[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 17th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15281 523 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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
291/23:40:36
600 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 212
0
293/08:05:14
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 211
9
294/03:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 211
9
295/09:59:09
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 211
9
297/11:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 212
0
304/00:37:30
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
1
304/02:12:00
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
1
Coasting Arc #1 (Orbit 2400)
---------------------------------------
Vector Time (GMT): 2016/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3842398
96 A = 6782453
49 meter
Y = -4029571
53 meter E =
0018042
Z = 3860105
10 I = 51
72016
XDOT = 6175
783769 Wp = 80
35823
YDOT = 1906
438496 meter/sec RA = 166
80777 deg
ZDOT = -4137
906015 TA = 53
10628
MA = 52
94107
Ha = 223
159 n
mi
Hp = 211
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12606295
80 X = 3868421
86
Y = -13220379
03 feet Y = -3986457
41 meter
Z = 12664386
82 Z = 3878834
56
XDOT = 20261
757773 XDOT = 6174
107181
YDOT = 6254
719476 feet/sec YDOT = 1975
490523 meter/sec
ZDOT = -13575
807137 ZDOT = -4107
909056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5593112
21 X = -1704780
60
Y = 17329657
47 feet Y = 5282079
60 meter
Z = 12746916
35 Z = 3885260
10
XDOT = -19791
844147 XDOT = -6032
554096
YDOT = 3548
227240 feet/sec YDOT = 1081
499663 meter/sec
ZDOT = -13444
890234 ZDOT = -4098
002543
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 16291
54060130
00016717 00000-0 10270-3 0 9005
2 25544 51
6428 167
7731 0006827 78
0372 282
1545 15
54288737 24014
Satellite: ISS
Catalog Number: 25544
Epoch time: 16291
54060130 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 167
7731 deg
Eccentricity:
0006827
Arg of perigee: 78
0372 deg
Mean anomaly: 282
1545 deg
Mean motion: 15
54288737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2401
Checksum: 303
Coasting Arc #2 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2016/291/23:40:36
600
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5592949
23 A = 6787123
14 meter
Y = 3246812
35 meter E =
0012311
Z = -2057450
11 I = 51
74901
XDOT = -4019
772406 Wp = 62
77544
YDOT = -3423
982728 meter/sec RA = 164
38963 deg
ZDOT = 5555
023700 TA = 274
51541
MA = 274
65604
Ha = 223
225 n
mi
Hp = 212
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18349570
98 X = -5618845
77
Y = 10652271
49 feet Y = 3184123
29 meter
Z = -6750164
41 Z = -2084683
11
XDOT = -13188
229678 XDOT = -4008
170418
YDOT = -11233
539133 feet/sec YDOT = -3468
869237 meter/sec
ZDOT = 18225
143373 ZDOT = 5535
524577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13215391
20 X = -4028051
24
Y = 16549983
00 feet Y = 5044434
82 meter
Z = -6869778
77 Z = -2093908
57
XDOT = -15260
131494 XDOT = -4651
288079
YDOT = -4697
004671 feet/sec YDOT = -1431
647024 meter/sec
ZDOT = 18140
369625 ZDOT = 5529
184662
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 16291
99067858
00016717 00000-0 10270-3 0 9019
2 25544 51
6412 165
5267 0006705 82
6540 277
5374 15
54245574 24087
Satellite: ISS
Catalog Number: 25544
Epoch time: 16291
99067858 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 165
5267 deg
Eccentricity:
0006705
Arg of perigee: 82
6540 deg
Mean anomaly: 277
5374 deg
Mean motion: 15
54245574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2408
Checksum: 330
Coasting Arc #3 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2016/292/23:40:36
600
