[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 22nd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
083/03:23:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
8
084/04:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 214
7
086/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 214
6
090/14:15:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
2
091/16:23:58
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
1
093/17:58:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 213
9
094/19:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2016/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2770725
42 A = 6777202
28 meter
Y = 3152234
64 meter E =
0013895
Z = -5333250
35 I = 51
88132
XDOT = -5504
003732 Wp = 85
06219
YDOT = 5317
673208 meter/sec RA = 134
30975 deg
ZDOT = 285
395942 TA = 187
64215
MA = 187
66334
Ha = 220
672 n
mi
Hp = 215
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9090306
48 X = 2761176
84
Y = 10341977
17 feet Y = 3183164
51 meter
Z = -17497540
51 Z = -5319814
65
XDOT = -18057
755027 XDOT = -5564
444527
YDOT = 17446
434408 feet/sec YDOT = 5255
785878 meter/sec
ZDOT = 936
338392 ZDOT = 258
511468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8944831
46 X = 2726384
63
Y = 10564188
28 feet Y = 3219964
59 meter
Z = -17439667
53 Z = -5315610
66
XDOT = -17717
737033 XDOT = -5400
366248
YDOT = 16343
544046 feet/sec YDOT = 4981
512225 meter/sec
ZDOT = 818
686769 ZDOT = 249
535727
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 16081
51566577
00016717 00000-0 10270-3 0 9005
2 25544 51
6418 135
2882 0002039 330
6509 29
4528 15
54188402 31345
Satellite: ISS
Catalog Number: 25544
Epoch time: 16081
51566577 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 135
2882 deg
Eccentricity:
0002039
Arg of perigee: 330
6509 deg
Mean anomaly: 29
4528 deg
Mean motion: 15
54188402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 304
Coasting Arc #2 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2016/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1420817
58 A = 6778592
69 meter
Y = -4397284
09 meter E =
0006885
Z = 4957202
77 I = 51
90764
XDOT = 5867
569493 Wp = 40
65086
YDOT = -4410
755730 meter/sec RA = 129
32829 deg
ZDOT = -2223
990087 TA = 71
00509
MA = 70
93050
Ha = 220
654 n
mi
Hp = 214
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4661475
00 X = -1395620
30
Y = -14426785
07 feet Y = -4413030
93 meter
Z = 16263788
60 Z = 4950362
74
XDOT = 19250
556081 XDOT = 5927
258705
YDOT = -14470
983367 feet/sec YDOT = -4344
807285 meter/sec
ZDOT = -7296
555403 ZDOT = -2195
341359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4658216
40 X = -1419824
36
Y = -14460479
20 feet Y = -4407554
06 meter
Z = 16234773
10 Z = 4948358
84
XDOT = 18349
970527 XDOT = 5593
071017
YDOT = -13987
631716 feet/sec YDOT = -4263
430147 meter/sec
ZDOT = -7171
370776 ZDOT = -2185
833813
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 16082
54443857
00016717 00000-0 10270-3 0 9015
2 25544 51
6411 130
1598 0002048 333
5184 26
5864 15
54245652 31507
Satellite: ISS
Catalog Number: 25544
Epoch time: 16082
54443857 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 130
1598 deg
Eccentricity:
0002048
Arg of perigee: 333
5184 deg
Mean anomaly: 26
5864 deg
Mean motion: 15
54245652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 296
Coasting Arc #3 (Orbit 3159)
---------------------------------------
Vector Time (GMT): 2016/083/03:23:00
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2599540
67 A = 6777510
79 meter
Y = -3411527
88 meter E =
0004549
Z = 5246250
11 I = 51
91383
XDOT = 5137
890766 Wp = 31
95244
YDOT = -5590
686553 meter/sec RA = 126
15056 deg
ZDOT = -1085
469433 TA = 68
42991
MA = 68
38144
Ha = 220
835 n
mi
Hp = 214
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8528676
75 X = -2586682
88
Y = -11192676
