[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 24th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
152/21:55:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
1
153/10:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 216
2
153/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 216
3
155/13:34:21
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
4
156/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
5
Coasting Arc #1 (Orbit 1806)
---------------------------------------
Vector Time (GMT): 2017/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6311018
69 A = 6789757
28 meter
Y = 2437038
05 meter E =
0009633
Z = 543701
37 I = 51
80908
XDOT = -1257
161448 Wp = 71
21813
YDOT = -4611
183812 meter/sec RA = 155
26085 deg
ZDOT = 5992
490912 TA = 294
63193
MA = 294
73224
Ha = 221
841 n
mi
Hp = 215
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20705441
88 X = -6340442
33
Y = 7995531
66 feet Y = 2366299
41 meter
Z = 1783797
15 Z = 512972
42
XDOT = -4124
545433 XDOT = -1234
613780
YDOT = -15128
555814 feet/sec YDOT = -4625
116607 meter/sec
ZDOT = 19660
403255 ZDOT = 5986
438304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2891140
60 X = -881219
66
Y = 22017072
96 feet Y = 6710803
84 meter
Z = 1647903
62 Z = 502281
02
XDOT = -13712
247285 XDOT = -4179
492972
YDOT = -3292
435278 feet/sec YDOT = -1003
534273 meter/sec
ZDOT = 19634
408565 ZDOT = 5984
567731
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 17144
56334412
00016717 00000-0 10270-3 0 9002
2 25544 51
6383 156
0737 0005162 190
1606 169
9443 15
53944016 18074
Satellite: ISS
Catalog Number: 25544
Epoch time: 17144
56334412 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 156
0737 deg
Eccentricity:
0005162
Arg of perigee: 190
1606 deg
Mean anomaly: 169
9443 deg
Mean motion: 15
53944016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1807
Checksum: 300
Coasting Arc #2 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2017/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6228397
55 A = 6788053
74 meter
Y = -1600407
80 meter E =
0010198
Z = -2157068
56 I = 51
83103
XDOT = -542
570401 Wp = 162
43931
YDOT = 5300
505063 meter/sec RA = 150
30179 deg
ZDOT = -5515
532399 TA = 41
42073
MA = 41
34346
Ha = 221
878 n
mi
Hp = 215
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20434375
15 X = 6256309
02
Y = -5250681
76 feet Y = -1530601
37 meter
Z = -7076996
60 Z = -2126744
66
XDOT = -1780
086616 XDOT = -575
009397
YDOT = 17390
108473 feet/sec YDOT = 5294
256842 meter/sec
ZDOT = -18095
578738 ZDOT = -5518
246360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4834502
99 X = 1473556
51
Y = -20582507
77 feet Y = -6273548
37 meter
Z = -6942995
21 Z = -2116224
94
XDOT = 13138
943658 XDOT = 4004
750027
YDOT = 9176
193482 feet/sec YDOT = 2796
903773 meter/sec
ZDOT = -18108
362961 ZDOT = -5519
429031
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 17145
52800275
00016717 00000-0 10270-3 0 9015
2 25544 51
6372 151
2656 0005033 192
5139 167
5889 15
53913304 18224
Satellite: ISS
Catalog Number: 25544
Epoch time: 17145
52800275 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 151
2656 deg
Eccentricity:
0005033
Arg of perigee: 192
5139 deg
Mean anomaly: 167
5889 deg
Mean motion: 15
53913304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 303
Coasting Arc #3 (Orbit 1837)
---------------------------------------
Vector Time (GMT): 2017/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5757810
44 A = 6784700
59 meter
Y = 606704
