2413 59
8157 15
53643357 5687
Satellite: ISS
Catalog Number: 25544
Epoch time: 15024
52606890 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 81
3127 deg
Eccentricity:
0005879
Arg of perigee: 300
2413 deg
Mean anomaly: 59
8157 deg
Mean motion: 15
53643357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 568
Checksum: 307
Coasting Arc #12 (Orbit 583)
---------------------------------------
Vector Time (GMT): 2015/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2086569
03 A = 6783381
27 meter
Y = 4941449
19 meter E =
0005353
Z = 4147283
35 I = 51
99288
XDOT = -4352
799701 Wp = 81
03334
YDOT = -5036
746418 meter/sec RA = 75
71888 deg
ZDOT = 3807
902870 TA = 329
88956
MA = 329
92032
Ha = 220
944 n
mi
Hp = 217
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6845698
91 X = -2161816
10
Y = 16212103
65 feet Y = 4917695
22 meter
Z = 13606572
68 Z = 4136964
41
XDOT = -14280
838913 XDOT = -4314
651251
YDOT = -16524
758590 feet/sec YDOT = -5085
208835 meter/sec
ZDOT = 12493
119652 ZDOT = 3786
850890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17337896
62 X = -5284590
89
Y = 3212170
17 feet Y = 979069
47 meter
Z = 13561490
41 Z = 4133542
28
XDOT = 6034
281488 XDOT = 1839
248998
YDOT = -19844
692599 feet/sec YDOT = -6048
662304 meter/sec
ZDOT = 12403
949573 ZDOT = 3780
723830
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 15025
55521215
00016717 00000-0 10270-3 0 9118
2 25544 51
6443 76
1855 0005868 304
7337 55
3262 15
53681769 5842
Satellite: ISS
Catalog Number: 25544
Epoch time: 15025
55521215 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 76
1855 deg
Eccentricity:
0005868
Arg of perigee: 304
7337 deg
Mean anomaly: 55
3262 deg
Mean motion: 15
53681769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 584
Checksum: 314
Coasting Arc #13 (Orbit 598)
---------------------------------------
Vector Time (GMT): 2015/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2813434
07 A = 6780279
05 meter
Y = -3690246
93 meter E =
0010123
Z = -4952239
29 I = 51
97481
XDOT = 4016
050029 Wp = 45
06424
YDOT = 6114
955242 meter/sec RA = 70
75339 deg
ZDOT = -2270
969786 TA = 202
80567
MA = 202
85066
Ha = 221
007 n
mi
Hp = 217
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9230426
75 X = 2878546
07
Y = -12107109
35 feet Y = -3658421
33 meter
Z = -16247504
24 Z = -4938414
08
XDOT = 13176
017156 XDOT = 3958
404094
YDOT = 20062
189113 feet/sec YDOT = 6159
542959 meter/sec
ZDOT = -7450
688273 ZDOT = -2251
600937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15267177
36 X = 4653435
66
Y = 798665
03 feet Y = 243433
10 meter
Z = -16187640
30 Z = -4933992
76
XDOT = -8934
928303 XDOT = -2723
366147
YDOT = 21167
484672 feet/sec YDOT = 6451
849328 meter/sec
ZDOT = -7368
933096 ZDOT = -2246
050808
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 15026
52001371
00016717 00000-0 10270-3 0 9123
2 25544 51
6451 71
3788 0005862 308
9066 51
1564 15
53698850 5996
Satellite: ISS
Catalog Number: 25544
Epoch time: 15026
52001371 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 71
3788 deg
Eccentricity:
0005862
Arg of perigee: 308
9066 deg
Mean anomaly: 51
1564 deg
Mean motion: 15
53698850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 599
Checksum: 313
Coasting Arc #14 (Orbit 614)
---------------------------------------
Vector Time (GMT): 2015/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3555285
96 A = 6778520
72 meter
Y = 2242106
09 meter E =
0003451
Z = 5319181
44 I = 51
95767
XDOT = -3507
458491 Wp = 331
91842
YDOT = -6797
836431 meter/sec RA = 65
78115 deg
ZDOT = 524
132276 TA = 113
12026
MA = 113
08388
Ha = 221
226 n
mi
Hp = 216
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11664324
03 X = -3605931
84
Y = 7355991
11 feet Y = 2202065
44 meter
Z = 17451382
69 Z = 5301787
68
XDOT = -11507
409747 XDOT = -3433
728820
YDOT = -22302
