[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 23rd 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
209/14:48:00
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
3
209/15:41:14
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
209/20:00:20
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
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
214/15:20:50
280 -0
6 0
7 0
7
N/A 0
1 -0
0 223
0
000/00:01:40
559 0
1 -0
0 212
6
216/02:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2017/202/12:49:52
952
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4510652
67 A = 6789076
31 meter
Y = 5059366
16 meter E =
0013906
Z = -330291
06 I = 51
38381
XDOT = -3762
330193 Wp = 111
34885
YDOT = 2977
609931 meter/sec RA = 226
05091 deg
ZDOT = -5978
365194 TA = 72
22251
MA = 72
07082
Ha = 222
988 n
mi
Hp = 212
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14798729
23 X = 4455346
63
Y = 16598970
35 feet Y = 5109498
15 meter
Z = -1083632
08 Z = -308513
68
XDOT = -12343
602994 XDOT = -3766
307381
YDOT = 9769
061455 feet/sec YDOT = 2935
515492 meter/sec
ZDOT = -19614
059034 ZDOT = -5996
650505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2781290
43 X = 847737
32
Y = -22067857
30 feet Y = -6726282
91 meter
Z = -988210
26 Z = -301206
49
XDOT = 13780
173749 XDOT = 4200
196959
YDOT = 2585
144798 feet/sec YDOT = 787
952135 meter/sec
ZDOT = -19695
289975 ZDOT = -6003
124384
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 17202
56626944
00016717 00000-0 10270-3 0 9001
2 25544 51
6379 226
9595 0006168 56
5504 303
6238 15
54200987 27091
Satellite: ISS
Catalog Number: 25544
Epoch time: 17202
56626944 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 226
9595 deg
Eccentricity:
0006168
Arg of perigee: 56
5504 deg
Mean anomaly: 303
6238 deg
Mean motion: 15
54200987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 326
Coasting Arc #2 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2017/203/12:49:52
952
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3685085
18 A = 6787407
55 meter
Y = -5325754
73 meter E =
0019923
Z = 1998016
58 I = 51
40095
XDOT = 5101
094655 Wp = 65
62204
YDOT = -1433
510403 meter/sec RA = 221
06229 deg
ZDOT = 5551
638241 TA = 316
53867
MA = 316
69553
Ha = 222
926 n
mi
Hp = 212
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12090174
49 X = -3634962
52
Y = -17472948
58 feet Y = -5366683
82 meter
Z = 6555172
49 Z = 1980237
02
XDOT = 16735
874854 XDOT = 5089
778762
YDOT = -4703
118119 feet/sec YDOT = -1376
530399 meter/sec
ZDOT = 18214
036223 ZDOT = 5576
389704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4840516
45 X = -1475389
41
Y = 20713735
52 feet Y = 6313546
59 meter
Z = 6477429
96 Z = 1974320
65
XDOT = -13113
242522 XDOT = -3996
916321
YDOT = -8831
381594 feet/sec YDOT = -2691
805110 meter/sec
ZDOT = 18323
606795 ZDOT = 5585
035351
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 17203
59505033
00016717 00000-0 10270-3 0 9011
2 25544 51
6372 221
8306 0006027 59
2335 300
9410 15
54223063 27254
Satellite: ISS
Catalog Number: 25544
Epoch time: 17203
59505033 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 221
8306 deg
Eccentricity:
0006027
Arg of perigee: 59
2335 deg
Mean anomaly: 300
9410 deg
Mean motion: 15
54223063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 269
Coasting Arc #3 (Orbit 2739)
---------------------------------------
Vector Time (GMT): 2017/204/12:49:52
952
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2478449
03 A = 6783973
65 meter
Y = 5262616
88 meter E =
0010974
Z = -3502797
40 I = 51
41429
XDOT = -6196
249523 Wp = 73
85916
YDOT = -71
144836 meter/sec RA = 216
06667 deg
ZDOT = -4499
900647 TA = 147
43594