93 meter E =
0011760
Z = 3533073
25 I = 51
84663
XDOT = 2166
954754 Wp = 115
96557
YDOT = -5807
926272 meter/sec RA = 145
33839 deg
ZDOT = 4512
134675 TA = 285
51964
MA = 285
64946
Ha = 221
629 n
mi
Hp = 215
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18890454
19 X = -5781329
06
Y = 1990501
75 feet Y = 542185
27 meter
Z = 11591447
67 Z = 3505046
06
XDOT = 7109
431608 XDOT = 2209
821346
YDOT = -19054
876219 feet/sec YDOT = -5783
454781 meter/sec
ZDOT = 14803
591453 ZDOT = 4522
764666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6715701
30 X = -2046945
76
Y = 17848361
45 feet Y = 5440180
57 meter
Z = 11467709
68 Z = 3495357
91
XDOT = -12591
696396 XDOT = -3837
949061
YDOT = -14315
464074 feet/sec YDOT = -4363
353450 meter/sec
ZDOT = 14851
387862 ZDOT = 4526
703020
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 17146
55696774
00016717 00000-0 10270-3 0 9027
2 25544 51
6360 146
1378 0005028 199
0779 161
0186 15
53940364 18383
Satellite: ISS
Catalog Number: 25544
Epoch time: 17146
55696774 = yrday
fracday
Element set: 902
Inclination: 51
6360 deg
RA of node: 146
1378 deg
Eccentricity:
0005028
Arg of perigee: 199
0779 deg
Mean anomaly: 161
0186 deg
Mean motion: 15
53940364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1838
Checksum: 334
Coasting Arc #4 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2017/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4954885
41 A = 6781094
51 meter
Y = 584360
48 meter E =
0007661
Z = -4598393
54 I = 51
86110
XDOT = -3550
306213 Wp = 99
01787
YDOT = 6061
235413 meter/sec RA = 140
36632 deg
ZDOT = -3060
801444 TA = 140
48705
MA = 140
43117
Ha = 221
584 n
mi
Hp = 215
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16256185
74 X = 4970319
68
Y = 1917193
18 feet Y = 639856
27 meter
Z = -15086592
98 Z = -4574286
40
XDOT = -11647
986264 XDOT = -3602
952628
YDOT = 19885
942956 feet/sec YDOT = 6021
239527 meter/sec
ZDOT = -10041
999488 ZDOT = -3078
175001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8801146
28 X = 2682589
39
Y = -13916694
91 feet Y = -4241808
61 meter
Z = -14980317
73 Z = -4566000
84
XDOT = 11904
223973 XDOT = 3628
407467
YDOT = 18401
841552 feet/sec YDOT = 5608
881305 meter/sec
ZDOT = -10119
606667 ZDOT = -3084
456112
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 17147
52162211
00016717 00000-0 10270-3 0 9030
2 25544 51
6365 141
3296 0004919 201
1568 158
9382 15
53923475 18537
Satellite: ISS
Catalog Number: 25544
Epoch time: 17147
52162211 = yrday
fracday
Element set: 903
Inclination: 51
6365 deg
RA of node: 141
3296 deg
Eccentricity:
0004919
Arg of perigee: 201
1568 deg
Mean anomaly: 158
9382 deg
Mean motion: 15
53923475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 311
Coasting Arc #5 (Orbit 1868)
---------------------------------------
Vector Time (GMT): 2017/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3934257
65 A = 6778562
86 meter
Y = -1851300
33 meter E =
0007022
Z = 5200410
00 I = 51
87761
XDOT = 4590
625053 Wp = 168
17942
YDOT = -5996
299543 meter/sec RA = 135
38855 deg
ZDOT = 1331
290437 TA = 269
03111
MA = 269
11156
Ha = 221
469 n
mi
Hp = 215
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12907669
45 X = -3938524
71
Y = -6073819
99 feet Y = -1895320
40 meter
Z = 17061712
59 Z = 5181287
87
XDOT = 15061
105816 XDOT = 4650
869266
YDOT = -19672
898763 feet/sec YDOT = -5944
627394 meter/sec
ZDOT = 4367
750777 ZDOT = 1353
735951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10947572
34 X = -3336820
05
Y = 9301199
