[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 17th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
290/03:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
6
294/08:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
299/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 212
8
303/19:34:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 212
6
Coasting Arc #1 (Orbit 61)
---------------------------------------
Vector Time (GMT): 2017/289/13:18:28
229
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1266431
86 A = 6779995
58 meter
Y = 4793709
87 meter E =
0011724
Z = -4633957
14 I = 51
79911
XDOT = -6979
333382 Wp = 85
06896
YDOT = 1032
751320 meter/sec RA = 152
14716 deg
ZDOT = 2983
239279 TA = 214
60092
MA = 214
67726
Ha = 222
093 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4154960
16 X = -1297432
51
Y = 15727394
60 feet Y = 4779373
93 meter
Z = -15203271
44 Z = -4640184
96
XDOT = -22898
075400 XDOT = -7004
854453
YDOT = 3388
291733 feet/sec YDOT = 954
561275 meter/sec
ZDOT = 9787
530442 ZDOT = 2949
273336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8007274
77 X = -2440617
35
Y = -14129364
59 feet Y = -4306630
33 meter
Z = -15231503
68 Z = -4642562
32
XDOT = 13132
795955 XDOT = 4002
876207
YDOT = -17804
591449 feet/sec YDOT = -5426
839474 meter/sec
ZDOT = 9636
773308 ZDOT = 2937
288504
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 17289
56535255
00016717 00000-0 10270-3 0 9000
2 25544 51
6389 153
2478 0004983 22
1446 337
9921 15
54200052 623
Satellite: ISS
Catalog Number: 25544
Epoch time: 17289
56535255 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 153
2478 deg
Eccentricity:
0004983
Arg of perigee: 22
1446 deg
Mean anomaly: 337
9921 deg
Mean motion: 15
54200052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 62
Checksum: 307
Coasting Arc #2 (Orbit 70)
---------------------------------------
Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2201540
48 A = 6777229
84 meter
Y = 3574683
78 meter E =
0017881
Z = -5335271
33 I = 51
80522
XDOT = -6560
217659 Wp = 75
30385
YDOT = 3946
030294 meter/sec RA = 149
31935 deg
ZDOT = -58
868207 TA = 194
11054
MA = 194
16056
Ha = 222
276 n
mi
Hp = 213
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7222901
85 X = 2187320
30
Y = 11727965
17 feet Y = 3599222
80 meter
Z = -17504171
04 Z = -5324611
72
XDOT = -21523
023814 XDOT = -6603
569695
YDOT = 12946
293616 feet/sec YDOT = 3872
427057 meter/sec
ZDOT = -193
137161 ZDOT = -90
841900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13479410
82 X = 4108524
42
Y = -3107672
88 feet Y = -947218
69 meter
Z = -17457357
63 Z = -5321002
60
XDOT = 4985
079014 XDOT = 1519
452084
YDOT = 23585
543572 feet/sec YDOT = 7188
873681 meter/sec
ZDOT = -335
441604 ZDOT = -102
242601
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 17290
14404836
00016717 00000-0 10270-3 0 9017
2 25544 51
6382 150
3634 0005055 28
3480 331
7947 15
54174604 718
Satellite: ISS
Catalog Number: 25544
Epoch time: 17290
14404836 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 150
3634 deg
Eccentricity:
0005055
Arg of perigee: 28
3480 deg
Mean anomaly: 331
7947 deg
Mean motion: 15
54174604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 71
Checksum: 289
Coasting Arc #3 (Orbit 86)
---------------------------------------
Vector Time (GMT): 2017/291/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -583154
87 A = 6778283
50 meter
Y = -4472438
24 meter E =
0010392
Z = 5055806
77 I = 51
83542
XDOT = 6785
512170 Wp = 43
85191
YDOT = -3037
369049 meter/sec RA = 144
33167 deg
ZDOT = -1894
594420 TA = 64
50786
MA = 64
40040
Ha = 222
295 n
mi
Hp = 213
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1913237
77 X = -557658
61
Y = -14673353