612962 feet/sec YDOT = -6836
646862 meter/sec
ZDOT = 1719
594080 ZDOT = 507
273019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12838136
08 X = -3913063
88
Y = -5287430
46 feet Y = -1611608
80 meter
Z = 17376511
71 Z = 5296360
77
XDOT = 11037
584103 XDOT = 3364
255635
YDOT = -21415
056512 feet/sec YDOT = -6527
309225 meter/sec
ZDOT = 1648
720571 ZDOT = 502
530030
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 15027
54911100
00016717 00000-0 10270-3 0 9137
2 25544 51
6446 66
2518 0005823 314
2409 45
8265 15
53753835 6154
Satellite: ISS
Catalog Number: 25544
Epoch time: 15027
54911100 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 66
2518 deg
Eccentricity:
0005823
Arg of perigee: 314
2409 deg
Mean anomaly: 45
8265 deg
Mean motion: 15
53753835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 615
Checksum: 295
Coasting Arc #15 (Orbit 629)
---------------------------------------
Vector Time (GMT): 2015/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266601
40 A = 6778960
50 meter
Y = -745824
24 meter E =
0010055
Z = -5222907
84 I = 51
94663
XDOT = 2782
089843 Wp = 78
40846
YDOT = 7023
461341 meter/sec RA = 60
80621 deg
ZDOT = 1273
787835 TA = 203
75813
MA = 203
80458
Ha = 221
318 n
mi
Hp = 216
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13998036
10 X = 4299994
96
Y = -2446929
93 feet Y = -697925
60 meter
Z = -17135524
42 Z = -5202100
62
XDOT = 9127
591349 XDOT = 2697
157555
YDOT = 23042
852170 feet/sec YDOT = 7054
097592 meter/sec
ZDOT = 4179
093948 ZDOT = 1287
096286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10376382
32 X = 3162721
33
Y = 9864694
34 feet Y = 3006758
84 meter
Z = -17046324
33 Z = -5195719
66
XDOT = -12353
527052 XDOT = -3765
355046
YDOT = 20288
959309 feet/sec YDOT = 6184
074797 meter/sec
ZDOT = 4234
714705 ZDOT = 1290
741042
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 15028
51386890
00016717 00000-0 10270-3 0 9148
2 25544 51
6458 61
4450 0005899 317
9918 42
0782 15
53764523 6303
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
51386890 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 61
4450 deg
Eccentricity:
0005899
Arg of perigee: 317
9918 deg
Mean anomaly: 42
0782 deg
Mean motion: 15
53764523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 630
Checksum: 325
Coasting Arc #16 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2015/028/18:42:58
179
Vector Time (MET): N/A
Weight (LBS) : 949942
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -416965
17 A = 6782787
50 meter
Y = 5455475
53 meter E =
0006257
Z = 4002248
39 I = 51
95678
XDOT = -5616
460222 Wp = 73
63080
YDOT = -3363
821151 meter/sec RA = 59
45364 deg
ZDOT = 3996
652981 TA = 334
93039
MA = 334
96076
Ha = 220
562 n
mi
Hp = 216
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1367995
97 X = -497379
81
Y = 17898541
76 feet Y = 5450363
10 meter
Z = 13130736
20 Z = 4000027
59
XDOT = -18426
706766 XDOT = -5597
841798
YDOT = -11036
158633 feet/sec YDOT = -3426
523986 meter/sec
ZDOT = 13112
378545 ZDOT = 3969
414793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12244112
72 X = 3732005
56
Y = 13137269
62 feet Y = 4004239
78 meter
Z = 13120186
50 Z = 3999032
85
XDOT = -19669
654166 XDOT = -5995
310590
YDOT = 5341
555730 feet/sec YDOT = 1628
106186 meter/sec
ZDOT = 12996
438959 ZDOT = 3961
314595
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 15028
83543990
00016717 00000-0 10270-3 0 9150
2 25544 51
6446 59
8425 0006040 309
6641 50
3979 15
54044258 6355
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
83543990 = yrday
fracday
Element set: 915
Inclination: 51
6446 deg
RA of node: 59
8425 deg
Eccentricity:
0006040
Arg of perigee: 309
6641 deg
Mean anomaly: 50
3979 deg
Mean motion: 15
54044258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 319
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