[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 17th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 67 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
There are no maneuvers
Coasting Arc #1 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2016/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5161107
08 A = 6785314
15 meter
Y = -3283396
09 meter E =
0005049
Z = -2940520
29 I = 51
72150
XDOT = 4858
979076 Wp = 92
56297
YDOT = -3151
066087 meter/sec RA = 10
17023 deg
ZDOT = -5017
494259 TA = 120
93506
MA = 120
88542
Ha = 221
201 n
mi
Hp = 214
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16932766
00 X = -5109723
94
Y = -10772296
90 feet Y = -3340823
94 meter
Z = -9647376
27 Z = -2965466
64
XDOT = 15941
532403 XDOT = 4918
226813
YDOT = -10338
143331 feet/sec YDOT = -3096
398846 meter/sec
ZDOT = -16461
595338 ZDOT = -4993
746388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19751707
36 X = -6020320
40
Y = -3246616
47 feet Y = -989568
70 meter
Z = -9755119
25 Z = -2973360
35
XDOT = 10431
915295 XDOT = 3179
647782
YDOT = -14389
921171 feet/sec YDOT = -4386
047973 meter/sec
ZDOT = -16357
780420 ZDOT = -4985
851472
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 16106
52611860
00016717 00000-0 10270-3 0 9000
2 25544 51
6447 10
5796 0001651 30
2064 329
9184 15
54219945 35239
Satellite: ISS
Catalog Number: 25544
Epoch time: 16106
52611860 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 10
5796 deg
Eccentricity:
0001651
Arg of perigee: 30
2064 deg
Mean anomaly: 329
9184 deg
Mean motion: 15
54219945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 293
Coasting Arc #2 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2016/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3825553
44 A = 6781420
11 meter
Y = 3686025
33 meter E =
0010754
Z = 4206590
36 I = 51
67684
XDOT = -6312
732984 Wp = 96
77305
YDOT = 2344
914053 meter/sec RA = 5
18906 deg
ZDOT = 3676
884884 TA = 315
53324
MA = 315
61952
Ha = 221
178 n
mi
Hp = 214
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12551028
36 X = 3763617
22
Y = 12093258
97 feet Y = 3728459
27 meter
Z = 13801149
46 Z = 4225023
22
XDOT = -20711
066221 XDOT = -6356
345983
YDOT = 7693
287575 feet/sec YDOT = 2274
077334 meter/sec
ZDOT = 12063
270616 ZDOT = 3646
113015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16326000
65 X = 4976165
00
Y = 5919477
93 feet Y = 1804256
87 meter
Z = 13880505
59 Z = 4230778
10
XDOT = -15372
080352 XDOT = -4685
410091
YDOT = 14352
843385 feet/sec YDOT = 4374
746664 meter/sec
ZDOT = 11929
103977 ZDOT = 3635
990892
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 16107
55488310
00016717 00000-0 10270-3 0 9017
2 25544 51
6446 5
4500 0001731 35
1503 324
9764 15
54234364 35393
Satellite: ISS
Catalog Number: 25544
Epoch time: 16107
55488310 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 5
4500 deg
Eccentricity:
0001731
Arg of perigee: 35
1503 deg
Mean anomaly: 324
9764 deg
Mean motion: 15
54234364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 284
Coasting Arc #3 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2016/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2152579
08 A = 6778077
45 meter
Y = -4000109
27 meter E =
0014395
Z = -5043830
48 I = 51
63450
XDOT = 7262
310364 Wp = 70
96053
YDOT = -1491
986633 meter/sec RA =
19530 deg
ZDOT = -1916
009383 TA = 180
42915
MA = 180
43039
Ha = 221
177 n
mi
Hp = 213
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7062267
31 X = -2083188
01
Y = -13123718
06 feet Y = -4023793
33 meter
Z = -16548000
27 Z = -5054118
29
XDOT = 23826
477572 XDOT = 7287
761567
YDOT = -4894
969269 feet/sec YDOT = -1410
