[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 16th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
233/21:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 212
9
237/07:37:09
920 1
3 4
6 4
6
N/A 4
4 -0
5 219
8
000/00:14:15
840 0
4 -0
0 215
9
239/10:11:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
0
Coasting Arc #1 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2016/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4401789
45 A = 6785802
07 meter
Y = -4912441
54 meter E =
0009694
Z = -1577836
48 I = 51
97477
XDOT = 2700
038624 Wp = 140
97675
YDOT = 4264
975827 meter/sec RA = 121
08061 deg
ZDOT = -5772
661727 TA = 56
20078
MA = 56
10851
Ha = 220
141 n
mi
Hp = 212
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14441566
45 X = 4464058
79
Y = -16116934
19 feet Y = -4862869
60 meter
Z = -5176628
87 Z = -1556302
86
XDOT = 8858
394436 XDOT = 2680
186535
YDOT = 13992
702846 feet/sec YDOT = 4295
058526 meter/sec
ZDOT = -18939
178895 ZDOT = -5759
594013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21224717
23 X = -6469293
81
Y = 4335850
62 feet Y = 1321567
27 meter
Z = -5081699
88 Z = -1548902
12
XDOT = 1427
257441 XDOT = 435
028068
YDOT = -15040
372457 feet/sec YDOT = -4584
305525 meter/sec
ZDOT = -18882
788675 ZDOT = -5755
473988
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 16228
52915288
00016717 00000-0 10270-3 0 9006
2 25544 51
6438 121
9286 0001575 132
5417 227
5869 15
54990865 14218
Satellite: ISS
Catalog Number: 25544
Epoch time: 16228
52915288 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 121
9286 deg
Eccentricity:
0001575
Arg of perigee: 132
5417 deg
Mean anomaly: 227
5869 deg
Mean motion: 15
54990865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 328
Coasting Arc #2 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2016/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672446
96 A = 6782089
06 meter
Y = 3595644
10 meter E =
0013753
Z = 3340837
26 I = 51
97896
XDOT = -1189
764562 Wp = 92
36363
YDOT = -5938
550342 meter/sec RA = 116
12165 deg
ZDOT = 4710
279221 TA = 306
37769
MA = 306
50450
Ha = 220
114 n
mi
Hp = 212
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15329550
39 X = -4728535
12
Y = 11796732
63 feet Y = 3543080
09 meter
Z = 10960752
15 Z = 3318003
88
XDOT = -3903
427041 XDOT = -1146
149818
YDOT = -19483
432880 feet/sec YDOT = -5951
611194 meter/sec
ZDOT = 15453
671986 ZDOT = 4704
605723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19388903
58 X = 5909737
81
Y = -647521
43 feet Y = -197364
53 meter
Z = 10860351
63 Z = 3310235
18
XDOT = -8114
800386 XDOT = -2473
391158
YDOT = 16765
517623 feet/sec YDOT = 5110
129772 meter/sec
ZDOT = 15429
879404 ZDOT = 4703
027242
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 16229
55739162
00016717 00000-0 10270-3 0 9016
2 25544 51
6443 116
7960 0001436 128
6258 231
5024 15
55019547 14375
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
55739162 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 116
7960 deg
Eccentricity:
0001436
Arg of perigee: 128
6258 deg
Mean anomaly: 231
5024 deg
Mean motion: 15
55019547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 305
Coasting Arc #3 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2016/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597035
79 A = 6777550
09 meter
Y = -1780016
81 meter E =
0011028
Z = -4661710
79 I = 51
97732
XDOT = -256
567055 Wp = 76
45119
YDOT = 7063
831666 meter/sec RA = 111
15045 deg
ZDOT = -2953
582863 TA = 164
26365
MA = 164
22935
Ha = 219
942 n
mi
Hp = 212
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15082138
43 X = 4639242
84
Y = -5839950
15 feet Y = -1728373
81 meter
Z = -15294326
73 Z = -4639277
45
XDOT = -841
755430 XDOT = -321
190610
YDOT = 23175
300741 feet/sec YDOT = 7060
601153 meter/sec
ZDOT = -9690
