[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 24th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
084/04:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
7
086/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 214
7
090/14:15:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
3
091/16:23:58
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
2
093/17:58:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
0
094/19:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2016/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 147858
17 A = 6781988
19 meter
Y = 5428548
85 meter E =
0006335
Z = -4068247
41 I = 51
93906
XDOT = -5820
601599 Wp = 92
97723
YDOT = 3086
824901 meter/sec RA = 124
35421 deg
ZDOT = 3912
344454 TA = 217
42753
MA = 217
47166
Ha = 220
778 n
mi
Hp = 214
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 485098
98 X = 106905
57
Y = 17810199
65 feet Y = 5429972
66 meter
Z = -13347268
41 Z = -4067629
51
XDOT = -19096
461939 XDOT = -5873
691106
YDOT = 10127
378283 feet/sec YDOT = 3021
438858 meter/sec
ZDOT = 12835
775767 ZDOT = 3883
940021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 744400
88 X = 226893
39
Y = 17802602
53 feet Y = 5426233
25 meter
Z = -13345460
54 Z = -4067696
37
XDOT = -17780
782432 XDOT = -5419
582485
YDOT = 10260
634037 feet/sec YDOT = 3127
441254 meter/sec
ZDOT = 12711
854210 ZDOT = 3874
573163
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 16083
50891392
00016717 00000-0 10270-3 0 9002
2 25544 51
6416 125
3507 0002074 344
8096 15
2994 15
54241754 31658
Satellite: ISS
Catalog Number: 25544
Epoch time: 16083
50891392 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 125
3507 deg
Eccentricity:
0002074
Arg of perigee: 344
8096 deg
Mean anomaly: 15
2994 deg
Mean motion: 15
54241754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3165
Checksum: 304
Coasting Arc #2 (Orbit 3175)
---------------------------------------
Vector Time (GMT): 2016/084/04:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3724751
59 A = 6777032
29 meter
Y = 1918677
53 meter E =
0014545
Z = -5339091
54 I = 51
93329
XDOT = -3771
705685 Wp = 81
21424
YDOT = 6660
719291 meter/sec RA = 120
90508 deg
ZDOT = -236
047934 TA = 186
53251
MA = 186
55149
Ha = 220
757 n
mi
Hp = 214
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12220313
60 X = 3728954
67
Y = 6294873
80 feet Y = 1960352
83 meter
Z = -17516704
53 Z = -5320987
71
XDOT = -12374
362485 XDOT = -3844
760563
YDOT = 21852
753578 feet/sec YDOT = 6618
133058 meter/sec
ZDOT = -774
435478 ZDOT = -254
548459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9602676
88 X = -2926895
91
Y = 9974417
06 feet Y = 3040202
32 meter
Z = -17438349
67 Z = -5315208
98
XDOT = -16593
133377 XDOT = -5057
587053
YDOT = -17480
406641 feet/sec YDOT = -5328
027944 meter/sec
ZDOT = -855
910196 ZDOT = -260
881428
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 16084
21619019
00016717 00000-0 10270-3 0 9016
2 25544 51
6401 121
8217 0001818 345
1519 14
9580 15
54247992 31769
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
21619019 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 121
8217 deg
Eccentricity:
0001818
Arg of perigee: 345
1519 deg
Mean anomaly: 14
9580 deg
Mean motion: 15
54247992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3176
Checksum: 299
Coasting Arc #3 (Orbit 3191)
---------------------------------------
Vector Time (GMT): 2016/085/04:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2743029
28 A = 6778091
81 meter
Y = -3504911
91 meter E =
0006145
Z = 5109935
10 I = 51
95145
XDOT = 4434
760581 Wp = 40
17532
YDOT = -6012
450270 meter/sec RA = 115
92437 deg
ZDOT = -1737
620390 TA = 66
57527
MA = 66
51067
Ha = 220
957 n
mi
Hp = 214
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8999439
89 X = -2728454
59
Y = -11499054
84 feet Y = -3535504
03 meter
Z = 16764878
95 Z = 5096646
02
XDOT = 14549
739438 XDOT = 4510
104344
YDOT = -19725
886714 feet/sec YDOT = -5962