MA = 147
36820
Ha = 223
050 n
mi
Hp = 212
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8131394
46 X = 2436431
37
Y = 17265803
43 feet Y = 5290097
98 meter
Z = -11492117
44 Z = -3490859
67
XDOT = -20328
902633 XDOT = -6173
135606
YDOT = -233
414815 feet/sec YDOT = -140
305841 meter/sec
ZDOT = -14763
453566 ZDOT = -4529
943336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7012423
00 X = 2137386
53
Y = -17783280
30 feet Y = -5420343
83 meter
Z = -11440156
14 Z = -3486959
59
XDOT = 12344
317225 XDOT = 3762
547890
YDOT = 14431
950059 feet/sec YDOT = 4398
858378 meter/sec
ZDOT = -14896
191853 ZDOT = -4540
359277
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 17204
55953080
00016717 00000-0 10270-3 0 9028
2 25544 51
6369 217
0210 0006190 62
7094 297
4688 15
54199527 27404
Satellite: ISS
Catalog Number: 25544
Epoch time: 17204
55953080 = yrday
fracday
Element set: 902
Inclination: 51
6369 deg
RA of node: 217
0210 deg
Eccentricity:
0006190
Arg of perigee: 62
7094 deg
Mean anomaly: 297
4688 deg
Mean motion: 15
54199527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2740
Checksum: 316
Coasting Arc #4 (Orbit 2755)
---------------------------------------
Vector Time (GMT): 2017/205/12:49:52
952
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1007917
76 A = 6780162
88 meter
Y = -4878726
19 meter E =
0013355
Z = 4588117
62 I = 51
42756
XDOT = 6930
953206 Wp = 93
94436
YDOT = 1389
594131 meter/sec RA = 211
06333 deg
ZDOT = 2991
774161 TA = 326
11024
MA = 326
19550
Ha = 223
031 n
mi
Hp = 212
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3306816
79 X = -975573
95
Y = -16006319
50 feet Y = -4889816
88 meter
Z = 15052879
34 Z = 4583299
80
XDOT = 22739
347790 XDOT = 6900
367043
YDOT = 4559
035864 feet/sec YDOT = 1466
929530 meter/sec
ZDOT = 9815
532025 ZDOT = 3025
367622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9137600
02 X = -2785140
49
Y = 13574257
53 feet Y = 4137433
69 meter
Z = 15032307
75 Z = 4581847
40
XDOT = -11495
372351 XDOT = -3503
789493
YDOT = -18802
871985 feet/sec YDOT = -5731
115381 meter/sec
ZDOT = 9963
785469 ZDOT = 3036
961811
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 17205
58830587
00016717 00000-0 10270-3 0 9039
2 25544 51
6359 211
8918 0006131 64
6780 295
5008 15
54210867 27561
Satellite: ISS
Catalog Number: 25544
Epoch time: 17205
58830587 = yrday
fracday
Element set: 903
Inclination: 51
6359 deg
RA of node: 211
8918 deg
Eccentricity:
0006131
Arg of perigee: 64
6780 deg
Mean anomaly: 295
5008 deg
Mean motion: 15
54210867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2756
Checksum: 324
Coasting Arc #5 (Orbit 2770)
---------------------------------------
Vector Time (GMT): 2017/206/12:49:52
952
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -665666
56 A = 6777598
99 meter
Y = 4299970
62 meter E =
0020224
Z = -5214300
14 I = 51
44766
XDOT = -7148
500178 Wp = 77
65765
YDOT = -2486
018786 meter/sec RA = 206
05217 deg
ZDOT = -1137
015077 TA = 181
38851
MA = 181
39413
Ha = 223
071 n
mi
Hp = 212
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2183945
40 X = -688372
54
Y = 14107515
16 feet Y = 4292399
96 meter
Z = -17107283
92 Z = -5217588
63
XDOT = -23453
084575 XDOT = -7114
646635
YDOT = -8156
229614 feet/sec YDOT = -2565
768834 meter/sec
ZDOT = -3730
364425 ZDOT = -1171
657392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11435433
03 X = 3485519
99
Y = -8514901
69 feet Y = -2595342
04 meter
Z = -17122443
91 Z = -5218920
90
XDOT = 10188
454333 XDOT = 3105
440881
YDOT = 21494
702106 feet/sec YDOT = 6551
585202 meter/sec
ZDOT = -3883
114766 ZDOT = -1183
573381
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 17206
55278098
