[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 8th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 ET - UTC (sec) : 68 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
314/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 215
7
322/07:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 216
8
322/20:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 217
0
324/22:00:36
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 217
3
326/13:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 2726)
---------------------------------------
Vector Time (GMT): 2016/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4106321
12 A = 6789962
12 meter
Y = 5161779
43 meter E =
0004379
Z = -1617612
29 I = 51
99124
XDOT = -2924
240691 Wp = 100
37072
YDOT = 4125
608624 meter/sec RA = 62
54698 deg
ZDOT = 5753
996816 TA = 242
03349
MA = 242
07782
Ha = 223
166 n
mi
Hp = 215
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13472182
17 X = 4056153
37
Y = 16934971
87 feet Y = 5207418
54 meter
Z = -5307126
92 Z = -1597786
45
XDOT = -9593
965523 XDOT = -2998
107798
YDOT = 13535
461364 feet/sec YDOT = 4092
494863 meter/sec
ZDOT = 18877
942309 ZDOT = 5739
611914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21573107
30 X = -6575483
11
Y = -1948872
22 feet Y = -594016
25 meter
Z = -5221254
58 Z = -1591438
40
XDOT = -3205
946449 XDOT = -977
172478
YDOT = -14805
815660 feet/sec YDOT = -4512
812613 meter/sec
ZDOT = 18814
156203 ZDOT = 5734
554811
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 16312
50311535
00016717 00000-0 10270-3 0 9003
2 25544 51
6431 63
2713 0007159 184
8145 175
2940 15
53539505 27274
Satellite: ISS
Catalog Number: 25544
Epoch time: 16312
50311535 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 63
2713 deg
Eccentricity:
0007159
Arg of perigee: 184
8145 deg
Mean anomaly: 175
2940 deg
Mean motion: 15
53539505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2727
Checksum: 291
Coasting Arc #2 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2016/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3692522
91 A = 6791012
64 meter
Y = -5685892
45 meter E =
0017499
Z = 91277
00 I = 51
97833
XDOT = 3916
830055 Wp = 153
36325
YDOT = -2647
608509 meter/sec RA = 57
60272 deg
ZDOT = -6043
959833 TA = 25
65759
MA = 25
57087
Ha = 223
097 n
mi
Hp = 215
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12114576
49 X = -3629110
76
Y = -18654502
80 feet Y = -5726830
16 meter
Z = 299465
24 Z = 73493
58
XDOT = 12850
492305 XDOT = 3975
504544
YDOT = -8686
379622 feet/sec YDOT = -2603
479977 meter/sec
ZDOT = -19829
264544 ZDOT = -6024
790004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21922879
32 X = 6682093
62
Y = 3765754
72 feet Y = 1147802
04 meter
Z = 222646
11 Z = 67862
54
XDOT = -2155
667656 XDOT = -657
047502
YDOT = 13829
416150 feet/sec YDOT = 4215
206043 meter/sec
ZDOT = -19744
794084 ZDOT = -6018
213237
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 16313
53232747
00016717 00000-0 10270-3 0 9015
2 25544 51
6422 58
1455 0007280 188
4208 171
6823 15
53550946 27435
Satellite: ISS
Catalog Number: 25544
Epoch time: 16313
53232747 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 58
1455 deg
Eccentricity:
0007280
Arg of perigee: 188
4208 deg
Mean anomaly: 171
6823 deg
Mean motion: 15
53550946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 304
Coasting Arc #3 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2016/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3092117
19 A = 6790085
39 meter
Y = 5875638
11 meter E =
0010617
Z = 1413167
06 I = 51
95829
XDOT = -4853
489812 Wp = 91
24951
YDOT = 1145
445010 meter/sec RA = 52
65735 deg
ZDOT = 5819
396494 TA = 284
07761
MA = 284
19559
Ha = 222
899 n
mi
Hp = 215