232489 ZDOT = -2954
986317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15815625
85 X = -4820602
76
Y = -3800099
46 feet Y = -1158270
32 meter
Z = -15195972
19 Z = -4631732
32
XDOT = 13509
543550 XDOT = 4117
708874
YDOT = -17490
450164 feet/sec YDOT = -5331
089210 meter/sec
ZDOT = -9697
566101 ZDOT = -2955
818148
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 16230
52135726
00016717 00000-0 10270-3 0 9022
2 25544 51
6441 111
9847 0001324 132
9302 227
1963 15
55054331 14528
Satellite: ISS
Catalog Number: 25544
Epoch time: 16230
52135726 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 111
9847 deg
Eccentricity:
0001324
Arg of perigee: 132
9302 deg
Mean anomaly: 227
1963 deg
Mean motion: 15
55054331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 274
Coasting Arc #4 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2016/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4219149
74 A = 6774864
79 meter
Y = -299465
55 meter E =
0004609
Z = 5289294
92 I = 51
97835
XDOT = 1524
984448 Wp = 124
86450
YDOT = -7478
344116 meter/sec RA = 106
16784 deg
ZDOT = 789
990099 TA = 317
60808
MA = 317
64367
Ha = 220
085 n
mi
Hp = 212
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13842354
79 X = -4241180
05
Y = -982498
54 feet Y = -346769
84 meter
Z = 17353329
79 Z = 5268746
28
XDOT = 5003
229817 XDOT = 1604
658494
YDOT = -24535
249724 feet/sec YDOT = -7460
845199 meter/sec
ZDOT = 2591
831034 ZDOT = 797
591799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11084266
74 X = 3378484
50
Y = 8533618
11 feet Y = 2601046
80 meter
Z = 17263560
96 Z = 5261933
38
XDOT = -17099
506146 XDOT = -5211
929473
YDOT = 16876
998669 feet/sec YDOT = 5144
109194 meter/sec
ZDOT = 2626
334705 ZDOT = 800
506818
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 16231
54958346
00016717 00000-0 10270-3 0 9037
2 25544 51
6434 106
8523 0001432 137
7581 222
3683 15
55053460 14681
Satellite: ISS
Catalog Number: 25544
Epoch time: 16231
54958346 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 106
8523 deg
Eccentricity:
0001432
Arg of perigee: 137
7581 deg
Mean anomaly: 222
3683 deg
Mean motion: 15
55053460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 302
Coasting Arc #5 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2016/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3644777
80 A = 6775329
73 meter
Y = 2436053
15 meter E =
0014697
Z = -5178934
29 I = 51
98792
XDOT = -2586
435510 Wp = 104
66077
YDOT = 7051
860973 meter/sec RA = 101
18149 deg
ZDOT = 1496
702912 TA = 179
70082
MA = 179
69993
Ha = 219
815 n
mi
Hp = 213
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11957932
40 X = 3642422
91
Y = 7992300
36 feet Y = 2476798
00 meter
Z = -16991254
22 Z = -5161235
07
XDOT = -8485
680806 XDOT = -2672
369181
YDOT = 23136
026813 feet/sec YDOT = 7022
457332 meter/sec
ZDOT = 4910
442625 ZDOT = 1483
929721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5864490
25 X = -1787496
63
Y = -13231998
81 feet Y = -4033113
24 meter
Z = -16914304
41 Z = -5155479
98
XDOT = 18671
948333 XDOT = 5691
209852
YDOT = -14479
868559 feet/sec YDOT = -4413
463937 meter/sec
ZDOT = 4853
397665 ZDOT = 1479
315608
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 16232
51353996
00016717 00000-0 10270-3 0 9046
2 25544 51
6431 102
0403 0001257 143
8972 216
2266 15
55074087 14834
Satellite: ISS
Catalog Number: 25544
Epoch time: 16232
51353996 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 102
0403 deg
Eccentricity:
0001257
Arg of perigee: 143
8972 deg
Mean anomaly: 216
2266 deg
Mean motion: 15
55074087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 294
Coasting Arc #6 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2016/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2905585
62 A = 6778670
84 meter
Y = -4353700
74 meter E =
0010210
Z = 4300018
