[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 26th 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) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
209/15:41:12
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
3
209/22:00:48
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
4
212/23:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 212
1
216/02:50:00
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
4
219/05:45:00
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
3
221/12:26:03
848 -0
5 0
8 0
8
N/A 0
6 -0
0 222
8
000/00:02:03
697 0
0 -0
0 213
0
Coasting Arc #1 (Orbit 2785)
---------------------------------------
Vector Time (GMT): 2017/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -868076
90 A = 6777281
45 meter
Y = 4176186
38 meter E =
0020755
Z = -5284704
77 I = 51
47650
XDOT = -7274
222968 Wp = 81
41110
YDOT = -2296
414862 meter/sec RA = 201
22386 deg
ZDOT = -618
894159 TA = 182
65042
MA = 182
66144
Ha = 223
105 n
mi
Hp = 212
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2848021
34 X = -889041
61
Y = 13701398
89 feet Y = 4166361
87 meter
Z = -17338270
23 Z = -5288972
35
XDOT = -23865
560918 XDOT = -7244
996995
YDOT = -7534
169494 feet/sec YDOT = -2377
596738 meter/sec
ZDOT = -2030
492647 ZDOT = -654
158452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12932618
05 X = 3941861
98
Y = -5283143
99 feet Y = -1610302
29 meter
Z = -17357734
63 Z = -5290637
51
XDOT = 6500
123386 XDOT = 1981
237608
YDOT = 23104
067965 feet/sec YDOT = 7042
119916 meter/sec
ZDOT = -2186
039888 ZDOT = -666
304958
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 17207
51724625
00016717 00000-0 10270-3 0 9006
2 25544 51
6373 202
2739 0006226 71
9117 288
2714 15
54207307 27863
Satellite: ISS
Catalog Number: 25544
Epoch time: 17207
51724625 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 202
2739 deg
Eccentricity:
0006226
Arg of perigee: 71
9117 deg
Mean anomaly: 288
2714 deg
Mean motion: 15
54207307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2786
Checksum: 303
Coasting Arc #2 (Orbit 2801)
---------------------------------------
Vector Time (GMT): 2017/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2617168
40 A = 6777625
52 meter
Y = -3514706
67 meter E =
0010296
Z = 5163053
02 I = 51
50829
XDOT = 6879
098138 Wp = 66
89464
YDOT = 3122
563315 meter/sec RA = 196
21276 deg
ZDOT = -1355
263904 TA = 36
17829
MA = 36
10869
Ha = 222
976 n
mi
Hp = 212
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8586510
51 X = 2631197
10
Y = -11531189
87 feet Y = -3485361
35 meter
Z = 16939150
32 Z = 5175800
23
XDOT = 22569
219612 XDOT = 6850
252643
YDOT = 10244
630299 feet/sec YDOT = 3199
328798 meter/sec
ZDOT = -4446
403883 ZDOT = -1321
917949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14302427
14 X = -4359379
79
Y = -455823
44 feet Y = -138934
98 meter
Z = 16996003
03 Z = 5180381
72
XDOT = -4387
666462 XDOT = -1337
360738
YDOT = -23383
397956 feet/sec YDOT = -7127
259697 meter/sec
ZDOT = -4299
435594 ZDOT = -1310
467969
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 17208
54601384
00016717 00000-0 10270-3 0 9017
2 25544 51
6368 197
1444 0006160 74
2742 285
9089 15
54227558 28027
Satellite: ISS
Catalog Number: 25544
Epoch time: 17208
54601384 = yrday
fracday
Element set: 901
Inclination: 51
6368 deg
RA of node: 197
1444 deg
Eccentricity:
0006160
Arg of perigee: 74
2742 deg
Mean anomaly: 285
9089 deg
Mean motion: 15
54227558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2802
Checksum: 318
Coasting Arc #3 (Orbit 2816)
---------------------------------------
Vector Time (GMT): 2017/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213437