00016717 00000-0 10270-3 0 9041
2 25544 51
6361 207
0830 0006180 68
8435 291
3378 15
54207199 27716
Satellite: ISS
Catalog Number: 25544
Epoch time: 17206
55278098 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 207
0830 deg
Eccentricity:
0006180
Arg of perigee: 68
8435 deg
Mean anomaly: 291
3378 deg
Mean motion: 15
54207199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2771
Checksum: 321
Coasting Arc #6 (Orbit 2786)
---------------------------------------
Vector Time (GMT): 2017/207/12:49:52
952
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2382028
79 A = 6777271
50 meter
Y = -3558368
71 meter E =
0009281
Z = 5246069
68 I = 51
47729
XDOT = 6854
929959 Wp = 68
41968
YDOT = 3349
700223 meter/sec RA = 201
03887 deg
ZDOT = -835
932177 TA = 29
60872
MA = 29
55621
Ha = 222
950 n
mi
Hp = 212
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7815055
09 X = 2396160
04
Y = -11674438
03 feet Y = -3531652
36 meter
Z = 17211514
69 Z = 5257674
84
XDOT = 22489
927688 XDOT = 6821
023726
YDOT = 10989
830127 feet/sec YDOT = 3426
167146 meter/sec
ZDOT = -2742
559637 ZDOT = -802
715979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13648509
00 X = -4160065
54
Y = 3049534
89 feet Y = 929498
24 meter
Z = 17263324
31 Z = 5261861
25
XDOT = -8339
466245 XDOT = -2541
869312
YDOT = -22542
988395 feet/sec YDOT = -6871
102863 meter/sec
ZDOT = -2596
216236 ZDOT = -791
326709
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
58155047
00016717 00000-0 10270-3 0 9054
2 25544 51
6367 201
9534 0006102 71
7255 288
4561 15
54224463 27874
Satellite: ISS
Catalog Number: 25544
Epoch time: 17207
58155047 = yrday
fracday
Element set: 905
Inclination: 51
6367 deg
RA of node: 201
9534 deg
Eccentricity:
0006102
Arg of perigee: 71
7255 deg
Mean anomaly: 288
4561 deg
Mean motion: 15
54224463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2787
Checksum: 312
Coasting Arc #7 (Orbit 2801)
---------------------------------------
Vector Time (GMT): 2017/208/12:49:52
952
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3988951
85 A = 6779484
19 meter
Y = 2776185
10 meter E =
0016652
Z = -4741995
01 I = 51
51579
XDOT = -5967
761105 Wp = 96
99519
YDOT = -3956
367468 meter/sec RA = 196
03130 deg
ZDOT = 2710
031205 TA = 199
85818
MA = 199
92308
Ha = 223
089 n
mi
Hp = 212
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13087112
38 X = -3996665
52
Y = 9108218
82 feet Y = 2731534
86 meter
Z = -15557726
42 Z = -4761390
49
XDOT = -19579
268718 XDOT = -5936
240212
YDOT = -12980
208229 feet/sec YDOT = -4022
926819 meter/sec
ZDOT = 8891
178495 ZDOT = 2681
118654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15707426
67 X = 4787623
65
Y = 2195739
42 feet Y = 669261
38 meter
Z = -15643864
22 Z = -4768249
81
XDOT = 5669
286430 XDOT = 1727
998504
YDOT = 21739
727847 feet/sec YDOT = 6626
269048 meter/sec
ZDOT = 8763
927235 ZDOT = 2671
245021
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
54601899
00016717 00000-0 10270-3 0 9063
2 25544 51
6371 197
1451 0006196 74
2665 285
9171 15
54208627 28020
Satellite: ISS
Catalog Number: 25544
Epoch time: 17208
54601899 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 197
1451 deg
Eccentricity:
0006196
Arg of perigee: 74
2665 deg
Mean anomaly: 285
9171 deg
Mean motion: 15
54208627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2802
Checksum: 327
Coasting Arc #8 (Orbit 2817)
---------------------------------------
Vector Time (GMT): 2017/209/12:49:52
952
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5346839
85 A = 6783131
90 meter
Y = -1936817
38 meter E =
0017761
Z = 3684277
64 I = 51
55958
XDOT = 4580
007254 Wp = 82
39055
YDOT = 4386
947031 meter/sec RA = 191
03404 deg
ZDOT = -4320