632523 meter/sec
ZDOT = -6286
120024 ZDOT = -1880
668796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11881916
55 X = -3621608
16
Y = -8914749
47 feet Y = -2717215
64 meter
Z = -16591901
91 Z = -5057211
70
XDOT = 18860
843422 XDOT = 5748
785075
YDOT = -13724
522296 feet/sec YDOT = -4183
234396 meter/sec
ZDOT = -6132
283634 ZDOT = -1869
120052
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 16108
51933851
00016717 00000-0 10270-3 0 9020
2 25544 51
6451
6413 0001729 34
2521 325
8743 15
54278349 35541
Satellite: ISS
Catalog Number: 25544
Epoch time: 16108
51933851 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node:
6413 deg
Eccentricity:
0001729
Arg of perigee: 34
2521 deg
Mean anomaly: 325
8743 deg
Mean motion: 15
54278349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 295
Coasting Arc #4 (Orbit 3569)
---------------------------------------
Vector Time (GMT): 2016/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 298130
81 A = 6776849
49 meter
Y = 4197807
59 meter E =
0003693
Z = 5308915
94 I = 51
59847
XDOT = -7647
781480 Wp = 65
02242
YDOT = 605
315471 meter/sec RA = 355
19273 deg
ZDOT = -47
602169 TA = 25
44031
MA = 25
42213
Ha = 221
132 n
mi
Hp = 214
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 978119
44 X = 225379
10
Y = 13772334
62 feet Y = 4200735
24 meter
Z = 17417703
22 Z = 5310187
07
XDOT = -25091
146589 XDOT = -7653
750636
YDOT = 1985
943146 feet/sec YDOT = 519
759509 meter/sec
ZDOT = -156
175095 ZDOT = -84
767995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6855046
03 X = 2089418
03
Y = 11978267
90 feet Y = 3650976
05 meter
Z = 17422392
09 Z = 5310345
11
XDOT = -20765
145898 XDOT = -6329
216470
YDOT = 12353
268573 feet/sec YDOT = 3765
276261 meter/sec
ZDOT = -317
752321 ZDOT = -96
850907
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 16109
54808055
00016717 00000-0 10270-3 0 9032
2 25544 51
6451 355
5118 0001640 35
6245 324
5017 15
54299015 35706
Satellite: ISS
Catalog Number: 25544
Epoch time: 16109
54808055 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 355
5118 deg
Eccentricity:
0001640
Arg of perigee: 35
6245 deg
Mean anomaly: 324
5017 deg
Mean motion: 15
54299015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3570
Checksum: 292
Coasting Arc #5 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2016/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1558243
51 A = 6778247
54 meter
Y = -4304305
22 meter E =
0013369
Z = -5010979
45 I = 51
57099
XDOT = 7382
960953 Wp = 98
00817
YDOT = 339
291600 meter/sec RA = 350
18781 deg
ZDOT = 2007
179452 TA = 191
52224
MA = 191
55287
Ha = 221
141 n
mi
Hp = 214
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5112347
46 X = 1630600
94
Y = -14121736
27 feet Y = -4286475
82 meter
Z = -16440221
29 Z = -5003233
64
XDOT = 24222
312837 XDOT = 7368
868074
YDOT = 1113
161416 feet/sec YDOT = 421
774182 meter/sec
ZDOT = 6585
234421 ZDOT = 2043
010136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1806860
54 X = -550731
09
Y = -14947508
05 feet Y = -4556000
45 meter
Z = -16405720
53 Z = -5000463
62
XDOT = 20930
001480 XDOT = 6379
464451
YDOT = -9918
432798 feet/sec YDOT = -3023
138317 meter/sec
ZDOT = 6740
811158 ZDOT = 2054
599241
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 16110
51251731
00016717 00000-0 10270-3 0 9045
2 25544 51
6449 350
7026 0001670 35
9233 324
2032 15
54301345 35851
Satellite: ISS
Catalog Number: 25544
Epoch time: 16110
51251731 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 350
7026 deg
Eccentricity:
0001670
Arg of perigee: 35
9233 deg
Mean anomaly: 324
2032 deg
Mean motion: 15
54301345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 270