80 feet Y = -4478816
34 meter
Z = 16587292
55 Z = 5053036
37
XDOT = 22262
179034 XDOT = 6828
175704
YDOT = -9965
121553 feet/sec YDOT = -2961
250488 meter/sec
ZDOT = -6215
860958 ZDOT = -1861
527940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14575674
44 X = -4442665
57
Y = -2627877
02 feet Y = -800976
92 meter
Z = 16575585
72 Z = 5052238
53
XDOT = -2749
205876 XDOT = -837
957951
YDOT = -23230
611945 feet/sec YDOT = -7080
690521 meter/sec
ZDOT = -6068
811965 ZDOT = -1849
773887
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 17291
17283596
00016717 00000-0 10270-3 0 9020
2 25544 51
6369 145
2340 0005110 30
4224 329
7224 15
54198022 874
Satellite: ISS
Catalog Number: 25544
Epoch time: 17291
17283596 = yrday
fracday
Element set: 902
Inclination: 51
6369 deg
RA of node: 145
2340 deg
Eccentricity:
0005110
Arg of perigee: 30
4224 deg
Mean anomaly: 329
7224 deg
Mean motion: 15
54198022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 87
Checksum: 288
Coasting Arc #4 (Orbit 101)
---------------------------------------
Vector Time (GMT): 2017/292/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -916021
98 A = 6781457
90 meter
Y = 5198803
89 meter E =
0010763
Z = -4265253
84 I = 51
87140
XDOT = -6496
089303 Wp = 82
71304
YDOT = 1824
202733 meter/sec RA = 139
35290 deg
ZDOT = 3627
759588 TA = 224
25719
MA = 224
34331
Ha = 222
391 n
mi
Hp = 213
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3005321
44 X = -953369
34
Y = 17056443
22 feet Y = 5188351
03 meter
Z = -13993614
95 Z = -4269794
96
XDOT = -21312
628946 XDOT = -6533
627483
YDOT = 5984
917102 feet/sec YDOT = 1751
349530 meter/sec
ZDOT = 11902
098385 ZDOT = 3596
111540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15447184
96 X = 4708301
98
Y = 7794576
94 feet Y = 2375787
05 meter
Z = -14014439
65 Z = -4271601
21
XDOT = 7
233330 XDOT = 2
204719
YDOT = 21078
526166 feet/sec YDOT = 6424
734775 meter/sec
ZDOT = 11761
484237 ZDOT = 3584
900395
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 17292
13732254
00016717 00000-0 10270-3 0 9038
2 25544 51
6364 140
4260 0005181 33
9995 326
1489 15
54177544 1026
Satellite: ISS
Catalog Number: 25544
Epoch time: 17292
13732254 = yrday
fracday
Element set: 903
Inclination: 51
6364 deg
RA of node: 140
4260 deg
Eccentricity:
0005181
Arg of perigee: 33
9995 deg
Mean anomaly: 326
1489 deg
Mean motion: 15
54177544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 102
Checksum: 298
Coasting Arc #5 (Orbit 117)
---------------------------------------
Vector Time (GMT): 2017/293/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2265317
90 A = 6785256
05 meter
Y = -5653742
15 meter E =
0016332
Z = 2979763
57 I = 51
90883
XDOT = 5804
673128 Wp = 81
27165
YDOT = -324
460617 meter/sec RA = 134
38455 deg
ZDOT = -5002
765959 TA = 64
78473
MA = 64
61550
Ha = 222
344 n
mi
Hp = 213
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7432145
33 X = 2313896
59
Y = -18549022
81 feet Y = -5628137
91 meter
Z = 9776127
20 Z = 2990886
59
XDOT = 19044
203177 XDOT = 5832
171504
YDOT = -1064
503335 feet/sec YDOT = -259
395523 meter/sec
ZDOT = -16413
274143 ZDOT = -4974
501137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15778413
04 X = -4809260
29
Y = -12221406
35 feet Y = -3725084
66 meter
Z = 9826220
19 Z = 2995031
91
XDOT = 3394
400270 XDOT = 1034
613202
YDOT = -17545
673477 feet/sec YDOT = -5347
921276 meter/sec
ZDOT = -16287
852927 ZDOT = -4964
537572
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 17293
16610355
00016717 00000-0 10270-3 0 9040
2 25544 51
6366 135
2959 0005186 36
4778 323
6727 15
54222181 1189
Satellite: ISS
Catalog Number: 25544
Epoch time: 17293
16610355 = yrday
fracday
Element set: 904
Inclination: 51
6366 deg
RA of node: 135
