[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 17th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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
027/19:27:44
236 2
4 2
8 2
8
N/A 1
5 -0
2 222
4
000/00:09:28
472 -0
3 0
0 213
1
Coasting Arc #1 (Orbit 2107)
---------------------------------------
Vector Time (GMT): 2016/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4340506
17 A = 6777243
75 meter
Y = 952483
32 meter E =
0006777
Z = 5110963
76 I = 51
98175
XDOT = 405
653687 Wp = 67
02993
YDOT = -7464
220375 meter/sec RA = 103
57319 deg
ZDOT = 1736
295079 TA = 6
28471
MA = 6
27621
Ha = 222
021 n
mi
Hp = 213
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14240505
82 X = -4375661
12
Y = 3124945
27 feet Y = 903748
36 meter
Z = 16768253
80 Z = 5089793
47
XDOT = 1330
884799 XDOT = 480
656191
YDOT = -24488
911991 feet/sec YDOT = -7459
264715 meter/sec
ZDOT = 5696
506165 ZDOT = 1738
447828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8595979
95 X = -2620054
69
Y = -11905567
47 feet Y = -3628816
96 meter
Z = 16676277
05 Z = 5082929
25
XDOT = 22099
755929 XDOT = 6736
005607
YDOT = -7965
631913 feet/sec YDOT = -2427
924607 meter/sec
ZDOT = 5707
219262 ZDOT = 1739
560431
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 16015
55124352
00016717 00000-0 10270-3 0 9007
2 25544 51
6424 104
2216 0005982 18
8944 341
2430 15
54505728 21088
Satellite: ISS
Catalog Number: 25544
Epoch time: 16015
55124352 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 104
2216 deg
Eccentricity:
0005982
Arg of perigee: 18
8944 deg
Mean anomaly: 341
2430 deg
Mean motion: 15
54505728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2108
Checksum: 279
Coasting Arc #2 (Orbit 2122)
---------------------------------------
Vector Time (GMT): 2016/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4073262
44 A = 6776335
07 meter
Y = 982899
21 meter E =
0017847
Z = -5340014
80 I = 51
98451
XDOT = -1394
708406 Wp = 73
56522
YDOT = 7521
513746 meter/sec RA = 98
59366 deg
ZDOT = 326
383807 TA = 199
50216
MA = 199
57052
Ha = 222
029 n
mi
Hp = 213
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13363721
92 X = 4087908
03
Y = 3224734
95 feet Y = 1028531
02 meter
Z = -17519733
60 Z = -5320192
46
XDOT = -4575
814981 XDOT = -1480
297590
YDOT = 24676
882370 feet/sec YDOT = 7505
438637 meter/sec
ZDOT = 1070
813014 ZDOT = 319
400816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2660729
00 X = 810990
20
Y = 13598039
72 feet Y = 4144682
51 meter
Z = -17433957
71 Z = -5313870
31
XDOT = -23361
517320 XDOT = -7120
590479
YDOT = 5878
857117 feet/sec YDOT = 1791
875649 meter/sec
ZDOT = 1039
129447 ZDOT = 316
726655
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 16016
51555041
00016717 00000-0 10270-3 0 9018
2 25544 51
6418 99
4123 0006149 21
9837 338
1579 15
54491176 21232
Satellite: ISS
Catalog Number: 25544
Epoch time: 16016
51555041 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 99
4123 deg
Eccentricity:
0006149
Arg of perigee: 21
9837 deg
Mean anomaly: 338
1579 deg
Mean motion: 15
54491176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2123
Checksum: 304
Coasting Arc #3 (Orbit 2138)
---------------------------------------
Vector Time (GMT): 2016/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3658948
37 A = 6777936
61 meter
Y = -2903792
80 meter E =
0012471
Z = 4907313
78 I = 51
99496
XDOT = 2295
766434 Wp = 42
90405
YDOT = -6924
903480 meter/sec RA = 93
61395 deg
ZDOT = -2373
477408 TA = 70
28119
MA = 70
14670
Ha = 222
080 n
mi
Hp = 212
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12004423
77 X = -3650043
02
Y = -9526879
25 feet Y = -2944659
85 meter
Z = 16100110
83 Z = 4889561
19
XDOT = 7532
042106 XDOT = 2384
561068
YDOT = -22719
499606 feet/sec YDOT = -6898
734191 meter/sec
ZDOT = -7786
999370 ZDOT = -2362
109609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3382996
61 X = 1031137
37
Y = -15029254