31 I = 52
00501
XDOT = 3448
220831 Wp = 78
56433
YDOT = -5846
096288 meter/sec RA = 96
20214 deg
ZDOT = -3579
933462 TA = 47
77768
MA = 47
69109
Ha = 219
774 n
mi
Hp = 212
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9532761
23 X = -2877572
82
Y = -14283795
08 feet Y = -4386035
99 meter
Z = 14107671
62 Z = 4285972
28
XDOT = 11313
060469 XDOT = 3530
726601
YDOT = -19180
105931 feet/sec YDOT = -5807
074928 meter/sec
ZDOT = -11745
188523 ZDOT = -3562
982282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 713033
34 X = 217332
56
Y = 17207540
16 feet Y = 5244858
24 meter
Z = 14047023
96 Z = 4281532
90
XDOT = -18495
943834 XDOT = -5637
563680
YDOT = 10317
618484 feet/sec YDOT = 3144
810114 meter/sec
ZDOT = -11670
078624 ZDOT = -3557
039964
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 16233
54175252
00016717 00000-0 10270-3 0 9058
2 25544 51
6433 96
9071 0001044 146
8412 213
2807 15
55114694 14998
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
54175252 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 96
9071 deg
Eccentricity:
0001044
Arg of perigee: 146
8412 deg
Mean anomaly: 213
2807 deg
Mean motion: 15
55114694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 300
Coasting Arc #7 (Orbit 1504)
---------------------------------------
Vector Time (GMT): 2016/233/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3859047
22 A = 6775390
91 meter
Y = -2154039
07 meter E =
0004948
Z = 5131848
68 I = 51
99535
XDOT = 1846
031361 Wp = 72
50437
YDOT = -7261
274503 meter/sec RA = 94
31289 deg
ZDOT = -1656
905923 TA = 33
41598
MA = 33
38476
Ha = 219
883 n
mi
Hp = 212
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12660916
09 X = -3859601
39
Y = -7067057
33 feet Y = -2197196
22 meter
Z = 16836773
88 Z = 5113101
46
XDOT = 6056
533335 XDOT = 1935
140001
YDOT = -23823
079079 feet/sec YDOT = -7240
132838 meter/sec
ZDOT = -5436
043055 ZDOT = -1647
721485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3203390
57 X = 976393
45
Y = -14238003
11 feet Y = -4339743
35 meter
Z = 16755196
41 Z = 5106983
87
XDOT = 23537
766833 XDOT = 7174
311331
YDOT = -1063
343979 feet/sec YDOT = -324
107245 meter/sec
ZDOT = -5394
635515 ZDOT = -1644
284905
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 16233
92733159
00016717 00000-0 10270-3 0 9067
2 25544 51
6434 94
9792 0001525 157
2132 202
9089 15
55107408 15056
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
92733159 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 94
9792 deg
Eccentricity:
0001525
Arg of perigee: 157
2132 deg
Mean anomaly: 202
9089 deg
Mean motion: 15
55107408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 307
Coasting Arc #8 (Orbit 1519)
---------------------------------------
Vector Time (GMT): 2016/234/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3348053
57 A = 6779010
39 meter
Y = 4120324
08 meter E =
0009134
Z = -4225055
60 I = 52
00762
XDOT = -2820
809379 Wp = 117
55630
YDOT = 6085
668660 meter/sec RA = 89
33588 deg
ZDOT = 3701
527462 TA = 190
24601
MA = 190
26464
Ha = 219
778 n
mi
Hp = 212
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10984427
72 X = 3322253
55
Y = 13518123
62 feet Y = 4157619
67 meter
Z = -13861730
97 Z = -4208854
73
XDOT = -9254
623948 XDOT = -2906
631489
YDOT = 19966
104528 feet/sec YDOT = 6053
644914 meter/sec
ZDOT = 12144
118969 ZDOT = 3687
615868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9621934
46 X = -2932765
62
Y = 14586095
04 feet Y = 4445841
77 meter
Z = -13791631
98 Z = -4203689
43
XDOT = -20773
672776 XDOT = -6331
815462
YDOT = -2285
745039 feet/sec YDOT = -696
695088 meter/sec
ZDOT = 12082
240324 ZDOT = 3682
666851
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 16234
89127691
00016717 00000-0 10270-3 0 9073
2 25544 51
6421 90
1682 0001660 157
5347 202
5879 15
55102379 15201
Satellite: ISS