2959 deg
Eccentricity:
0005186
Arg of perigee: 36
4778 deg
Mean anomaly: 323
6727 deg
Mean motion: 15
54222181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 118
Checksum: 313
Coasting Arc #6 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2017/294/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3297075
32 A = 6788170
93 meter
Y = 5755838
05 meter E =
0013705
Z = -1416306
97 I = 51
94081
XDOT = -4808
536527 Wp = 39
38189
YDOT = -1331
486519 meter/sec RA = 129
42850 deg
ZDOT = 5823
924463 TA = 305
23950
MA = 305
36769
Ha = 222
430 n
mi
Hp = 213
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10817176
23 X = -3354313
68
Y = 18883983
11 feet Y = 5718647
75 meter
Z = -4646676
41 Z = -1432463
05
XDOT = -15776
038475 XDOT = -4821
580632
YDOT = -4368
394090 feet/sec YDOT = -1385
331334 meter/sec
ZDOT = 19107
363725 ZDOT = 5800
533885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15418931
85 X = 4699690
43
Y = 15336039
29 feet Y = 4674424
78 meter
Z = -4719127
13 Z = -1438389
95
XDOT = -7242
575964 XDOT = -2207
537154
YDOT = 13088
634069 feet/sec YDOT = 3989
415664 meter/sec
ZDOT = 19003
779048 ZDOT = 5792
351854
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 17294
13058244
00016717 00000-0 10270-3 0 9052
2 25544 51
6367 130
4876 0005238 41
4387 318
7162 15
54223898 1336
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
13058244 = yrday
fracday
Element set: 905
Inclination: 51
6367 deg
RA of node: 130
4876 deg
Eccentricity:
0005238
Arg of perigee: 41
4387 deg
Mean anomaly: 318
7162 deg
Mean motion: 15
54223898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 133
Checksum: 312
Coasting Arc #7 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3330854
68 A = 6777051
85 meter
Y = 2539468
44 meter E =
0018658
Z = -5343460
17 I = 51
91223
XDOT = -4702
381488 Wp = 77
20109
YDOT = 6040
409356 meter/sec RA = 128
23287 deg
ZDOT = -56
691535 TA = 192
23710
MA = 192
28248
Ha = 222
400 n
mi
Hp = 213
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10928000
90 X = 3328166
71
Y = 8331589
37 feet Y = 2576700
91 meter
Z = -17531037
30 Z = -5327286
19
XDOT = -15427
760789 XDOT = -4769
302078
YDOT = 19817
615999 feet/sec YDOT = 5987
449936 meter/sec
ZDOT = -185
995851 ZDOT = -79
697851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8101335
84 X = -2469287
16
Y = -11211757
88 feet Y = -3417343
80 meter
Z = -17459630
49 Z = -5321695
37
XDOT = 19758
886592 XDOT = 6022
508633
YDOT = -13807
647680 feet/sec YDOT = -4208
571013 meter/sec
ZDOT = -288
879464 ZDOT = -88
050461
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 17294
38777577
00016717 00000-0 10270-3 0 9067
2 25544 51
6402 129
2063 0005223 39
2652 320
8879 15
54235421 1372
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
38777577 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 129
2063 deg
Eccentricity:
0005223
Arg of perigee: 39
2652 deg
Mean anomaly: 320
8879 deg
Mean motion: 15
54235421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 313
Coasting Arc #8 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2138294
09 A = 6778118
81 meter
Y = -3964891
88 meter E =
0010641
Z = 5059640
10 I = 51
93532
XDOT = 5240
445939 Wp = 49
33902
YDOT = -5270
345289 meter/sec RA = 123
25218 deg
ZDOT = -1905
925906 TA = 59
10453
MA = 58
99994
Ha = 222
419 n
mi
Hp = 213
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7015400
57 X = -2118376
61
Y = -13008175
47 feet Y = -3988692
10 meter
Z = 16599869
11 Z = 5049301
25
XDOT = 17193
064105 XDOT = 5308
249168
YDOT = -17291
159086 feet/sec YDOT = -5211
364041 meter/sec
ZDOT = -6253
037750 ZDOT = -1880
303772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3229112
76 X = 984233
57
Y = 14474249
68 feet Y = 4411751
30 meter