13 feet Y = -4580916
66 meter
Z = 16023671
29 Z = 4884015
01
XDOT = 22674
648198 XDOT = 6911
232771
YDOT = -3188
033403 feet/sec YDOT = -971
712581 meter/sec
ZDOT = -7736
396276 ZDOT = -2358
053585
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 16017
54412672
00016717 00000-0 10270-3 0 9025
2 25544 51
6423 94
2808 0006223 25
3863 334
7595 15
54561508 21395
Satellite: ISS
Catalog Number: 25544
Epoch time: 16017
54412672 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 94
2808 deg
Eccentricity:
0006223
Arg of perigee: 25
3863 deg
Mean anomaly: 334
7595 deg
Mean motion: 15
54561508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2139
Checksum: 304
Coasting Arc #4 (Orbit 2153)
---------------------------------------
Vector Time (GMT): 2016/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3165152
05 A = 6781608
89 meter
Y = 4549469
62 meter E =
0010132
Z = -3913403
96 I = 52
00775
XDOT = -3083
973413 Wp = 68
67272
YDOT = 5678
521138 meter/sec RA = 88
64436 deg
ZDOT = 4119
302054 TA = 244
28113
MA = 244
38576
Ha = 222
146 n
mi
Hp = 212
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10384357
11 X = 3133053
07
Y = 14926081
44 feet Y = 4584685
08 meter
Z = -12839251
83 Z = -3898106
34
XDOT = -10118
023007 XDOT = -3167
252539
YDOT = 18630
318694 feet/sec YDOT = 5643
568349 meter/sec
ZDOT = 13514
770517 ZDOT = 4104
118831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8688468
83 X = -2648245
30
Y = 16025302
90 feet Y = 4884512
32 meter
Z = -12773775
62 Z = -3893446
81
XDOT = -20058
594368 XDOT = -6113
859563
YDOT = -187
816899 feet/sec YDOT = -57
246591 meter/sec
ZDOT = 13447
840823 ZDOT = 4098
901883
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 16018
50840464
00016717 00000-0 10270-3 0 9037
2 25544 51
6415 89
4714 0006316 30
7379 329
4142 15
54572629 21545
Satellite: ISS
Catalog Number: 25544
Epoch time: 16018
50840464 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 89
4714 deg
Eccentricity:
0006316
Arg of perigee: 30
7379 deg
Mean anomaly: 329
4142 deg
Mean motion: 15
54572629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2154
Checksum: 306
Coasting Arc #5 (Orbit 2169)
---------------------------------------
Vector Time (GMT): 2016/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2527692
86 A = 6785554
09 meter
Y = -5817700
63 meter E =
0016859
Z = 2398408
58 I = 52
02010
XDOT = 3809
124667 Wp = 84
60232
YDOT = -3894
429776 meter/sec RA = 83
68545 deg
ZDOT = -5398
025559 TA = 68
73755
MA = 68
55760
Ha = 222
181 n
mi
Hp = 212
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8292955
57 X = -2474100
39
Y = -19086944
32 feet Y = -5845667
41 meter
Z = 7868794
56 Z = 2386259
68
XDOT = 12497
128174 XDOT = 3878
611157
YDOT = -12777
000578 feet/sec YDOT = -3851
444873 meter/sec
ZDOT = -17710
057607 ZDOT = -5379
353291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13083085
68 X = 3987724
52
Y = -16208835
29 feet Y = -4940452
99 meter
Z = 7817225
29 Z = 2382690
27
XDOT = 15973
786732 XDOT = 4868
810196
YDOT = 4337
318096 feet/sec YDOT = 1322
014556 meter/sec
ZDOT = -17628
324068 ZDOT = -5373
113176
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 16019
53695065
00016717 00000-0 10270-3 0 9047
2 25544 51
6421 84
3400 0006509 33
2010 326
9550 15
54600150 21706
Satellite: ISS
Catalog Number: 25544
Epoch time: 16019
53695065 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 84
3400 deg
Eccentricity:
0006509
Arg of perigee: 33
2010 deg
Mean anomaly: 326
9550 deg
Mean motion: 15
54600150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2170
Checksum: 267
Coasting Arc #6 (Orbit 2184)
---------------------------------------
Vector Time (GMT): 2016/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1798506
69 A = 6787938
89 meter
Y = 6506199
30 meter E =
0017406
Z = -631579
87 I = 52
02279
XDOT = -4423
199909 Wp = 38
97998
YDOT = 1795
795032 meter/sec RA = 78
73628 deg
ZDOT = 6006
269571 TA = 314