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6254356
47 A = 6788809
46 meter
Y = -2606571
88 meter E =
0018236
Z = 307936
93 I = 51
78594
XDOT = 2090
568683 Wp = 115
77637
YDOT = 4273
825108 meter/sec RA = 159
42607 deg
ZDOT = -6015
214510 TA = 60
91110
MA = 60
72862
Ha = 223
286 n
mi
Hp = 211
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20519542
21 X = 6281543
11
Y = -8551745
03 feet Y = -2536479
45 meter
Z = 1010291
78 Z = 338385
94
XDOT = 6858
821140 XDOT = 2071
842333
YDOT = 14021
735920 feet/sec YDOT = 4297
098229 meter/sec
ZDOT = -19734
955742 ZDOT = -6005
104516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15765382
78 X = 4805288
67
Y = -15663615
45 feet Y = -4774269
99 meter
Z = 1143897
56 Z = 348659
98
XDOT = 10620
662588 XDOT = 3237
177957
YDOT = 9194
709416 feet/sec YDOT = 2802
547430 meter/sec
ZDOT = -19691
380945 ZDOT = -6001
932912
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 16293
01942034
00016717 00000-0 10270-3 0 9023
2 25544 51
6413 160
3970 0006919 85
3921 274
8022 15
54290066 24246
Satellite: ISS
Catalog Number: 25544
Epoch time: 16293
01942034 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 160
3970 deg
Eccentricity:
0006919
Arg of perigee: 85
3921 deg
Mean anomaly: 274
8022 deg
Mean motion: 15
54290066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2424
Checksum: 293
Coasting Arc #4 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2016/293/08:05:14
000
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5252582
55 A = 6787238
09 meter
Y = 3824698
29 meter E =
0012641
Z = -1958966
95 I = 51
79009
XDOT = -4272
332062 Wp = 63
04502
YDOT = -3014
175560 meter/sec RA = 157
66896 deg
ZDOT = 5603
931501 TA = 275
40156
MA = 275
54576
Ha = 223
273 n
mi
Hp = 211
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17232882
37 X = -5285444
88
Y = 12548222
73 feet Y = 3765776
55 meter
Z = -6427056
92 Z = -1984563
27
XDOT = -14016
837473 XDOT = -4265
531364
YDOT = -9889
027429 feet/sec YDOT = -3061
913357 meter/sec
ZDOT = 18385
602037 ZDOT = 5583
193764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21208140
75 X = 6464241
30
Y = -1784721
87 feet Y = -543983
22 meter
Z = -6539627
13 Z = -1993278
35
XDOT = 6807
191290 XDOT = 2074
831905
YDOT = 14247
430979 feet/sec YDOT = 4342
616962 meter/sec
ZDOT = 18295
337817 ZDOT = 5576
418967
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 16293
34090182
00016717 00000-0 10270-3 0 9038
2 25544 51
6402 158
7955 0006901 84
7200 275
4740 15
54265957 24292
Satellite: ISS
Catalog Number: 25544
Epoch time: 16293
34090182 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 158
7955 deg
Eccentricity:
0006901
Arg of perigee: 84
7200 deg
Mean anomaly: 275
4740 deg
Mean motion: 15
54265957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 314
Coasting Arc #5 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2016/294/03:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3729823
40 A = 6784388
94 meter
Y = -4660468
42 meter E =
0019612
Z = 3206748
69 I = 51
80257
XDOT = 5828
749139 Wp = 91
72187
YDOT = 1338
453235 meter/sec RA = 153
67627 deg
ZDOT = -4809
526309 TA = 51
25159
MA = 51
07648
Ha = 223
191 n
mi
Hp = 211
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12236953
43 X = 3766083
43
Y = -15290250
71 feet Y = -4618556
16 meter
Z = 10520829
05 Z = 3224955
86
XDOT = 19123
192714 XDOT = 5836
712080
YDOT = 4391
250771 feet/sec YDOT = 1403
678557 meter/sec
ZDOT = -15779
285792 ZDOT = -4781
191851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12370001
42 X = -3770376
43
Y = -15126796
14 feet Y = -4610647
46 meter
Z = 10601214
24 Z = 3231250
10
XDOT = 7253
296546 XDOT = 2210
804787
YDOT = -16959
698118 feet/sec YDOT = -5169
315986 meter/sec
ZDOT = -15655
516301 ZDOT = -4771
801369