21 A = 6780382
51 meter
Y = 2820628
94 meter E =
0015390
Z = -4515987
89 I = 51
54883
XDOT = -5886
836052 Wp = 98
09537
YDOT = -3731
742258 meter/sec RA = 191
20950 deg
ZDOT = 3168
797435 TA = 203
77160
MA = 203
84276
Ha = 223
114 n
mi
Hp = 212
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13823612
90 X = -4222728
92
Y = 9254031
95 feet Y = 2773459
51 meter
Z = -14816233
23 Z = -4536477
73
XDOT = -19313
766575 XDOT = -5860
061466
YDOT = -12243
248879 feet/sec YDOT = -3797
423188 meter/sec
ZDOT = 10396
317044 ZDOT = 3140
266377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15501641
52 X = 4724900
34
Y = 5807236
12 feet Y = 1770045
57 meter
Z = -14907221
97 Z = -4543721
26
XDOT = 1703
464067 XDOT = 519
215848
YDOT = 21757
948237 feet/sec YDOT = 6631
822623 meter/sec
ZDOT = 10270
704636 ZDOT = 3130
510773
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 17209
51048344
00016717 00000-0 10270-3 0 9027
2 25544 51
6367 192
3365 0006212 77
3792 282
8055 15
54202531 28171
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
51048344 = yrday
fracday
Element set: 902
Inclination: 51
6367 deg
RA of node: 192
3365 deg
Eccentricity:
0006212
Arg of perigee: 77
3792 deg
Mean anomaly: 282
8055 deg
Mean motion: 15
54202531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2817
Checksum: 302
Coasting Arc #4 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2017/209/15:41:12
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -168752
50 A = 6777198
86 meter
Y = -4271907
30 meter E =
0008742
Z = 5251092
62 I = 51
54583
XDOT = 7595
124570 Wp = 93
06785
YDOT = 729
203901 meter/sec RA = 190
47367 deg
ZDOT = 835
649288 TA = 348
93122
MA = 348
95044
Ha = 222
944 n
mi
Hp = 212
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -553649
93 X = -146477
27
Y = -14015443
91 feet Y = -4273669
92 meter
Z = 17227994
15 Z = 5250326
94
XDOT = 24918
387696 XDOT = 7582
346814
YDOT = 2392
401250 feet/sec YDOT = 814
066291 meter/sec
ZDOT = 2741
631521 ZDOT = 872
512554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 894041
79 X = 272503
94
Y = 14001274
46 feet Y = 4267588
46 meter
Z = 17225213
54 Z = 5250245
09
XDOT = -23914
503379 XDOT = -7289
140630
YDOT = -2052
959998 feet/sec YDOT = -625
742207 meter/sec
ZDOT = 2904
509962 ZDOT = 885
294636
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 17209
70337644
00016717 00000-0 10270-3 0 9033
2 25544 51
6390 191
3754 0005968 77
3790 282
8029 15
54266576 28207
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
70337644 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 191
3754 deg
Eccentricity:
0005968
Arg of perigee: 77
3790 deg
Mean anomaly: 282
8029 deg
Mean motion: 15
54266576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 334
Coasting Arc #5 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2017/209/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3735690
99 A = 6779625
95 meter
Y = -3163294
55 meter E =
0013619
Z = 4681586
34 I = 51
56061
XDOT = 6334
813500 Wp = 70
33178
YDOT = 3286
940622 meter/sec RA = 189
12718 deg
ZDOT = -2822
761807 TA = 47
73230
MA = 47
61689
Ha = 222
875 n
mi
Hp = 212
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12256204
05 X = 3748045
57
Y = -10378262
97 feet Y = -3121450
50 meter
Z = 15359535
25 Z = 4699762
93
XDOT = 20783
508858 XDOT = 6311
298677
YDOT = 10783
925926 feet/sec YDOT = 3357
649367 meter/sec
ZDOT = -9261
029549 ZDOT = -2792
046685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11608087
16 X = 3538144
97
Y = 10985725
70 feet Y = 3348449
19 meter
Z = 15440348
00 Z = 4706218
07
XDOT = -7709
566604 XDOT = -2349
875901
YDOT = 21023
