[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 19th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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
294/03:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 211
9
295/09:59:09
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 211
9
297/11:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 212
0
304/00:37:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
2
304/02:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
2
307/03:37:48
263 -0
9 4
9 4
9
N/A 4
7 -0
0 222
7
000/00:01:36
527 1
2 0
0 215
3
308/04:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 2431)
---------------------------------------
Vector Time (GMT): 2016/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5929037
31 A = 6788725
61 meter
Y = -3199070
25 meter E =
0019143
Z = 778574
26 I = 51
80115
XDOT = 2884
722530 Wp = 113
36524
YDOT = 3869
053036 meter/sec RA = 156
86806 deg
ZDOT = -5961
766925 TA = 58
23475
MA = 58
04839
Ha = 223
336 n
mi
Hp = 211
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19452222
13 X = 5960587
40
Y = -10495637
31 feet Y = -3132591
34 meter
Z = 2554377
49 Z = 807453
46
XDOT = 9464
312762 XDOT = 2870
203738
YDOT = 12693
743558 feet/sec YDOT = 3901
230494 meter/sec
ZDOT = -19559
602771 ZDOT = -5947
788788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12381281
70 X = -3773814
66
Y = 18291722
93 feet Y = 5575317
15 meter
Z = 2681217
74 Z = 817235
17
XDOT = -13038
172131 XDOT = -3974
034866
YDOT = -5917
306306 feet/sec YDOT = -1803
594962 meter/sec
ZDOT = -19499
042273 ZDOT = -5943
308085
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 16293
53379389
00016717 00000-0 10270-3 0 9005
2 25544 51
6418 157
8342 0006861 86
4471 273
7467 15
54239901 24324
Satellite: ISS
Catalog Number: 25544
Epoch time: 16293
53379389 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 157
8342 deg
Eccentricity:
0006861
Arg of perigee: 86
4471 deg
Mean anomaly: 273
7467 deg
Mean motion: 15
54239901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2432
Checksum: 333
Coasting Arc #2 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2016/294/03:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3726371
51 A = 6784401
69 meter
Y = -4661280
90 meter E =
0019620
Z = 3209604
07 I = 51
80259
XDOT = 5831
575244 Wp = 91
67214
YDOT = 1334
891535 meter/sec RA = 153
67612 deg
ZDOT = -4807
080317 TA = 51
26292
MA = 51
08771
Ha = 223
207 n
mi
Hp = 211
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12225628
31 X = 3762627
00
Y = -15292916
34 feet Y = -4619407
27 meter
Z = 10530197
07 Z = 3227794
45
XDOT = 19132
464710 XDOT = 5839
565920
YDOT = 4379
565403 feet/sec YDOT = 1400
148615 meter/sec
ZDOT = -15771
260881 ZDOT = -4778
732062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12375013
82 X = -3771904
21
Y = -15116231
69 feet Y = -4607427
42 meter
Z = 10610508
96 Z = 3234083
13
XDOT = 7244
596427 XDOT = 2208
152991
YDOT = -16970
815035 feet/sec YDOT = -5172
704423 meter/sec
ZDOT = -15647
430474 ZDOT = -4769
336809
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 16294
17675290
00016717 00000-0 10270-3 0 9017
2 25544 51
6382 154
6271 0006878 88
1019 272
0921 15
54297234 24426
Satellite: ISS
Catalog Number: 25544
Epoch time: 16294
17675290 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 154
6271 deg
Eccentricity:
0006878
Arg of perigee: 88
1019 deg
Mean anomaly: 272
0921 deg
Mean motion: 15
54297234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 317
Coasting Arc #3 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2016/295/03:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4824027
39 A = 6787600
57 meter
Y = 4470419
45 meter E =
0013078
Z = -1673561
79 I = 51
84214
XDOT = -4382
227169 Wp = 64
73095
YDOT = -2600
713686 meter/sec RA = 148
71206 deg
ZDOT = 5725
040924 TA = 276
99166
MA = 277
14038
Ha = 223
297 n
mi
Hp = 211