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10144741
43 X = 3019319
82
Y = 19277027
93 feet Y = 5909809
27 meter
Z = 4636374
88 Z = 1428010
97
XDOT = -15923
523004 XDOT = -4894
206301
YDOT = 3758
021686 feet/sec YDOT = 1090
942598 meter/sec
ZDOT = 19092
508181 ZDOT = 5795
720154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21115728
82 X = -6436074
15
Y = -5296129
41 feet Y = -1614260
24 meter
Z = 4700272
97 Z = 1432643
20
XDOT = 7498
009078 XDOT = 2285
393167
YDOT = -12933
575689 feet/sec YDOT = -3942
153870 meter/sec
ZDOT = 18988
583695 ZDOT = 5787
720310
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 16314
56153468
00016717 00000-0 10270-3 0 9022
2 25544 51
6431 53
0198 0007165 192
2869 167
8109 15
53569474 27598
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
56153468 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 53
0198 deg
Eccentricity:
0007165
Arg of perigee: 192
2869 deg
Mean anomaly: 167
8109 deg
Mean motion: 15
53569474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 334
Coasting Arc #4 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5356239
91 A = 6787747
46 meter
Y = -3078449
08 meter E =
0014632
Z = 2789553
72 I = 51
94017
XDOT = 566
742867 Wp = 127
41358
YDOT = -5661
047717 meter/sec RA = 50
59179 deg
ZDOT = -5149
320277 TA = 21
07510
MA = 21
01487
Ha = 222
797 n
mi
Hp = 215
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17572965
57 X = -5334968
48
Y = -10099898
57 feet Y = -3138227
10 meter
Z = 9152079
12 Z = 2763585
82
XDOT = 1859
392609 XDOT = 655
017617
YDOT = -18572
991196 feet/sec YDOT = -5654
216669 meter/sec
ZDOT = -16894
095398 ZDOT = -5146
352478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19744225
64 X = -6018039
97
Y = -4800102
91 feet Y = -1463071
37 meter
Z = 9038926
29 Z = 2755064
73
XDOT = -3621
794963 XDOT = -1103
923105
YDOT = -16950
021563 feet/sec YDOT = -5166
366572 meter/sec
ZDOT = -16880
013471 ZDOT = -5145
028106
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 16314
94748711
00016717 00000-0 10270-3 0 9036
2 25544 51
6410 51
1000 0006640 194
4291 165
6672 15
53565859 27657
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
94748711 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 51
1000 deg
Eccentricity:
0006640
Arg of perigee: 194
4291 deg
Mean anomaly: 165
6672 deg
Mean motion: 15
53565859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 307
Coasting Arc #5 (Orbit 2779)
---------------------------------------
Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5362131
99 A = 6790163
29 meter
Y = 3927862
33 meter E =
0003353
Z = -1388320
40 I = 51
92746
XDOT = -1872
799463 Wp = 78
07707
YDOT = 4611
102913 meter/sec RA = 45
64013 deg
ZDOT = 5825
021439 TA = 266
86969
MA = 266
90805
Ha = 222
533 n
mi
Hp = 215
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17592296
55 X = 5324555
09
Y = 12886687
44 feet Y = 3987615
12 meter
Z = -4554856
95 Z = -1362363
46
XDOT = -6144
355193 XDOT = -1952
518805
YDOT = 15128
290396 feet/sec YDOT = 4589
714561 meter/sec
ZDOT = 19110
962727 ZDOT = 5815
729811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20634553
16 X = 6289411
80
Y = 7126489
15 feet Y = 2172153
89 meter
Z = -4441925
37 Z = -1353898
85
XDOT = -1015
580278 XDOT = -309
548869
YDOT = 14800
180928 feet/sec YDOT = 4511
095147 meter/sec
ZDOT = 19069
377996 ZDOT = 5812
346413
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 16315
91236125
00016717 00000-0 10270-3 0 9046
2 25544 51
6413 46
2943 0006560 198
2031 161
8887 15
53572335 27806
Satellite: ISS
Catalog Number: 25544
Epoch time: 16315
91236125 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 46
2943 deg
Eccentricity:
0006560
Arg of perigee: 198
2031 deg
Mean anomaly: 161
8887 deg
Mean motion: 15