Catalog Number: 25544
Epoch time: 16234
89127691 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 90
1682 deg
Eccentricity:
0001660
Arg of perigee: 157
5347 deg
Mean anomaly: 202
5879 deg
Mean motion: 15
55102379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1520
Checksum: 308
Coasting Arc #9 (Orbit 1535)
---------------------------------------
Vector Time (GMT): 2016/235/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2655949
18 A = 6783502
44 meter
Y = -5629393
09 meter E =
0014384
Z = 2678505
92 I = 52
02182
XDOT = 3685
409919 Wp = 107
24077
YDOT = -4236
372889 meter/sec RA = 84
37161 deg
ZDOT = -5230
271968 TA = 42
66251
MA = 42
55090
Ha = 219
764 n
mi
Hp = 212
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8713744
04 X = -2605813
45
Y = -18469137
43 feet Y = -5658813
18 meter
Z = 8787749
09 Z = 2665726
23
XDOT = 12091
239893 XDOT = 3757
914482
YDOT = -13898
861183 feet/sec YDOT = -4194
755141 meter/sec
ZDOT = -17159
684935 ZDOT = -5212
192863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14793344
85 X = 4509011
51
Y = -14112287
20 feet Y = -4301425
14 meter
Z = 8732880
67 Z = 2661782
03
XDOT = 15993
038506 XDOT = 4874
678137
YDOT = 6156
959048 feet/sec YDOT = 1876
641118 meter/sec
ZDOT = -17079
903283 ZDOT = -5205
954521
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 16235
91947879
00016717 00000-0 10270-3 0 9086
2 25544 51
6427 85
0353 0001486 161
4326 198
6882 15
55099194 15368
Satellite: ISS
Catalog Number: 25544
Epoch time: 16235
91947879 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 85
0353 deg
Eccentricity:
0001486
Arg of perigee: 161
4326 deg
Mean anomaly: 198
6882 deg
Mean motion: 15
55099194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1536
Checksum: 348
Coasting Arc #10 (Orbit 1550)
---------------------------------------
Vector Time (GMT): 2016/236/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1823417
28 A = 6786403
84 meter
Y = 6487240
82 meter E =
0009791
Z = -770300
37 I = 52
02702
XDOT = -4388
385003 Wp = 45
93714
YDOT = 1937
483265 meter/sec RA = 79
41942 deg
ZDOT = 5982
538845 TA = 305
77936
MA = 305
87034
Ha = 219
749 n
mi
Hp = 213
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5982340
15 X = 1754481
56
Y = 21283598
49 feet Y = 6507246
01 meter
Z = -2527232
19 Z = -761610
50
XDOT = -14397
588593 XDOT = -4438
784773
YDOT = 6356
572392 feet/sec YDOT = 1888
127939 meter/sec
ZDOT = 19627
752115 ZDOT = 5961
098724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18119392
72 X = -5522790
90
Y = 12674870
30 feet Y = 3863300
47 meter
Z = -2490407
88 Z = -759076
32
XDOT = -9863
696265 XDOT = -3006
454622
YDOT = -10297
681728 feet/sec YDOT = -3138
733391 meter/sec
ZDOT = 19533
680050 ZDOT = 5953
865679
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 16236
88341282
00016717 00000-0 10270-3 0 9090
2 25544 51
6427 80
2233 0001243 161
9967 198
1231 15
55049848 15510
Satellite: ISS
Catalog Number: 25544
Epoch time: 16236
88341282 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 80
2233 deg
Eccentricity:
0001243
Arg of perigee: 161
9967 deg
Mean anomaly: 198
1231 deg
Mean motion: 15
55049848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1551
Checksum: 314
Coasting Arc #11 (Orbit 1557)
---------------------------------------
Vector Time (GMT): 2016/237/07:44:17
840
Vector Time (MET): N/A
Weight (LBS) : 929483
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4286860
41 A = 6780107
81 meter
Y = 2441113
07 meter E =
0007812
Z = -4658887
11 I = 51
99549
XDOT = -779
689125 Wp = 124
38664
YDOT = 7022
796200 meter/sec RA = 77
21734 deg
ZDOT = 2961
538963 TA = 174
99520
MA = 174
98738
Ha = 219
773 n
mi
Hp = 215
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14064502
66 X = 4281875
45
Y = 8008901
15 feet Y = 2489023
52 meter
Z = -15285062
70 Z = -4638074
91
XDOT = -2558