Coasting Arc #6 (Orbit 3600)
---------------------------------------
Vector Time (GMT): 2016/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3271763
73 A = 6781523
86 meter
Y = 4259633
44 meter E =
0011871
Z = 4133128
30 I = 51
55083
XDOT = -6544
110214 Wp = 70
52834
YDOT = -1361
297824 meter/sec RA = 345
18788 deg
ZDOT = -3764
620271 TA = 58
32962
MA = 58
21391
Ha = 221
153 n
mi
Hp = 213
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10734132
98 X = -3339230
09
Y = 13975175
34 feet Y = 4222669
56 meter
Z = 13560132
23 Z = 4117070
42
XDOT = -21470
177866 XDOT = -6510
114308
YDOT = -4466
200209 feet/sec YDOT = -1434
288681 meter/sec
ZDOT = -12351
116376 ZDOT = -3796
327661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2945695
97 X = -897848
13
Y = 17428698
22 feet Y = 5312267
22 meter
Z = 13489539
51 Z = 4111611
64
XDOT = -19696
237964 XDOT = -6003
413331
YDOT = 6369
434216 feet/sec YDOT = 1941
403549 meter/sec
ZDOT = -12488
568158 ZDOT = -3806
515575
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 16111
54123815
00016717 00000-0 10270-3 0 9051
2 25544 51
6449 345
5732 0001747 35
4827 324
6442 15
54344937 36018
Satellite: ISS
Catalog Number: 25544
Epoch time: 16111
54123815 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 345
5732 deg
Eccentricity:
0001747
Arg of perigee: 35
4827 deg
Mean anomaly: 324
6442 deg
Mean motion: 15
54344937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3601
Checksum: 303
Coasting Arc #7 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2016/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4649893
48 A = 6785478
74 meter
Y = -4056799
77 meter E =
0006300
Z = -2821136
51 I = 51
53224
XDOT = 5195
142917 Wp = 53
23690
YDOT = 2425
079077 meter/sec RA = 340
19574 deg
ZDOT = 5087
117301 TA = 274
68732
MA = 274
75927
Ha = 221
152 n
mi
Hp = 214
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15255556
02 X = 4708616
13
Y = -13309710
54 feet Y = -4004473
46 meter
Z = -9255697
21 Z = -2798405
16
XDOT = 17044
432144 XDOT = 5142
927520
YDOT = 7956
296185 feet/sec YDOT = 2482
883074 meter/sec
ZDOT = 16690
017392 ZDOT = 5112
227408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6894559
80 X = 2101461
83
Y = -19083448
02 feet Y = -5816634
96 meter
Z = -9156165
79 Z = -2790799
33
XDOT = 17276
488102 XDOT = 5265
873573
YDOT = -1799
752271 feet/sec YDOT = -548
564492 meter/sec
ZDOT = 16798
594512 ZDOT = 5120
211607
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 16112
50565545
00016717 00000-0 10270-3 0 9069
2 25544 51
6441 340
7635 0001667 36
4148 323
7118 15
54315628 36168
Satellite: ISS
Catalog Number: 25544
Epoch time: 16112
50565545 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 340
7635 deg
Eccentricity:
0001667
Arg of perigee: 36
4148 deg
Mean anomaly: 323
7118 deg
Mean motion: 15
54315628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 301
Coasting Arc #8 (Orbit 3631)
---------------------------------------
Vector Time (GMT): 2016/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5625341
58 A = 6788247
29 meter
Y = 3608715
81 meter E =
0014104
Z = 1154248
96 I = 51
51148
XDOT = -3474
284090 Wp = 115
78519
YDOT = -3526
121670 meter/sec RA = 335
21215 deg
ZDOT = -5858
159280 TA = 51
65699
MA = 51
53032
Ha = 221
173 n
mi
Hp = 213
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18455845
07 X = -5670884
00
Y = 11839618
81 feet Y = 3545554
93 meter
Z = 3786906
05 Z = 1126811
10
XDOT = -11398
569849 XDOT = -3406
138945
YDOT = -11568
640651 feet/sec YDOT = -3564
592783 meter/sec
ZDOT = -19219
682678 ZDOT = -5874
871054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10040889