24 feet Y = 2835005
53 meter
Z = 16977620
83 Z = 5174778
83
XDOT = -10934
727400 XDOT = -3332
904912
YDOT = -21067
530738 feet/sec YDOT = -6421
383369 meter/sec
ZDOT = 4467
749705 ZDOT = 1361
770110
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 17148
55058273
00016717 00000-0 10270-3 0 9047
2 25544 51
6369 136
2017 0004847 206
2161 153
8746 15
53924014 18695
Satellite: ISS
Catalog Number: 25544
Epoch time: 17148
55058273 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 136
2017 deg
Eccentricity:
0004847
Arg of perigee: 206
2161 deg
Mean anomaly: 153
8746 deg
Mean motion: 15
53924014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1869
Checksum: 316
Coasting Arc #6 (Orbit 1883)
---------------------------------------
Vector Time (GMT): 2017/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2777987
42 A = 6778050
47 meter
Y = 3170685
60 meter E =
0013348
Z = -5318668
87 I = 51
89836
XDOT = -5268
403408 Wp = 113
14780
YDOT = 5532
465912 meter/sec RA = 130
40816 deg
ZDOT = 542
378000 TA = 162
03900
MA = 161
99179
Ha = 221
249 n
mi
Hp = 215
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9114131
95 X = 2768161
05
Y = 10402511
82 feet Y = 3201696
62 meter
Z = -17449701
01 Z = -5305197
73
XDOT = -17284
788083 XDOT = -5332
511944
YDOT = 18151
134882 feet/sec YDOT = 5473
192542 meter/sec
ZDOT = 1779
455379 ZDOT = 516
630613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13229693
68 X = 4032410
63
Y = -4278868
40 feet Y = -1304199
09 meter
Z = -17390750
67 Z = -5300700
80
XDOT = 9373
621351 XDOT = 2857
079788
YDOT = 22161
243471 feet/sec YDOT = 6754
747010 meter/sec
ZDOT = 1664
936936 ZDOT = 507
472778
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 17149
51523069
00016717 00000-0 10270-3 0 9055
2 25544 51
6369 131
3946 0004808 210
0043 150
0834 15
53920077 18840
Satellite: ISS
Catalog Number: 25544
Epoch time: 17149
51523069 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 131
3946 deg
Eccentricity:
0004808
Arg of perigee: 210
0043 deg
Mean anomaly: 150
0834 deg
Mean motion: 15
53920077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1884
Checksum: 299
Coasting Arc #7 (Orbit 1899)
---------------------------------------
Vector Time (GMT): 2017/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1599454
45 A = 6779669
98 meter
Y = -4388604
13 meter E =
0002976
Z = 4911131
61 I = 51
92449
XDOT = 5598
856645 Wp = 99
63389
YDOT = -4681
345289 meter/sec RA = 125
43101 deg
ZDOT = -2359
105805 TA = 13
36975
MA = 13
36187
Ha = 221
135 n
mi
Hp = 215
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5247553
98 X = -1574116
93
Y = -14398307
52 feet Y = -4406349
13 meter
Z = 16112636
52 Z = 4903423
06
XDOT = 18368
952247 XDOT = 5662
247937
YDOT = -15358
744388 feet/sec YDOT = -4618
380406 meter/sec
ZDOT = -7739
848443 ZDOT = -2331
754784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15347588
08 X = -4677944
85
Y = -610193
03 feet Y = -185986
83 meter
Z = 16079314
11 Z = 4900974
94
XDOT = -7117
489266 XDOT = -2169
410728
YDOT = -21796
942189 feet/sec YDOT = -6643
707979 meter/sec
ZDOT = -7618
368738 ZDOT = -2322
078791
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 17150
54418682
00016717 00000-0 10270-3 0 9065
2 25544 51
6370 126
2668 0004856 215
1918 144
8915 15
53943661 19000
Satellite: ISS
Catalog Number: 25544
Epoch time: 17150
54418682 = yrday
fracday
Element set: 906
Inclination: 51
6370 deg
RA of node: 126
2668 deg
Eccentricity:
0004856
Arg of perigee: 215
1918 deg
Mean anomaly: 144
8915 deg