76 feet Y = -3440524
92 meter
Z = 17212106
65 Z = 5233654
01
XDOT = 16856
597000 XDOT = 5205
298084
YDOT = -18342
147483 feet/sec YDOT = -5532
854522 meter/sec
ZDOT = -3561
251419 ZDOT = -1060
346281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14133678
39 X = 4307945
17
Y = 340175
29 feet Y = 103685
43 meter
Z = 17157924
44 Z = 5229735
37
XDOT = 3637
585143 XDOT = 1108
735952
YDOT = 23633
071678 feet/sec YDOT = 7203
360247 meter/sec
ZDOT = -3451
188046 ZDOT = -1051
922116
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 16083
18741907
00016717 00000-0 10270-3 0 9024
2 25544 51
6386 126
9509 0002001 338
5187 21
5881 15
54198601 31606
Satellite: ISS
Catalog Number: 25544
Epoch time: 16083
18741907 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 126
9509 deg
Eccentricity:
0002001
Arg of perigee: 338
5187 deg
Mean anomaly: 21
5881 deg
Mean motion: 15
54198601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3160
Checksum: 304
Coasting Arc #4 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2016/084/03:23:00
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1407791
82 A = 6779808
30 meter
Y = 4725368
41 meter E =
0009558
Z = -4662403
36 I = 51
94079
XDOT = -5434
197734 Wp = 100
38826
YDOT = 4523
998733 meter/sec RA = 121
17217 deg
ZDOT = 2947
709212 TA = 198
84874
MA = 198
88415
Ha = 220
779 n
mi
Hp = 214
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4618739
56 X = 1377494
92
Y = 15503177
19 feet Y = 4740941
13 meter
Z = -15296598
93 Z = -4655638
99
XDOT = -17828
732722 XDOT = -5498
701050
YDOT = 14842
515528 feet/sec YDOT = 4462
869732 meter/sec
ZDOT = 9670
961983 ZDOT = 2921
153824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15113555
05 X = -4606611
58
Y = -5842655
01 feet Y = -1780841
25 meter
Z = -15267974
10 Z = -4653678
51
XDOT = -1083
975044 XDOT = -330
395593
YDOT = -22135
022407 feet/sec YDOT = -6746
754830 meter/sec
ZDOT = 9554
834632 ZDOT = 2912
313596
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 16084
15187909
00016717 00000-0 10270-3 0 9039
2 25544 51
6392 122
1417 0001905 346
0765 14
0335 15
54249169 31750
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
15187909 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 122
1417 deg
Eccentricity:
0001905
Arg of perigee: 346
0765 deg
Mean anomaly: 14
0335 deg
Mean motion: 15
54249169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 303
Coasting Arc #5 (Orbit 3175)
---------------------------------------
Vector Time (GMT): 2016/084/04:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3720236
62 A = 6776988
20 meter
Y = 1926561
81 meter E =
0014555
Z = -5339351
44 I = 51
93348
XDOT = -3777
348290 Wp = 81
22931
YDOT = 6657
823602 meter/sec RA = 120
90510 deg
ZDOT = -227
971683 TA = 186
59416
MA = 186
61333
Ha = 220
739 n
mi
Hp = 214
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12205500
72 X = 3724353
14
Y = 6320740
84 feet Y = 1968186
13 meter
Z = -17517557
21 Z = -5321269
75
XDOT = -12392
874968 XDOT = -3850
409599
YDOT = 21843
253288 feet/sec YDOT = 6615
174235 meter/sec
ZDOT = -747
938594 ZDOT = -246
499634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9623130
95 X = -2933130
31
Y = 9952738
03 feet Y = 3033594
55 meter
Z = -17439299
86 Z = -5315498
60
XDOT = -16580
201504 XDOT = -5053
645418
YDOT = -17494
035439 feet/sec YDOT = -5332
182002 meter/sec
ZDOT = -829
532013 ZDOT = -252
841358
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 16084
21617630
00016717 00000-0 10270-3 0 9046
2 25544 51
6403 121
8217 0001829 345
4996 14
6104 15
54262643 31764
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
21617630 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 121
8217 deg
Eccentricity:
0001829
Arg of perigee: 345
4996 deg
Mean anomaly: 14
6104 deg
Mean motion: 15
54262643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3176