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 16294
17674582
00016717 00000-0 10270-3 0 9043
2 25544 51
6382 154
6272 0006865 88
1475 272
0464 15
54304289 24420
Satellite: ISS
Catalog Number: 25544
Epoch time: 16294
17674582 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 154
6272 deg
Eccentricity:
0006865
Arg of perigee: 88
1475 deg
Mean anomaly: 272
0464 deg
Mean motion: 15
54304289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 327
Coasting Arc #6 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2016/295/03:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 880841
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4828640
36 A = 6787581
51 meter
Y = 4467642
50 meter E =
0013077
Z = -1667508
83 I = 51
84212
XDOT = -4375
737026 Wp = 64
67530
YDOT = -2606
747410 meter/sec RA = 148
71218 deg
ZDOT = 5727
303667 TA = 277
11563
MA = 277
26431
Ha = 223
276 n
mi
Hp = 211
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15841995
93 X = -4870139
63
Y = 14657619
74 feet Y = 4413413
30 meter
Z = -5470829
51 Z = -1691066
50
XDOT = -14356
092606 XDOT = -4374
083716
YDOT = -8552
320900 feet/sec YDOT = -2655
670379 meter/sec
ZDOT = 18790
366363 ZDOT = 5706
051206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11300238
64 X = 3444312
74
Y = 18356821
51 feet Y = 5595159
20 meter
Z = -5574615
49 Z = -1699142
80
XDOT = -9866
434811 XDOT = -3007
289330
YDOT = 11712
242623 feet/sec YDOT = 3569
891552 meter/sec
ZDOT = 18697
769832 ZDOT = 5699
080245
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 16295
14117818
00016717 00000-0 10270-3 0 9056
2 25544 51
6385 149
8192 0007055 92
9867 267
2093 15
54306147 24575
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
14117818 = yrday
fracday
Element set: 905
Inclination: 51
6385 deg
RA of node: 149
8192 deg
Eccentricity:
0007055
Arg of perigee: 92
9867 deg
Mean anomaly: 267
2093 deg
Mean motion: 15
54306147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2457
Checksum: 335
Coasting Arc #7 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2016/295/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 895949
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1252839
67 A = 6777046
30 meter
Y = -4095423
42 meter E =
0009766
Z = 5244177
46 I = 51
81923
XDOT = 6804
114560 Wp = 80
96862
YDOT = -3401
814405 meter/sec RA = 147
33633 deg
ZDOT = -1028
000041 TA = 18
85859
MA = 18
82244
Ha = 223
142 n
mi
Hp = 211
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4110366
38 X = -1232424
83
Y = -13436428
55 feet Y = -4109319
17 meter
Z = 17205306
63 Z = 5238141
13
XDOT = 22323
210498 XDOT = 6846
642474
YDOT = -11160
808415 feet/sec YDOT = -3325
488483 meter/sec
ZDOT = -3372
703546 ZDOT = -994
843433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4036750
85 X = 1230401
66
Y = 13491616
59 feet Y = 4112244
74 meter
Z = 17179529
22 Z = 5236320
51
XDOT = -21511
967898 XDOT = -6556
847815
YDOT = 10558
738643 feet/sec YDOT = 3218
303538 meter/sec
ZDOT = -3227
071344 ZDOT = -983
611346
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 16295
46265243
00016717 00000-0 10270-3 0 9068
2 25544 51
6429 148
2171 0006610 92
7067 267
4842 15
54339470 24625
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
46265243 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 148
2171 deg
Eccentricity:
0006610
Arg of perigee: 92
7067 deg
Mean anomaly: 267
4842 deg
Mean motion: 15
54339470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 317
Coasting Arc #8 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2016/296/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 895949
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -357392
62 A = 6779529
11 meter
Y = 4912733
99 meter E =
0017149
Z = -4674618
24 I = 51
85383
XDOT = -6701
711799 Wp = 104