696840 feet/sec YDOT = 6408
022797 meter/sec
ZDOT = -9125
691279 ZDOT = -2781
510702
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 17209
96056728
00016717 00000-0 10270-3 0 9043
2 25544 51
6374 190
0905 0005866 79
1031 281
0782 15
54227568 28247
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
96056728 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 190
0905 deg
Eccentricity:
0005866
Arg of perigee: 79
1031 deg
Mean anomaly: 281
0782 deg
Mean motion: 15
54227568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 324
Coasting Arc #6 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2017/210/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5144423
12 A = 6783290
85 meter
Y = 2521828
92 meter E =
0011495
Z = -3641879
63 I = 51
60497
XDOT = -4974
377118 Wp = 91
95227
YDOT = -3839
215846 meter/sec RA = 184
13259 deg
ZDOT = 4379
784337 TA = 224
85364
MA = 224
94661
Ha = 222
996 n
mi
Hp = 212
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16878028
59 X = -5154550
23
Y = 8273716
92 feet Y = 2464243
93 meter
Z = -11948423
97 Z = -3666893
95
XDOT = -16320
134903 XDOT = -4952
350931
YDOT = -12595
852513 feet/sec YDOT = -3894
719640 meter/sec
ZDOT = 14369
371183 ZDOT = 4355
674006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10279228
98 X = -3133108
99
Y = -15652336
84 feet Y = -4770832
27 meter
Z = -12059389
67 Z = -3675701
97
XDOT = 9335
223842 XDOT = 2845
376227
YDOT = -17090
831238 feet/sec YDOT = -5209
285361 meter/sec
ZDOT = 14263
300400 ZDOT = 4347
453962
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 17210
92503431
00016717 00000-0 10270-3 0 9050
2 25544 51
6370 185
2808 0006019 83
5427 276
6411 15
54236691 28392
Satellite: ISS
Catalog Number: 25544
Epoch time: 17210
92503431 = yrday
fracday
Element set: 905
Inclination: 51
6370 deg
RA of node: 185
2808 deg
Eccentricity:
0006019
Arg of perigee: 83
5427 deg
Mean anomaly: 276
6411 deg
Mean motion: 15
54236691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 306
Coasting Arc #7 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2017/211/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6169491
71 A = 6786876
81 meter
Y = -1798851
82 meter E =
0019425
Z = 2157955
00 I = 51
64960
XDOT = 3189
300277 Wp = 102
48210
YDOT = 4300
958974 meter/sec RA = 179
15188 deg
ZDOT = -5495
192615 TA = 53
56967
MA = 53
39074
Ha = 222
887 n
mi
Hp = 212
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20241114
53 X = 6178666
22
Y = -5901744
83 feet Y = -1729809
14 meter
Z = 7079904
84 Z = 2187946
46
XDOT = 10463
583586 XDOT = 3167
661518
YDOT = 14110
757790 feet/sec YDOT = 4336
503069 meter/sec
ZDOT = -18028
847162 ZDOT = -5479
752537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8674950
78 X = 2644125
00
Y = 19167138
97 feet Y = 5842143
96 meter
Z = 7212792
44 Z = 2198459
14
XDOT = -11088
081024 XDOT = -3379
647096
YDOT = 11822
982254 feet/sec YDOT = 3603
644991 meter/sec
ZDOT = -17961
172214 ZDOT = -5474
565291
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 17211
95379458
00016717 00000-0 10270-3 0 9065
2 25544 51
6368 180
1512 0005888 85
5379 274
6446 15
54268642 28551
Satellite: ISS
Catalog Number: 25544
Epoch time: 17211
95379458 = yrday
fracday
Element set: 906
Inclination: 51
6368 deg
RA of node: 180
1512 deg
Eccentricity:
0005888
Arg of perigee: 85
5379 deg
Mean anomaly: 274
6446 deg
Mean motion: 15
54268642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 350
Coasting Arc #8 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2017/212/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6680936
91 A = 6788886
55 meter
Y = 1072269
32 meter E =
0015573
Z = -492887