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15826861
50 X = -4865528
65
Y = 14666730
47 feet Y = 4416241
83 meter
Z = -5490688
30 Z = -1697097
06
XDOT = -14377
385725 XDOT = -4380
629855
YDOT = -8532
525218 feet/sec YDOT = -2649
709545 meter/sec
ZDOT = 18782
942665 ZDOT = 5703
756799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11312144
15 X = 3447941
54
Y = 18343623
69 feet Y = 5591136
50 meter
Z = -5594376
67 Z = -1705166
01
XDOT = -9852
115886 XDOT = -3002
924922
YDOT = 11736
065679 feet/sec YDOT = 3577
152819 meter/sec
ZDOT = 18690
206629 ZDOT = 5696
774980
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 16295
14119042
00016717 00000-0 10270-3 0 9024
2 25544 51
6386 149
8192 0007070 92
9358 267
2604 15
54296598 24574
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
14119042 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 149
8192 deg
Eccentricity:
0007070
Arg of perigee: 92
9358 deg
Mean anomaly: 267
2604 deg
Mean motion: 15
54296598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2457
Checksum: 332
Coasting Arc #4 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2016/295/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 895949
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1261033
95 A = 6777070
72 meter
Y = -4091332
44 meter E =
0009770
Z = 5245427
38 I = 51
81926
XDOT = 6802
165587 Wp = 81
03092
YDOT = -3408
136242 meter/sec RA = 147
33634 deg
ZDOT = -1019
893140 TA = 18
71806
MA = 18
68216
Ha = 223
164 n
mi
Hp = 211
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4137250
50 X = -1240670
31
Y = -13423006
70 feet Y = -4105320
11 meter
Z = 17209407
42 Z = 5239351
12
XDOT = 22316
816231 XDOT = 6844
724958
YDOT = -11181
549350 feet/sec YDOT = -3331
831938 meter/sec
ZDOT = -3346
106103 ZDOT = -986
745923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4063842
80 X = 1238659
29
Y = 13478565
31 feet Y = 4108266
71 meter
Z = 17183454
63 Z = 5237516
97
XDOT = -21506
638736 XDOT = -6555
223487
YDOT = 10577
589870 feet/sec YDOT = 3224
049392 meter/sec
ZDOT = -3200
514012 ZDOT = -975
516671
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 16295
46266671
00016717 00000-0 10270-3 0 9031
2 25544 51
6429 148
2170 0006626 92
6623 267
5288 15
54329266 24625
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
46266671 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 148
2170 deg
Eccentricity:
0006626
Arg of perigee: 92
6623 deg
Mean anomaly: 267
5288 deg
Mean motion: 15
54329266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 330
Coasting Arc #5 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2016/296/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 895949
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -345087
49 A = 6779544
60 meter
Y = 4908568
62 meter E =
0017200
Z = -4679992
04 I = 51
85381
XDOT = -6702
498291 Wp = 104
37068
YDOT = 2291
560665 meter/sec RA = 142
35137 deg
ZDOT = 2902
472384 TA = 194
42892
MA = 194
47810
Ha = 223
162 n
mi
Hp = 211
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1132176
80 X = -377217
05
Y = 16104227
75 feet Y = 4904529
75 meter
Z = -15354304
59 Z = -4681746
68
XDOT = -21989
823791 XDOT = -6741
724092
YDOT = 7518
243650 feet/sec YDOT = 2216
389645 meter/sec
ZDOT = 9522
547193 ZDOT = 2869
817551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 976911
45 X = 297762
61
Y = -16106335
69 feet Y = -4909211
12 meter
Z = -15362754
95 Z = -4682567
71
XDOT = 20850
354231 XDOT = 6355
187970
YDOT = -7666
682522 feet/sec YDOT = -2336
804833 meter/sec
ZDOT = 9379
263432 ZDOT = 2858
799494
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 16296
42709634
00016717 00000-0 10270-3 0 9040
2 25544 51
6427 143
4081 0006691 95
2483 264
9434 15
54306205 24774
Satellite: ISS
Catalog Number: 25544
Epoch time: 16296
42709634 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 143
4081 deg
Eccentricity:
0006691
Arg of perigee: 95
2483 deg
Mean anomaly: 264