Z = 16554547
88 Z = 5045826
19
XDOT = -20304
664135 XDOT = -6188
861628
YDOT = 11586
018270 feet/sec YDOT = 3531
418369 meter/sec
ZDOT = -6138
632145 ZDOT = -1871
055078
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 17295
41654796
00016717 00000-0 10270-3 0 9070
2 25544 51
6399 124
0772 0005127 42
0142 318
1403 15
54262897 1534
Satellite: ISS
Catalog Number: 25544
Epoch time: 17295
41654796 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 124
0772 deg
Eccentricity:
0005127
Arg of perigee: 42
0142 deg
Mean anomaly: 318
1403 deg
Mean motion: 15
54262897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 308
Coasting Arc #9 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 995163
71 A = 6781346
62 meter
Y = 5187667
18 meter E =
0011343
Z = -4261826
81 I = 51
96326
XDOT = -5403
286308 Wp = 86
15347
YDOT = 4024
017888 meter/sec RA = 118
27868 deg
ZDOT = 3645
577283 TA = 220
97835
MA = 221
06365
Ha = 222
446 n
mi
Hp = 213
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3264972
79 X = 957782
27
Y = 17019905
44 feet Y = 5198586
59 meter
Z = -13982371
43 Z = -4257083
50
XDOT = -17727
317283 XDOT = -5465
591253
YDOT = 13202
158426 feet/sec YDOT = 3963
246433 meter/sec
ZDOT = 11960
555390 ZDOT = 3619
177611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1207417
51 X = 368020
86
Y = -17304539
59 feet Y = -5274423
67 meter
Z = -13962055
43 Z = -4255634
49
XDOT = 19375
167493 XDOT = 5905
551052
YDOT = -8179
356554 feet/sec YDOT = -2493
067878 meter/sec
ZDOT = 11842
852598 ZDOT = 3609
701472
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 17296
38102078
00016717 00000-0 10270-3 0 9089
2 25544 51
6402 119
2682 0005126 44
9476 315
2091 15
54236003 1682
Satellite: ISS
Catalog Number: 25544
Epoch time: 17296
38102078 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 119
2682 deg
Eccentricity:
0005126
Arg of perigee: 44
9476 deg
Mean anomaly: 315
2091 deg
Mean motion: 15
54236003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 168
Checksum: 295
Coasting Arc #10 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 105227
33 A = 6785208
86 meter
Y = -6096664
09 meter E =
0017092
Z = 2964022
39 I = 51
99148
XDOT = 5293
492542 Wp = 83
95966
YDOT = -2363
616371 meter/sec RA = 113
31621 deg
ZDOT = -5023
081563 TA = 62
33937
MA = 62
16599
Ha = 222
485 n
mi
Hp = 212
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 345234
04 X = 158995
92
Y = -20002178
76 feet Y = -6095186
64 meter
Z = 9724482
90 Z = 2964664
34
XDOT = 17367
101515 XDOT = 5343
929965
YDOT = -7754
646885 feet/sec YDOT = -2304
139061 meter/sec
ZDOT = -16479
926388 ZDOT = -4997
244215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5166863
05 X = -1574859
86
Y = 19324530
58 feet Y = 5890116
92 meter
Z = 9728204
02 Z = 2965156
59
XDOT = -17432
311750 XDOT = -5313
368621
YDOT = 3621
193346 feet/sec YDOT = 1103
739732 meter/sec
ZDOT = -16364
936765 ZDOT = -4988
032726
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 17297
40978586
00016717 00000-0 10270-3 0 9099
2 25544 51
6406 114
1383 0005296 47
6995 312
4606 15
54264255 1841
Satellite: ISS
Catalog Number: 25544
Epoch time: 17297
40978586 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 114
1383 deg
Eccentricity:
0005296
Arg of perigee: 47
6995 deg
Mean anomaly: 312
4606 deg
Mean motion: 15
54264255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 184
Checksum: 334
Coasting Arc #11 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1033081
48 A = 6788220
01 meter
Y = 6558371
51 meter E =
0013734
Z = -1390432
30 I = 52
01173
XDOT = -4952
400290 Wp = 42
94601
YDOT = 448
287475 meter/sec RA = 108
36491 deg
ZDOT = 5837
625953 TA = 301
97911
MA = 302
11253
Ha = 222
564 n
mi
Hp = 212
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3389374