41117
YDOT = 2280
114669 meter/sec RA = 142
35127 deg
ZDOT = 2913
416055 TA = 194
50711
MA = 194
55640
Ha = 223
136 n
mi
Hp = 211
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1172547
96 X = -389593
95
Y = 16117893
66 feet Y = 4908557
11 meter
Z = -15336674
02 Z = -4676432
83
XDOT = -21987
243435 XDOT = -6740
862826
YDOT = 7480
691171 feet/sec YDOT = 2204
952863 meter/sec
ZDOT = 9558
451624 ZDOT = 2880
765225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1017348
34 X = 310087
77
Y = -16120143
35 feet Y = -4913419
69 meter
Z = -15345387
43 Z = -4677274
09
XDOT = 20847
129709 XDOT = 6354
205135
YDOT = -7632
074050 feet/sec YDOT = -2326
256170 meter/sec
ZDOT = 9415
187180 ZDOT = 2869
749052
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 16296
42707498
00016717 00000-0 10270-3 0 9079
2 25544 51
6427 143
4081 0006672 95
2886 264
9028 15
54318646 24771
Satellite: ISS
Catalog Number: 25544
Epoch time: 16296
42707498 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 143
4081 deg
Eccentricity:
0006672
Arg of perigee: 95
2886 deg
Mean anomaly: 264
9028 deg
Mean motion: 15
54318646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 344
Coasting Arc #9 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2016/297/09:59:09
000
Vector Time (MET): N/A
Weight (LBS) : 895949
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1842201
51 A = 6783314
73 meter
Y = -5472305
43 meter E =
0018712
Z = 3543393
58 I = 51
89136
XDOT = 6153
559834 Wp = 91
49722
YDOT = -859
390277 meter/sec RA = 137
37772 deg
ZDOT = -4506
430480 TA = 46
84097
MA = 46
68471
Ha = 223
074 n
mi
Hp = 211
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6043968
22 X = 1886044
86
Y = -17953757
96 feet Y = -5451459
33 meter
Z = 11625307
04 Z = 3552449
45
XDOT = 20188
844600 XDOT = 6184
602933
YDOT = -2819
521905 feet/sec YDOT = -790
403741 meter/sec
ZDOT = -14784
876903 ZDOT = -4476
462268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5596268
71 X = -1705742
70
Y = 18072226
19 feet Y = 5508414
54 meter
Z = 11665811
48 Z = 3555739
34
XDOT = -18903
701898 XDOT = -5761
848339
YDOT = 3647
503109 feet/sec YDOT = 1111
758948 meter/sec
ZDOT = -14653
561082 ZDOT = -4466
405418
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 16297
45578440
00016717 00000-0 10270-3 0 9087
2 25544 51
6423 138
2790 0006695 98
1554 262
0358 15
54350775 24937
Satellite: ISS
Catalog Number: 25544
Epoch time: 16297
45578440 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 138
2790 deg
Eccentricity:
0006695
Arg of perigee: 98
1554 deg
Mean anomaly: 262
0358 deg
Mean motion: 15
54350775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 338
Coasting Arc #10 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2016/297/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5710727
22 A = 6785079
21 meter
Y = 2093300
71 meter E =
0019618
Z = 2989456
02 I = 51
89655
XDOT = 501
929091 Wp = 88
17471
YDOT = -5803
488446 meter/sec RA = 137
19861 deg
ZDOT = 4994
988446 TA = 305
91964
MA = 306
10154
Ha = 223
176 n
mi
Hp = 212
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18735981
69 X = -5748232
25
Y = 6867784
49 feet Y = 2029230
01 meter
Z = 9807926
57 Z = 2961623
23
XDOT = 1646
748985 XDOT = 542
524122
YDOT = -19040
316425 feet/sec YDOT = -5797
648253 meter/sec
ZDOT = 16387
757368 ZDOT = 4997
525673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15822663
76 X = 4822747
91
Y = -12256761
78 feet Y = -3735860
99 meter
Z = 9685762
73 Z = 2952220
48
XDOT = 3424
323172 XDOT = 1043
733703
YDOT = 17452
784492 feet/sec YDOT = 5319
608713 meter/sec
ZDOT = 16399
780210 ZDOT = 4998
653008
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 16297
52007852
00016717 00000-0 10270-3 0 9090
2 25544 51
6410 137
9577 0006588 99
1008 261