47 I = 51
68776
XDOT = -1175
496808 Wp = 59
45245
YDOT = -4638
418861 meter/sec RA = 174
18135 deg
ZDOT = 5991
262502 TA = 295
23491
MA = 295
39625
Ha = 223
042 n
mi
Hp = 212
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21919084
34 X = -6690036
58
Y = 3517943
97 feet Y = 997507
69 meter
Z = -1617084
87 Z = -525363
20
XDOT = -3856
616824 XDOT = -1152
643804
YDOT = -15217
909648 feet/sec YDOT = -4651
436526 meter/sec
ZDOT = 19656
373037 ZDOT = 5985
607667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6919181
18 X = -2108966
42
Y = -21082253
28 feet Y = -6425870
80 meter
Z = -1760874
76 Z = -536714
63
XDOT = 12862
845313 XDOT = 3920
595251
YDOT = -5823
932220 feet/sec YDOT = -1775
134541 meter/sec
ZDOT = 19632
017783 ZDOT = 5983
839020
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 17212
91825970
00016717 00000-0 10270-3 0 9078
2 25544 51
6360 175
3425 0006126 91
8840 268
3014 15
54237558 28701
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
91825970 = yrday
fracday
Element set: 907
Inclination: 51
6360 deg
RA of node: 175
3425 deg
Eccentricity:
0006126
Arg of perigee: 91
8840 deg
Mean anomaly: 268
3014 deg
Mean motion: 15
54237558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 313
Coasting Arc #9 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2655469
31 A = 6779409
47 meter
Y = 4062127
16 meter E =
0017220
Z = -4749968
94 I = 51
65936
XDOT = -7015
296188 Wp = 103
67875
YDOT = -1412
215539 meter/sec RA = 173
89677 deg
ZDOT = 2718
504308 TA = 193
22051
MA = 193
26570
Ha = 223
091 n
mi
Hp = 212
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8712169
67 X = -2677622
90
Y = 13327188
85 feet Y = 4032308
22 meter
Z = -15583887
61 Z = -4762921
93
XDOT = -23016
063610 XDOT = -7012
188088
YDOT = -4633
253082 feet/sec YDOT = -1490
648080 meter/sec
ZDOT = 8918
977387 ZDOT = 2684
433930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15819823
76 X = -4821882
28
Y = -1200900
03 feet Y = -366034
33 meter
Z = -15641752
82 Z = -4767606
26
XDOT = -7036
534478 XDOT = -2144
735709
YDOT = -21331
505512 feet/sec YDOT = -6501
842880 meter/sec
ZDOT = 8768
484664 ZDOT = 2672
634126
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 17212
98255778
00016717 00000-0 10270-3 0 9089
2 25544 51
6375 175
0218 0006201 93
3056 266
8806 15
54236209 28719
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
98255778 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 175
0218 deg
Eccentricity:
0006201
Arg of perigee: 93
3056 deg
Mean anomaly: 266
8806 deg
Mean motion: 15
54236209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 322
Coasting Arc #10 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227268
45 A = 6783182
72 meter
Y = -3797292
35 meter E =
0017765
Z = 3689228
90 I = 51
70439
XDOT = 5890
905378 Wp = 89
23407
YDOT = 2331
183119 meter/sec RA = 168
90828 deg
ZDOT = -4332
331990 TA = 46
83115
MA = 46
68281
Ha = 223
030 n
mi
Hp = 212
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13868990
98 X = 4251496
29
Y = -12458308
22 feet Y = -3749884
88 meter
Z = 12103769
37 Z = 3709822
14
XDOT = 19327
117381 XDOT = 5885
443809
YDOT = 7648
238579 feet/sec YDOT = 2397
028906 meter/sec
ZDOT = -14213
687631 ZDOT = -4303
729193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17633653
89 X = 5374737
71
Y = 5863955
08 feet Y = 1787333
51 meter
Z = 12195403
59 Z = 3717159
02
XDOT = 3338
857168 XDOT = 1017
683665
YDOT = 19381
236398 feet/sec YDOT = 5907
400854 meter/sec
ZDOT = -14087
491564 ZDOT = -4293
867429
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 17214
01131638
00016717 00000-0 10270-3 0 9094
2 25544 51
6376 169
8912 0006174 97