Mean motion: 15
53943661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1900
Checksum: 319
Coasting Arc #8 (Orbit 1914)
---------------------------------------
Vector Time (GMT): 2017/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 472305
59 A = 6783007
34 meter
Y = 5433618
47 meter E =
0007002
Z = -4040248
53 I = 51
95456
XDOT = -5599
849937 Wp = 147
68872
YDOT = 3425
150576 meter/sec RA = 120
46170 deg
ZDOT = 3949
162541 TA = 163
21214
MA = 163
18896
Ha = 220
938 n
mi
Hp = 216
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1549559
03 X = 431135
89
Y = 17826832
24 feet Y = 5438670
24 meter
Z = -13255408
58 Z = -4038053
77
XDOT = -18372
211079 XDOT = -5656
917776
YDOT = 11237
370656 feet/sec YDOT = 3362
209853 meter/sec
ZDOT = 12956
570017 ZDOT = 3921
821866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17168573
71 X = 5232981
27
Y = 5066624
32 feet Y = 1544307
09 meter
Z = -13246597
01 Z = -4037562
77
XDOT = 3992
560545 XDOT = 1216
932454
YDOT = 20051
029515 feet/sec YDOT = 6111
553796 meter/sec
ZDOT = 12835
321944 ZDOT = 3912
206129
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 17151
50883001
00016717 00000-0 10270-3 0 9074
2 25544 51
6379 121
4594 0004747 218
8420 141
2392 15
53929399 19159
Satellite: ISS
Catalog Number: 25544
Epoch time: 17151
50883001 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 121
4594 deg
Eccentricity:
0004747
Arg of perigee: 218
8420 deg
Mean anomaly: 141
2392 deg
Mean motion: 15
53929399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1915
Checksum: 317
Coasting Arc #9 (Orbit 1930)
---------------------------------------
Vector Time (GMT): 2017/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 548087
46 A = 6786591
26 meter
Y = -6166601
15 meter E =
0011582
Z = 2763409
17 I = 51
98229
XDOT = 5358
732934 Wp = 120
65839
YDOT = -1845
289432 meter/sec RA = 115
50290 deg
ZDOT = -5170
350602 TA = 28
18490
MA = 28
12226
Ha = 220
779 n
mi
Hp = 216
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1798187
21 X = 603579
97
Y = -20231631
08 feet Y = -6160161
98 meter
Z = 9066303
04 Z = 2766205
97
XDOT = 17581
144798 XDOT = 5404
084248
YDOT = -6054
099186 feet/sec YDOT = -1785
110522 meter/sec
ZDOT = -16963
092525 ZDOT = -5144
209459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18310079
51 X = -5580912
23
Y = -8777875
30 feet Y = -2675496
39 meter
Z = 9079654
06 Z = 2767478
56
XDOT = -51
146799 XDOT = -15
589544
YDOT = -17354
754039 feet/sec YDOT = -5289
729031 meter/sec
ZDOT = -16847
383596 ZDOT = -5135
082520
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 17152
53777981
00016717 00000-0 10270-3 0 9088
2 25544 51
6378 116
3313 0004686 223
6655 136
4127 15
53953263 19313
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
53777981 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 116
3313 deg
Eccentricity:
0004686
Arg of perigee: 223
6655 deg
Mean anomaly: 136
4127 deg
Mean motion: 15
53953263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1931
Checksum: 325
Coasting Arc #10 (Orbit 1936)
---------------------------------------
Vector Time (GMT): 2017/152/21:55:46
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1607471
36 A = 6781717
93 meter
Y = 4921106
37 meter E =
0008489
Z = -4389117
00 I = 51
97068
XDOT = -4973
845675 Wp = 143
69793
YDOT = 4699
165037 meter/sec RA = 113
44584 deg
ZDOT = 3443
855227 TA = 161
11946
MA = 161
08797
Ha = 220
842 n
mi
Hp = 216
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5273856
16 X = 1573643
03
Y = 16145362