0890 15
54319806 24949
Satellite: ISS
Catalog Number: 25544
Epoch time: 16297
52007852 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 137
9577 deg
Eccentricity:
0006588
Arg of perigee: 99
1008 deg
Mean anomaly: 261
0890 deg
Mean motion: 15
54319806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2494
Checksum: 333
Coasting Arc #11 (Orbit 2508)
---------------------------------------
Vector Time (GMT): 2016/298/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5203630
91 A = 6781036
14 meter
Y = -715381
67 meter E =
0014118
Z = -4301648
66 I = 51
90593
XDOT = -2064
320923 Wp = 84
64524
YDOT = 6447
806063 meter/sec RA = 132
23034 deg
ZDOT = -3578
275593 TA = 148
97291
MA = 148
88944
Ha = 223
051 n
mi
Hp = 212
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17072279
88 X = 5232139
51
Y = -2347052
72 feet Y = -657032
09 meter
Z = -14113020
54 Z = -4276301
17
XDOT = -6772
706441 XDOT = -2118
886610
YDOT = 21154
219367 feet/sec YDOT = 6424
416080 meter/sec
ZDOT = -11739
749321 ZDOT = -3588
436663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15507440
98 X = -4726668
01
Y = 7720986
88 feet Y = 2353356
80 meter
Z = -14001942
05 Z = -4267791
94
XDOT = 132
841967 XDOT = 40
490231
YDOT = -21052
843216 feet/sec YDOT = -6416
906612 meter/sec
ZDOT = -11785
256637 ZDOT = -3592
146223
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 16298
48448642
00016717 00000-0 10270-3 0 9104
2 25544 51
6407 133
1484 0006468 103
0848 257
1027 15
54329768 25097
Satellite: ISS
Catalog Number: 25544
Epoch time: 16298
48448642 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 133
1484 deg
Eccentricity:
0006468
Arg of perigee: 103
0848 deg
Mean anomaly: 257
1027 deg
Mean motion: 15
54329768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2509
Checksum: 325
Coasting Arc #12 (Orbit 2524)
---------------------------------------
Vector Time (GMT): 2016/299/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4391638
23 A = 6777890
49 meter
Y = -814637
75 meter E =
0011908
Z = 5090009
25 I = 51
91626
XDOT = 3322
311430 Wp = 114
61115
YDOT = -6684
050496 meter/sec RA = 127
25296 deg
ZDOT = 1788
607772 TA = 318
12253
MA = 318
21356
Ha = 223
243 n
mi
Hp = 212
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14408261
92 X = -4406927
72
Y = -2672696
03 feet Y = -863833
05 meter
Z = 16699505
42 Z = 5068638
46
XDOT = 10899
971882 XDOT = 3388
118877
YDOT = -21929
299528 feet/sec YDOT = -6646
530075 meter/sec
ZDOT = 5868
135735 ZDOT = 1804
907329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14568489
11 X = 4440475
48
Y = -2369022
93 feet Y = -722078
19 meter
Z = 16606072
76 Z = 5061530
98
XDOT = -3022
393244 XDOT = -921
225461
YDOT = 23242
541366 feet/sec YDOT = 7084
326608 meter/sec
ZDOT = 5940
566718 ZDOT = 1810
684736
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 16299
51318177
00016717 00000-0 10270-3 0 9119
2 25544 51
6407 128
0183 0006625 106
0926 254
0957 15
54314560 25251
Satellite: ISS
Catalog Number: 25544
Epoch time: 16299
51318177 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 128
0183 deg
Eccentricity:
0006625
Arg of perigee: 106
0926 deg
Mean anomaly: 254
0957 deg
Mean motion: 15
54314560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2525
Checksum: 304
Coasting Arc #13 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2016/300/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3401253
36 A = 6776708
74 meter
Y = 2451106
17 meter E =
0021222
Z = -5342433
12 I = 51
92945
XDOT = -4233
154813 Wp = 97
56372
YDOT = 6371
838534 meter/sec RA = 122
26982 deg
ZDOT = 226
417722 TA = 174
60142
MA = 174
57850
Ha = 222
997 n
mi
Hp = 212
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11158967
71 X = 3399543
29
Y = 8041686
89 feet Y = 2489131
21 meter
Z = -17527667