2662 262
9193 15
54224576 28874
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
01131638 = yrday
fracday
Element set: 909
Inclination: 51
6376 deg
RA of node: 169
8912 deg
Eccentricity:
0006174
Arg of perigee: 97
2662 deg
Mean anomaly: 262
9193 deg
Mean motion: 15
54224576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 332
Coasting Arc #11 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2017/214/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5405998
40 A = 6786725
78 meter
Y = 3419663
14 meter E =
0010691
Z = -2270634
43 I = 51
74945
XDOT = -4317
763160 Wp = 73
63737
YDOT = -3225
133658 meter/sec RA = 163
93434 deg
ZDOT = 5446
892875 TA = 261
15084
MA = 261
27191
Ha = 223
050 n
mi
Hp = 212
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17736215
23 X = -5432806
68
Y = 11219367
26 feet Y = 3359059
83 meter
Z = -7449588
01 Z = -2296959
73
XDOT = -14165
889633 XDOT = -4307
836015
YDOT = -10581
147171 feet/sec YDOT = -3273
362626 meter/sec
ZDOT = 17870
383447 ZDOT = 5425
942664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18642733
59 X = -5682305
20
Y = -9546717
03 feet Y = -2909839
35 meter
Z = -7566542
94 Z = -2306282
29
XDOT = 1171
482386 XDOT = 357
067831
YDOT = -16316
320881 feet/sec YDOT = -4973
214604 meter/sec
ZDOT = 17778
154232 ZDOT = 5418
781410
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 17214
97577431
00016717 00000-0 10270-3 0 9106
2 25544 51
6388 165
0831 0006224 99
8134 260
3721 15
54246201 29029
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
97577431 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 165
0831 deg
Eccentricity:
0006224
Arg of perigee: 99
8134 deg
Mean anomaly: 260
3721 deg
Mean motion: 15
54246201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 299
Coasting Arc #12 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2017/215/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6140603
36 A = 6788826
73 meter
Y = -2823933
36 meter E =
0018841
Z = 549096
48 I = 51
78672
XDOT = 2442
152004 Wp = 121
24499
YDOT = 4117
226256 meter/sec RA = 158
97051 deg
ZDOT = -5994
382260 TA = 52
83967
MA = 52
66776
Ha = 223
035 n
mi
Hp = 212
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20146336
47 X = 6169057
74
Y = -9264873
23 feet Y = -2755105
90 meter
Z = 1801497
65 Z = 578994
19
XDOT = 8012
309723 XDOT = 2425
047978
YDOT = 13507
960156 feet/sec YDOT = 4144
440787 meter/sec
ZDOT = -19666
608465 ZDOT = -5982
560488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18415769
24 X = 5613126
46
Y = 12331929
42 feet Y = 3758772
09 meter
Z = 1934193
16 Z = 589542
08
XDOT = -6367
337421 XDOT = -1940
764446
YDOT = 12653
185955 feet/sec YDOT = 3856
691079 meter/sec
ZDOT = -19614
886444 ZDOT = -5978
617388
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 17216
00452833
00016717 00000-0 10270-3 0 9111
2 25544 51
6380 159
9535 0006148 103
9616 256
2220 15
54251976 29181
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
00452833 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 159
9535 deg
Eccentricity:
0006148
Arg of perigee: 103
9616 deg
Mean anomaly: 256
2220 deg
Mean motion: 15
54251976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 306
Coasting Arc #13 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 859529
44 A = 6777159
17 meter
Y = 4156263
18 meter E =
0020600
Z = -5301504
52 I = 51
75388
XDOT = -7257
452829 Wp = 97
58971
YDOT = 2339
149511 meter/sec RA = 158
24266 deg
ZDOT = 656
731658 TA = 178
68578
MA = 178
68036
Ha = 222
979 n
mi
Hp = 212
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2819978
49 X = 838740
89
Y = 13636034
06 feet Y = 4165759
11 meter
Z = -17393387