436818 meter/sec
ZDOT = -5700
854299 ZDOT = -1715
893433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13551800
47 X = 4130588
78
Y = -5610752
08 feet Y = -1710157
23 meter
Z = 16707708
15 Z = 5092509
44
XDOT = 14569
439005 XDOT = 4440
765009
YDOT = 18441
822958 feet/sec YDOT = 5621
067638 meter/sec
ZDOT = -5605
449750 ZDOT = -1708
541084
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 16085
24495224
00016717 00000-0 10270-3 0 9021
2 25544 51
6394 116
6916 0001766 349
8644 10
2472 15
54205705 31923
Satellite: ISS
Catalog Number: 25544
Epoch time: 16085
24495224 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 116
6916 deg
Eccentricity:
0001766
Arg of perigee: 349
8644 deg
Mean anomaly: 10
2472 deg
Mean motion: 15
54205705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3192
Checksum: 308
Coasting Arc #4 (Orbit 3206)
---------------------------------------
Vector Time (GMT): 2016/086/04:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1761754
41 A = 6781037
48 meter
Y = 4904074
87 meter E =
0007784
Z = -4346579
37 I = 51
97580
XDOT = -4793
873108 Wp = 98
98966
YDOT = 4833
714542 meter/sec RA = 110
95175 deg
ZDOT = 3514
811557 TA = 206
60734
MA = 206
64731
Ha = 220
814 n
mi
Hp = 214
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5780034
15 X = 1727898
84
Y = 16089484
48 feet Y = 4923586
08 meter
Z = -14260431
00 Z = -4338104
06
XDOT = -15727
930143 XDOT = -4864
642175
YDOT = 15858
643512 feet/sec YDOT = 4779
711058 meter/sec
ZDOT = 11531
533979 ZDOT = 3491
351406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17057199
37 X = -5199034
37
Y = 1535606
75 feet Y = 468052
94 meter
Z = -14224417
73 Z = -4335602
52
XDOT = -11149
300189 XDOT = -3398
306698
YDOT = -18105
776458 feet/sec YDOT = -5518
640664 meter/sec
ZDOT = 11428
777331 ZDOT = 3483
491331
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 16086
20940936
00016717 00000-0 10270-3 0 9034
2 25544 51
6403 111
8834 0001868 347
7195 12
3912 15
54241716 32072
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
20940936 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 111
8834 deg
Eccentricity:
0001868
Arg of perigee: 347
7195 deg
Mean anomaly: 12
3912 deg
Mean motion: 15
54241716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3207
Checksum: 300
Coasting Arc #5 (Orbit 3210)
---------------------------------------
Vector Time (GMT): 2016/086/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4547561
43 A = 6780734
60 meter
Y = -2369518
47 meter E =
0009818
Z = -4446766
14 I = 51
97832
XDOT = 308
927198 Wp = 57
69223
YDOT = 6880
785712 meter/sec RA = 109
78727 deg
ZDOT = -3350
874053 TA = 178
57582
MA = 178
57302
Ha = 220
889 n
mi
Hp = 214
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14919820
95 X = 4595320
62
Y = -7774010
72 feet Y = -2318398
18 meter
Z = -14589127
75 Z = -4424558
75
XDOT = 1013
540677 XDOT = 248
238805
YDOT = 22574
756274 feet/sec YDOT = 6883
900561 meter/sec
ZDOT = -10993
681276 ZDOT = -3349
521685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16605550
30 X = 5061371
73
Y = -3179637
43 feet Y = -969153
49 meter
Z = -14492223
91 Z = -4417229
85
XDOT = -5618
785083 XDOT = -1712
605693
YDOT = 20737
494593 feet/sec YDOT = 6320
788352 meter/sec
ZDOT = -10988
955325 ZDOT = -3349
433583
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 16086
46659722
00016717 00000-0 10270-3 0 9043
2 25544 51
6411 110
6038 0002093 354
0141 6
0986 15
54244229 32115
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
46659722 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 110
6038 deg
Eccentricity:
0002093
Arg of perigee: 354
0141 deg
Mean anomaly: 6
0986 deg
Mean motion: 15
54244229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3211
Checksum: 282
Coasting Arc #6 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2016/087/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4342808
90 A = 6777729
81 meter
Y = 637175
83 meter E =
0003949
Z = 5161210
67 I = 51