398670 TA = 53
64689
MA = 53
48310
Ha = 222
942 n
mi
Hp = 212
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17542125
49 X = 5350204
29
Y = -6354387
72 feet Y = -1877006
61 meter
Z = 12087525
06 Z = 3710258
74
XDOT = 15026
270518 XDOT = 4551
596963
YDOT = 14392
870836 feet/sec YDOT = 4438
004980 meter/sec
ZDOT = -14174
536318 ZDOT = -4298
219660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17226554
84 X = -5250653
91
Y = -6968027
16 feet Y = -2123854
68 meter
Z = 12202666
84 Z = 3719372
85
XDOT = -2107
959652 XDOT = -642
506102
YDOT = -19555
758201 feet/sec YDOT = -5960
595100 meter/sec
ZDOT = -14077
099769 ZDOT = -4290
700009
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
57478301
00016717 00000-0 10270-3 0 9078
2 25544 51
6368 192
0158 0006105 77
4529 282
7306 15
54240445 28184
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
57478301 = yrday
fracday
Element set: 907
Inclination: 51
6368 deg
RA of node: 192
0158 deg
Eccentricity:
0006105
Arg of perigee: 77
4529 deg
Mean anomaly: 282
7306 deg
Mean motion: 15
54240445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2818
Checksum: 316
Coasting Arc #9 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2017/209/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3163345
08 A = 6780994
14 meter
Y = 4125352
02 meter E =
0014806
Z = -4368767
72 I = 51
55657
XDOT = -6681
367353 Wp = 73
27482
YDOT = 1505
055882 meter/sec RA = 190
67424 deg
ZDOT = -3422
123972 TA = 161
95321
MA = 161
90059
Ha = 223
051 n
mi
Hp = 212
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10378428
73 X = 3138200
26
Y = 13534619
49 feet Y = 4160586
15 meter
Z = -14333227
44 Z = -4353462
40
XDOT = -21920
496565 XDOT = -6681
077928
YDOT = 4937
847381 feet/sec YDOT = 1430
341947 meter/sec
ZDOT = -11227
440854 ZDOT = -3454
578849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7320196
10 X = -2231195
77
Y = -15467094
36 feet Y = -4714370
36 meter
Z = -14266143
04 Z = -4348320
40
XDOT = 21269
142362 XDOT = 6482
834592
YDOT = 405
444082 feet/sec YDOT = 123
579356 meter/sec
ZDOT = -11371
144363 ZDOT = -3465
924802
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
63908114
00016717 00000-0 10270-3 0 9086
2 25544 51
6386 191
6952 0006155 77
5438 282
6403 15
54245131 28191
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
63908114 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 191
6952 deg
Eccentricity:
0006155
Arg of perigee: 77
5438 deg
Mean anomaly: 282
6403 deg
Mean motion: 15
54245131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 321
Coasting Arc #10 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2017/209/15:41:14
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -154485
05 A = 6777175
02 meter
Y = -4270533
57 meter E =
0008709
Z = 5252650
15 I = 51
54583
XDOT = 7595
491970 Wp = 93
31354
YDOT = 739
548121 meter/sec RA = 190
47406 deg
ZDOT = 822
989615 TA = 348
80728
MA = 348
82664
Ha = 222
925 n
mi
Hp = 212
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -506840
70 X = -132233
80
Y = -14010936
91 feet Y = -4272136
77 meter
Z = 17233104
17 Z = 5251953
72
XDOT = 24919
593079 XDOT = 7582
660009
YDOT = 2426
338980 feet/sec YDOT = 824
414317 meter/sec
ZDOT = 2700
097163 ZDOT = 859
854535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 849241
40 X = 258848
78
Y = 13997403
87 feet Y = 4266408
70 meter
Z = 17230629
53 Z = 5251895
88
XDOT = -23917
108663 XDOT = -7289
934720
YDOT = -2079
961734 feet/sec YDOT = -633
972337 meter/sec
ZDOT = 2862
981448 ZDOT = 872
636745
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
70337756
00016717 00000-0 10270-3 0 9093
2 25544 51
6390 191
3758 0005935 77
8849 282
2969 15
54272239 28205