60 X = -3060463
15
Y = 19515862
15 feet Y = 5948434
78 meter
Z = 3667030
01 Z = 1117710
75
XDOT = -14135
903714 XDOT = -4308
623452
YDOT = -3616
314961 feet/sec YDOT = -1102
252800 meter/sec
ZDOT = -19291
561049 ZDOT = -5880
067808
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 16113
53435719
00016717 00000-0 10270-3 0 9073
2 25544 51
6438 335
6338 0001659 45
2850 314
8438 15
54319221 36323
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
53435719 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 335
6338 deg
Eccentricity:
0001659
Arg of perigee: 45
2850 deg
Mean anomaly: 314
8438 deg
Mean motion: 15
54319221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3632
Checksum: 310
Coasting Arc #9 (Orbit 3647)
---------------------------------------
Vector Time (GMT): 2016/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6087866
57 A = 6788454
77 meter
Y = -2924585
56 meter E =
0014733
Z = 608322
42 I = 51
48303
XDOT = 1585
814317 Wp = 50
57301
YDOT = 4559
265461 meter/sec RA = 330
22961 deg
ZDOT = 5961
582195 TA = 316
01054
MA = 316
12771
Ha = 221
050 n
mi
Hp = 213
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19973315
53 X = 6117162
53
Y = -9595096
98 feet Y = -2856343
15 meter
Z = 1995808
46 Z = 637967
63
XDOT = 5202
802876 XDOT = 1505
754237
YDOT = 14958
220017 feet/sec YDOT = 4576
551734 meter/sec
ZDOT = 19558
996703 ZDOT = 5969
091159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12131076
10 X = 3697552
00
Y = -18528445
54 feet Y = -5647470
20 meter
Z = 2125128
05 Z = 647739
03
XDOT = 10725
570826 XDOT = 3269
153988
YDOT = 9300
175923 feet/sec YDOT = 2834
693621 meter/sec
ZDOT = 19590
701759 ZDOT = 5971
245896
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 16114
56304580
00016717 00000-0 10270-3 0 9089
2 25544 51
6428 330
5027 0001589 43
2474 316
8804 15
54369501 36485
Satellite: ISS
Catalog Number: 25544
Epoch time: 16114
56304580 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 330
5027 deg
Eccentricity:
0001589
Arg of perigee: 43
2474 deg
Mean anomaly: 316
8804 deg
Mean motion: 15
54369501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3648
Checksum: 308
Coasting Arc #10 (Orbit 3662)
---------------------------------------
Vector Time (GMT): 2016/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6067034
51 A = 6786266
59 meter
Y = 1936463
51 meter E =
0005847
Z = -2343715
19 I = 51
44747
XDOT = 333
667167 Wp = 117
89228
YDOT = -5449
159903 meter/sec RA = 325
24355 deg
ZDOT = -5379
009975 TA = 88
31536
MA = 88
24839
Ha = 221
051 n
mi
Hp = 213
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19904968
86 X = -6076852
63
Y = 6353226
75 feet Y = 1868562
93 meter
Z = -7689354
29 Z = -2373211
81
XDOT = 1094
708553 XDOT = 420
705658
YDOT = -17877
821204 feet/sec YDOT = -5444
942121 meter/sec
ZDOT = -17647
670523 ZDOT = -5377
177493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13444541
56 X = -4097896
27
Y = 15931833
69 feet Y = 4856022
91 meter
Z = -7817827
20 Z = -2382873
73
XDOT = -7315
256057 XDOT = -2229
690046
YDOT = -14808
016415 feet/sec YDOT = -4513
483403 meter/sec
ZDOT = -17638
633697 ZDOT = -5376
255551
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 16115
52743427
00016717 00000-0 10270-3 0 9094
2 25544 51
6420 325
6931 0001555 44
3374 315
7903 15
54352567 36639
Satellite: ISS
Catalog Number: 25544
Epoch time: 16115
52743427 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 325
6931 deg
Eccentricity:
0001555
Arg of perigee: 44
3374 deg
Mean anomaly: 315
7903 deg
Mean motion: 15
54352567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3663
Checksum: 307
Coasting Arc #11 (Orbit 3678)