94 X = -1099587
97
Y = 21516966
89 feet Y = 6546446
99 meter
Z = -4561785
75 Z = -1395612
49
XDOT = -16248
032446 XDOT = -4985
402035
YDOT = 1470
759433 feet/sec YDOT = 392
721966 meter/sec
ZDOT = 19152
316118 ZDOT = 5813
488029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8176025
20 X = 2492052
48
Y = -20184185
16 feet Y = -6152139
64 meter
Z = -4585727
53 Z = -1397729
75
XDOT = 14806
051341 XDOT = 4512
884449
YDOT = 1702
851558 feet/sec YDOT = 519
029155 meter/sec
ZDOT = 19045
131647 ZDOT = 5804
956126
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 17298
37425135
00016717 00000-0 10270-3 0 9105
2 25544 51
6392 109
3297 0005229 51
2925 308
8695 15
54223711 1990
Satellite: ISS
Catalog Number: 25544
Epoch time: 17298
37425135 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 109
3297 deg
Eccentricity:
0005229
Arg of perigee: 51
2925 deg
Mean anomaly: 308
8695 deg
Mean motion: 15
54223711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 319
Coasting Arc #12 (Orbit 214)
---------------------------------------
Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1864688
78 A = 6789006
54 meter
Y = -6513098
09 meter E =
0013063
Z = -387040
81 I = 52
02434
XDOT = 4450
097419 Wp = 115
15907
YDOT = 1622
510258 meter/sec RA = 103
42034 deg
ZDOT = -6027
598934 TA = 68
99029
MA = 68
85060
Ha = 222
563 n
mi
Hp = 212
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6117745
35 X = 1939261
49
Y = -21368432
06 feet Y = -6491828
91 meter
Z = -1269818
93 Z = -377801
28
XDOT = 14600
057148 XDOT = 4460
903029
YDOT = 5323
196385 feet/sec YDOT = 1672
334576 meter/sec
ZDOT = -19775
587053 ZDOT = -6005
955104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10500545
23 X = -3200566
19
Y = 19592857
49 feet Y = 5971902
96 meter
Z = -1227852
59 Z = -374249
47
XDOT = -11844
757464 XDOT = -3610
282075
YDOT = -7546
514294 feet/sec YDOT = -2300
177557 meter/sec
ZDOT = -19679
767780 ZDOT = -5998
393219
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 17299
40301147
00016717 00000-0 10270-3 0 9117
2 25544 51
6399 104
2007 0005053 56
1053 304
0580 15
54217883 2154
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
40301147 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 104
2007 deg
Eccentricity:
0005053
Arg of perigee: 56
1053 deg
Mean anomaly: 304
0580 deg
Mean motion: 15
54217883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 215
Checksum: 275
Coasting Arc #13 (Orbit 216)
---------------------------------------
Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2966539
65 A = 6787108
20 meter
Y = -5740345
10 meter E =
0009072
Z = -2079525
81 I = 52
01726
XDOT = 3581
762649 Wp = 104
90679
YDOT = 3859
530150 meter/sec RA = 102
77581 deg
ZDOT = -5566
813779 TA = 97
96554
MA = 97
86257
Ha = 222
569 n
mi
Hp = 212
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9732741
63 X = 3040610
75
Y = -18833153
22 feet Y = -5706757
12 meter
Z = -6822591
22 Z = -2064934
96
XDOT = 11751
189793 XDOT = 3565
379521
YDOT = 12662
500493 feet/sec YDOT = 3899
492144 meter/sec
ZDOT = -18263
824733 ZDOT = -5549
454224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2954230
72 X = 900449
52
Y = 21013741
24 feet Y = 6404988
33 meter
Z = -6756986
80 Z = -2059529
58
XDOT = -15480
448656 XDOT = -4718
440750
YDOT = -3647
887901 feet/sec YDOT = -1111
876232 meter/sec
ZDOT = -18187
349717 ZDOT = -5543
504194
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 17299
53160628
00016717 00000-0 10270-3 0 9129
2 25544 51
6376 103
5550 0005216 59
5007 300
6661 15
54272002 2179
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
53160628 = yrday
fracday
Element set: 912
Inclination: 51
6376 deg
RA of node: 103
5550 deg
Eccentricity:
0005216
Arg of perigee: 59