Checksum: 294
Coasting Arc #6 (Orbit 3191)
---------------------------------------
Vector Time (GMT): 2016/085/04:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2733381
78 A = 6778048
65 meter
Y = -3517869
81 meter E =
0006192
Z = 5106126
10 I = 51
95170
XDOT = 4442
351063 Wp = 40
30412
YDOT = -6002
777895 meter/sec RA = 115
92424 deg
ZDOT = -1751
782052 TA = 66
58689
MA = 66
52179
Ha = 220
930 n
mi
Hp = 214
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8967788
00 X = -2718644
41
Y = -11541567
62 feet Y = -3548353
13 meter
Z = 16752382
20 Z = 5092884
28
XDOT = 14574
642594 XDOT = 4517
654895
YDOT = -19694
153199 feet/sec YDOT = -5952
679786 meter/sec
ZDOT = -5747
316444 ZDOT = -1730
018321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13584000
94 X = 4140403
49
Y = -5568592
25 feet Y = -1697306
92 meter
Z = 16695418
92 Z = 5088763
69
XDOT = 14535
096071 XDOT = 4430
297282
YDOT = 18455
025013 feet/sec YDOT = 5625
091624 meter/sec
ZDOT = -5651
753684 ZDOT = -1722
654523
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 16085
24492666
00016717 00000-0 10270-3 0 9051
2 25544 51
6396 116
6916 0001774 350
2819 9
8299 15
54226029 31927
Satellite: ISS
Catalog Number: 25544
Epoch time: 16085
24492666 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 116
6916 deg
Eccentricity:
0001774
Arg of perigee: 350
2819 deg
Mean anomaly: 9
8299 deg
Mean motion: 15
54226029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3192
Checksum: 332
Coasting Arc #7 (Orbit 3206)
---------------------------------------
Vector Time (GMT): 2016/086/04:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1745193
32 A = 6781006
43 meter
Y = 4920633
87 meter E =
0007733
Z = -4334404
40 I = 51
97614
XDOT = -4801
584265 Wp = 98
77207
YDOT = 4812
175500 meter/sec RA = 110
95151 deg
ZDOT = 3533
947202 TA = 207
04795
MA = 207
08827
Ha = 220
780 n
mi
Hp = 214
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5725699
88 X = 1711094
68
Y = 16143811
91 feet Y = 4939958
53 meter
Z = -14220486
88 Z = -4326010
13
XDOT = -15753
229217 XDOT = -4872
204858
YDOT = 15787
977361 feet/sec YDOT = 4758
086617 meter/sec
ZDOT = 11594
314966 ZDOT = 3510
449955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17095659
83 X = -5210757
12
Y = 1468878
16 feet Y = 447714
06 meter
Z = -14184828
55 Z = -4323535
74
XDOT = -11079
271901 XDOT = -3376
962075
YDOT = -18109
632987 feet/sec YDOT = -5519
816134 meter/sec
ZDOT = 11491
400703 ZDOT = 3502
578934
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 16086
20936932
00016717 00000-0 10270-3 0 9068
2 25544 51
6406 111
8833 0001873 348
2184 11
8924 15
54267497 32075
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
20936932 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 111
8833 deg
Eccentricity:
0001873
Arg of perigee: 348
2184 deg
Mean anomaly: 11
8924 deg
Mean motion: 15
54267497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3207
Checksum: 317
Coasting Arc #8 (Orbit 3210)
---------------------------------------
Vector Time (GMT): 2016/086/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4548637
47 A = 6780607
61 meter
Y = -2343252
23 meter E =
0009906
Z = -4459463
36 I = 51
97835
XDOT = 286
857036 Wp = 57
79171
YDOT = 6892
240686 meter/sec RA = 109
78697 deg
ZDOT = -3329
234327 TA = 178
72297
MA = 178
72044
Ha = 220
852 n
mi
Hp = 214
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14923351
27 X = 4596164
54
Y = -7687835
39 feet Y = -2292121
20 meter
Z = -14630785
31 Z = -4437251
31
XDOT = 941
132009 XDOT = 225
937073
YDOT = 22612
338208 feet/sec YDOT = 6895
107439 meter/sec
ZDOT = -10922
684801 ZDOT = -3327
989736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16584660
03 X = 5055004
38
Y = -3095950
11 feet Y = -943645
59 meter
Z = -14533865
61 Z = -4429922
24
XDOT = -5693
231738 XDOT = -1735
297034
YDOT = 20754