97830
XDOT = 733
484479 Wp = 97
61043
YDOT = -7479
743643 meter/sec RA = 104
81449 deg
ZDOT = 1539
074084 TA = 337
62718
MA = 337
64440
Ha = 221
102 n
mi
Hp = 214
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14248060
68 X = -4374682
33
Y = 2090471
89 feet Y = 588434
06 meter
Z = 16933105
88 Z = 5140036
73
XDOT = 2406
445141 XDOT = 809
594097
YDOT = -24539
841350 feet/sec YDOT = -7471
115592 meter/sec
ZDOT = 5049
455657 ZDOT = 1542
822962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14391809
79 X = -4386623
62
Y = -1834303
44 feet Y = -559095
69 meter
Z = 16840977
48 Z = 5133129
94
XDOT = 8733
378468 XDOT = 2661
933757
YDOT = -21954
684500 feet/sec YDOT = -6691
787835 meter/sec
ZDOT = 5067
016492 ZDOT = 1544
426627
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 16087
49534533
00016717 00000-0 10270-3 0 9050
2 25544 51
6409 105
4746 0002251 359
8604
2547 15
54267601 32278
Satellite: ISS
Catalog Number: 25544
Epoch time: 16087
49534533 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 105
4746 deg
Eccentricity:
0002251
Arg of perigee: 359
8604 deg
Mean anomaly:
2547 deg
Mean motion: 15
54267601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 302
Coasting Arc #7 (Orbit 3241)
---------------------------------------
Vector Time (GMT): 2016/088/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4021786
57 A = 6777072
71 meter
Y = 1205504
60 meter E =
0014866
Z = -5332495
84 I = 51
98392
XDOT = -1648
679560 Wp = 84
81614
YDOT = 7465
002589 meter/sec RA = 99
83705 deg
ZDOT = 446
529076 TA = 189
41436
MA = 189
44226
Ha = 221
006 n
mi
Hp = 214
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13194837
84 X = 4033910
59
Y = 3955067
60 feet Y = 1250546
11 meter
Z = -17495065
10 Z = -5312929
54
XDOT = -5409
053675 XDOT = -1734
201606
YDOT = 24491
478311 feet/sec YDOT = 7446
087824 meter/sec
ZDOT = 1464
990406 ZDOT = 438
311617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11884742
18 X = 3622469
42
Y = 7173579
05 feet Y = 2186506
90 meter
Z = -17410234
79 Z = -5306639
56
XDOT = -10881
539766 XDOT = -3316
693321
YDOT = 21474
601278 feet/sec YDOT = 6545
458469 meter/sec
ZDOT = 1427
992897 ZDOT = 435
252235
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 16088
45979378
00016717 00000-0 10270-3 0 9068
2 25544 51
6417 100
6663 0002235 1
2848 358
8310 15
54247509 32424
Satellite: ISS
Catalog Number: 25544
Epoch time: 16088
45979378 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 100
6663 deg
Eccentricity:
0002235
Arg of perigee: 1
2848 deg
Mean anomaly: 358
8310 deg
Mean motion: 15
54247509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3242
Checksum: 316
Coasting Arc #8 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2016/089/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3588331
51 A = 6778735
28 meter
Y = -3003945
69 meter E =
0008481
Z = 4901059
36 I = 51
99369
XDOT = 2461
103103 Wp = 46
81964
YDOT = -6859
479395 meter/sec RA = 94
86146 deg
ZDOT = -2394
138463 TA = 66
55999
MA = 66
47084
Ha = 221
117 n
mi
Hp = 214
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11772741
18 X = -3578281
35
Y = -9855464
86 feet Y = -3044016
14 meter
Z = 16079591
09 Z = 4883652
73
XDOT = 8074
485247 XDOT = 2549
254366
YDOT = -22504
853657 feet/sec YDOT = -6831
465049 meter/sec
ZDOT = -7854
784985 ZDOT = -2381
968198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9229508
51 X = -2813154
19
Y = -12367470
40 feet Y = -3769604
98 meter
Z = 16004459
40 Z = 4878159
23
XDOT = 12281
145505 XDOT = 3743
293150
YDOT = -19294
977863 feet/sec YDOT = -5881
109253 meter/sec
ZDOT = -7800
694086 ZDOT = -2377
651558
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 16089
48853280
00016717 00000-0 10270-3 0 9076
2 25544 51
6408 95
5372 0002310 7
6020 352
5168 15
54296581 32582
Satellite: ISS
Catalog Number: 25544
Epoch time: 16089
48853280 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 95
5372 deg
Eccentricity:
0002310
Arg of perigee: 7
6020 deg