73 Z = -5325914
83
XDOT = -13888
303193 XDOT = -4305
191577
YDOT = 20904
982066 feet/sec YDOT = 6324
097793 meter/sec
ZDOT = 742
840295 ZDOT = 205
678257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13383371
13 X = -4079251
52
Y = -3548650
17 feet Y = -1081628
57 meter
Z = -17455740
71 Z = -5320509
77
XDOT = 5369
747565 XDOT = 1636
699058
YDOT = -23485
283666 feet/sec YDOT = -7158
314461 meter/sec
ZDOT = 651
006216 ZDOT = 198
426695
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 16300
47757526
00016717 00000-0 10270-3 0 9123
2 25544 51
6387 123
2084 0006613 110
3871 249
7992 15
54357829 25401
Satellite: ISS
Catalog Number: 25544
Epoch time: 16300
47757526 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 123
2084 deg
Eccentricity:
0006613
Arg of perigee: 110
3871 deg
Mean anomaly: 249
7992 deg
Mean motion: 15
54357829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2540
Checksum: 318
Coasting Arc #14 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2016/301/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2309260
95 A = 6778260
49 meter
Y = -3990042
22 meter E =
0011255
Z = 4959632
24 I = 51
95170
XDOT = 4816
611602 Wp = 86
59723
YDOT = -5550
476869 meter/sec RA = 117
28957 deg
ZDOT = -2217
738840 TA = 24
95262
MA = 24
89825
Ha = 223
010 n
mi
Hp = 212
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7576315
44 X = -2288563
83
Y = -13090689
71 feet Y = -4015749
74 meter
Z = 16271759
32 Z = 4948464
88
XDOT = 15802
531503 XDOT = 4889
093483
YDOT = -18210
225949 feet/sec YDOT = -5496
209222 meter/sec
ZDOT = -7276
046063 ZDOT = -2194
163955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11966164
20 X = 3647286
85
Y = 9335169
29 feet Y = 2845359
60 meter
Z = 16223513
57 Z = 4944926
94
XDOT = -7338
156655 XDOT = -2236
670148
YDOT = 21898
760525 feet/sec YDOT = 6674
742208 meter/sec
ZDOT = -7171
915318 ZDOT = -2185
999789
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 16301
50625585
00016717 00000-0 10270-3 0 9138
2 25544 51
6392 118
0787 0006459 114
9139 245
2685 15
54356926 25568
Satellite: ISS
Catalog Number: 25544
Epoch time: 16301
50625585 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 118
0787 deg
Eccentricity:
0006459
Arg of perigee: 114
9139 deg
Mean anomaly: 245
2685 deg
Mean motion: 15
54356926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2556
Checksum: 330
Coasting Arc #15 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2016/302/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1240662
14 A = 6781700
66 meter
Y = 5310178
54 meter E =
0013660
Z = -4046471
55 I = 51
97660
XDOT = -5053
527146 Wp = 113
06488
YDOT = 4184
193272 meter/sec RA = 112
31625 deg
ZDOT = 3946
849077 TA = 197
78294
MA = 197
83080
Ha = 222
912 n
mi
Hp = 212
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4070413
84 X = 1200846
59
Y = 17421845
60 feet Y = 5323829
47 meter
Z = -13275825
28 Z = -4040541
78
XDOT = -16579
813471 XDOT = -5119
112773
YDOT = 13727
668214 feet/sec YDOT = 4127
314982 meter/sec
ZDOT = 12948
979910 ZDOT = 3922
140109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10536833
26 X = -3211626
78
Y = -14482044
00 feet Y = -4414127
01 meter
Z = -13250737
95 Z = -4038824
93
XDOT = 9045
210685 XDOT = 2756
980217
YDOT = -18313
354678 feet/sec YDOT = -5581
910506 meter/sec
ZDOT = 12840
093357 ZDOT = 3913
660455
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 16302
47063682
00016717 00000-0 10270-3 0 9140
2 25544 51
6384 113
2681 0006619 118
0379 242
1444 15
54378483 25716
Satellite: ISS
Catalog Number: 25544
Epoch time: 16302
47063682 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 113
2681 deg
Eccentricity:
0006619
Arg of perigee: 118
0379 deg
Mean anomaly: 242
1444 deg
Mean motion: 15