5007 deg
Mean anomaly: 300
6661 deg
Mean motion: 15
54272002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 217
Checksum: 282
Coasting Arc #14 (Orbit 232)
---------------------------------------
Vector Time (GMT): 2017/300/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3432693
13 A = 6783659
21 meter
Y = 4641999
26 meter E =
0016876
Z = 3545719
60 I = 52
01198
XDOT = -2801
312540 Wp = 84
21461
YDOT = -5535
572253 meter/sec RA = 97
82167 deg
ZDOT = 4518
332944 TA = 317
39217
MA = 317
52296
Ha = 222
653 n
mi
Hp = 212
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11262116
57 X = -3501569
74
Y = 15229656
37 feet Y = 4603227
52 meter
Z = 11632938
31 Z = 3528876
94
XDOT = -9190
657941 XDOT = -2761
152315
YDOT = -18161
326288 feet/sec YDOT = -5566
673778 meter/sec
ZDOT = 14823
926982 ZDOT = 4504
822488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 80080
57 X = 24408
56
Y = -18987390
63 feet Y = -5787356
66 meter
Z = 11557488
51 Z = 3522722
50
XDOT = 16871
398581 XDOT = 5142
402288
YDOT = 9092
013971 feet/sec YDOT = 2771
245858 meter/sec
ZDOT = 14764
789092 ZDOT = 4500
307715
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 17300
56036093
00016717 00000-0 10270-3 0 9134
2 25544 51
6377 98
4252 0005105 65
2201 294
9482 15
54266748 2332
Satellite: ISS
Catalog Number: 25544
Epoch time: 17300
56036093 = yrday
fracday
Element set: 913
Inclination: 51
6377 deg
RA of node: 98
4252 deg
Eccentricity:
0005105
Arg of perigee: 65
2201 deg
Mean anomaly: 294
9482 deg
Mean motion: 15
54266748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 233
Checksum: 300
Coasting Arc #15 (Orbit 247)
---------------------------------------
Vector Time (GMT): 2017/301/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3807994
28 A = 6779822
28 meter
Y = -3132534
97 meter E =
0015645
Z = -4668467
84 I = 52
00289
XDOT = 1968
427380 Wp = 69
65172
YDOT = 6784
909726 meter/sec RA = 92
85868 deg
ZDOT = -2949
751593 TA = 171
09184
MA = 171
06405
Ha = 222
647 n
mi
Hp = 212
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12493419
57 X = 3865417
59
Y = -10277345
72 feet Y = -3089630
47 meter
Z = -15316495
54 Z = -4649829
91
XDOT = 6458
095080 XDOT = 1906
739081
YDOT = 22260
202512 feet/sec YDOT = 6806
577000 meter/sec
ZDOT = -9677
662706 ZDOT = -2940
339506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3759061
66 X = -1145762
00
Y = 15815202
34 feet Y = 4820473
67 meter
Z = -15233293
59 Z = -4643107
89
XDOT = -17549
558011 XDOT = -5349
105282
YDOT = -13445
038814 feet/sec YDOT = -4098
047830 meter/sec
ZDOT = -9636
912066 ZDOT = -2937
330798
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 17301
52481586
00016717 00000-0 10270-3 0 9143
2 25544 51
6380 93
6175 0005250 68
5391 291
6321 15
54263786 2485
Satellite: ISS
Catalog Number: 25544
Epoch time: 17301
52481586 = yrday
fracday
Element set: 914
Inclination: 51
6380 deg
RA of node: 93
6175 deg
Eccentricity:
0005250
Arg of perigee: 68
5391 deg
Mean anomaly: 291
6321 deg
Mean motion: 15
54263786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 248
Checksum: 312
Coasting Arc #16 (Orbit 263)
---------------------------------------
Vector Time (GMT): 2017/302/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4054706
64 A = 6777333
80 meter
Y = 1363666
18 meter E =
0008007
Z = 5249803
72 I = 51
99537
XDOT = -1123
806047 Wp = 92
90692
YDOT = -7514
747529 meter/sec RA = 87
88462 deg
ZDOT = 1082
209732 TA = 346
77406
MA = 346
79504
Ha = 222
769 n
mi
Hp = 212
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13302843
31 X = -4095155
53
Y = 4473970
40 feet Y = 1318097
78 meter
Z = 17223765
50 Z = 5230008
60
XDOT = -3687
027712 XDOT = -1044
947534
YDOT = -24654
683495 feet/sec YDOT = -7526
873717 meter/sec