308258 feet/sec YDOT = 6325
913157 meter/sec
ZDOT = -10918
429133 ZDOT = -3327
937200
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 16086
46655275
00016717 00000-0 10270-3 0 9075
2 25544 51
6414 110
6037 0002099 354
4449 5
6680 15
54271514 32111
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
46655275 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 110
6037 deg
Eccentricity:
0002099
Arg of perigee: 354
4449 deg
Mean anomaly: 5
6680 deg
Mean motion: 15
54271514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3211
Checksum: 300
Coasting Arc #9 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2016/087/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4338611
57 A = 6777597
33 meter
Y = 596101
48 meter E =
0003893
Z = 5169490
89 I = 51
97836
XDOT = 763
943694 Wp = 96
95703
YDOT = -7484
138108 meter/sec RA = 104
81380 deg
ZDOT = 1502
738498 TA = 338
63713
MA = 338
65337
Ha = 221
057 n
mi
Hp = 214
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14234289
94 X = -4370066
24
Y = 1955713
52 feet Y = 547408
99 meter
Z = 16960271
93 Z = 5148338
35
XDOT = 2506
376948 XDOT = 840
276692
YDOT = -24554
258886 feet/sec YDOT = -7475
168198 meter/sec
ZDOT = 4930
244417 ZDOT = 1506
635884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14342577
60 X = -4371617
65
Y = -1960478
71 feet Y = -597553
91 meter
Z = 16868243
55 Z = 5141440
64
XDOT = 8825
054881 XDOT = 2689
876728
YDOT = -21945
173075 feet/sec YDOT = -6688
888753 meter/sec
ZDOT = 4948
451401 ZDOT = 1508
287987
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 16087
49528074
00016717 00000-0 10270-3 0 9086
2 25544 51
6412 105
4744 0002253
3404 359
7750 15
54300507 32279
Satellite: ISS
Catalog Number: 25544
Epoch time: 16087
49528074 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 105
4744 deg
Eccentricity:
0002253
Arg of perigee:
3404 deg
Mean anomaly: 359
7750 deg
Mean motion: 15
54300507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 289
Coasting Arc #10 (Orbit 3241)
---------------------------------------
Vector Time (GMT): 2016/088/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4009231
65 A = 6776976
02 meter
Y = 1261307
00 meter E =
0014846
Z = -5328898
42 I = 51
98415
XDOT = -1686
870878 Wp = 85
19794
YDOT = 7453
318483 meter/sec RA = 99
83596 deg
ZDOT = 497
409304 TA = 189
51705
MA = 189
54521
Ha = 220
952 n
mi
Hp = 214
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13153647
14 X = 4020715
13
Y = 4138146
33 feet Y = 1306204
53 meter
Z = -17483262
52 Z = -5309394
66
XDOT = -5534
353273 XDOT = -1772
506587
YDOT = 24453
144630 feet/sec YDOT = 7433
976007 meter/sec
ZDOT = 1631
920288 ZDOT = 489
006045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11798752
26 X = 3596259
69
Y = 7340392
71 feet Y = 2237351
70 meter
Z = -17398713
65 Z = -5303127
92
XDOT = -10982
044100 XDOT = -3347
327042
YDOT = 21411
998481 feet/sec YDOT = 6526
377137 meter/sec
ZDOT = 1594
117274 ZDOT = 485
886945
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 16088
45970680
00016717 00000-0 10270-3 0 9098
2 25544 51
6419 100
6660 0002234 1
7880 358
3281 15
54285970 32429
Satellite: ISS
Catalog Number: 25544
Epoch time: 16088
45970680 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 100
6660 deg
Eccentricity:
0002234
Arg of perigee: 1
7880 deg
Mean anomaly: 358
3281 deg
Mean motion: 15
54285970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3242
Checksum: 311
Coasting Arc #11 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2016/089/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3563917
97 A = 6778703
01 meter
Y = -3070901
43 meter E =
0008630
Z = 4877199
27 I = 51
99420
XDOT = 2505
873969 Wp = 47
60758
YDOT = -6821
529741 meter/sec RA = 94
86012 deg
ZDOT = -2455
593452 TA = 66
40834
MA = 66
31773
Ha = 221
052 n
mi
Hp = 214
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11692644