035187 XDOT = -872
547695
YDOT = 23040
669949 feet/sec YDOT = 7013
558134 meter/sec
ZDOT = 9716
335179 ZDOT = 2957
525562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8438277
88 X = 2571987
10
Y = -13910708
98 feet Y = -4239984
10 meter
Z = -15194522
59 Z = -4631290
49
XDOT = 21935
905334 XDOT = 6686
063946
YDOT = 2711
137535 feet/sec YDOT = 826
354721 meter/sec
ZDOT = 9697
524593 ZDOT = 2955
805496
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 16237
33325012
00016717 00000-0 10270-3 0 9106
2 25544 51
6434 77
9781 0003419 254
5833 105
4942 15
54176195 15589
Satellite: ISS
Catalog Number: 25544
Epoch time: 16237
33325012 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 77
9781 deg
Eccentricity:
0003419
Arg of perigee: 254
5833 deg
Mean anomaly: 105
4942 deg
Mean motion: 15
54176195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1558
Checksum: 309
Coasting Arc #12 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2016/238/07:44:17
840
Vector Time (MET): N/A
Weight (LBS) : 929483
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4191897
43 A = 6783907
49 meter
Y = -3960285
65 meter E =
0008778
Z = 3565088
81 I = 51
99967
XDOT = 1786
642658 Wp = 91
67716
YDOT = -5949
434882 meter/sec RA = 72
25443 deg
ZDOT = -4498
896777 TA = 46
46358
MA = 46
39069
Ha = 219
850 n
mi
Hp = 215
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13752944
33 X = -4164618
55
Y = -12993063
14 feet Y = -4007009
61 meter
Z = 11696485
60 Z = 3544792
11
XDOT = 5861
688511 XDOT = 1874
891560
YDOT = -19519
143315 feet/sec YDOT = -5928
962166 meter/sec
ZDOT = -14760
160030 ZDOT = -4490
003217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13177263
68 X = -4016429
97
Y = 13651881
37 feet Y = 4161093
44 meter
Z = 11608479
65 Z = 3538264
60
XDOT = -18442
872182 XDOT = -5621
387441
YDOT = -5258
726404 feet/sec YDOT = -1602
859808 meter/sec
ZDOT = -14720
195883 ZDOT = -4486
715705
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 16238
36205377
00016717 00000-0 10270-3 0 9112
2 25544 51
6431 72
8506 0003440 257
3332 102
7436 15
54166683 15741
Satellite: ISS
Catalog Number: 25544
Epoch time: 16238
36205377 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 72
8506 deg
Eccentricity:
0003440
Arg of perigee: 257
3332 deg
Mean anomaly: 102
7436 deg
Mean motion: 15
54166683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 297
Coasting Arc #13 (Orbit 1588)
---------------------------------------
Vector Time (GMT): 2016/239/07:44:17
840
Vector Time (MET): N/A
Weight (LBS) : 929483
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3925561
31 A = 6787272
16 meter
Y = 5116414
65 meter E =
0004487
Z = -2108141
23 I = 52
00189
XDOT = -2835
775932 Wp = 8
72610
YDOT = 4461
117031 meter/sec RA = 67
29930 deg
ZDOT = 5552
405976 TA = 328
05159
MA = 328
07879
Ha = 219
614 n
mi
Hp = 215
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12879138
16 X = 3878296
87
Y = 16786137
30 feet Y = 5160048
58 meter
Z = -6916473
87 Z = -2089186
91
XDOT = -9303
726810 XDOT = -2912
421502
YDOT = 14636
210733 feet/sec YDOT = 4428
977068 meter/sec
ZDOT = 18216
555041 ZDOT = 5538
444327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16737325
84 X = 5101536
91
Y = -12985953
84 feet Y = -3958118
73 meter
Z = -6834555
04 Z = -2083172
38
XDOT = 13725
841267 XDOT = 4183
636418
YDOT = 8146
299465 feet/sec YDOT = 2482
992077 meter/sec
ZDOT = 18154
697001 ZDOT = 5533
551646
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 16239
32655051
00016717 00000-0 10270-3 0 9128
2 25544 51
6444 68
0418 0003595 262
6540 97
4204 15
54202018 15897
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
32655051 = yrday
fracday
Element set: 912
Inclination: 51
6444 deg
RA of node: 68
0418 deg
Eccentricity:
0003595
Arg of perigee: 262
6540 deg
Mean anomaly: 97
4204 deg
Mean motion: 15