9434 deg
Mean motion: 15
54306205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 318
Coasting Arc #6 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2016/297/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 895949
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1826250
18 A = 6783322
25 meter
Y = -5470079
11 meter E =
0018703
Z = 3555081
93 I = 51
89129
XDOT = 6159
642514 Wp = 91
36132
YDOT = -877
576818 meter/sec RA = 137
37784 deg
ZDOT = -4494
594170 TA = 46
80849
MA = 46
65239
Ha = 223
105 n
mi
Hp = 211
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5991634
44 X = 1870013
03
Y = -17946453
78 feet Y = -5449411
85 meter
Z = 11663654
62 Z = 3564060
11
XDOT = 20208
800899 XDOT = 6190
831031
YDOT = -2879
189035 feet/sec YDOT = -808
521448 meter/sec
ZDOT = -14746
043866 ZDOT = -4464
596055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5543849
91 X = -1689765
45
Y = 18063833
55 feet Y = 5505856
47 meter
Z = 11703818
66 Z = 3567323
93
XDOT = -18922
781074 XDOT = -5767
663671
YDOT = 3703
738782 feet/sec YDOT = 1128
899581 meter/sec
ZDOT = -14614
594280 ZDOT = -4454
528337
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 16297
45581486
00016717 00000-0 10270-3 0 9058
2 25544 51
6423 138
2791 0006715 98
1191 262
0724 15
54336126 24939
Satellite: ISS
Catalog Number: 25544
Epoch time: 16297
45581486 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 138
2791 deg
Eccentricity:
0006715
Arg of perigee: 98
1191 deg
Mean anomaly: 262
0724 deg
Mean motion: 15
54336126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 321
Coasting Arc #7 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2016/297/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5712052
98 A = 6785154
96 meter
Y = 2108606
82 meter E =
0019653
Z = 2976289
04 I = 51
89671
XDOT = 482
656849 Wp = 88
03076
YDOT = -5796
383924 meter/sec RA = 137
19870 deg
ZDOT = 5005
076385 TA = 305
89247
MA = 306
07476
Ha = 223
206 n
mi
Hp = 212
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18740331
29 X = -5749665
10
Y = 6918001
39 feet Y = 2044520
69 meter
Z = 9764727
82 Z = 2948449
55
XDOT = 1583
519847 XDOT = 523
124866
YDOT = -19017
007626 feet/sec YDOT = -5790
759955 meter/sec
ZDOT = 16420
854280 ZDOT = 5007
519682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15811281
50 X = 4819278
60
Y = -12305836
79 feet Y = -3750819
05 meter
Z = 9642532
23 Z = 2939043
83
XDOT = 3474
101939 XDOT = 1058
906271
YDOT = 17412
125519 feet/sec YDOT = 5307
215858 meter/sec
ZDOT = 16432
464839 ZDOT = 5008
615283
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 16297
52010959
00016717 00000-0 10270-3 0 9069
2 25544 51
6411 137
9578 0006609 99
0738 261
1162 15
54305127 24948
Satellite: ISS
Catalog Number: 25544
Epoch time: 16297
52010959 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 137
9578 deg
Eccentricity:
0006609
Arg of perigee: 99
0738 deg
Mean anomaly: 261
1162 deg
Mean motion: 15
54305127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2494
Checksum: 321
Coasting Arc #8 (Orbit 2508)
---------------------------------------
Vector Time (GMT): 2016/298/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5210925
06 A = 6781132
67 meter
Y = -738144
57 meter E =
0014078
Z = -4289022
47 I = 51
90612
XDOT = -2040
924981 Wp = 84
76981
YDOT = 6444
500555 meter/sec RA = 132
23068 deg
ZDOT = -3597
611756 TA = 148
61999
MA = 148
53591
Ha = 223
087 n
mi
Hp = 212
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17096210
83 X = 5239626
33
Y = -2421734
17 feet Y = -679712
35 meter
Z = -14071596
03 Z = -4263639
08
XDOT = -6695
948100 XDOT = -2095
361516
YDOT = 21143
374525 feet/sec YDOT = 6421
372922 meter/sec
ZDOT = -11803
188177 ZDOT = -3607
658859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15505942
35 X = -4726211
23
Y = 7799309
39 feet Y = 2377229
50 meter
Z = -13960356
75 Z = -4255116
74
XDOT = 68
924330 XDOT = 21
008136
YDOT = -21017