54378483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2571
Checksum: 310
Coasting Arc #16 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2016/303/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 910476
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -201469
58 A = 6785581
89 meter
Y = -6241344
62 meter E =
0019749
Z = 2629295
65 I = 52
00106
XDOT = 5052
822514 Wp = 108
85034
YDOT = -2390
104654 meter/sec RA = 107
35613 deg
ZDOT = -5260
466650 TA = 41
64838
MA = 41
49815
Ha = 222
774 n
mi
Hp = 212
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -660989
43 X = -144434
59
Y = -20476852
43 feet Y = -6243278
48 meter
Z = 8626298
07 Z = 2628455
97
XDOT = 16577
501685 XDOT = 5104
727434
YDOT = -7841
550703 feet/sec YDOT = -2333
310805 meter/sec
ZDOT = -17258
748853 ZDOT = -5235
794448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8856211
60 X = 2699373
29
Y = 18475694
60 feet Y = 5631391
71 meter
Z = 8623667
20 Z = 2628493
76
XDOT = -10804
579326 XDOT = -3293
235779
YDOT = 13223
850233 feet/sec YDOT = 4030
629551 meter/sec
ZDOT = -17150
310062 ZDOT = -5227
414507
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 16303
49930073
00016717 00000-0 10270-3 0 9151
2 25544 51
6383 108
1379 0006393 121
6965 238
4811 15
54410159 25872
Satellite: ISS
Catalog Number: 25544
Epoch time: 16303
49930073 = yrday
fracday
Element set: 915
Inclination: 51
6383 deg
RA of node: 108
1379 deg
Eccentricity:
0006393
Arg of perigee: 121
6965 deg
Mean anomaly: 238
4811 deg
Mean motion: 15
54410159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2587
Checksum: 317
Coasting Arc #17 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2016/304/00:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4378418
38 A = 6778015
74 meter
Y = 1289429
90 meter E =
0012667
Z = 5003837
92 I = 51
98093
XDOT = 230
873613 Wp = 122
80069
YDOT = -7379
881535 meter/sec RA = 104
59756 deg
ZDOT = 2093
209038 TA = 306
88536
MA = 307
00140
Ha = 222
945 n
mi
Hp = 212
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14364889
69 X = -4416818
80
Y = 4230413
06 feet Y = 1240253
14 meter
Z = 16416791
09 Z = 4982474
76
XDOT = 757
459361 XDOT = 303
212008
YDOT = -24212
209759 feet/sec YDOT = -7376
895130 meter/sec
ZDOT = 6867
483722 ZDOT = 2094
506837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6706710
30 X = -2044205
30
Y = 13503200
82 feet Y = 4115775
61 meter
Z = 16323023
15 Z = 4975257
46
XDOT = -16321
293210 XDOT = -4974
730170
YDOT = -16458
307073 feet/sec YDOT = -5016
491996 meter/sec
ZDOT = 6874
413906 ZDOT = 2095
321359
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 16304
07792374
00016717 00000-0 10270-3 0 9167
2 25544 51
6383 105
2555 0006522 122
5019 237
6765 15
54399728 25967
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
07792374 = yrday
fracday
Element set: 916
Inclination: 51
6383 deg
RA of node: 105
2555 deg
Eccentricity:
0006522
Arg of perigee: 122
5019 deg
Mean anomaly: 237
6765 deg
Mean motion: 15
54399728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 328
Coasting Arc #18 (Orbit 2596)
---------------------------------------
Vector Time (GMT): 2016/304/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4312155
98 A = 6777091
01 meter
Y = 454965
15 meter E =
0010783
Z = 5201830
37 I = 51
97994
XDOT = 830
738213 Wp = 123
65143
YDOT = -7511
555381 meter/sec RA = 104
26656 deg
ZDOT = 1337
828678 TA = 313
52033
MA = 313
60988
Ha = 222
887 n
mi
Hp = 212
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14147493
38 X = -4342191
93
Y = 1492667
81 feet Y = 406576
16 meter
Z = 17066372
59 Z = 5180809
47
XDOT = 2725
519070 XDOT = 908
173839
YDOT = -24644
210569 feet/sec YDOT = -7501
832444 meter/sec
ZDOT = 4389
201699 ZDOT = 1342
052926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3234887