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
70337756 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 191
3758 deg
Eccentricity:
0005935
Arg of perigee: 77
8849 deg
Mean anomaly: 282
2969 deg
Mean motion: 15
54272239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 352
Coasting Arc #11 (Orbit 2822)
---------------------------------------
Vector Time (GMT): 2017/209/20:00:20
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6481982
78 A = 6788661
00 meter
Y = -1791598
39 meter E =
0018931
Z = 867979
57 I = 51
59052
XDOT = 2029
025788 Wp = 61
80372
YDOT = -4425
020380 meter/sec RA = 189
57714 deg
ZDOT = 5929
076940 TA = 307
59812
MA = 307
76984
Ha = 222
940 n
mi
Hp = 212
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21266347
70 X = -6465683
07
Y = -5877947
46 feet Y = -1863993
20 meter
Z = 2847701
99 Z = 836532
05
XDOT = 6656
908754 XDOT = 2049
556537
YDOT = -14517
783398 feet/sec YDOT = -4402
215710 meter/sec
ZDOT = 19452
352165 ZDOT = 5938
983012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14058975
74 X = 4285175
81
Y = -17027160
52 feet Y = -5189878
53 meter
Z = 2708915
48 Z = 825677
44
XDOT = 9341
264442 XDOT = 2847
217402
YDOT = 10863
971961 feet/sec YDOT = 3311
338654 meter/sec
ZDOT = 19496
775955 ZDOT = 5942
617311
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
89626931
00016717 00000-0 10270-3 0 9101
2 25544 51
6397 190
4142 0005927 78
5958 281
5860 15
54260815 28231
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
89626931 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 190
4142 deg
Eccentricity:
0005927
Arg of perigee: 78
5958 deg
Mean anomaly: 281
5860 deg
Mean motion: 15
54260815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2823
Checksum: 336
Coasting Arc #12 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2017/210/20:00:20
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5773710
33 A = 6786350
91 meter
Y = 2494002
14 meter E =
0010099
Z = -2553556
24 I = 51
61484
XDOT = -3993
767253 Wp = 105
02860
YDOT = 3868
375870 meter/sec RA = 184
60073 deg
ZDOT = -5271
930179 TA = 103
65171
MA = 103
53923
Ha = 222
987 n
mi
Hp = 212
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18942619
20 X = 5757796
43
Y = 8182421
71 feet Y = 2558478
76 meter
Z = -8377809
17 Z = -2525548
21
XDOT = -13102
910935 XDOT = -4011
119426
YDOT = 12691
521882 feet/sec YDOT = 3823
617926 meter/sec
ZDOT = -17296
358855 ZDOT = -5291
372550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14984617
07 X = -4567311
28
Y = 14257982
74 feet Y = 4345833
14 meter
Z = -8254314
83 Z = -2515915
16
XDOT = -5529
913855 XDOT = -1685
517743
YDOT = -15836
590980 feet/sec YDOT = -4826
992931 meter/sec
ZDOT = -17382
875263 ZDOT = -5298
300380
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
86073212
00016717 00000-0 10270-3 0 9119
2 25544 51
6398 185
6051 0005808 81
4375 278
7435 15
54228351 28382
Satellite: ISS
Catalog Number: 25544
Epoch time: 17210
86073212 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 185
6051 deg
Eccentricity:
0005808
Arg of perigee: 81
4375 deg
Mean anomaly: 278
7435 deg
Mean motion: 15
54228351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 315
Coasting Arc #13 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2017/211/20:00:20
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4603745
60 A = 6782635
35 meter
Y = -3065935
55 meter E =
0017069
Z = 3911767
59 I = 51
63404
XDOT = 5636
924468 Wp = 94
13037
YDOT = -3256
123629 meter/sec RA = 179
61693 deg
ZDOT = 4065
523577 TA = 313
29808
MA = 313
44031
Ha = 223
110 n
mi
Hp = 212
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15104152
23 X = -4588120
63
Y = -10058843
68 feet Y = -3117330
51 meter