55 Z = -5297379
49
XDOT = -23810
540778 XDOT = -7286
260469
YDOT = 7674
375036 feet/sec YDOT = 2257
830629 meter/sec
ZDOT = 2154
631424 ZDOT = 621
407842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1614087
68 X = 491973
92
Y = 13852885
38 feet Y = 4222359
46 meter
Z = -17375727
94 Z = -5296121
88
XDOT = -23439
637524 XDOT = -7144
401517
YDOT = 5239
102174 feet/sec YDOT = 1596
878343 meter/sec
ZDOT = 1997
991952 ZDOT = 608
987947
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 17216
13312155
00016717 00000-0 10270-3 0 9128
2 25544 51
6399 159
3154 0005965 103
1679 257
0140 15
54240560 29209
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
13312155 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 159
3154 deg
Eccentricity:
0005965
Arg of perigee: 103
1679 deg
Mean anomaly: 257
0140 deg
Mean motion: 15
54240560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 291
Coasting Arc #14 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 883899
88 A = 6778999
84 meter
Y = -4685015
78 meter E =
0012064
Z = 4809593
87 I = 51
79167
XDOT = 7110
191116 Wp = 81
40241
YDOT = -1311
715427 meter/sec RA = 153
25259 deg
ZDOT = -2577
168375 TA = 33
93216
MA = 33
85505
Ha = 222
847 n
mi
Hp = 212
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2899934
00 X = 912861
01
Y = -15370786
68 feet Y = -4674969
75 meter
Z = 15779507
46 Z = 4813957
59
XDOT = 23327
398675 XDOT = 7136
849041
YDOT = -4303
528304 feet/sec YDOT = -1232
055239 meter/sec
ZDOT = -8455
276822 ZDOT = -2542
565153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3996936
68 X = 1218266
30
Y = -15101793
56 feet Y = -4603026
68 meter
Z = 15799490
01 Z = 4815684
56
XDOT = 22547
172935 XDOT = 6872
378311
YDOT = -2742
944731 feet/sec YDOT = -836
049554 meter/sec
ZDOT = -8301
950187 ZDOT = -2530
434417
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 17217
16187198
00016717 00000-0 10270-3 0 9130
2 25544 51
6410 154
1858 0005864 106
7230 253
4559 15
54288586 29368
Satellite: ISS
Catalog Number: 25544
Epoch time: 17217
16187198 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 154
1858 deg
Eccentricity:
0005864
Arg of perigee: 106
7230 deg
Mean anomaly: 253
4559 deg
Mean motion: 15
54288586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 332
Coasting Arc #15 (Orbit 2950)
---------------------------------------
Vector Time (GMT): 2017/218/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2444844
11 A = 6782631
19 meter
Y = 5047999
56 meter E =
0012289
Z = -3826940
42 I = 51
83205
XDOT = -6402
679921 Wp = 107
40158
YDOT = 77
300598 meter/sec RA = 148
27388 deg
ZDOT = 4199
859138 TA = 206
80141
MA = 206
86496
Ha = 222
918 n
mi
Hp = 212
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8021142
10 X = -2482521
42
Y = 16561678
36 feet Y = 5020449
17 meter
Z = -12555578
81 Z = -3838907
77
XDOT = -21006
167719 XDOT = -6423
468933
YDOT = 253
610887 feet/sec YDOT = 5
585048 meter/sec
ZDOT = 13779
065412 ZDOT = 4168
706994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8942312
06 X = -2725616
72
Y = 16040940
48 feet Y = 4889278
66 meter
Z = -12609272
52 Z = -3843306
26
XDOT = -19901
966790 XDOT = -6066
119478
YDOT = -391
176389 feet/sec YDOT = -119
230563 meter/sec
ZDOT = 13641
169536 ZDOT = 4157
828475
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 17218
12632516
00016717 00000-0 10270-3 0 9147
2 25544 51
6405 149
3779 0006074 109
5120 250
6689 15
54281645 29512
Satellite: ISS
Catalog Number: 25544
Epoch time: 17218
12632516 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 149
3779 deg
Eccentricity:
0006074
Arg of perigee: 109
5120 deg
Mean anomaly: 250
6689 deg
Mean motion: 15