961440 feet/sec YDOT = -6406
274647 meter/sec
ZDOT = -11848
196049 ZDOT = -3611
330156
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 16298
48452762
00016717 00000-0 10270-3 0 9078
2 25544 51
6408 133
1485 0006492 103
0572 257
1306 15
54312285 25096
Satellite: ISS
Catalog Number: 25544
Epoch time: 16298
48452762 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 133
1485 deg
Eccentricity:
0006492
Arg of perigee: 103
0572 deg
Mean anomaly: 257
1306 deg
Mean motion: 15
54312285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2509
Checksum: 308
Coasting Arc #9 (Orbit 2524)
---------------------------------------
Vector Time (GMT): 2016/299/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4406766
66 A = 6777983
94 meter
Y = -784130
00 meter E =
0012006
Z = 5081811
00 I = 51
91643
XDOT = 3296
621962 Wp = 114
58515
YDOT = -6688
698666 meter/sec RA = 127
25359 deg
ZDOT = 1818
405883 TA = 317
85180
MA = 317
94406
Ha = 223
283 n
mi
Hp = 212
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14457895
87 X = -4422356
34
Y = -2572604
99 feet Y = -833496
16 meter
Z = 16672608
28 Z = 5060365
98
XDOT = 10815
688853 XDOT = 3362
338548
YDOT = -21944
549429 feet/sec YDOT = -6651
466027 meter/sec
ZDOT = 5965
898565 ZDOT = 1834
580425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14581385
35 X = 4444406
25
Y = -2479917
39 feet Y = -755878
82 meter
Z = 16578845
77 Z = 5053232
19
XDOT = -2945
388371 XDOT = -897
754376
YDOT = 23227
380899 feet/sec YDOT = 7079
705698 meter/sec
ZDOT = 6037
782966 ZDOT = 1840
316248
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 16299
51323529
00016717 00000-0 10270-3 0 9082
2 25544 51
6407 128
0185 0006651 106
0639 254
1247 15
54294820 25252
Satellite: ISS
Catalog Number: 25544
Epoch time: 16299
51323529 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 128
0185 deg
Eccentricity:
0006651
Arg of perigee: 106
0639 deg
Mean anomaly: 254
1247 deg
Mean motion: 15
54294820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2525
Checksum: 308
Coasting Arc #10 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2016/300/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3425418
27 A = 6776768
06 meter
Y = 2414659
63 meter E =
0021250
Z = -5343685
72 I = 51
92948
XDOT = -4208
379723 Wp = 97
36413
YDOT = 6389
428170 meter/sec RA = 122
27072 deg
ZDOT = 187
528499 TA = 174
43135
MA = 174
40768
Ha = 223
042 n
mi
Hp = 212
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11238248
91 X = 3424120
05
Y = 7922111
64 feet Y = 2452957
20 meter
Z = -17531777
29 Z = -5327049
03
XDOT = -13807
020090 XDOT = -4280
426110
YDOT = 20962
690848 feet/sec YDOT = 6341
964424 meter/sec
ZDOT = 615
250981 ZDOT = 166
909362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13415416
24 X = -4089018
87
Y = -3408789
90 feet Y = -1038999
16 meter
Z = -17459326
02 Z = -5321602
57
XDOT = 5282
766937 XDOT = 1610
187362
YDOT = -23507
983866 feet/sec YDOT = -7165
233482 meter/sec
ZDOT = 523
940902 ZDOT = 159
697187
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 16300
47764175
00016717 00000-0 10270-3 0 9097
2 25544 51
6387 123
2088 0006643 110
3670 249
8197 15
54335864 25408
Satellite: ISS
Catalog Number: 25544
Epoch time: 16300
47764175 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 123
2088 deg
Eccentricity:
0006643
Arg of perigee: 110
3670 deg
Mean anomaly: 249
8197 deg
Mean motion: 15
54335864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2540
Checksum: 319
Coasting Arc #11 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2016/301/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2342932
81 A = 6778268
81 meter
Y = -3951059
83 meter E =
0011171
Z = 4975056
89 I = 51
95152
XDOT = 4795
758421 Wp = 86
79626
YDOT = -5586
075363 meter/sec RA = 117
29063 deg
ZDOT = -2173
022286 TA = 24
29795
MA = 24
24532
Ha = 223
063 n
mi
Hp = 212
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7686787