Z = 12833883
17 Z = 3889442
07
XDOT = 18493
846679 XDOT = 5653
168198
YDOT = -10682
820306 feet/sec YDOT = -3192
997001 meter/sec
ZDOT = 13338
331946 ZDOT = 4092
945148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15039484
21 X = 4584034
79
Y = -10278282
88 feet Y = -3132820
62 meter
Z = 12735584
94 Z = 3881806
29
XDOT = 2208
881462 XDOT = 673
267070
YDOT = 19977
716548 feet/sec YDOT = 6089
208004 meter/sec
ZDOT = 13460
058779 ZDOT = 4102
625916
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
88948846
00016717 00000-0 10270-3 0 9127
2 25544 51
6388 180
4750 0005970 84
1007 276
0826 15
54229812 28548
Satellite: ISS
Catalog Number: 25544
Epoch time: 17211
88948846 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 180
4750 deg
Eccentricity:
0005970
Arg of perigee: 84
1007 deg
Mean anomaly: 276
0826 deg
Mean motion: 15
54229812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2854
Checksum: 329
Coasting Arc #14 (Orbit 2868)
---------------------------------------
Vector Time (GMT): 2017/212/20:00:20
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3045551
75 A = 6778959
01 meter
Y = 3597525
69 meter E =
0017550
Z = -4888220
24 I = 51
65305
XDOT = -6817
479655 Wp = 78
45841
YDOT = 2536
314787 meter/sec RA = 174
62509 deg
ZDOT = -2384
770607 TA = 168
15723
MA = 168
11591
Ha = 222
971 n
mi
Hp = 212
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9991967
70 X = 3028841
31
Y = 11802905
80 feet Y = 3631489
87 meter
Z = -16037467
97 Z = -4873466
45
XDOT = -22367
059237 XDOT = -6833
750755
YDOT = 8321
242740 feet/sec YDOT = 2459
986213 meter/sec
ZDOT = -7824
050547 ZDOT = -2417
926974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14649715
16 X = -4465233
18
Y = 5158136
79 feet Y = 1572200
09 meter
Z = -15972722
16 Z = -4868485
72
XDOT = 668
303707 XDOT = 203
698970
YDOT = -22746
030205 feet/sec YDOT = -6932
990006 meter/sec
ZDOT = -7971
056139 ZDOT = -2429
577911
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
85394375
00016717 00000-0 10270-3 0 9138
2 25544 51
6373 175
6661 0005905 88
9799 271
2030 15
54250213 28696
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
85394375 = yrday
fracday
Element set: 913
Inclination: 51
6373 deg
RA of node: 175
6661 deg
Eccentricity:
0005905
Arg of perigee: 88
9799 deg
Mean anomaly: 271
2030 deg
Mean motion: 15
54250213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2869
Checksum: 328
Coasting Arc #15 (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 = -2666528
08 A = 6779389
85 meter
Y = 4059848
94 meter E =
0017171
Z = -4745654
89 I = 51
65944
XDOT = -7010
007113 Wp = 103
92736
YDOT = -1420
365636 meter/sec RA = 173
89710 deg
ZDOT = 2727
997711 TA = 193
07368
MA = 193
11824
Ha = 223
058 n
mi
Hp = 212
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8748451
71 X = -2688676
32
Y = 13319714
38 feet Y = 4029906
37 meter
Z = -15569733
90 Z = -4758661
59
XDOT = -22998
711002 XDOT = -7006
854384
YDOT = -4659
992244 feet/sec YDOT = -1498
738782 meter/sec
ZDOT = 8950
123723 ZDOT = 2693
953134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15830628
28 X = -4825175
50
Y = -1236427
14 feet Y = -376862
99 meter
Z = -15627836
33 Z = -4763364
51
XDOT = -7007
445203 XDOT = -2135
869298
YDOT = -21328
419223 feet/sec YDOT = -6500
902179 meter/sec
ZDOT = 8799
746269 ZDOT = 2682
162663
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
98253952
00016717 00000-0 10270-3 0 9148
2 25544 51
6375 175
0220 0006168 93
8960 266
2897 15
54248768 28710
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
98253952 = yrday
fracday
Element set: 914
Inclination: 51
6375 deg
RA of node: 175
0220 deg
Eccentricity:
0006168
Arg of perigee: 93
8960 deg
Mean anomaly: 266