54202018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1589
Checksum: 299
Coasting Arc #14 (Orbit 1590)
---------------------------------------
Vector Time (GMT): 2016/239/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910045
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2163569
92 A = 6789036
10 meter
Y = -6393663
10 meter E =
0009086
Z = -675846
01 I = 52
00520
XDOT = 4685
355012 Wp = 159
76571
YDOT = -955
176589 meter/sec RA = 66
81863 deg
ZDOT = -5995
183692 TA = 27
49724
MA = 27
44920
Ha = 219
608 n
mi
Hp = 215
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7098326
51 X = -2088630
62
Y = -20976584
98 feet Y = -6417438
59 meter
Z = -2217342
56 Z = -686173
84
XDOT = 15371
899647 XDOT = 4724
809600
YDOT = -3133
781459 feet/sec YDOT = -902
561350 meter/sec
ZDOT = -19669
237835 ZDOT = -5972
327742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12493078
87 X = -3807890
44
Y = 18279207
02 feet Y = 5571502
30 meter
Z = -2261312
81 Z = -689248
15
XDOT = -10496
634781 XDOT = -3199
374281
YDOT = -9582
063963 feet/sec YDOT = -2920
613096 meter/sec
ZDOT = -19569
142755 ZDOT = -5964
674712
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 16239
45514915
00016717 00000-0 10270-3 0 9136
2 25544 51
6434 67
4007 0003744 262
8739 97
1988 15
54159822 15914
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
45514915 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 67
4007 deg
Eccentricity:
0003744
Arg of perigee: 262
8739 deg
Mean anomaly: 97
1988 deg
Mean motion: 15
54159822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1591
Checksum: 334
Coasting Arc #15 (Orbit 1606)
---------------------------------------
Vector Time (GMT): 2016/240/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910045
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1266364
48 A = 6786755
52 meter
Y = 6239755
36 meter E =
0010246
Z = 2334767
99 I = 51
98329
XDOT = -5328
043239 Wp = 67
43665
YDOT = -957
243320 meter/sec RA = 61
86888 deg
ZDOT = 5433
047814 TA = 318
47600
MA = 318
55379
Ha = 219
501 n
mi
Hp = 215
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4154739
11 X = 1185154
67
Y = 20471638
31 feet Y = 6253462
68 meter
Z = 7659999
95 Z = 2340722
19
XDOT = -17480
456821 XDOT = -5343
334206
YDOT = -3140
562074 feet/sec YDOT = -1016
910427 meter/sec
ZDOT = 17824
960019 ZDOT = 5407
128704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13612002
77 X = 4148938
44
Y = -15832927
48 feet Y = -4825876
30 meter
Z = 7684869
50 Z = 2342348
22
XDOT = 7197
754275 XDOT = 2193
875503
YDOT = 14808
942802 feet/sec YDOT = 4513
765766 meter/sec
ZDOT = 17711
825940 ZDOT = 5398
564546
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 16240
48393935
00016717 00000-0 10270-3 0 9149
2 25544 51
6421 62
2707 0003738 268
2921 91
7803 15
54214268 16076
Satellite: ISS
Catalog Number: 25544
Epoch time: 16240
48393935 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 62
2707 deg
Eccentricity:
0003738
Arg of perigee: 268
2921 deg
Mean anomaly: 91
7803 deg
Mean motion: 15
54214268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1607
Checksum: 309
Coasting Arc #16 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2016/241/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910045
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -160764
08 A = 6783120
61 meter
Y = -5642567
80 meter E =
0002501
Z = -3764168
32 I = 51
95361
XDOT = 5756
081526 Wp = 54
93762
YDOT = 2693
176695 meter/sec RA = 56
91120 deg
ZDOT = -4283
574421 TA = 169
85081
MA = 169
84576
Ha = 219
524 n
mi
Hp = 215
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -527441
22 X = -79371
08
Y = -18512361
54 feet Y = -5643910
60 meter
Z = -12349633
59 Z = -3764751
37
XDOT = 18884
781908 XDOT = 5746
345384
YDOT = 8835
881546 feet/sec YDOT = 2757
490464 meter/sec
ZDOT = -14053