42 X = -2322744
03
Y = -12962794
72 feet Y = -3977146
73 meter
Z = 16322365
14 Z = 4963724
72
XDOT = 15734
115555 XDOT = 4868
422706
YDOT = -18327
018909 feet/sec YDOT = -5532
039887 meter/sec
ZDOT = -7129
338209 ZDOT = -2149
548256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12022002
89 X = 3664306
48
Y = 9175430
81 feet Y = 2796671
31 meter
Z = 16273391
39 Z = 4960129
70
XDOT = -7242
272206 XDOT = -2207
444568
YDOT = 21977
668948 feet/sec YDOT = 6698
793495 meter/sec
ZDOT = -7025
643256 ZDOT = -2141
416064
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 16301
50633774
00016717 00000-0 10270-3 0 9104
2 25544 51
6392 118
0792 0006493 114
9055 245
2773 15
54332051 25560
Satellite: ISS
Catalog Number: 25544
Epoch time: 16301
50633774 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 118
0792 deg
Eccentricity:
0006493
Arg of perigee: 114
9055 deg
Mean anomaly: 245
2773 deg
Mean motion: 15
54332051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2556
Checksum: 298
Coasting Arc #12 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2016/302/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1283171
48 A = 6781666
16 meter
Y = 5274760
66 meter E =
0013855
Z = -4079616
74 I = 51
97627
XDOT = -5039
989728 Wp = 113
24858
YDOT = 4240
831426 meter/sec RA = 112
31727 deg
ZDOT = 3903
149660 TA = 197
05440
MA = 197
10101
Ha = 222
967 n
mi
Hp = 212
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4209880
17 X = 1243909
83
Y = 17305645
20 feet Y = 5288890
05 meter
Z = -13384569
35 Z = -4073479
12
XDOT = -16535
399369 XDOT = -5105
997426
YDOT = 13913
488931 feet/sec YDOT = 4184
102157 meter/sec
ZDOT = 12805
609122 ZDOT = 3878
505425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10621522
96 X = -3237440
20
Y = -14320862
66 feet Y = -4364998
94 meter
Z = -13358566
03 Z = -4071690
93
XDOT = 8943
645891 XDOT = 2726
023267
YDOT = -18461
255049 feet/sec YDOT = -5626
990539 meter/sec
ZDOT = 12696
996658 ZDOT = 3870
044581
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 16302
47073457
00016717 00000-0 10270-3 0 9118
2 25544 51
6384 113
2686 0006653 118
0434 242
1393 15
54351796 25712
Satellite: ISS
Catalog Number: 25544
Epoch time: 16302
47073457 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 113
2686 deg
Eccentricity:
0006653
Arg of perigee: 118
0434 deg
Mean anomaly: 242
1393 deg
Mean motion: 15
54351796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2571
Checksum: 304
Coasting Arc #13 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2016/303/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -251797
33 A = 6785552
39 meter
Y = -6217162
13 meter E =
0019716
Z = 2681629
09 I = 52
00072
XDOT = 5049
932259 Wp = 108
37168
YDOT = -2469
717286 meter/sec RA = 107
35700 deg
ZDOT = -5226
396983 TA = 41
47936
MA = 41
32988
Ha = 222
837 n
mi
Hp = 212
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -826106
71 X = -195283
23
Y = -20397513
56 feet Y = -6219661
69 meter
Z = 8797995
70 Z = 2680543
66
XDOT = 16568
019221 XDOT = 5102
562143
YDOT = -8102
747000 feet/sec YDOT = -2412
951700 meter/sec
ZDOT = -17146
971729 ZDOT = -5201
737054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8976752
40 X = 2736114
13
Y = 18336417
70 feet Y = 5588940
11 meter
Z = 8794284
64 Z = 2680497
96
XDOT = -10700
795103 XDOT = -3261
602348
YDOT = 13450
304868 feet/sec YDOT = 4099
652924 meter/sec
ZDOT = -17038
573342 ZDOT = -5193
357155
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 16303
49941701
00016717 00000-0 10270-3 0 9128
2 25544 51
6383 108
1386 0006434 121
7517 238
4264 15
54379917 25878
Satellite: ISS
Catalog Number: 25544
Epoch time: 16303
49941701 = yrday
fracday
Element set: 912
Inclination: 51
6383 deg
RA of node: 108
1386 deg
Eccentricity:
0006434
Arg of perigee: 121
7517 deg
Mean anomaly: 238
4264 deg
Mean motion: 15
54379917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2587
Checksum: 320