---------------------------------------
Vector Time (GMT): 2016/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5578658
90 A = 6782434
13 meter
Y = -717048
70 meter E =
0012455
Z = 3779645
64 I = 51
40867
XDOT = -2070
765009 Wp = 91
20619
YDOT = 6079
830206 meter/sec RA = 320
24517 deg
ZDOT = 4197
572629 TA = 314
32189
MA = 314
42393
Ha = 220
944 n
mi
Hp = 213
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18302686
67 X = 5567902
27
Y = -2352521
98 feet Y = -654724
50 meter
Z = 12400412
20 Z = 3806719
74
XDOT = -6793
848455 XDOT = -2158
987652
YDOT = 19946
949496 feet/sec YDOT = 6056
180323 meter/sec
ZDOT = 13771
563744 ZDOT = 4187
298801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13984686
51 X = 4262532
45
Y = -11917135
76 feet Y = -3632342
98 meter
Z = 12518120
47 Z = 3815523
12
XDOT = 4253
422303 XDOT = 1296
443118
YDOT = 19451
117551 feet/sec YDOT = 5928
700630 meter/sec
ZDOT = 13725
749145 ZDOT = 4183
608339
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 16116
55610445
00016717 00000-0 10270-3 0 9103
2 25544 51
6416 320
5616 0001607 44
4043 315
7238 15
54374266 36798
Satellite: ISS
Catalog Number: 25544
Epoch time: 16116
55610445 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 320
5616 deg
Eccentricity:
0001607
Arg of perigee: 44
4043 deg
Mean anomaly: 315
7238 deg
Mean motion: 15
54374266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3679
Checksum: 295
Coasting Arc #12 (Orbit 3693)
---------------------------------------
Vector Time (GMT): 2016/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4731237
70 A = 6778630
71 meter
Y = -724084
03 meter E =
0013174
Z = -4812664
63 I = 51
37101
XDOT = 3521
234443 Wp = 69
40088
YDOT = -6319
781737 meter/sec RA = 315
23406 deg
ZDOT = -2511
870643 TA = 175
77891
MA = 175
76779
Ha = 221
063 n
mi
Hp = 213
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15522433
39 X = -4699410
95
Y = -2375603
76 feet Y = -776813
95 meter
Z = -15789582
13 Z = -4835570
85
XDOT = 11552
606441 XDOT = 3603
843890
YDOT = -20734
192051 feet/sec YDOT = -6279
943072 meter/sec
ZDOT = -8241
045416 ZDOT = -2494
564404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14105389
20 X = -4299322
63
Y = 6669407
16 feet Y = 2032835
30 meter
Z = -15888906
16 Z = -4842938
60
XDOT = -1515
763909 XDOT = -462
004839
YDOT = -22648
714013 feet/sec YDOT = -6903
328031 meter/sec
ZDOT = -8164
651370 ZDOT = -2488
585738
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 16117
52047300
00016717 00000-0 10270-3 0 9116
2 25544 51
6405 315
7513 0001608 51
5113 308
6184 15
54395412 36940
Satellite: ISS
Catalog Number: 25544
Epoch time: 16117
52047300 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 315
7513 deg
Eccentricity:
0001608
Arg of perigee: 51
5113 deg
Mean anomaly: 308
6184 deg
Mean motion: 15
54395412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3694
Checksum: 280
Coasting Arc #13 (Orbit 3709)
---------------------------------------
Vector Time (GMT): 2016/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3617819
01 A = 6776715
81 meter
Y = 2247447
23 meter E =
0003940
Z = 5267664
55 I = 51
34259
XDOT = -4598
210791 Wp = 91
16310
YDOT = 6117
332954 meter/sec RA = 310
21272 deg
ZDOT = 547
648040 TA = 353
58982
MA = 353
59486
Ha = 221
009 n
mi
Hp = 213
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11869484
93 X = 3566830
23
Y = 7373514
52 feet Y = 2287619
00 meter
Z = 17282364
00 Z = 5285115
38
XDOT = -15085
993408 XDOT = -4668
934857
YDOT = 20069
990006 feet/sec YDOT = 6065
517262 meter/sec
ZDOT = 1796
745538 ZDOT = 525
139001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13861132
05 X = 4224873
05