27 X = -3553005
00
Y = -10075135
93 feet Y = -3110694
05 meter
Z = 16001309
93 Z = 4859913
33
XDOT = 8221
371288 XDOT = 2593
896065
YDOT = -22380
346919 feet/sec YDOT = -6793
015466 meter/sec
ZDOT = -8056
408962 ZDOT = -2443
206016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9099572
93 X = -2773549
83
Y = -12562075
92 feet Y = -3828920
74 meter
Z = 15926714
50 Z = 4854462
58
XDOT = 12381
753413 XDOT = 3773
958440
YDOT = -19148
646113 feet/sec YDOT = -5836
507335 meter/sec
ZDOT = -8001
380779 ZDOT = -2438
820861
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 16089
48841814
00016717 00000-0 10270-3 0 9100
2 25544 51
6410 95
5368 0002305 8
1746 351
9444 15
54341244 32582
Satellite: ISS
Catalog Number: 25544
Epoch time: 16089
48841814 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 95
5368 deg
Eccentricity:
0002305
Arg of perigee: 8
1746 deg
Mean anomaly: 351
9444 deg
Mean motion: 15
54341244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 306
Coasting Arc #12 (Orbit 3272)
---------------------------------------
Vector Time (GMT): 2016/090/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3057699
84 A = 6782332
75 meter
Y = 4631438
70 meter E =
0006686
Z = -3903954
75 I = 52
00993
XDOT = -3214
652122 Wp = 84
40080
YDOT = 5597
514560 meter/sec RA = 89
89261 deg
ZDOT = 4129
463377 TA = 228
70993
MA = 228
76752
Ha = 221
060 n
mi
Hp = 214
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10031823
63 X = 3024646
51
Y = 15195008
86 feet Y = 4665446
78 meter
Z = -12808250
51 Z = -3889181
84
XDOT = -10546
758929 XDOT = -3297
065247
YDOT = 18364
549080 feet/sec YDOT = 5561
105744 meter/sec
ZDOT = 13548
108193 ZDOT = 4113
646673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6556795
59 X = 1998511
30
Y = 17033911
28 feet Y = 5191936
16 meter
Z = -12744856
16 Z = -3884632
16
XDOT = -13141
003888 XDOT = -4005
377985
YDOT = 15126
385146 feet/sec YDOT = 4610
522193 meter/sec
ZDOT = 13478
373339 ZDOT = 4108
208194
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 16090
45282689
00016717 00000-0 10270-3 0 9119
2 25544 51
6429 90
7282 0002415 11
3754 348
7453 15
54334766 32733
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
45282689 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 90
7282 deg
Eccentricity:
0002415
Arg of perigee: 11
3754 deg
Mean anomaly: 348
7453 deg
Mean motion: 15
54334766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3273
Checksum: 316
Coasting Arc #13 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2016/090/14:15:30
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3915840
83 A = 6777935
39 meter
Y = 2248068
48 meter E =
0005100
Z = 5050869
09 I = 51
99286
XDOT = -1630
175152 Wp = 98
76013
YDOT = -7237
544307 meter/sec RA = 89
19116 deg
ZDOT = 1955
048671 TA = 332
35715
MA = 332
38426
Ha = 221
076 n
mi
Hp = 214
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12847246
80 X = -3965223
30
Y = 7375552
77 feet Y = 2204003
27 meter
Z = 16571092
82 Z = 5031726
70
XDOT = -5348
343673 XDOT = -1558
618796
YDOT = -23745
224103 feet/sec YDOT = -7255
373744 meter/sec
ZDOT = 6414
201677 ZDOT = 1947
304086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4831815
19 X = -1472737
27
Y = 14102049
82 feet Y = 4298304
78 meter
Z = 16487492
21 Z = 5025387
63
XDOT = -18723
287255 XDOT = -5706
857955
YDOT = -13885
921923 feet/sec YDOT = -4232
429002 meter/sec
ZDOT = 6381
817615 ZDOT = 1945
178009
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 16090
64570770
00016717 00000-0 10270-3 0 9122
2 25544 51
6403 89
7664 0002462 6
2495 353
8688 15
54356214 32766
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
64570770 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 89
7664 deg
Eccentricity:
0002462
Arg of perigee: 6
2495 deg
Mean anomaly: 353
8688 deg
Mean motion: 15