54281645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2951
Checksum: 313
Coasting Arc #16 (Orbit 2966)
---------------------------------------
Vector Time (GMT): 2017/219/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3743560
34 A = 6786419
37 meter
Y = -5122041
39 meter E =
0019739
Z = 2382866
32 I = 51
87204
XDOT = 5289
316009 Wp = 108
10533
YDOT = 1340
978432 meter/sec RA = 143
30758 deg
ZDOT = -5396
609030 TA = 45
34444
MA = 45
18371
Ha = 222
854 n
mi
Hp = 212
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12282022
11 X = 3788983
57
Y = -16804597
74 feet Y = -5079924
45 meter
Z = 7817802
90 Z = 2401161
18
XDOT = 17353
398980 XDOT = 5300
141268
YDOT = 4399
535537 feet/sec YDOT = 1400
187850 meter/sec
ZDOT = -17705
410204 ZDOT = -5370
889363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12963447
03 X = 3951258
66
Y = -16245219
39 feet Y = -4951542
87 meter
Z = 7899525
48 Z = 2407775
37
XDOT = 16072
235536 XDOT = 4898
817391
YDOT = 4222
787417 feet/sec YDOT = 1287
105605 meter/sec
ZDOT = -17591
748845 ZDOT = -5361
965048
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 17219
15507189
00016717 00000-0 10270-3 0 9159
2 25544 51
6407 144
2490 0005990 111
8796 248
2994 15
54284957 29677
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
15507189 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 144
2490 deg
Eccentricity:
0005990
Arg of perigee: 111
8796 deg
Mean anomaly: 248
2994 deg
Mean motion: 15
54284957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2967
Checksum: 350
Coasting Arc #17 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -145338
45 A = 6778783
68 meter
Y = -4700603
81 meter E =
0011765
Z = 4872502
20 I = 51
84878
XDOT = 6746
574882 Wp = 84
01950
YDOT = -2736
473716 meter/sec RA = 142
70606 deg
ZDOT = -2432
466937 TA = 29
77811
MA = 29
71121
Ha = 222
990 n
mi
Hp = 212
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -476832
18 X = -116431
99
Y = -15421928
51 feet Y = -4702067
59 meter
Z = 15985899
61 Z = 4871866
28
XDOT = 22134
432026 XDOT = 6788
488927
YDOT = -8977
932140 feet/sec YDOT = -2660
794506 meter/sec
ZDOT = -7980
534569 ZDOT = -2399
593115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10620144
38 X = -3237020
01
Y = -11195721
17 feet Y = -3412455
81 meter
Z = 15983760
35 Z = 4871850
16
XDOT = 9914
579208 XDOT = 3021
963743
YDOT = -20619
258878 feet/sec YDOT = -6284
750106 meter/sec
ZDOT = -7834
615516 ZDOT = -2387
990809
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 17219
28366508
00016717 00000-0 10270-3 0 9162
2 25544 51
6397 143
6086 0006203 111
1124 249
0692 15
54282769 29690
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
28366508 = yrday
fracday
Element set: 916
Inclination: 51
6397 deg
RA of node: 143
6086 deg
Eccentricity:
0006203
Arg of perigee: 111
1124 deg
Mean anomaly: 249
0692 deg
Mean motion: 15
54282769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 326
Coasting Arc #18 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1336072
62 A = 6782397
32 meter
Y = 5376674
94 meter E =
0012694
Z = -3926250
96 I = 51
88707
XDOT = -6319
168916 Wp = 110
61466
YDOT = 1410
255724 meter/sec RA = 137
73038 deg
ZDOT = 4087
920574 TA = 202
08741
MA = 202
14216
Ha = 222
939 n
mi
Hp = 212
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4383440
35 X = -1377025
32
Y = 17640009
65 feet Y = 5361505
13 meter
Z = -12881400
80 Z = -3932840
47
XDOT = -20732
181482 XDOT = -6354
325817
YDOT = 4626
823243 feet/sec YDOT = 1339
393867 meter/sec
ZDOT = 13411
812908 ZDOT = 4057
139275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8695620
97 X = 2650425
27
Y = 15937321
48 feet Y = 4857695