84 X = -985993
81
Y = 13966074
44 feet Y = 4256859
49 meter
Z = 16974244
17 Z = 5173749
62
XDOT = -21400
299621 XDOT = -6522
811325
YDOT = -10346
761527 feet/sec YDOT = -3153
692913 meter/sec
ZDOT = 4408
970472 ZDOT = 1343
854200
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 16304
14221440
00016717 00000-0 10270-3 0 9177
2 25544 51
6396 104
9351 0006437 122
8522 237
3251 15
54421667 25974
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
14221440 = yrday
fracday
Element set: 917
Inclination: 51
6396 deg
RA of node: 104
9351 deg
Eccentricity:
0006437
Arg of perigee: 122
8522 deg
Mean anomaly: 237
3251 deg
Mean motion: 15
54421667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2597
Checksum: 295
Coasting Arc #19 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2016/305/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3968633
80 A = 6776739
66 meter
Y = 1462245
05 meter E =
0020439
Z = -5312449
22 I = 51
98632
XDOT = -1775
047820 Wp = 104
68712
YDOT = 7411
126409 meter/sec RA = 99
28640 deg
ZDOT = 711
110877 TA = 172
10139
MA = 172
06915
Ha = 222
745 n
mi
Hp = 212
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13020452
11 X = 3977793
94
Y = 4797391
89 feet Y = 1506675
89 meter
Z = -17429295
34 Z = -5293147
90
XDOT = -5823
647703 XDOT = -1861
243367
YDOT = 24314
719188 feet/sec YDOT = 7390
794724 meter/sec
ZDOT = 2333
040934 ZDOT = 702
278121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8626790
79 X = 2629445
83
Y = -11002553
16 feet Y = -3353578
20 meter
Z = -17345021
85 Z = -5286762
66
XDOT = 20509
594708 XDOT = 6251
324467
YDOT = 12451
735330 feet/sec YDOT = 3795
288929 meter/sec
ZDOT = 2293
087448 ZDOT = 698
933054
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 16305
10657797
00016717 00000-0 10270-3 0 9183
2 25544 51
6404 100
1249 0006444 125
8941 234
2811 15
54398180 26123
Satellite: ISS
Catalog Number: 25544
Epoch time: 16305
10657797 = yrday
fracday
Element set: 918
Inclination: 51
6404 deg
RA of node: 100
1249 deg
Eccentricity:
0006444
Arg of perigee: 125
8941 deg
Mean anomaly: 234
2811 deg
Mean motion: 15
54398180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 300
Coasting Arc #20 (Orbit 2627)
---------------------------------------
Vector Time (GMT): 2016/306/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 895244
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3499312
72 A = 6778863
71 meter
Y = -3278408
62 meter E =
0011706
Z = 4781400
40 I = 51
99851
XDOT = 2607
265489 Wp = 92
09005
YDOT = -6703
106634 meter/sec RA = 94
31078 deg
ZDOT = -2682
667088 TA = 24
26461
MA = 24
20953
Ha = 222
812 n
mi
Hp = 212
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11480684
78 X = -3485619
26
Y = -10755933
78 feet Y = -3317463
52 meter
Z = 15687009
18 Z = 4764434
54
XDOT = 8554
020634 XDOT = 2695
059161
YDOT = -21991
819664 feet/sec YDOT = -6673
459665 meter/sec
ZDOT = -8801
401206 ZDOT = -2669
787780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13678147
11 X = -4169099
24
Y = 7919106
30 feet Y = 2413743
60 meter
Z = 15613280
83 Z = 4758928
00
XDOT = -17923
126993 XDOT = -5462
969107
YDOT = -13684
175444 feet/sec YDOT = -4170
936675 meter/sec
ZDOT = -8743
828359 ZDOT = -2665
118884
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 16306
13522293
00016717 00000-0 10270-3 0 9190
2 25544 51
6410 94
9956 0006419 128
6695 231
5033 15
54413945 26284
Satellite: ISS
Catalog Number: 25544
Epoch time: 16306
13522293 = yrday
fracday
Element set: 919
Inclination: 51
6410 deg
RA of node: 94
9956 deg
Eccentricity:
0006419
Arg of perigee: 128
6695 deg
Mean anomaly: 231
5033 deg
Mean motion: 15
54413945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2628
Checksum: 318
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