Coasting Arc #14 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2016/304/00:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4380664
93 A = 6778198
74 meter
Y = 1369872
37 meter E =
0012877
Z = 4980659
56 I = 51
98131
XDOT = 169
779247 Wp = 122
61045
YDOT = -7361
267437 meter/sec RA = 104
59934 deg
ZDOT = 2163
144262 TA = 306
36606
MA = 306
48482
Ha = 223
002 n
mi
Hp = 212
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14372260
26 X = -4419852
12
Y = 4494331
93 feet Y = 1320666
09 meter
Z = 16340746
60 Z = 4959283
57
XDOT = 557
018528 XDOT = 241
574311
YDOT = -24151
139885 feet/sec YDOT = -7358
967263 meter/sec
ZDOT = 7096
929995 ZDOT = 2164
143951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6517465
10 X = -1986523
36
Y = 13687274
54 feet Y = 4171881
28 meter
Z = 16246908
88 Z = 4952057
83
XDOT = -16399
954787 XDOT = -4998
706219
YDOT = -16282
303734 feet/sec YDOT = -4962
846178 meter/sec
ZDOT = 7102
551596 ZDOT = 2164
857726
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 16304
07805106
00016717 00000-0 10270-3 0 9132
2 25544 51
6383 105
2562 0006558 122
5842 237
5945 15
54370727 25965
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
07805106 = yrday
fracday
Element set: 913
Inclination: 51
6383 deg
RA of node: 105
2562 deg
Eccentricity:
0006558
Arg of perigee: 122
5842 deg
Mean anomaly: 237
5945 deg
Mean motion: 15
54370727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 311
Coasting Arc #15 (Orbit 2596)
---------------------------------------
Vector Time (GMT): 2016/304/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4321030
66 A = 6777244
99 meter
Y = 537732
02 meter E =
0010988
Z = 5186728
30 I = 51
98021
XDOT = 769
906335 Wp = 123
79449
YDOT = -7504
508667 meter/sec RA = 104
26844 deg
ZDOT = 1411
339672 TA = 312
66034
MA = 312
75289
Ha = 222
947 n
mi
Hp = 212
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14176609
78 X = -4351918
11
Y = 1764212
67 feet Y = 489239
03 meter
Z = 17016825
14 Z = 5165662
22
XDOT = 2525
939420 XDOT = 846
910591
YDOT = -24621
091427 feet/sec YDOT = -7495
468399 meter/sec
ZDOT = 4630
379501 ZDOT = 1415
267358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2987564
11 X = -910609
54
Y = 14081808
22 feet Y = 4292135
15 meter
Z = 16924484
85 Z = 5158582
98
XDOT = -21435
546460 XDOT = -6533
554561
YDOT = -10167
101581 feet/sec YDOT = -3098
932562 meter/sec
ZDOT = 4648
848418 ZDOT = 1416
968998
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 16304
14234301
00016717 00000-0 10270-3 0 9144
2 25544 51
6397 104
9358 0006476 122
9286 237
2490 15
54391873 25972
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
14234301 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 104
9358 deg
Eccentricity:
0006476
Arg of perigee: 122
9286 deg
Mean anomaly: 237
2490 deg
Mean motion: 15
54391873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2597
Checksum: 320
Coasting Arc #16 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2016/305/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3990975
97 A = 6776799
64 meter
Y = 1367360
94 meter E =
0020505
Z = -5321090
23 I = 51
98625
XDOT = -1710
493903 Wp = 104
25484
YDOT = 7434
004732 meter/sec RA = 99
28865 deg
ZDOT = 624
500584 TA = 171
70655
MA = 171
67261
Ha = 222
812 n
mi
Hp = 212
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13093753
19 X = 4001237
44
Y = 4486092
32 feet Y = 1412047
79 meter
Z = -17457645
12 Z = -5301677
70
XDOT = -5611
856637 XDOT = -1796
529352
YDOT = 24389
779304 feet/sec YDOT = 7414
395823 meter/sec
ZDOT = 2048
886429 ZDOT = 615
981811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8353543
27 X = 2546159
99
Y = -11168819
65 feet Y = -3404256
23 meter
Z = -17372868
29 Z = -5295250
25
XDOT = 20634
967035 XDOT = 6289
537952
YDOT = 12291
767950 feet/sec YDOT = 3746
530871 meter/sec
ZDOT = 2010
304018 ZDOT = 612
740665
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 16305