721855 ZDOT = -4255
636983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14114282
73 X = -4302033
37
Y = 11988989
79 feet Y = 3654244
09 meter
Z = -12351126
30 Z = -3764623
30
XDOT = -4187
465675 XDOT = -1276
339538
YDOT = -19280
639999 feet/sec YDOT = -5876
739072 meter/sec
ZDOT = -13932
089008 ZDOT = -4246
500730
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 16241
44842827
00016717 00000-0 10270-3 0 9156
2 25544 51
6407 57
4628 0003731 272
0202 88
0523 15
54197950 16229
Satellite: ISS
Catalog Number: 25544
Epoch time: 16241
44842827 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 57
4628 deg
Eccentricity:
0003731
Arg of perigee: 272
0202 deg
Mean anomaly: 88
0523 deg
Mean motion: 15
54197950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 299
Coasting Arc #17 (Orbit 1637)
---------------------------------------
Vector Time (GMT): 2016/242/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910045
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1085565
86 A = 6779539
19 meter
Y = 4684848
37 meter E =
0004309
Z = 4777468
26 I = 51
92342
XDOT = -5890
927749 Wp = 136
40588
YDOT = -4109
486657 meter/sec RA = 51
94040 deg
ZDOT = 2686
763615 TA = 287
14278
MA = 287
18996
Ha = 219
644 n
mi
Hp = 215
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3561567
78 X = -1161078
83
Y = 15370237
44 feet Y = 4672286
87 meter
Z = 15674108
46 Z = 4772011
30
XDOT = -19327
190777 XDOT = -5857
587520
YDOT = -13482
567773 feet/sec YDOT = -4175
176402 meter/sec
ZDOT = 8814
841258 ZDOT = 2658
228641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14136453
79 X = 4308791
11
Y = -7061480
44 feet Y = -2152339
24 meter
Z = 15649370
87 Z = 4769928
24
XDOT = 1594
952068 XDOT = 486
141390
YDOT = 22485
926586 feet/sec YDOT = 6853
710423 meter/sec
ZDOT = 8690
865315 ZDOT = 2648
975748
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 16242
47721184
00016717 00000-0 10270-3 0 9163
2 25544 51
6412 52
3329 0003709 277
0559 83
0172 15
54175057 16388
Satellite: ISS
Catalog Number: 25544
Epoch time: 16242
47721184 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 52
3329 deg
Eccentricity:
0003709
Arg of perigee: 277
0559 deg
Mean anomaly: 83
0172 deg
Mean motion: 15
54175057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 305
Coasting Arc #18 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2016/243/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910045
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2423335
03 A = 6777274
25 meter
Y = -3486150
91 meter E =
0011142
Z = -5292244
46 I = 51
89432
XDOT = 5637
897889 Wp = 78
80180
YDOT = 5125
194949 meter/sec RA = 46
95947 deg
ZDOT = -793
806883 TA = 183
62692
MA = 183
63501
Ha = 219
573 n
mi
Hp = 215
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7950574
23 X = 2487844
94
Y = -11437502
98 feet Y = -3458691
22 meter
Z = -17363006
75 Z = -5280315
79
XDOT = 18497
040318 XDOT = 5584
023545
YDOT = 16814
944058 feet/sec YDOT = 5187
940414 meter/sec
ZDOT = -2604
353290 ZDOT = -766
551074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13924453
34 X = -4244173
38
Y = 1403089
22 feet Y = 427661
59 meter
Z = -17310200
69 Z = -5276149
17
XDOT = 676
408566 XDOT = 206
169331
YDOT = -23987
710496 feet/sec YDOT = -7311
454159 meter/sec
ZDOT = -2486
166472 ZDOT = -757
783541
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 16243
44168848
00016717 00000-0 10270-3 0 9174
2 25544 51
6399 47
5233 0003614 279
8517 80
2227 15
54221616 16531
Satellite: ISS
Catalog Number: 25544
Epoch time: 16243
44168848 = yrday
fracday
Element set: 917
Inclination: 51
6399 deg
RA of node: 47
5233 deg
Eccentricity:
0003614
Arg of perigee: 279
8517 deg
Mean anomaly: 80
2227 deg
Mean motion: 15
54221616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 319
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