53572335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2780
Checksum: 306
Coasting Arc #6 (Orbit 2795)
---------------------------------------
Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5061221
88 A = 6790930
97 meter
Y = -4510607
85 meter E =
0015575
Z = -153375
08 I = 51
90738
XDOT = 3248
400719 Wp = 158
13166
YDOT = -3446
856910 meter/sec RA = 40
69157 deg
ZDOT = -6035
812938 TA = 23
51516
MA = 23
44402
Ha = 222
401 n
mi
Hp = 216
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16605058
65 X = -5009661
89
Y = -14798582
20 feet Y = -4566917
55 meter
Z = -503199
07 Z = -177836
37
XDOT = 10657
482673 XDOT = 3316
022998
YDOT = -11308
585662 feet/sec YDOT = -3410
153282 meter/sec
ZDOT = -19802
535887 ZDOT = -6019
868245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20379053
24 X = -6211535
43
Y = -8905165
44 feet Y = -2714294
43 meter
Z = -609454
48 Z = -185761
73
XDOT = 6086
209391 XDOT = 1855
076622
YDOT = -12616
602884 feet/sec YDOT = -3845
540559 meter/sec
ZDOT = -19732
033959 ZDOT = -6014
323951
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 16316
94155572
00016717 00000-0 10270-3 0 9057
2 25544 51
6419 41
1683 0006517 202
0338 158
0535 15
53574155 27960
Satellite: ISS
Catalog Number: 25544
Epoch time: 16316
94155572 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 41
1683 deg
Eccentricity:
0006517
Arg of perigee: 202
0338 deg
Mean anomaly: 158
0535 deg
Mean motion: 15
53574155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2796
Checksum: 311
Coasting Arc #7 (Orbit 2811)
---------------------------------------
Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4476792
90 A = 6789677
40 meter
Y = 4824812
46 meter E =
0009644
Z = 1658104
80 I = 51
87845
XDOT = -4563
546003 Wp = 88
47782
YDOT = 2255
420255 meter/sec RA = 35
74112 deg
ZDOT = 5729
930655 TA = 289
61290
MA = 289
71697
Ha = 222
225 n
mi
Hp = 216
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14687640
74 X = 4414453
30
Y = 15829437
21 feet Y = 4874526
45 meter
Z = 5439976
38 Z = 1679700
98
XDOT = -14972
263788 XDOT = -4616
261807
YDOT = 7399
672754 feet/sec YDOT = 2204
093030 meter/sec
ZDOT = 18798
985090 ZDOT = 5707
633381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19024495
64 X = 5798666
27
Y = 10165577
10 feet Y = 3098467
90 meter
Z = 5533608
55 Z = 1686643
89
XDOT = -11100
650404 XDOT = -3383
478243
YDOT = 10544
635868 feet/sec YDOT = 3214
005013 meter/sec
ZDOT = 18700
893613 ZDOT = 5700
032373
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 16317
97074445
00016717 00000-0 10270-3 0 9061
2 25544 51
6419 36
0428 0006557 206
4586 153
6233 15
53594592 28129
Satellite: ISS
Catalog Number: 25544
Epoch time: 16317
97074445 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 36
0428 deg
Eccentricity:
0006557
Arg of perigee: 206
4586 deg
Mean anomaly: 153
6233 deg
Mean motion: 15
53594592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2812
Checksum: 324
Coasting Arc #8 (Orbit 2826)
---------------------------------------
Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3552097
91 A = 6786817
78 meter
Y = -4907378
69 meter E =
0006919
Z = -3052139
64 I = 51
84371
XDOT = 5755
508341 Wp = 170
53617
YDOT = -1094
816096 meter/sec RA = 30
78338 deg
ZDOT = -4946
236089 TA = 44
36774
MA = 44
31232
Ha = 221
986 n
mi
Hp = 216
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11653864
55 X = -3482131
94
Y = -16100323
78 feet Y = -4946709
44 meter
Z = -10013581
48 Z = -3069225
38
XDOT = 18882
901382 XDOT = 5791
350469
YDOT = -3591
916326 feet/sec YDOT = -1030
253747 meter/sec
ZDOT = -16227
808690 ZDOT = -4918
189399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16412568
03 X = -5002550
74
Y = -11143434
72 feet Y = -3396518
90 meter
Z = -10087431
40 Z = -3074649
09
XDOT = 15786