23282
MA = 314
37560
Ha = 222
378 n
mi
Hp = 212
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5900612
51 X = 1728687
01
Y = 21345798
22 feet Y = 6525921
04 meter
Z = -2072112
42 Z = -623012
51
XDOT = -14511
810725 XDOT = -4472
127772
YDOT = 5891
715984 feet/sec YDOT = 1746
058007 meter/sec
ZDOT = 19705
608828 ZDOT = 5984
664235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15946529
25 X = -4860502
12
Y = 15372572
75 feet Y = 4685560
18 meter
Z = -2036219
85 Z = -620639
81
XDOT = -11036
806392 XDOT = -3364
018588
YDOT = -8896
543098 feet/sec YDOT = -2711
666336 meter/sec
ZDOT = 19611
550286 ZDOT = 5977
600527
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 16020
50119910
00016717 00000-0 10270-3 0 9057
2 25544 51
6417 79
5299 0006673 36
4206 323
7399 15
54550859 21859
Satellite: ISS
Catalog Number: 25544
Epoch time: 16020
50119910 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 79
5299 deg
Eccentricity:
0006673
Arg of perigee: 36
4206 deg
Mean anomaly: 323
7399 deg
Mean motion: 15
54550859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2185
Checksum: 320
Coasting Arc #7 (Orbit 2200)
---------------------------------------
Vector Time (GMT): 2016/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -886949
44 A = 6787169
54 meter
Y = -6607963
34 meter E =
0010140
Z = -1271723
06 I = 52
01439
XDOT = 4906
603927 Wp = 101
56666
YDOT = 462
782656 meter/sec RA = 73
78928 deg
ZDOT = -5868
151429 TA = 92
18549
MA = 92
06938
Ha = 222
312 n
mi
Hp = 212
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2909939
10 X = -806814
25
Y = -21679669
75 feet Y = -6617433
67 meter
Z = -4172319
75 Z = -1275837
29
XDOT = 16097
781914 XDOT = 4929
568860
YDOT = 1518
315800 feet/sec YDOT = 517
780258 meter/sec
ZDOT = -19252
465319 ZDOT = -5844
260907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17461069
61 X = 5322134
02
Y = -13169985
25 feet Y = -4014211
51 meter
Z = -4188867
98 Z = -1276766
96
XDOT = 5694
429875 XDOT = 1735
662226
YDOT = 13597
273091 feet/sec YDOT = 4144
448838 meter/sec
ZDOT = -19148
930269 ZDOT = -5836
593946
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 16021
52971515
00016717 00000-0 10270-3 0 9068
2 25544 51
6422 74
3984 0006707 41
5801 318
5861 15
54631308 22019
Satellite: ISS
Catalog Number: 25544
Epoch time: 16021
52971515 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 74
3984 deg
Eccentricity:
0006707
Arg of perigee: 41
5801 deg
Mean anomaly: 318
5861 deg
Mean motion: 15
54631308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2201
Checksum: 291
Coasting Arc #8 (Orbit 2216)
---------------------------------------
Vector Time (GMT): 2016/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -137190
99 A = 6784127
88 meter
Y = 6084049
08 meter E =
0019099
Z = 2974559
92 I = 51
99355
XDOT = -5204
731151 Wp = 70
05197
YDOT = -2580
682381 meter/sec RA = 68
83594 deg
ZDOT = 5018
696802 TA = 323
81875
MA = 323
94780
Ha = 222
457 n
mi
Hp = 211
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -450101
66 X = -219662
99
Y = 19960790
94 feet Y = 6082053
65 meter
Z = 9759054
87 Z = 2973693
47
XDOT = -17075
889602 XDOT = -5199
864726
YDOT = -8466
805713 feet/sec YDOT = -2638
858153 meter/sec
ZDOT = 16465
540688 ZDOT = 4993
425675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17470623
01 X = -5325045
89
Y = 9670051
80 feet Y = 2947431
79 meter
Z = 9754093
93 Z = 2973047
83
XDOT = -699
692711 XDOT = -213
266338
YDOT = -17827
864728 feet/sec YDOT = -5433
933169 meter/sec
ZDOT = 16356
431595 ZDOT = 4985
440350
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 16022
55821568
00016717 00000-0 10270-3 0 9075
2 25544 51
6414 69
2671 0006849 45
8582 314
3133 15
54627419 22177
Satellite: ISS
Catalog Number: 25544
Epoch time: 16022
55821568 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 69
2671 deg
Eccentricity:
0006849
Arg of perigee: 45
8582 deg
Mean anomaly: 314
3133 deg
Mean motion: 15