54356214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 322
Coasting Arc #14 (Orbit 3290)
---------------------------------------
Vector Time (GMT): 2016/091/14:15:30
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4163240
55 A = 6776750
20 meter
Y = -373858
01 meter E =
0015576
Z = -5347272
72 I = 51
98688
XDOT = 737
815612 Wp = 81
20180
YDOT = 7621
807772 meter/sec RA = 84
21356 deg
ZDOT = 43
984098 TA = 189
20162
MA = 189
23020
Ha = 221
056 n
mi
Hp = 214
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13658925
70 X = 4193086
49
Y = -1226568
28 feet Y = -327135
46 meter
Z = -17543545
67 Z = -5326976
19
XDOT = 2420
654894 XDOT = 652
318169
YDOT = 25005
931010 feet/sec YDOT = 7629
580476 meter/sec
ZDOT = 144
304784 ZDOT = 47
359920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9339502
96 X = 2846680
50
Y = -10194825
54 feet Y = -3107382
82 meter
Z = -17455255
15 Z = -5320361
77
XDOT = 17908
197408 XDOT = 5458
418570
YDOT = 16149
560620 feet/sec YDOT = 4922
386077 meter/sec
ZDOT = 157
618075 ZDOT = 48
041989
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 16091
61010772
00016717 00000-0 10270-3 0 9132
2 25544 51
6399 84
9572 0002520 11
9225 348
1987 15
54337550 32912
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
61010772 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 84
9572 deg
Eccentricity:
0002520
Arg of perigee: 11
9225 deg
Mean anomaly: 348
1987 deg
Mean motion: 15
54337550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3291
Checksum: 308
Coasting Arc #15 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2016/091/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700728
86 A = 6781656
20 meter
Y = 4683270
37 meter E =
0010943
Z = 4084870
12 I = 52
00460
XDOT = -3656
457685 Wp = 89
35258
YDOT = -5510
366528 meter/sec RA = 83
79738 deg
ZDOT = 3891
266098 TA = 320
55269
MA = 320
63231
Ha = 221
126 n
mi
Hp = 214
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8860658
98 X = -2772740
19
Y = 15365060
26 feet Y = 4652666
73 meter
Z = 13401804
86 Z = 4071575
34
XDOT = -11996
252247 XDOT = -3613
469760
YDOT = -18078
630340 feet/sec YDOT = -5551
014779 meter/sec
ZDOT = 12766
621057 ZDOT = 3873
608800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12442156
99 X = 3792369
45
Y = 12702638
81 feet Y = 3871764
31 meter
Z = 13343178
95 Z = 4067000
94
XDOT = -19707
683044 XDOT = -6006
901792
YDOT = 5942
149350 feet/sec YDOT = 1811
167122 meter/sec
ZDOT = 12690
853478 ZDOT = 3868
172140
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 16091
73869390
00016717 00000-0 10270-3 0 9144
2 25544 51
6413 84
3170 0002490 12
8863 347
2353 15
54351412 32933
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
73869390 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 84
3170 deg
Eccentricity:
0002490
Arg of perigee: 12
8863 deg
Mean anomaly: 347
2353 deg
Mean motion: 15
54351412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 301
Coasting Arc #16 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2016/092/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3371904
97 A = 6778109
81 meter
Y = -3109458
49 meter E =
0014056
Z = -5003322
50 I = 51
98946
XDOT = 3021
724417 Wp = 65
39316
YDOT = 6706
209777 meter/sec RA = 78
82738 deg
ZDOT = -2130
325308 TA = 183
92563
MA = 183
93667
Ha = 221
044 n
mi
Hp = 214
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11062680
33 X = 3430729
06
Y = -10201635
46 feet Y = -3071423
14 meter
Z = -16415100
06 Z = -4986799
49
XDOT = 9913
794019 XDOT = 2956
857524
YDOT = 22002
000580 feet/sec YDOT = 6739
637826 meter/sec
ZDOT = -6989
256261 ZDOT = -2115
804692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7105461
98 X = -2165744
81
Y = -13354393
48 feet Y = -4070419
13 meter
Z = -16342715
72 Z = -4981259
75
XDOT = 22812
846022 XDOT = 6953
355467
YDOT = -3656
493678 feet/sec YDOT = -1114
499273 meter/sec
ZDOT = -6927