994212 XDOT = 4811
875836
YDOT = -8697
505903 feet/sec YDOT = -2650
999799 meter/sec
ZDOT = -16104
769027 ZDOT = -4908
733599
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 16318
93560295
00016717 00000-0 10270-3 0 9072
2 25544 51
6432 31
2371 0006411 210
3957 149
6825 15
53613172 28277
Satellite: ISS
Catalog Number: 25544
Epoch time: 16318
93560295 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 31
2371 deg
Eccentricity:
0006411
Arg of perigee: 210
3957 deg
Mean anomaly: 149
6825 deg
Mean motion: 15
53613172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2827
Checksum: 303
Coasting Arc #9 (Orbit 2842)
---------------------------------------
Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2380479
23 A = 6783422
68 meter
Y = 4793941
71 meter E =
0010209
Z = 4167154
87 I = 51
80362
XDOT = -6684
250866 Wp = 140
81175
YDOT = 46
206658 meter/sec RA = 25
81647 deg
ZDOT = 3752
470134 TA = 270
60320
MA = 270
72019
Ha = 221
876 n
mi
Hp = 216
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7809971
22 X = 2306452
42
Y = 15728155
21 feet Y = 4820147
82 meter
Z = 13671767
94 Z = 4178539
27
XDOT = -21929
956909 XDOT = -6702
499157
YDOT = 151
596648 feet/sec YDOT = -28
643246 meter/sec
ZDOT = 12311
253721 ZDOT = 3719
954491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12859134
41 X = 3919464
17
Y = 11902682
26 feet Y = 3627937
55 meter
Z = 13720662
26 Z = 4182057
86
XDOT = -19615
398736 XDOT = -5978
773535
YDOT = 7116
118811 feet/sec YDOT = 2168
993014 meter/sec
ZDOT = 12168
855387 ZDOT = 3709
067122
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 16319
96477969
00016717 00000-0 10270-3 0 9082
2 25544 51
6427 26
1115 0006391 213
6983 146
3764 15
53612389 28435
Satellite: ISS
Catalog Number: 25544
Epoch time: 16319
96477969 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 26
1115 deg
Eccentricity:
0006391
Arg of perigee: 213
6983 deg
Mean anomaly: 146
3764 deg
Mean motion: 15
53612389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2843
Checksum: 341
Coasting Arc #10 (Orbit 2857)
---------------------------------------
Vector Time (GMT): 2016/320/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -958329
52 A = 6780354
11 meter
Y = -4539090
15 meter E =
0008222
Z = -4951286
19 I = 51
76449
XDOT = 7276
288201 Wp = 100
77844
YDOT = 890
294246 meter/sec RA = 20
83880 deg
ZDOT = -2229
155226 TA = 147
50680
MA = 147
45616
Ha = 221
702 n
mi
Hp = 216
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3144125
73 X = -883449
24
Y = -14892028
04 feet Y = -4549387
92 meter
Z = -16244377
27 Z = -4955759
96
XDOT = 23872
336618 XDOT = 7276
620443
YDOT = 2920
912879 feet/sec YDOT = 971
664544 meter/sec
ZDOT = -7313
501396 ZDOT = -2193
807145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8408267
80 X = -2562840
03
Y = -12663015
93 feet Y = -3859687
26 meter
Z = -16263052
56 Z = -4956978
42
XDOT = 22342
362043 XDOT = 6809
951951
YDOT = -5660
774541 feet/sec YDOT = -1725
404080 meter/sec
ZDOT = -7158
890755 ZDOT = -2182
029902
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 16320
92962841
00016717 00000-0 10270-3 0 9099
2 25544 51
6431 21
3060 0006330 217
6786 142
3924 15
53637196 28587
Satellite: ISS
Catalog Number: 25544
Epoch time: 16320
92962841 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 21
3060 deg
Eccentricity:
0006330
Arg of perigee: 217
6786 deg
Mean anomaly: 142
3924 deg
Mean motion: 15
53637196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2858
Checksum: 310
Coasting Arc #11 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2016/321/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -563336
87 A = 6778785
34 meter
Y = 4188455
12 meter E =
0006041
Z = 5302123
54 I = 51
72885
XDOT = -7460
542781 Wp = 197
25670
YDOT = -1682