09 feet Y = 4938893
34 meter
Z = -14399990
15 Z = -4381390
22
XDOT = -16318
391323 XDOT = -5042
751913
YDOT = 15417
208127 feet/sec YDOT = 4643
158624 meter/sec
ZDOT = 11298
737621 ZDOT = 3419
526693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14274933
32 X = -4350999
68
Y = -9255849
52 feet Y = -2821182
93 meter
Z = -14366680
92 Z = -4378964
34
XDOT = 2497
400299 XDOT = 761
207611
YDOT = -21237
952019 feet/sec YDOT = -6473
327775 meter/sec
ZDOT = 11190
560822 ZDOT = 3410
882939
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 17152
92363534
00016717 00000-0 10270-3 0 9097
2 25544 51
6367 114
4049 0004940 221
2586 138
8194 15
53955079 19379
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
92363534 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 114
4049 deg
Eccentricity:
0004940
Arg of perigee: 221
2586 deg
Mean anomaly: 138
8194 deg
Mean motion: 15
53955079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1937
Checksum: 330
Coasting Arc #11 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2017/153/10:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4574160
81 A = 6780322
14 meter
Y = 1568457
32 meter E =
0007655
Z = 4753003
10 I = 51
97320
XDOT = 417
407157 Wp = 153
94227
YDOT = -7144
519612 meter/sec RA = 110
83778 deg
ZDOT = 2750
970975 TA = 268
91768
MA = 269
00538
Ha = 220
697 n
mi
Hp = 216
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15007089
27 X = -4614447
61
Y = 5145857
35 feet Y = 1517080
40 meter
Z = 15593842
18 Z = 4730685
38
XDOT = 1369
446052 XDOT = 483
905098
YDOT = -23440
024975 feet/sec YDOT = -7139
480240 meter/sec
ZDOT = 9025
495325 ZDOT = 2753
159691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5249567
82 X = -1600068
27
Y = 15073352
21 feet Y = 4594357
75 meter
Z = 15495050
21 Z = 4722891
30
XDOT = -16560
419921 XDOT = -5047
615992
YDOT = -15085
014897 feet/sec YDOT = -4597
912541 meter/sec
ZDOT = 9036
332188 ZDOT = 2754
274051
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 17153
50241731
00016717 00000-0 10270-3 0 9108
2 25544 51
6371 111
5243 0004861 227
4863 132
5880 15
53973485 19460
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
50241731 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 111
5243 deg
Eccentricity:
0004861
Arg of perigee: 227
4863 deg
Mean anomaly: 132
5880 deg
Mean motion: 15
53973485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 302
Coasting Arc #12 (Orbit 1946)
---------------------------------------
Vector Time (GMT): 2017/153/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4301025
88 A = 6778308
19 meter
Y = 197591
35 meter E =
0010519
Z = -5244070
68 I = 51
96915
XDOT = -1756
557914 Wp = 95
44618
YDOT = 7364
881757 meter/sec RA = 110
33372 deg
ZDOT = -1166
150245 TA = 163
42812
MA = 163
39371
Ha = 220
658 n
mi
Hp = 216
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14110977
30 X = 4323969
95
Y = 648265
59 feet Y = 245816
95 meter
Z = -17204956
30 Z = -5223121
79
XDOT = -5762
985282 XDOT = -1833
118789
YDOT = 24162
997891 feet/sec YDOT = 7344
810731 meter/sec
ZDOT = -3825
952248 ZDOT = -1174
868604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1184035
37 X = 360893
98
Y = -14188408
74 feet Y = -4324626
99 meter
Z = -17112497
40 Z = -5215889
21
XDOT = 22893
800223 XDOT = 6978
030308
YDOT = 6560
994033 feet/sec YDOT = 1999
790981 meter/sec
ZDOT = -3865
655684 ZDOT = -1178
251852
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 17153
56672763
00016717 00000-0 10270-3 0 9118
2 25544 51
6387 111