345633 ZDOT = -2111
454949
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 16092
70308408
00016717 00000-0 10270-3 0 9151
2 25544 51
6422 79
5080 0002560 15
7413 344
3819 15
54377615 33085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16092
70308408 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 79
5080 deg
Eccentricity:
0002560
Arg of perigee: 15
7413 deg
Mean anomaly: 344
3819 deg
Mean motion: 15
54377615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 300
Coasting Arc #17 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2016/093/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3966178
72 A = 6776513
33 meter
Y = 1302091
43 meter E =
0003796
Z = 5335375
67 I = 51
97741
XDOT = -2233
250933 Wp = 54
68870
YDOT = -7338
450438 meter/sec RA = 73
84989 deg
ZDOT = 132
869559 TA = 34
06374
MA = 34
03938
Ha = 221
128 n
mi
Hp = 213
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13012397
37 X = -4006361
16
Y = 4271953
50 feet Y = 1257514
84 meter
Z = 17504513
35 Z = 5316011
28
XDOT = -7326
938756 XDOT = -2151
669996
YDOT = -24076
280966 feet/sec YDOT = -7362
967976 meter/sec
ZDOT = 435
923750 ZDOT = 122
219888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1112385
24 X = 339055
02
Y = 13758007
21 feet Y = 4193440
60 meter
Z = 17420100
36 Z = 5309646
59
XDOT = -24116
515471 XDOT = -7350
713915
YDOT = 1463
522838 feet/sec YDOT = 446
081761 meter/sec
ZDOT = 390
963134 ZDOT = 119
165563
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 16093
73175495
00016717 00000-0 10270-3 0 9164
2 25544 51
6422 74
3787 0002523 16
0417 344
0815 15
54415353 33242
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
73175495 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 74
3787 deg
Eccentricity:
0002523
Arg of perigee: 16
0417 deg
Mean anomaly: 344
0815 deg
Mean motion: 15
54415353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 300
Coasting Arc #18 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2016/093/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4215740
72 A = 6776702
70 meter
Y = 337075
16 meter E =
0005267
Z = 5292519
71 I = 51
97888
XDOT = -1576
878824 Wp = 41
09324
YDOT = -7467
576393 meter/sec RA = 73
51585 deg
ZDOT = -776
153836 TA = 56
31052
MA = 56
26032
Ha = 221
111 n
mi
Hp = 213
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13831170
33 X = -4244905
38
Y = 1105889
63 feet Y = 289769
41 meter
Z = 17363909
81 Z = 5271969
87
XDOT = -5173
486956 XDOT = -1489
487117
YDOT = -24499
922549 feet/sec YDOT = -7484
721542 meter/sec
ZDOT = -2546
436470 ZDOT = -783
600889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3594741
56 X = 1095677
23
Y = 13516599
33 feet Y = 4119859
48 meter
Z = 17274518
92 Z = 5265273
37
XDOT = -22189
067197 XDOT = -6763
227682
YDOT = 9213
358034 feet/sec YDOT = 2808
231529 meter/sec
ZDOT = -2577
451301 ZDOT = -785
607157
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 16093
79604609
00016717 00000-0 10270-3 0 9175
2 25544 51
6436 74
0584 0002510 15
4772 344
6457 15
54419414 33253
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
79604609 = yrday
fracday
Element set: 917
Inclination: 51
6436 deg
RA of node: 74
0584 deg
Eccentricity:
0002510
Arg of perigee: 15
4772 deg
Mean anomaly: 344
6457 deg
Mean motion: 15
54419414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 312
Coasting Arc #19 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2016/094/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4591712
09 A = 6779010
66 meter
Y = 1478289
71 meter E =
0011374
Z = -4773196
76 I = 51
97563
XDOT = 522
819928 Wp = 95
68228
YDOT = 7141
896386 meter/sec RA = 68
53910 deg
ZDOT = 2719
292677 TA = 201
07990
MA = 201
12682
Ha = 221
096 n
mi
Hp = 213
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15064672
20 X = 4598026
31
Y = 4850031
87 feet Y = 1529672
05 meter
Z = -15660094