925216 meter/sec RA = 15
85359 deg
ZDOT = 531
298324 TA = 247
64704
MA = 247
71107
Ha = 221
500 n
mi
Hp = 216
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1848218
07 X = -635887
29
Y = 13741650
66 feet Y = 4181749
56 meter
Z = 17395418
43 Z = 5299210
95
XDOT = -24476
846395 XDOT = -7443
750260
YDOT = -5521
408188 feet/sec YDOT = -1766
260150 meter/sec
ZDOT = 1743
104739 ZDOT = 495
096893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3573735
12 X = 1089274
47
Y = 13414558
93 feet Y = 4088757
56 meter
Z = 17381814
67 Z = 5297977
11
XDOT = -23717
135807 XDOT = -7228
982994
YDOT = 4241
458406 feet/sec YDOT = 1292
796522 meter/sec
ZDOT = 1584
920319 ZDOT = 483
083713
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 16321
95879351
00016717 00000-0 10270-3 0 9108
2 25544 51
6430 16
1800 0006501 222
7688 137
2959 15
53662043 28746
Satellite: ISS
Catalog Number: 25544
Epoch time: 16321
95879351 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 16
1800 deg
Eccentricity:
0006501
Arg of perigee: 222
7688 deg
Mean anomaly: 137
2959 deg
Mean motion: 15
53662043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 308
Coasting Arc #12 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/322/07:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4582573
66 A = 6782849
84 meter
Y = 2420367
55 meter E =
0005287
Z = 4370487
56 I = 51
72909
XDOT = -5465
432920 Wp = 113
73718
YDOT = -4141
194521 meter/sec RA = 13
86516 deg
ZDOT = -3436
061534 TA = 11
06262
MA = 11
05100
Ha = 221
865 n
mi
Hp = 216
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15034690
50 X = -4630528
54
Y = 7940838
42 feet Y = 2368853
76 meter
Z = 14338869
94 Z = 4348109
85
XDOT = -17931
210368 XDOT = -5402
027638
YDOT = -13586
596199 feet/sec YDOT = -4201
957946 meter/sec
ZDOT = -11273
167763 ZDOT = -3462
457907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16672329
93 X = 5081726
16
Y = -3734544
70 feet Y = -1138289
23 meter
Z = 14240386
76 Z = 4340469
88
XDOT = 13437
051664 XDOT = 4095
613347
YDOT = 16548
708057 feet/sec YDOT = 5044
046216 meter/sec
ZDOT = -11387
915558 ZDOT = -3471
036662
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 16322
34473081
00016717 00000-0 10270-3 0 9113
2 25544 51
6426 14
2526 0006766 219
9083 140
1572 15
53607655 28804
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
34473081 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 14
2526 deg
Eccentricity:
0006766
Arg of perigee: 219
9083 deg
Mean anomaly: 140
1572 deg
Mean motion: 15
53607655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 301
Coasting Arc #13 (Orbit 2887)
---------------------------------------
Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3333709
02 A = 6780643
92 meter
Y = -3293490
04 meter E =
0010501
Z = -4909542
23 I = 51
70462
XDOT = 6571
550632 Wp = 138
34333
YDOT = 3172
000526 meter/sec RA = 11
16501 deg
ZDOT = 2329
574565 TA = 154
48216
MA = 154
43028
Ha = 221
396 n
mi
Hp = 217
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10937365
57 X = 3394138
67
Y = -10805413
53 feet Y = -3255872
12 meter
Z = -16107422
03 Z = -4893201
09
XDOT = 21560
205487 XDOT = 6524
275872
YDOT = 10406
825874 feet/sec YDOT = 3245
223562 meter/sec
ZDOT = 7642
961170 ZDOT = 2361
383301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10751734
22 X = 3277128
59
Y = -11095256
14 feet Y = -3381834
07 meter
Z = -16035194
84 Z = -4887527
39
XDOT = 20968
980125 XDOT = 6391
345142
YDOT = 9050
711320 feet/sec YDOT = 2758
656810 meter/sec
ZDOT = 7781
604845 ZDOT = 2371
833157
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 16322
85930994
00016717 00000-0 10270-3 0 9121
2 25544 51
6423 11
6931 0006281 225
7659 134
2978 15
53640249 28886
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