2034 0004738 227
7923 132
2828 15
53958313 19478
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
56672763 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 111
2034 deg
Eccentricity:
0004738
Arg of perigee: 227
7923 deg
Mean anomaly: 132
2828 deg
Mean motion: 15
53958313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1947
Checksum: 320
Coasting Arc #13 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2017/154/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3787762
60 A = 6777947
41 meter
Y = -1864881
00 meter E =
0001887
Z = 5303238
17 I = 51
97928
XDOT = 2551
854819 Wp = 216
83319
YDOT = -7195
976249 meter/sec RA = 105
35945 deg
ZDOT = -709
435167 TA = 239
90197
MA = 239
92068
Ha = 220
533 n
mi
Hp = 216
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12427042
65 X = -3792388
23
Y = -6118375
98 feet Y = -1907264
52 meter
Z = 17399075
35 Z = 5284826
89
XDOT = 8372
227096 XDOT = 2635
578568
YDOT = -23608
845960 feet/sec YDOT = -7166
971507 meter/sec
ZDOT = -2327
543199 ZDOT = -696
836043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6374044
22 X = -1942808
68
Y = 12411644
24 feet Y = 3783069
16 meter
Z = 17318094
13 Z = 5278555
09
XDOT = -22526
064047 XDOT = -6865
944322
YDOT = -8407
344099 feet/sec YDOT = -2562
558481 meter/sec
ZDOT = -2270
717017 ZDOT = -692
114547
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 17154
59567142
00016717 00000-0 10270-3 0 9127
2 25544 51
6394 106
0762 0004802 233
4052 126
6659 15
53976959 19638
Satellite: ISS
Catalog Number: 25544
Epoch time: 17154
59567142 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 106
0762 deg
Eccentricity:
0004802
Arg of perigee: 233
4052 deg
Mean anomaly: 126
6659 deg
Mean motion: 15
53976959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 329
Coasting Arc #14 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2017/155/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3221751
77 A = 6779889
42 meter
Y = 3475721
27 meter E =
0009459
Z = -4856979
14 I = 51
99355
XDOT = -3193
893398 Wp = 130
61746
YDOT = 6489
898059 meter/sec RA = 100
38609 deg
ZDOT = 2522
898249 TA = 164
10377
MA = 164
07406
Ha = 220
308 n
mi
Hp = 216
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10570051
75 X = 3206238
97
Y = 11403285
01 feet Y = 3511662
69 meter
Z = -15934970
94 Z = -4841366
13
XDOT = -10478
652879 XDOT = -3278
482896
YDOT = 21292
316467 feet/sec YDOT = 6453
708634 meter/sec
ZDOT = 8277
225228 ZDOT = 2507
178136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11438239
43 X = 3486375
38
Y = -10634910
57 feet Y = -3241520
74 meter
Z = -15866617
72 Z = -4836145
08
XDOT = 20481
461978 XDOT = 6242
749611
YDOT = 9771
016318 feet/sec YDOT = 2978
205774 meter/sec
ZDOT = 8206
719101 ZDOT = 2501
407982
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 17155
56030368
00016717 00000-0 10270-3 0 9131
2 25544 51
6396 101
2677 0004656 236
2803 123
7906 15
53970591 19789
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
56030368 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 101
2677 deg
Eccentricity:
0004656
Arg of perigee: 236
2803 deg
Mean anomaly: 123
7906 deg
Mean motion: 15
53970591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 324
Coasting Arc #15 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2017/155/13:34:21
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3071811
11 A = 6786959
53 meter
Y = 5453003
37 meter E =
0009406
Z = 2616297
95 I = 52
01730
XDOT = -3371
930151 Wp = 86
85110
YDOT = -4434
671406 meter/sec RA = 100