2897 deg
Mean motion: 15
54248768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 342
Coasting Arc #16 (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 = 4240861
24 A = 6783170
66 meter
Y = -3791830
10 meter E =
0017750
Z = 3679177
95 I = 51
70452
XDOT = 5878
347627 Wp = 89
54773
YDOT = 2342
498290 meter/sec RA = 168
90858 deg
ZDOT = -4343
320204 TA = 46
66755
MA = 46
51974
Ha = 222
992 n
mi
Hp = 212
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13913586
76 X = 4265075
82
Y = -12440387
47 feet Y = -3744270
70 meter
Z = 12070793
79 Z = 3699837
18
XDOT = 19285
917411 XDOT = 5872
813838
YDOT = 7685
361845 feet/sec YDOT = 2408
203244 meter/sec
ZDOT = -14249
738203 ZDOT = -4314
778583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17640134
33 X = 5376712
94
Y = 5911778
29 feet Y = 1801910
02 meter
Z = 12162719
18 Z = 3707196
81
XDOT = 3289
862160 XDOT = 1002
749986
YDOT = 19363
400721 feet/sec YDOT = 5901
964540 meter/sec
ZDOT = -14123
814358 ZDOT = -4304
938616
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
01128900
00016717 00000-0 10270-3 0 9159
2 25544 51
6376 169
8914 0006140 97
8883 262
2967 15
54239517 28873
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
01128900 = yrday
fracday
Element set: 915
Inclination: 51
6376 deg
RA of node: 169
8914 deg
Eccentricity:
0006140
Arg of perigee: 97
8883 deg
Mean anomaly: 262
2967 deg
Mean motion: 15
54239517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 336
Coasting Arc #17 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2017/214/15:21:40
559
Vector Time (MET): N/A
Weight (LBS) : 902208
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -240723
50 A = 6777704
99 meter
Y = 4324916
67 meter E =
0019728
Z = -5230254
18 I = 51
70986
XDOT = -7501
533706 Wp = 97
82902
YDOT = 982
033503 meter/sec RA = 165
59866 deg
ZDOT = 1158
431676 TA = 183
28297
MA = 183
29593
Ha = 222
975 n
mi
Hp = 212
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -789775
25 X = -263662
21
Y = 14189359
14 feet Y = 4322096
76 meter
Z = -17159626
58 Z = -5231479
01
XDOT = -24611
331055 XDOT = -7517
584574
YDOT = 3221
894695 feet/sec YDOT = 898
056446 meter/sec
ZDOT = 3800
628859 ZDOT = 1121
952975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 438431
75 X = 133634
00
Y = -14197265
31 feet Y = -4327326
47 meter
Z = -17165659
83 Z = -5232093
12
XDOT = 23542
669267 XDOT = 7175
805592
YDOT = -3668
488414 feet/sec YDOT = -1118
155269 meter/sec
ZDOT = 3639
107871 ZDOT = 1109
200079
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
65425443
00016717 00000-0 10270-3 0 9162
2 25544 51
6409 166
6910 0005504 94
4224 265
7557 15
54150308 28970
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
65425443 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 166
6910 deg
Eccentricity:
0005504
Arg of perigee: 94
4224 deg
Mean anomaly: 265
7557 deg
Mean motion: 15
54150308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2897
Checksum: 316
Coasting Arc #18 (Orbit 2912)
---------------------------------------
Vector Time (GMT): 2017/215/15:21:40
559
Vector Time (MET): N/A
Weight (LBS) : 902208
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1970289
66 A = 6780091
51 meter
Y = -4550125
28 meter E =
0013263
Z = 4614424
36 I = 51
74899
XDOT = 7067
197937 Wp = 78
11160
YDOT = 14
363638 meter/sec RA = 160
60889 deg
ZDOT = -2993
489698 TA = 41
71806
MA = 41
61699
Ha = 222
884 n
mi
Hp = 212
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6464204
91 X = 1998609
59
Y = -14928232
56 feet Y = -4527934
10 meter
Z = 15139187
53 Z = 4624063
81
XDOT = 23186
344938 XDOT = 7081
052801
YDOT = 47
124795 feet/sec YDOT = 93
471494 meter/sec
ZDOT = -9821
160428 ZDOT = -2959