85930994 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 11
6931 deg
Eccentricity:
0006281
Arg of perigee: 225
7659 deg
Mean anomaly: 134
2978 deg
Mean motion: 15
53640249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2888
Checksum: 331
Coasting Arc #14 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4645183
20 A = 6783742
69 meter
Y = 2754933
84 meter E =
0005890
Z = 4098987
44 I = 51
68281
XDOT = -5550
173600 Wp = 107
09696
YDOT = -3649
028875 meter/sec RA = 6
18257 deg
ZDOT = -3834
367624 TA = 22
49976
MA = 22
47394
Ha = 221
333 n
mi
Hp = 217
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15240102
37 X = -4695555
65
Y = 9038496
85 feet Y = 2702706
46 meter
Z = 13448121
53 Z = 4076299
85
XDOT = -18209
230972 XDOT = -5490
330832
YDOT = -11971
879510 feet/sec YDOT = -3710
759877 meter/sec
ZDOT = -12579
946272 ZDOT = -3861
184052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14917758
34 X = -4546932
74
Y = 9700143
20 feet Y = 2956603
65 meter
Z = 13348214
35 Z = 4068535
73
XDOT = -17925
310093 XDOT = -5463
634516
YDOT = -10082
533054 feet/sec YDOT = -3073
156075 meter/sec
ZDOT = -12696
629130 ZDOT = -3869
932559
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 16323
88846722
00016717 00000-0 10270-3 0 9131
2 25544 51
6420 6
5678 0006289 229
6156 130
4448 15
53634868 29046
Satellite: ISS
Catalog Number: 25544
Epoch time: 16323
88846722 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 6
5678 deg
Eccentricity:
0006289
Arg of perigee: 229
6156 deg
Mean anomaly: 130
4448 deg
Mean motion: 15
53634868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 331
Coasting Arc #15 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2016/324/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5702687
14 A = 6787126
30 meter
Y = -2209426
01 meter E =
0002057
Z = -2944848
09 I = 51
66274
XDOT = 4155
294184 Wp = 207
19540
YDOT = 4047
616537 meter/sec RA = 1
20448 deg
ZDOT = 5006
741931 TA = 119
22405
MA = 119
20347
Ha = 221
034 n
mi
Hp = 217
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18709603
46 X = 5741274
58
Y = -7248773
00 feet Y = -2145438
90 meter
Z = -9661575
10 Z = -2917051
98
XDOT = 13632
854936 XDOT = 4085
403081
YDOT = 13279
581815 feet/sec YDOT = 4093
692907 meter/sec
ZDOT = 16426
318672 ZDOT = 5026
757822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18296090
79 X = 5576648
47
Y = -8378105
78 feet Y = -2553646
64 meter
Z = -9539413
53 Z = -2907613
24
XDOT = 13697
971059 XDOT = 4175
141579
YDOT = 11099
541050 feet/sec YDOT = 3383
140112 meter/sec
ZDOT = 16513
139733 ZDOT = 5033
204991
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 16324
85329819
00016717 00000-0 10270-3 0 9143
2 25544 51
6426 1
7612 0006353 233
6169 126
4398 15
53654133 29190
Satellite: ISS
Catalog Number: 25544
Epoch time: 16324
85329819 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 1
7612 deg
Eccentricity:
0006353
Arg of perigee: 233
6169 deg
Mean anomaly: 126
4398 deg
Mean motion: 15
53654133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 317
Coasting Arc #16 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2016/324/22:00:36
000
Vector Time (MET): N/A
Weight (LBS) : 909067
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6778332
73 A = 6790657
18 meter
Y = -149670
45 meter E =
0005392
Z = -320782
05 I = 51
67371
XDOT = 386
743513 Wp = 29
07441
YDOT = 4751
286363 meter/sec RA =
87849 deg
ZDOT = 6002
291595 TA = 327
47182
MA = 327
50503
Ha = 220
994 n
mi
Hp = 217
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22238624
45 X = 6781060
84
Y = -491044
79 feet Y = -73855
32 meter
Z = -1052434
56 Z = -287847
73
XDOT = 1268
843547 XDOT = 304
427894
YDOT = 15588
209853 feet/sec YDOT = 4755
150779 meter/sec
ZDOT = 19692
557727 ZDOT = 6003