Mean anomaly: 352
5168 deg
Mean motion: 15
54296581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 312
Coasting Arc #9 (Orbit 3272)
---------------------------------------
Vector Time (GMT): 2016/090/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3097407
21 A = 6782314
73 meter
Y = 4561476
55 meter E =
0006826
Z = -3954996
05 I = 52
00919
XDOT = -3165
900073 Wp = 85
78533
YDOT = 5670
320697 meter/sec RA = 89
89396 deg
ZDOT = 4066
936805 TA = 226
52010
MA = 226
57688
Ha = 221
134 n
mi
Hp = 214
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10162097
16 X = 3065381
20
Y = 14965474
25 feet Y = 4595934
40 meter
Z = -12975708
83 Z = -3940027
74
XDOT = -10386
811264 XDOT = -3248
827230
YDOT = 18603
414361 feet/sec YDOT = 5634
454180 meter/sec
ZDOT = 13342
968520 ZDOT = 4051
355672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6735044
67 X = 2052841
62
Y = 16838533
66 feet Y = 5132385
06 meter
Z = -12911452
87 Z = -3935410
84
XDOT = -13049
961035 XDOT = -3977
628124
YDOT = 15381
654975 feet/sec YDOT = 4688
328436 meter/sec
ZDOT = 13274
244752 ZDOT = 4045
989800
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 16090
45297110
00016717 00000-0 10270-3 0 9080
2 25544 51
6427 90
7289 0002427 10
6491 349
4713 15
54283345 32734
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
45297110 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 90
7289 deg
Eccentricity:
0002427
Arg of perigee: 10
6491 deg
Mean anomaly: 349
4713 deg
Mean motion: 15
54283345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3273
Checksum: 308
Coasting Arc #10 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2016/090/14:15:30
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3894598
66 A = 6778189
40 meter
Y = 2340903
34 meter E =
0005276
Z = 5025303
39 I = 51
99305
XDOT = -1694
295255 Wp = 99
14974
YDOT = -7199
739665 meter/sec RA = 89
19309 deg
ZDOT = 2038
098097 TA = 331
13243
MA = 331
16161
Ha = 221
145 n
mi
Hp = 214
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12777554
65 X = -3944896
63
Y = 7680129
07 feet Y = 2297070
55 meter
Z = 16487215
84 Z = 5006261
96
XDOT = -5558
711465 XDOT = -1623
560295
YDOT = -23621
193125 feet/sec YDOT = -7218
290721 meter/sec
ZDOT = 6686
673548 ZDOT = 2030
040033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4577639
41 X = -1395264
49
Y = 14283953
85 feet Y = 4353749
13 meter
Z = 16404037
65 Z = 4999950
68
XDOT = -18786
989994 XDOT = -5726
274550
YDOT = -13671
093059 feet/sec YDOT = -4166
949164 meter/sec
ZDOT = 6652
920248 ZDOT = 2027
810092
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 16090
64585817
00016717 00000-0 10270-3 0 9096
2 25544 51
6401 89
7671 0002470 5
5753 354
5427 15
54306381 32769
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
64585817 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 89
7671 deg
Eccentricity:
0002470
Arg of perigee: 5
5753 deg
Mean anomaly: 354
5427 deg
Mean motion: 15
54306381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 319
Coasting Arc #11 (Orbit 3290)
---------------------------------------
Vector Time (GMT): 2016/091/14:15:30
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4150970
14 A = 6776917
55 meter
Y = -494804
26 meter E =
0015590
Z = -5347218
20 I = 51
98671
XDOT = 821
615752 Wp = 80
30791
YDOT = 7612
975415 meter/sec RA = 84
21619 deg
ZDOT = -64
265264 TA = 189
06766
MA = 189
09584
Ha = 221
141 n
mi
Hp = 214
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13618668
44 X = 4182169
18
Y = -1623373
56 feet Y = -448211
36 meter
Z = -17543366
78 Z = -5326977
97
XDOT = 2695
589738 XDOT = 736
736676
YDOT = 24976
953461 feet/sec YDOT = 7621
688676 meter/sec
ZDOT = -210
844041 ZDOT = -60
480858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9042156
87 X = 2756049
41
Y = -10460645
80 feet Y = -3188404
84 meter
Z = -17455299
44 Z = -5320375
27
XDOT = 18073
921613 XDOT = 5508
931308
YDOT = 15962
860841 feet/sec YDOT = 4865
479984 meter/sec
ZDOT = -195
753160 ZDOT = -59