Y = -716053
19 feet Y = -218253
01 meter
Z = 17357700
90 Z = 5290627
24
XDOT = -883
399018 XDOT = -269
260021
YDOT = 24089
958965 feet/sec YDOT = 7342
619493 meter/sec
ZDOT = 1697
805732 ZDOT = 517
491187
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 16118
54912404
00016717 00000-0 10270-3 0 9126
2 25544 51
6408 310
6204 0001646 55
8087 304
3221 15
54374675 37105
Satellite: ISS
Catalog Number: 25544
Epoch time: 16118
54912404 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 310
6204 deg
Eccentricity:
0001646
Arg of perigee: 55
8087 deg
Mean anomaly: 304
3221 deg
Mean motion: 15
54374675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3710
Checksum: 285
Coasting Arc #14 (Orbit 3724)
---------------------------------------
Vector Time (GMT): 2016/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2386552
73 A = 6777243
76 meter
Y = -3745155
74 meter E =
0014953
Z = -5132795
88 I = 51
32407
XDOT = 5246
256412 Wp = 97
20999
YDOT = -5376
768042 meter/sec RA = 305
18701 deg
ZDOT = 1485
755604 TA = 187
16951
MA = 187
19092
Ha = 221
057 n
mi
Hp = 213
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7829897
40 X = -2319562
93
Y = -12287256
36 feet Y = -3771469
21 meter
Z = -16839881
48 Z = -5144226
54
XDOT = 17212
127336 XDOT = 5298
773627
YDOT = -17640
315100 feet/sec YDOT = -5317
807268 meter/sec
ZDOT = 4874
526259 ZDOT = 1511
368435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13473708
90 X = -4106786
47
Y = -5393844
32 feet Y = -1644043
75 meter
Z = -16888788
66 Z = -5147702
78
XDOT = 3120
293541 XDOT = 951
065471
YDOT = -23389
298206 feet/sec YDOT = -7129
058093 meter/sec
ZDOT = 4986
791535 ZDOT = 1519
974060
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 16119
51347287
00016717 00000-0 10270-3 0 9136
2 25544 51
6401 305
8094 0001627 61
1771 298
9545 15
54430076 37251
Satellite: ISS
Catalog Number: 25544
Epoch time: 16119
51347287 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 305
8094 deg
Eccentricity:
0001627
Arg of perigee: 61
1771 deg
Mean anomaly: 298
9545 deg
Mean motion: 15
54430076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3725
Checksum: 311
Coasting Arc #15 (Orbit 3740)
---------------------------------------
Vector Time (GMT): 2016/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1113386
95 A = 6780295
66 meter
Y = 5053876
13 meter E =
0010980
Z = 4374142
98 I = 51
31667
XDOT = -5518
156437 Wp = 69
23244
YDOT = 4135
556084 meter/sec RA = 300
16671 deg
ZDOT = -3362
951115 TA = 54
98014
MA = 54
87715
Ha = 220
994 n
mi
Hp = 213
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3652844
31 X = 1035542
62
Y = 16580958
43 feet Y = 5065891
55 meter
Z = 14350862
79 Z = 4379362
45
XDOT = -18104
187787 XDOT = -5547
655239
YDOT = 13568
097387 feet/sec YDOT = 4073
683418 meter/sec
ZDOT = -11033
304182 ZDOT = -3389
828838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12827976
34 X = 3909967
19
Y = 11094659
39 feet Y = 3381652
18 meter
Z = 14372552
76 Z = 4380754
08
XDOT = -5417
904626 XDOT = -1651
377330
YDOT = 20754
964458 feet/sec YDOT = 6326
113167 meter/sec
ZDOT = -11150
814110 ZDOT = -3398
768141
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 16120
54210225
00016717 00000-0 10270-3 0 9143
2 25544 51
6402 300
6791 0001529 61
9632 298
1676 15
54432171 37417
Satellite: ISS
Catalog Number: 25544
Epoch time: 16120
54210225 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 300
6791 deg
Eccentricity:
0001529
Arg of perigee: 61
9632 deg
Mean anomaly: 298
1676 deg
Mean motion: 15
54432171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3741
Checksum: 284
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