34355 deg
ZDOT = 5268
161344 TA = 302
44508
MA = 302
53601
Ha = 220
337 n
mi
Hp = 216
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10078120
46 X = -3145268
55
Y = 17890430
99 feet Y = 5418241
38 meter
Z = 8583654
69 Z = 2601197
85
XDOT = -11062
762963 XDOT = -3347
680302
YDOT = -14549
446871 feet/sec YDOT = -4472
243396 meter/sec
ZDOT = 17283
993911 ZDOT = 5251
839961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18839348
19 X = 5742233
33
Y = 8238375
37 feet Y = 2511056
81 meter
Z = 8516060
81 Z = 2595695
33
XDOT = -12719
459239 XDOT = -3876
891176
YDOT = 11239
832184 feet/sec YDOT = 3425
900850 meter/sec
ZDOT = 17212
674503 ZDOT = 5246
423189
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 17155
62461269
00016717 00000-0 10270-3 0 9147
2 25544 51
6397 100
9475 0004652 236
4779 123
5929 15
53962030 19795
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
62461269 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 100
9475 deg
Eccentricity:
0004652
Arg of perigee: 236
4779 deg
Mean anomaly: 123
5929 deg
Mean motion: 15
53962030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 336
Coasting Arc #16 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2017/156/13:34:21
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3490205
88 A = 6783266
31 meter
Y = -4285771
79 meter E =
0002279
Z = -3933879
56 I = 52
01097
XDOT = 2652
070331 Wp = 102
19015
YDOT = 5913
486229 meter/sec RA = 95
38901 deg
ZDOT = -4091
958050 TA = 125
18017
MA = 125
15882
Ha = 220
223 n
mi
Hp = 216
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11450806
68 X = 3556980
20
Y = -14060931
08 feet Y = -4246368
26 meter
Z = -12906429
00 Z = -3916763
18
XDOT = 8701
018147 XDOT = 2605
624046
YDOT = 19401
201540 feet/sec YDOT = 5942
884123 meter/sec
ZDOT = -13425
059220 ZDOT = -4079
187266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15345002
19 X = -4677156
67
Y = -9763488
43 feet Y = -2975911
27 meter
Z = -12830115
64 Z = -3910619
25
XDOT = 17492
830794 XDOT = 5331
814826
YDOT = -9934
696255 feet/sec YDOT = -3028
095418 meter/sec
ZDOT = -13369
678997 ZDOT = -4075
078158
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 17156
58924216
00016717 00000-0 10270-3 0 9150
2 25544 51
6406 96
1405 0004644 240
6448 119
4241 15
53984247 19948
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
58924216 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 96
1405 deg
Eccentricity:
0004644
Arg of perigee: 240
6448 deg
Mean anomaly: 119
4241 deg
Mean motion: 15
53984247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
Checksum: 322
Coasting Arc #17 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2017/156/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1523588
30 A = 6789041
14 meter
Y = 6477083
45 meter E =
0008853
Z = 1326239
30 I = 52
02807
XDOT = -4414
152343 Wp = 58
84637
YDOT = -2242
066997 meter/sec RA = 94
28719 deg
ZDOT = 5854
486479 TA = 315
51073
MA = 315
58179
Ha = 220
136 n
mi
Hp = 216
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4998649
27 X = -1602345
81
Y = 21250273
78 feet Y = 6459605
18 meter
Z = 4351178
80 Z = 1318647
35
XDOT = -14482
127111 XDOT = -4417
191483
YDOT = -7355
862851 feet/sec YDOT = -2291
446542 meter/sec
ZDOT = 19207
632806 ZDOT = 5833
036037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6488806
35 X = 1977788
18
Y = -20850808
89 feet Y = -6355326
55 meter
Z = 4316543
53 Z = 1315682
47
XDOT = 12541
530228 XDOT = 3822
658413
YDOT = 7876
439120 feet/sec YDOT = 2400
738644 meter/sec