10672649
00016717 00000-0 10270-3 0 9153
2 25544 51
6404 100
1258 0006485 125
9614 234
2141 15
54364684 26124
Satellite: ISS
Catalog Number: 25544
Epoch time: 16305
10672649 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 100
1258 deg
Eccentricity:
0006485
Arg of perigee: 125
9614 deg
Mean anomaly: 234
2141 deg
Mean motion: 15
54364684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 291
Coasting Arc #17 (Orbit 2627)
---------------------------------------
Vector Time (GMT): 2016/306/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3537179
50 A = 6778812
41 meter
Y = -3179398
42 meter E =
0011480
Z = 4820274
24 I = 51
99805
XDOT = 2541
047999 Wp = 92
33934
YDOT = -6763
908251 meter/sec RA = 94
31313 deg
ZDOT = -2591
900067 TA = 23
05854
MA = 23
00706
Ha = 222
887 n
mi
Hp = 212
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11604919
63 X = -3524779
23
Y = -10431097
19 feet Y = -3218884
01 meter
Z = 15814548
02 Z = 4803121
28
XDOT = 8336
771651 XDOT = 2629
085572
YDOT = -22191
300036 feet/sec YDOT = -6735
000404 meter/sec
ZDOT = -8503
609144 ZDOT = -2579
341841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13404254
02 X = -4085616
62
Y = 8133928
07 feet Y = 2479221
28 meter
Z = 15739983
03 Z = 4797546
83
XDOT = -18162
419307 XDOT = -5535
905405
YDOT = -13553
100041 feet/sec YDOT = -4130
984893 meter/sec
ZDOT = -8447
431843 ZDOT = -2574
777226
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 16306
13539432
00016717 00000-0 10270-3 0 9160
2 25544 51
6411 94
9966 0006466 128
7447 231
4285 15
54377585 26281
Satellite: ISS
Catalog Number: 25544
Epoch time: 16306
13539432 = yrday
fracday
Element set: 916
Inclination: 51
6411 deg
RA of node: 94
9966 deg
Eccentricity:
0006466
Arg of perigee: 128
7447 deg
Mean anomaly: 231
4285 deg
Mean motion: 15
54377585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2628
Checksum: 335
Coasting Arc #18 (Orbit 2642)
---------------------------------------
Vector Time (GMT): 2016/307/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3021895
10 A = 6782543
38 meter
Y = 4747402
20 meter E =
0012000
Z = -3799873
09 I = 52
01180
XDOT = -3257
714255 Wp = 118
09433
YDOT = 5472
543021 meter/sec RA = 89
34619 deg
ZDOT = 4251
144509 TA = 196
66846
MA = 196
70794
Ha = 222
692 n
mi
Hp = 212
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9914354
00 X = 2987042
48
Y = 15575466
54 feet Y = 4781000
09 meter
Z = -12466775
22 Z = -3785277
86
XDOT = -10688
038895 XDOT = -3339
318289
YDOT = 17954
537471 feet/sec YDOT = 5435
656905 meter/sec
ZDOT = 13947
324505 ZDOT = 4235
120578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17732193
44 X = 5404772
56
Y = -5294121
93 feet Y = -1613648
36 meter
Z = -12403694
86 Z = -3780646
19
XDOT = 13885
388500 XDOT = 4232
266415
YDOT = 14033
562162 feet/sec YDOT = 4277
429747 meter/sec
ZDOT = 13876
177272 ZDOT = 4229
458832
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 16307
09976501
00016717 00000-0 10270-3 0 9179
2 25544 51
6408 90
1879 0006420 132
1193 228
0507 15
54381594 26436
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
09976501 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 90
1879 deg
Eccentricity:
0006420
Arg of perigee: 132
1193 deg
Mean anomaly: 228
0507 deg
Mean motion: 15
54381594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2643
Checksum: 309
Coasting Arc #19 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2016/307/03:38:36
527
Vector Time (MET): N/A
Weight (LBS) : 894762
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3927811
81 A = 6780864
55 meter
Y = 2435692
95 meter E =
0014450
Z = -4975163
92 I = 51
99905
XDOT = -1617
310297 Wp = 116
76275
YDOT = 7146
218878 meter/sec RA = 89
05615 deg
ZDOT = 2220
376664 TA = 174
83969
MA = 174
82478
Ha = 222
675 n
mi
Hp = 215
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12886521
67 X = 3924451
19
Y = 7991118
60 feet Y = 2479597
47 meter