54627419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2217
Checksum: 316
Coasting Arc #9 (Orbit 2231)
---------------------------------------
Vector Time (GMT): 2016/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1317266
38 A = 6779795
80 meter
Y = -5043209
68 meter E =
0015229
Z = -4351530
53 I = 51
96786
XDOT = 5205
679041 Wp = 60
44005
YDOT = 4383
859111 meter/sec RA = 63
86991 deg
ZDOT = -3506
749171 TA = 174
01197
MA = 173
99375
Ha = 222
399 n
mi
Hp = 211
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4321740
09 X = 1394700
30
Y = -16545963
52 feet Y = -5028046
03 meter
Z = -14276674
98 Z = -4344943
82
XDOT = 17078
999478 XDOT = 5173
304669
YDOT = 14382
739864 feet/sec YDOT = 4441
891563 meter/sec
ZDOT = -11505
082581 ZDOT = -3481
540301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16421479
08 X = 5005266
82
Y = -4860548
85 feet Y = -1481495
29 meter
Z = -14247100
92 Z = -4342516
36
XDOT = -3684
979746 XDOT = -1123
181826
YDOT = 20937
280577 feet/sec YDOT = 6381
683120 meter/sec
ZDOT = -11396
601030 ZDOT = -3473
683994
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 16023
52241963
00016717 00000-0 10270-3 0 9089
2 25544 51
6422 64
4561 0006808 49
4080 310
7665 15
54664434 22324
Satellite: ISS
Catalog Number: 25544
Epoch time: 16023
52241963 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 64
4561 deg
Eccentricity:
0006808
Arg of perigee: 49
4080 deg
Mean anomaly: 310
7665 deg
Mean motion: 15
54664434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2232
Checksum: 297
Coasting Arc #10 (Orbit 2247)
---------------------------------------
Vector Time (GMT): 2016/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2541435
26 A = 6776468
77 meter
Y = 3588740
92 meter E =
0009551
Z = 5147370
58 I = 51
94090
XDOT = -4882
844441 Wp = 81
23489
YDOT = -5711
813321 meter/sec RA = 58
89112 deg
ZDOT = 1570
383081 TA = 353
70073
MA = 353
71273
Ha = 222
547 n
mi
Hp = 211
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8338042
19 X = -2606379
70
Y = 11774084
37 feet Y = 3559957
69 meter
Z = 16887698
76 Z = 5134867
53
XDOT = -16019
830842 XDOT = -4826
238705
YDOT = -18739
545017 feet/sec YDOT = -5766
100044 meter/sec
ZDOT = 5152
175463 ZDOT = 1546
801382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14468340
13 X = -4409950
07
Y = -819864
00 feet Y = -249894
55 meter
Z = 16832745
96 Z = 5130620
97
XDOT = 7157
776510 XDOT = 2181
690280
YDOT = -22540
384668 feet/sec YDOT = -6870
309247 meter/sec
ZDOT = 5051
019251 ZDOT = 1539
550668
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 16024
55088821
00016717 00000-0 10270-3 0 9096
2 25544 51
6410 59
3243 0006930 53
1512 307
0276 15
54697263 22489
Satellite: ISS
Catalog Number: 25544
Epoch time: 16024
55088821 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 59
3243 deg
Eccentricity:
0006930
Arg of perigee: 53
1512 deg
Mean anomaly: 307
0276 deg
Mean motion: 15
54697263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2248
Checksum: 299
Coasting Arc #11 (Orbit 2262)
---------------------------------------
Vector Time (GMT): 2016/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3750260
63 A = 6775832
81 meter
Y = -1931092
43 meter E =
0020513
Z = -5319949
18 I = 51
92238
XDOT = 4122
259245 Wp = 82
25707
YDOT = 6423
732679 meter/sec RA = 53
90471 deg
ZDOT = 578
796537 TA = 193
22820
MA = 193
28207
Ha = 222
459 n
mi
Hp = 211
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12304004
70 X = 3797417
28
Y = -6335605
07 feet Y = -1888890
89 meter
Z = -17453901
50 Z = -5301617
23
XDOT = 13524
472587 XDOT = 4047
309631
YDOT = 21075
238447 feet/sec YDOT = 6469
411446 meter/sec
ZDOT = 1898
938769 ZDOT = 598
638903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12124391
28 X = 3695514
46
Y = 6878269
70 feet Y = 2096496
60 meter
Z = -17373993
29 Z = -5295593
16
XDOT = -9657
968339 XDOT = -2943
748750
YDOT = 21996
687942 feet/sec YDOT = 6704