ZDOT = 19113
298495 ZDOT = 5825
733381
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 17156
84647444
00016717 00000-0 10270-3 0 9165
2 25544 51
6378 94
8565 0004939 241
0673 118
9985 15
53975613 19980
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
84647444 = yrday
fracday
Element set: 916
Inclination: 51
6378 deg
RA of node: 94
8565 deg
Eccentricity:
0004939
Arg of perigee: 241
0673 deg
Mean anomaly: 118
9985 deg
Mean motion: 15
53975613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1998
Checksum: 369
Coasting Arc #18 (Orbit 2012)
---------------------------------------
Vector Time (GMT): 2017/157/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2173043
38 A = 6786290
80 meter
Y = -5750755
17 meter E =
0004168
Z = -2868221
43 I = 52
02074
XDOT = 4029
443667 Wp = 183
98278
YDOT = 4064
919530 meter/sec RA = 89
33913 deg
ZDOT = -5100
905076 TA = 28
45577
MA = 28
43302
Ha = 220
026 n
mi
Hp = 216
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7129407
42 X = 2251120
93
Y = -18867306
99 feet Y = -5726017
87 meter
Z = -9410175
28 Z = -2857476
27
XDOT = 13219
959539 XDOT = 4008
467223
YDOT = 13336
350165 feet/sec YDOT = 4109
862742 meter/sec
ZDOT = -16735
252873 ZDOT = -5081
381546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8165646
66 X = -2488889
10
Y = 18467145
31 feet Y = 5628785
89 meter
Z = -9361724
24 Z = -2853453
55
XDOT = -11268
218213 XDOT = -3434
552911
YDOT = -13416
881569 feet/sec YDOT = -4089
465502 meter/sec
ZDOT = -16649
747092 ZDOT = -5074
842914
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 17157
81110099
00016717 00000-0 10270-3 0 9175
2 25544 51
6381 90
0486 0004845 245
6184 114
4463 15
53985633 20131
Satellite: ISS
Catalog Number: 25544
Epoch time: 17157
81110099 = yrday
fracday
Element set: 917
Inclination: 51
6381 deg
RA of node: 90
0486 deg
Eccentricity:
0004845
Arg of perigee: 245
6184 deg
Mean anomaly: 114
4463 deg
Mean motion: 15
53985633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2013
Checksum: 310
Coasting Arc #19 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2017/158/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2774510
11 A = 6782614
31 meter
Y = 4621944
87 meter E =
0007056
Z = 4114347
94 I = 52
00718
XDOT = -3573
501779 Wp = 126
36768
YDOT = -5583
000085 meter/sec RA = 84
38200 deg
ZDOT = 3853
345660 TA = 283
97232
MA = 284
05077
Ha = 219
878 n
mi
Hp = 216
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9102723
44 X = -2845973
44
Y = 15163861
12 feet Y = 4590518
35 meter
Z = 13498516
86 Z = 4100697
03
XDOT = -11724
087200 XDOT = -3529
523521
YDOT = -18316
929414 feet/sec YDOT = -5622
715968 meter/sec
ZDOT = 12642
210170 ZDOT = 3836
092615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9715908
14 X = 2961408
80
Y = -14834054
80 feet Y = -4521419
90 meter
Z = 13437416
52 Z = 4095724
56
XDOT = 10076
320125 XDOT = 3071
262374
YDOT = 18009
361945 feet/sec YDOT = 5489
253521 meter/sec
ZDOT = 12567
006296 ZDOT = 3830
423519
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 17158
84003141
00016717 00000-0 10270-3 0 9189
2 25544 51
6381 84
9197 0004949 248
8878 111
1745 15
53992196 20298
Satellite: ISS
Catalog Number: 25544
Epoch time: 17158
84003141 = yrday
fracday
Element set: 918
Inclination: 51
6381 deg
RA of node: 84
9197 deg
Eccentricity:
0004949
Arg of perigee: 248
8878 deg
Mean anomaly: 111
1745 deg
Mean motion: 15
53992196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 341
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