ZDOT = 3550
556865 ZDOT = 1076
942458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7734904
34 X = 2357598
84
Y = -11839744
33 feet Y = -3608754
07 meter
Z = 17135689
62 Z = 5222958
19
XDOT = 17356
853991 XDOT = 5290
369096
YDOT = 16454
436486 feet/sec YDOT = 5015
312241 meter/sec
ZDOT = 3528
326183 ZDOT = 1075
433820
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 17302
55356368
00016717 00000-0 10270-3 0 9157
2 25544 51
6381 88
4871 0005114 71
4541 288
7167 15
54262993 2642
Satellite: ISS
Catalog Number: 25544
Epoch time: 17302
55356368 = yrday
fracday
Element set: 915
Inclination: 51
6381 deg
RA of node: 88
4871 deg
Eccentricity:
0005114
Arg of perigee: 71
4541 deg
Mean anomaly: 288
7167 deg
Mean motion: 15
54262993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 264
Checksum: 323
Coasting Arc #17 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2017/303/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4228073
97 A = 6777201
13 meter
Y = 507053
80 meter E =
0019393
Z = -5289002
78 I = 51
99390
XDOT = 226
834074 Wp = 91
24225
YDOT = 7596
436654 meter/sec RA = 82
90826 deg
ZDOT = 912
072182 TA = 187
44127
MA = 187
47009
Ha = 222
649 n
mi
Hp = 212
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13871633
75 X = 4247781
53
Y = 1663562
34 feet Y = 554444
87 meter
Z = -17352371
33 Z = -5268415
93
XDOT = 744
206281 XDOT = 137
441358
YDOT = 24922
692436 feet/sec YDOT = 7598
473501 meter/sec
ZDOT = 2992
362801 ZDOT = 912
956479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11864455
39 X = -3616286
00
Y = 7588459
75 feet Y = 2312962
53 meter
Z = -17261066
89 Z = -5261173
19
XDOT = -15819
491258 XDOT = -4821
780935
YDOT = -17939
290975 feet/sec YDOT = -5467
895889 meter/sec
ZDOT = 2995
112759 ZDOT = 912
910369
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 17303
51801042
00016717 00000-0 10270-3 0 9169
2 25544 51
6392 83
6791 0005227 75
3028 284
8704 15
54278015 2792
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
51801042 = yrday
fracday
Element set: 916
Inclination: 51
6392 deg
RA of node: 83
6791 deg
Eccentricity:
0005227
Arg of perigee: 75
3028 deg
Mean anomaly: 284
8704 deg
Mean motion: 15
54278015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 305
Coasting Arc #18 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2017/303/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2302074
07 A = 6782545
16 meter
Y = -5069461
03 meter E =
0011741
Z = -3885846
75 I = 52
01247
XDOT = 4037
521500 Wp = 74
04014
YDOT = 5010
522985 meter/sec RA = 81
39583 deg
ZDOT = -4152
035083 TA = 152
52565
MA = 152
46353
Ha = 222
705 n
mi
Hp = 212
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7552736
46 X = 2377466
91
Y = -16632089
98 feet Y = -5043296
38 meter
Z = -12748841
05 Z = -3874480
33
XDOT = 13246
461615 XDOT = 4001
361316
YDOT = 16438
723704 feet/sec YDOT = 5055
470843 meter/sec
ZDOT = -13622
162347 ZDOT = -4132
509885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14538959
25 X = 4431474
78
Y = -11117230
95 feet Y = -3388531
99 meter
Z = -12697599
51 Z = -3870228
33
XDOT = 3269
894136 XDOT = 996
663733
YDOT = 19709
539801 feet/sec YDOT = 6007
467731 meter/sec
ZDOT = -13536
269791 ZDOT = -4125
855032
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 17303
83949074
00016717 00000-0 10270-3 0 9173
2 25544 51
6411 82
0792 0005403 73
3460 286
8285 15
54280992 2841
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
83949074 = yrday
fracday
Element set: 917
Inclination: 51
6411 deg
RA of node: 82
0792 deg
Eccentricity:
0005403
Arg of perigee: 73
3460 deg
Mean anomaly: 286
8285 deg
Mean motion: 15
54280992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 318
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