126201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5853242
06 X = -1784068
18
Y = 15134883
93 feet Y = 4613112
62 meter
Z = 15182487
20 Z = 4627622
10
XDOT = -22134
616266 XDOT = -6746
631038
YDOT = 1171
821351 feet/sec YDOT = 357
171148 meter/sec
ZDOT = -9669
116767 ZDOT = -2947
146791
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 17215
68307736
00016717 00000-0 10270-3 0 9171
2 25544 51
6404 161
5627 0005476 97
2660 262
9116 15
54174593 29138
Satellite: ISS
Catalog Number: 25544
Epoch time: 17215
68307736 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 161
5627 deg
Eccentricity:
0005476
Arg of perigee: 97
2660 deg
Mean anomaly: 262
9116 deg
Mean motion: 15
54174593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2913
Checksum: 323
Coasting Arc #19 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902208
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 900147
22 A = 6777441
51 meter
Y = 4143017
09 meter E =
0020053
Z = -5305016
88 I = 51
75384
XDOT = -7251
483782 Wp = 97
42032
YDOT = 2368
646693 meter/sec RA = 158
24434 deg
ZDOT = 618
884574 TA = 178
49246
MA = 178
48640
Ha = 222
932 n
mi
Hp = 212
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2953238
91 X = 879520
83
Y = 13592575
74 feet Y = 4152968
14 meter
Z = -17404911
01 Z = -5300694
15
XDOT = -23790
957291 XDOT = -7280
437871
YDOT = 7771
150566 feet/sec YDOT = 2287
393744 meter/sec
ZDOT = 2030
461202 ZDOT = 583
589400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1750970
97 X = 533695
95
Y = 13822399
86 feet Y = 4213067
48 meter
Z = -17386374
71 Z = -5299367
01
XDOT = -23430
828593 XDOT = -7141
716555
YDOT = 5327
394216 feet/sec YDOT = 1623
789757 meter/sec
ZDOT = 1873
944260 ZDOT = 571
178211
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
13318632
00016717 00000-0 10270-3 0 9180
2 25544 51
6399 159
3162 0005404 103
9654 256
2100 15
54138363 29201
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
13318632 = yrday
fracday
Element set: 918
Inclination: 51
6399 deg
RA of node: 159
3162 deg
Eccentricity:
0005404
Arg of perigee: 103
9654 deg
Mean anomaly: 256
2100 deg
Mean motion: 15
54138363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 295
Coasting Arc #20 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902208
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 804180
15 A = 6779172
33 meter
Y = -4670339
92 meter E =
0011328
Z = 4838617
86 I = 51
79129
XDOT = 7121
808748 Wp = 80
46149
YDOT = -1378
612673 meter/sec RA = 153
25514 deg
ZDOT = -2507
490111 TA = 34
14311
MA = 34
07030
Ha = 222
796 n
mi
Hp = 212
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2638386
32 X = 832842
10
Y = -15322637
52 feet Y = -4661187
04 meter
Z = 15874730
51 Z = 4842593
60
XDOT = 23365
514264 XDOT = 7148
875414
YDOT = -4523
007457 feet/sec YDOT = -1298
820287 meter/sec
ZDOT = -8226
673592 ZDOT = -2472
829466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3731795
04 X = 1137451
13
Y = -15074409
46 feet Y = -4594680
00 meter
Z = 15892993
95 Z = 4844184
56
XDOT = 22602
938269 XDOT = 6889
375584
YDOT = -2939
508924 feet/sec YDOT = -895
962320 meter/sec
ZDOT = -8073
083260 ZDOT = -2460
675778
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
16200342
00016717 00000-0 10270-3 0 9193
2 25544 51
6410 154
1870 0005300 107
5744 252
5988 15
54189748 29362
Satellite: ISS
Catalog Number: 25544
Epoch time: 17217
16200342 = yrday
fracday
Element set: 919
Inclination: 51
6410 deg
RA of node: 154
1870 deg
Eccentricity:
0005300
Arg of perigee: 107
5744 deg
Mean anomaly: 252
5988 deg
Mean motion: 15
54189748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 309
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