Z = -16322716
27 Z = -4956091
31
XDOT = -5306
136145 XDOT = -1707
886861
YDOT = 23445
599993 feet/sec YDOT = 7127
626638 meter/sec
ZDOT = 7284
700340 ZDOT = 2212
299788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6673076
46 X = 2033953
70
Y = -13714822
36 feet Y = -4180277
86 meter
Z = -16239617
67 Z = -4949835
47
XDOT = 22858
989491 XDOT = 6967
419997
YDOT = 2534
573141 feet/sec YDOT = 772
537893 meter/sec
ZDOT = 7248
060362 ZDOT = 2209
208798
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 16307
16405621
00016717 00000-0 10270-3 0 9188
2 25544 51
6425 89
8677 0003252 161
0196 199
1079 15
53479998 26448
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
16405621 = yrday
fracday
Element set: 918
Inclination: 51
6425 deg
RA of node: 89
8677 deg
Eccentricity:
0003252
Arg of perigee: 161
0196 deg
Mean anomaly: 199
1079 deg
Mean motion: 15
53479998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 340
Coasting Arc #20 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/03:38:36
527
Vector Time (MET): N/A
Weight (LBS) : 894762
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3704461
65 A = 6783735
58 meter
Y = -3798742
05 meter E =
0010687
Z = 4217268
23 I = 52
00739
XDOT = 2257
261923 Wp = 92
52453
YDOT = -6325
977883 meter/sec RA = 84
09530 deg
ZDOT = -3707
780945 TA = 35
33442
MA = 35
26364
Ha = 222
723 n
mi
Hp = 215
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12153745
56 X = -3682194
00
Y = -12463064
48 feet Y = -3840043
28 meter
Z = 13836181
87 Z = 4199326
57
XDOT = 7405
714971 XDOT = 2345
844110
YDOT = -20754
520613 feet/sec YDOT = -6300
240414 meter/sec
ZDOT = -12164
635647 ZDOT = -3696
600228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10964897
67 X = -3342100
81
Y = 13600076
23 feet Y = 4145303
23 meter
Z = 13758284
11 Z = 4193525
00
XDOT = -20489
212190 XDOT = -6245
111875
YDOT = -4238
309716 feet/sec YDOT = -1291
836801 meter/sec
ZDOT = -12114
529418 ZDOT = -3692
508566
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 16308
19331672
00016717 00000-0 10270-3 0 9197
2 25544 51
6426 84
7430 0003256 165
4260 194
6987 15
53485501 26607
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19331672 = yrday
fracday
Element set: 919
Inclination: 51
6426 deg
RA of node: 84
7430 deg
Eccentricity:
0003256
Arg of perigee: 165
4260 deg
Mean anomaly: 194
6987 deg
Mean motion: 15
53485501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 318
Coasting Arc #21 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 894762
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3714386
70 A = 6783759
34 meter
Y = 3816572
92 meter E =
0009884
Z = -4212767
86 I = 52
00843
XDOT = -2253
966091 Wp = 125
49675
YDOT = 6301
441026 meter/sec RA = 83
93537 deg
ZDOT = 3722
047450 TA = 182
57841
MA = 182
58351
Ha = 222
532 n
mi
Hp = 215
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12186308
07 X = 3691897
06
Y = 12521564
71 feet Y = 3857983
90 meter
Z = -13821416
87 Z = -4194778
52
XDOT = -7394
901874 XDOT = -2342
343446
YDOT = 20674
019113 feet/sec YDOT = 6275
741557 meter/sec
ZDOT = 12211
441766 ZDOT = 3710
883244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8043639
64 X = 2451701
36
Y = -15580386
43 feet Y = -4748901
78 meter
Z = -13743313
70 Z = -4188962
02
XDOT = 20839
647612 XDOT = 6351
924592
YDOT = 32
953681 feet/sec YDOT = 10
044282 meter/sec
ZDOT = 12161
411701 ZDOT = 3706
798287
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 16308
19331566
00016717 00000-0 10270-3 0 9201
2 25544 51
6436 84
7428 0003176 167
9361 192
1868 15
53492338 26602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19331566 = yrday
fracday
Element set: 920
Inclination: 51
6436 deg
RA of node: 84
7428 deg
Eccentricity:
0003176
Arg of perigee: 167
9361 deg
Mean anomaly: 192
1868 deg
Mean motion: 15
53492338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 327
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