37 Z = -4750876
26
XDOT = 1715
288478 XDOT = 429
709480
YDOT = 23431
418589 feet/sec YDOT = 7147
222608 meter/sec
ZDOT = 8921
563901 ZDOT = 2721
605424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1772813
36 X = 540353
51
Y = -15822305
32 feet Y = -4822638
66 meter
Z = -15563338
34 Z = -4743705
53
XDOT = 21495
288207 XDOT = 6551
763845
YDOT = -6361
219717 feet/sec YDOT = -1938
899770 meter/sec
ZDOT = 8930
310361 ZDOT = 2721
958598
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 16094
76041808
00016717 00000-0 10270-3 0 9180
2 25544 51
6429 69
2494 0002573 19
8950 340
2302 15
54400743 33409
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
76041808 = yrday
fracday
Element set: 918
Inclination: 51
6429 deg
RA of node: 69
2494 deg
Eccentricity:
0002573
Arg of perigee: 19
8950 deg
Mean anomaly: 340
2302 deg
Mean motion: 15
54400743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 303
Coasting Arc #20 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2016/094/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1454434
49 A = 6787885
85 meter
Y = -6492046
46 meter E =
0007724
Z = -1336512
75 I = 52
00383
XDOT = 4952
377962 Wp = 126
79990
YDOT = 89
121823 meter/sec RA = 68
34357 deg
ZDOT = -5850
033677 TA = 67
67323
MA = 67
59138
Ha = 221
091 n
mi
Hp = 213
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4771766
71 X = -1375238
53
Y = -21299365
02 feet Y = -6507868
26 meter
Z = -4384884
35 Z = -1343384
90
XDOT = 16247
959193 XDOT = 4979
430199
YDOT = 292
394434 feet/sec YDOT = 144
653187 meter/sec
ZDOT = -19193
023875 ZDOT = -5825
910619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16594257
56 X = -5057929
71
Y = 14170777
79 feet Y = 4319253
07 meter
Z = -4413569
02 Z = -1345255
84
XDOT = -6380
686988 XDOT = -1944
833394
YDOT = -13388
809952 feet/sec YDOT = -4080
909273 meter/sec
ZDOT = -19088
177933 ZDOT = -5818
076634
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 16094
82470936
00016717 00000-0 10270-3 0 9196
2 25544 51
6423 68
9286 0002427 19
9042 340
2205 15
54359514 33411
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
82470936 = yrday
fracday
Element set: 919
Inclination: 51
6423 deg
RA of node: 68
9286 deg
Eccentricity:
0002427
Arg of perigee: 19
9042 deg
Mean anomaly: 340
2205 deg
Mean motion: 15
54359514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 311
Coasting Arc #21 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2016/095/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 445207
66 A = 6784776
14 meter
Y = 6074844
61 meter E =
0014586
Z = 2971170
49 I = 51
98105
XDOT = -5423
997608 Wp = 73
48341
YDOT = -2065
467776 meter/sec RA = 63
39050 deg
ZDOT = 5019
514925 TA = 320
33027
MA = 320
43687
Ha = 221
097 n
mi
Hp = 213
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1460655
04 X = 362811
47
Y = 19930592
56 feet Y = 6079362
90 meter
Z = 9747934
67 Z = 2973132
27
XDOT = -17795
267744 XDOT = -5424
880557
YDOT = -6776
469081 feet/sec YDOT = -2126
126804 meter/sec
ZDOT = 16468
224820 ZDOT = 4993
164631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16768652
32 X = 5111085
23
Y = -10864154
29 feet Y = -3311394
23 meter
Z = 9755342
85 Z = 2973428
50
XDOT = 1936
419521 XDOT = 590
220670
YDOT = 17721
697791 feet/sec YDOT = 5401
573487 meter/sec
ZDOT = 16354
064017 ZDOT = 4984
718712
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 16095
85336152
00016717 00000-0 10270-3 0 9203
2 25544 51
6421 63
7983 0002587 21
1405 338
9854 15
54404751 33576
Satellite: ISS
Catalog Number: 25544
Epoch time: 16095
85336152 = yrday
fracday
Element set: 920
Inclination: 51
6421 deg
RA of node: 63
7983 deg
Eccentricity:
0002587
Arg of perigee: 21
1405 deg
Mean anomaly: 338
9854 deg
Mean motion: 15
54404751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 313
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