590485 meter/sec
ZDOT = 1983
727508 ZDOT = 604
640144
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 16025
51506375
00016717 00000-0 10270-3 0 9104
2 25544 51
6421 54
5132 0006883 55
8990 304
2815 15
54694595 22631
Satellite: ISS
Catalog Number: 25544
Epoch time: 16025
51506375 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 54
5132 deg
Eccentricity:
0006883
Arg of perigee: 55
8990 deg
Mean anomaly: 304
2815 deg
Mean motion: 15
54694595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2263
Checksum: 309
Coasting Arc #12 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2016/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4797752
98 A = 6777925
02 meter
Y = 193349
35 meter E =
0014682
Z = 4775808
32 I = 51
90900
XDOT = -2940
960964 Wp = 60
65132
YDOT = -6564
955636 meter/sec RA = 48
91879 deg
ZDOT = -2675
500496 TA = 55
70890
MA = 55
56999
Ha = 222
577 n
mi
Hp = 211
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15740659
37 X = -4822756
79
Y = 634348
27 feet Y = 139558
02 meter
Z = 15668662
48 Z = 4752441
82
XDOT = -9648
822059 XDOT = -2854
335292
YDOT = -21538
568359 feet/sec YDOT = -6597
359123 meter/sec
ZDOT = -8777
888768 ZDOT = -2689
576071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9469396
68 X = -2886272
11
Y = -12714894
00 feet Y = -3875499
69 meter
Z = 15567264
89 Z = 4744902
34
XDOT = 11433
487952 XDOT = 3484
927128
YDOT = -19388
602303 feet/sec YDOT = -5909
645982 meter/sec
ZDOT = -8837
628182 ZDOT = -2693
709070
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 16026
54350111
00016717 00000-0 10270-3 0 9114
2 25544 51
6407 49
3807 0007026 59
7946 300
3902 15
54757932 22796
Satellite: ISS
Catalog Number: 25544
Epoch time: 16026
54350111 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 49
3807 deg
Eccentricity:
0007026
Arg of perigee: 59
7946 deg
Mean anomaly: 300
3902 deg
Mean motion: 15
54757932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 304
Coasting Arc #13 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2016/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5552684
15 A = 6781949
88 meter
Y = 1376789
52 meter E =
0011925
Z = -3650110
17 I = 51
90182
XDOT = 1369
635650 Wp = 77
81654
YDOT = 6117
047138 meter/sec RA = 43
94245 deg
ZDOT = 4405
416518 TA = 239
06602
MA = 239
18328
Ha = 222
538 n
mi
Hp = 211
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18217467
69 X = 5554606
18
Y = 4517025
99 feet Y = 1438893
92 meter
Z = -11975427
06 Z = -3623132
54
XDOT = 4493
555283 XDOT = 1279
732336
YDOT = 20069
052290 feet/sec YDOT = 6131
860805 meter/sec
ZDOT = 14453
466267 ZDOT = 4411
851132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6905280
73 X = 2104729
57
Y = 17532232
59 feet Y = 5343824
49 meter
Z = -11858685
61 Z = -3614527
37
XDOT = -12541
765279 XDOT = -3822
730057
YDOT = 14701
328128 feet/sec YDOT = 4480
964813 meter/sec
ZDOT = 14480
145743 ZDOT = 4413
548422
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 16027
50764759
00016717 00000-0 10270-3 0 9129
2 25544 51
6418 44
5699 0007089 63
1254 297
0623 15
54760799 22948
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
50764759 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 44
5699 deg
Eccentricity:
0007089
Arg of perigee: 63
1254 deg
Mean anomaly: 297
0623 deg
Mean motion: 15
54760799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 341
Coasting Arc #14 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2016/027/19:32:28
472
Vector Time (MET): N/A
Weight (LBS) : 922190
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3404160
97 A = 6777201
50 meter
Y = -2527459
23 meter E =
0018545
Z = -5302949
98 I = 51
87469
XDOT = 5231
360020 Wp = 85
52776
YDOT = 5542
152797 meter/sec RA = 42
39851 deg
ZDOT = 720
312720 TA = 191
32111
MA = 191
36289
Ha = 222
440 n
mi
Hp = 213
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11168507
12 X = 3457929
60
Y = -8292189
09 feet Y = -2489091
24 meter