59 meter
Z = -12911349
13 Z = -3935379
21
XDOT = -11117
511832 XDOT = -3388
617606
YDOT = 16803
869348 feet/sec YDOT = 5121
819377 meter/sec
ZDOT = 13275
332207 ZDOT = 4046
321257
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 17220
24811309
00016717 00000-0 10270-3 0 9175
2 25544 51
6408 138
8007 0006106 114
4192 245
7598 15
54258442 29841
Satellite: ISS
Catalog Number: 25544
Epoch time: 17220
24811309 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 138
8007 deg
Eccentricity:
0006106
Arg of perigee: 114
4192 deg
Mean anomaly: 245
7598 deg
Mean motion: 15
54258442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 310
Coasting Arc #19 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2017/221/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2619202
05 A = 6786156
07 meter
Y = -5724835
79 meter E =
0019704
Z = 2507271
07 I = 51
92250
XDOT = 5520
659654 Wp = 108
38322
YDOT = 179
669101 meter/sec RA = 132
76608 deg
ZDOT = -5328
742372 TA = 43
58051
MA = 43
42502
Ha = 222
870 n
mi
Hp = 212
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8593182
59 X = 2670845
16
Y = -18782269
65 feet Y = -5695257
32 meter
Z = 8225954
94 Z = 2520119
56
XDOT = 18112
400438 XDOT = 5544
124147
YDOT = 589
465554 feet/sec YDOT = 241
536025 meter/sec
ZDOT = -17482
750564 ZDOT = -5301
868261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6666289
71 X = -2031885
10
Y = -19524961
97 feet Y = -5951208
41 meter
Z = 8283671
68 Z = 2524863
13
XDOT = 12244
181637 XDOT = 3732
026563
YDOT = -11586
117821 feet/sec YDOT = -3531
448712 meter/sec
ZDOT = -17363
786096 ZDOT = -5292
482002
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 17221
27685335
00016717 00000-0 10270-3 0 9188
2 25544 51
6399 133
6710 0006119 116
7238 243
4541 15
54290986 30006
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
27685335 = yrday
fracday
Element set: 918
Inclination: 51
6399 deg
RA of node: 133
6710 deg
Eccentricity:
0006119
Arg of perigee: 116
7238 deg
Mean anomaly: 243
4541 deg
Mean motion: 15
54290986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 308
Coasting Arc #20 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2017/221/12:27:05
697
Vector Time (MET): N/A
Weight (LBS) : 902191
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2716787
47 A = 6777441
08 meter
Y = 3227625
43 meter E =
0019671
Z = -5321190
15 I = 51
90015
XDOT = -5365
123488 Wp = 101
38678
YDOT = 5430
753602 meter/sec RA = 131
39666 deg
ZDOT = 552
815591 TA = 173
89133
MA = 173
86731
Ha = 222
825 n
mi
Hp = 213
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8913344
72 X = 2706340
63
Y = 10589322
27 feet Y = 3257947
91 meter
Z = -17457972
94 Z = -5308018
51
XDOT = -17602
111180 XDOT = -5428
138122
YDOT = 17817
433078 feet/sec YDOT = 5370
404813 meter/sec
ZDOT = 1813
699445 ZDOT = 526
600866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1104050
83 X = -336514
69
Y = -13870083
65 feet Y = -4227601
50 meter
Z = -17400118
70 Z = -5303556
18
XDOT = 23704
130176 XDOT = 7225
018878
YDOT = -4023
993292 feet/sec YDOT = -1226
513155 meter/sec
ZDOT = 1696
840079 ZDOT = 517
196856
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 17221
53403967
00016717 00000-0 10270-3 0 9197
2 25544 51
6421 132
3896 0005361 120
8319 239
3361 15
54131571 30049
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
53403967 = yrday
fracday
Element set: 919
Inclination: 51
6421 deg
RA of node: 132
3896 deg
Eccentricity:
0005361
Arg of perigee: 120
8319 deg
Mean anomaly: 239
3361 deg
Mean motion: 15
54131571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 290
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