970500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19285556
10 X = 5878237
50
Y = -11097192
06 feet Y = -3382424
14 meter
Z = -908193
42 Z = -276817
36
XDOT = 7667
419587 XDOT = 2337
029490
YDOT = 11727
498468 feet/sec YDOT = 3574
541533 meter/sec
ZDOT = 19698
942697 ZDOT = 6004
237734
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 16324
91761937
00016717 00000-0 10270-3 0 9152
2 25544 51
6438 1
4415 0006425 234
6748 125
3804 15
53659099 29203
Satellite: ISS
Catalog Number: 25544
Epoch time: 16324
91761937 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 1
4415 deg
Eccentricity:
0006425
Arg of perigee: 234
6748 deg
Mean anomaly: 125
3804 deg
Mean motion: 15
53659099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 319
Coasting Arc #17 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2016/325/22:00:36
000
Vector Time (MET): N/A
Weight (LBS) : 909067
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6649415
53 A = 6790105
32 meter
Y = -508749
29 meter E =
0010529
Z = -1240069
75 I = 51
63986
XDOT = 1451
743468 Wp = 179
59238
YDOT = -4744
460538 meter/sec RA = 355
91216 deg
ZDOT = -5848
574523 TA = 13
88999
MA = 13
86105
Ha = 220
865 n
mi
Hp = 217
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21815667
74 X = -6637208
59
Y = -1669124
96 feet Y = -583039
25 meter
Z = -4068470
31 Z = -1272341
55
XDOT = 4762
937887 XDOT = 1533
099416
YDOT = -15565
815413 feet/sec YDOT = -4727
771214 meter/sec
ZDOT = -19188
236624 ZDOT = -5841
324710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19763807
44 X = -6024008
51
Y = 9323753
46 feet Y = 2841880
06 meter
Z = -4209670
33 Z = -1283107
52
XDOT = -2770
605613 XDOT = -844
480591
YDOT = -14506
474337 feet/sec YDOT = -4421
573378 meter/sec
ZDOT = -19155
529925 ZDOT = -5838
605521
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 16325
94676783
00016717 00000-0 10270-3 0 9161
2 25544 51
6444 356
3155 0006487 237
7901 122
2623 15
53621833 29363
Satellite: ISS
Catalog Number: 25544
Epoch time: 16325
94676783 = yrday
fracday
Element set: 916
Inclination: 51
6444 deg
RA of node: 356
3155 deg
Eccentricity:
0006487
Arg of perigee: 237
7901 deg
Mean anomaly: 122
2623 deg
Mean motion: 15
53621833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 328
Coasting Arc #18 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2016/326/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6432426
42 A = 6790115
64 meter
Y = 1782825
25 meter E =
0012286
Z = 1201543
38 I = 51
61682
XDOT = -2311
477724 Wp = 148
43298
YDOT = -4381
227386 meter/sec RA = 352
70622 deg
ZDOT = -5856
787310 TA = 18
50494
MA = 18
46029
Ha = 220
811 n
mi
Hp = 217
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21103761
21 X = -6457720
98
Y = 5849164
21 feet Y = 1710752
10 meter
Z = 3942071
45 Z = 1170234
57
XDOT = -7583
588333 XDOT = -2233
863937
YDOT = -14374
105598 feet/sec YDOT = -4406
641896 meter/sec
ZDOT = -19215
181464 ZDOT = -5867
827484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2136166
09 X = -651103
42
Y = -21819325
96 feet Y = -6650530
55 meter
Z = 3804628
18 Z = 1159650
67
XDOT = 13851
666047 XDOT = 4221
987811
YDOT = -4724
927131 feet/sec YDOT = -1440
157790 meter/sec
ZDOT = -19262
631586 ZDOT = -5871
250107
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 16326
58998220
00016717 00000-0 10270-3 0 9176
2 25544 51
6416 353
1100 0006121 238
5494 121
5060 15
53662990 29465
Satellite: ISS
Catalog Number: 25544
Epoch time: 16326
58998220 = yrday
fracday
Element set: 917
Inclination: 51
6416 deg
RA of node: 353
1100 deg
Eccentricity:
0006121
Arg of perigee: 238
5494 deg
Mean anomaly: 121
5060 deg
Mean motion: 15
53662990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 305
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