Z = -17398129
87 Z = -5286283
04
XDOT = 17163
254660 XDOT = 5165
498595
YDOT = 18182
916000 feet/sec YDOT = 5600
285108 meter/sec
ZDOT = 2363
230708 ZDOT = 745
564671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1249049
68 X = -380710
34
Y = -13945027
81 feet Y = -4250444
48 meter
Z = -17325326
79 Z = -5280759
61
XDOT = 23420
012985 XDOT = 7138
419958
YDOT = -5153
864726 feet/sec YDOT = -1570
897969 meter/sec
ZDOT = 2471
645596 ZDOT = 753
357578
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 16027
82902877
00016717 00000-0 10270-3 0 9130
2 25544 51
6427 42
9655 0004881 54
8507 305
3103 15
54246842 22996
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
82902877 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 42
9655 deg
Eccentricity:
0004881
Arg of perigee: 54
8507 deg
Mean anomaly: 305
3103 deg
Mean motion: 15
54246842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 320
Coasting Arc #15 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2016/028/19:32:28
472
Vector Time (MET): N/A
Weight (LBS) : 922190
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4642428
20 A = 6779221
91 meter
Y = 1184220
05 meter E =
0012446
Z = 4789554
02 I = 51
85758
XDOT = -4222
644752 Wp = 59
65478
YDOT = -5838
520166 meter/sec RA = 37
41466 deg
ZDOT = -2638
121987 TA = 56
32661
MA = 56
20798
Ha = 222
512 n
mi
Hp = 212
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15231063
65 X = -4678590
62
Y = 3885236
38 feet Y = 1132103
37 meter
Z = 15713759
90 Z = 4766914
74
XDOT = -13853
821364 XDOT = -4144
228491
YDOT = -19155
249890 feet/sec YDOT = -5885
302252 meter/sec
ZDOT = -8655
255864 ZDOT = -2658
443467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4358780
33 X = -1328556
24
Y = 15204118
82 feet Y = 4634215
41 meter
Z = 15615326
35 Z = 4759551
47
XDOT = -22388
938485 XDOT = -6824
148450
YDOT = 2598
193263 feet/sec YDOT = 791
929306 meter/sec
ZDOT = -8742
215947 ZDOT = -2664
627421
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 16028
85778090
00016717 00000-0 10270-3 0 9143
2 25544 51
6427 37
8357 0004873 57
3316 302
8306 15
54294052 23157
Satellite: ISS
Catalog Number: 25544
Epoch time: 16028
85778090 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 37
8357 deg
Eccentricity:
0004873
Arg of perigee: 57
3316 deg
Mean anomaly: 302
8306 deg
Mean motion: 15
54294052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 314
Coasting Arc #16 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2016/029/19:32:28
472
Vector Time (MET): N/A
Weight (LBS) : 922190
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5634018
37 A = 6782916
68 meter
Y = 57935
22 meter E =
0010039
Z = -3784142
93 I = 51
84448
XDOT = 2789
311783 Wp = 83
21022
YDOT = 5730
395227 meter/sec RA = 32
43747 deg
ZDOT = 4251
419370 TA = 231
63273
MA = 231
72297
Ha = 222
461 n
mi
Hp = 212
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18484312
22 X = 5651333
28
Y = 190076
20 feet Y = 121035
19 meter
Z = -12415167
11 Z = -3756732
60
XDOT = 9151
285378 XDOT = 2704
374497
YDOT = 18800
509274 feet/sec YDOT = 5761
112446 meter/sec
ZDOT = 13948
226281 ZDOT = 4264
762397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9231600
55 X = 2813791
85
Y = -16106548
75 feet Y = -4909276
06 meter
Z = -12296297
82 Z = -3747911
58
XDOT = 19657
974416 XDOT = 5991
750602
YDOT = 602
646967 feet/sec YDOT = 183
686796 meter/sec
ZDOT = 14004
932370 ZDOT = 4268
703386
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 16029
82222262
00016717 00000-0 10270-3 0 9157
2 25544 51
6433 33
0265 0004859 61
0013 299
1627 15
54286470 23306
Satellite: ISS
Catalog Number: 25544
Epoch time: 16029
82222262 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 33
0265 deg
Eccentricity:
0004859
Arg of perigee: 61
0013 deg
Mean anomaly: 299
1627 deg
Mean motion: 15
54286470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 287
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