665563
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 16091
61029205
00016717 00000-0 10270-3 0 9100
2 25544 51
6397 84
9581 0002540 11
3013 348
8197 15
54280291 32910
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
61029205 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 84
9581 deg
Eccentricity:
0002540
Arg of perigee: 11
3013 deg
Mean anomaly: 348
8197 deg
Mean motion: 15
54280291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3291
Checksum: 294
Coasting Arc #12 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2016/091/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2641346
67 A = 6782044
73 meter
Y = 4771601
30 meter E =
0011181
Z = 4021403
89 I = 52
00514
XDOT = -3711
591800 Wp = 88
20586
YDOT = -5412
572425 meter/sec RA = 83
79927 deg
ZDOT = 3975
280586 TA = 320
65040
MA = 320
73158
Ha = 221
214 n
mi
Hp = 214
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8665835
54 X = -2714041
87
Y = 15654859
92 feet Y = 4741657
89 meter
Z = 13193582
32 Z = 4008395
90
XDOT = -12177
138450 XDOT = -3670
101441
YDOT = -17757
783545 feet/sec YDOT = -5453
845589 meter/sec
ZDOT = 13042
259139 ZDOT = 3957
351813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12773594
08 X = 3893391
48
Y = 12590386
71 feet Y = 3837549
87 meter
Z = 13136187
27 Z = 4003909
88
XDOT = -19454
951961 XDOT = -5929
869358
YDOT = 6179
215559 feet/sec YDOT = 1883
424902 meter/sec
ZDOT = 12965
294052 ZDOT = 3951
821627
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 16091
73888306
00016717 00000-0 10270-3 0 9119
2 25544 51
6411 84
3179 0002516 12
2852 347
8362 15
54292442 32934
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
73888306 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 84
3179 deg
Eccentricity:
0002516
Arg of perigee: 12
2852 deg
Mean anomaly: 347
8362 deg
Mean motion: 15
54292442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 307
Coasting Arc #13 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2016/092/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3312159
17 A = 6778472
88 meter
Y = -3239869
61 meter E =
0013802
Z = -4960564
14 I = 51
98989
XDOT = 3104
659037 Wp = 64
37387
YDOT = 6627
245681 meter/sec RA = 78
83041 deg
ZDOT = -2254
517080 TA = 183
67954
MA = 183
68970
Ha = 221
142 n
mi
Hp = 214
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10866663
95 X = 3372238
30
Y = -10629493
46 feet Y = -3202495
36 meter
Z = -16274816
74 Z = -4944328
31
XDOT = 10185
889229 XDOT = 3041
272246
YDOT = 21742
932024 feet/sec YDOT = 6661
609425 meter/sec
ZDOT = -7396
709581 ZDOT = -2239
589987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7568834
80 X = -2306980
85
Y = -13270056
91 feet Y = -4044713
34 meter
Z = -16203657
19 Z = -4938874
71
XDOT = 22636
341837 XDOT = 6899
556992
YDOT = -3953
215878 feet/sec YDOT = -1204
940200 meter/sec
ZDOT = -7333
017795 ZDOT = -2235
103824
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 16092
70331113
00016717 00000-0 10270-3 0 9127
2 25544 51
6420 79
5092 0002588 15
1045 345
0184 15
54314039 33085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16092
70331113 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 79
5092 deg
Eccentricity:
0002588
Arg of perigee: 15
1045 deg
Mean anomaly: 345
0184 deg
Mean motion: 15
54314039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 276
Coasting Arc #14 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2016/093/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 901911
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3913018
93 A = 6776739
02 meter
Y = 1472345
84 meter E =
0003659
Z = 5330591
01 I = 51
97732
XDOT = -2350
248082 Wp = 58
51302
YDOT = -7297
108343 meter/sec RA = 73
85389 deg
ZDOT = 291
982707 TA = 28
72787
MA = 28
70772
Ha = 221
236 n
mi
Hp = 214
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12837988
62 X = -3955085
91
Y = 4830530
99 feet Y = 1428353
18 meter
Z = 17488815
67 Z = 5311480
27
XDOT = -7710
787670 XDOT = -2269
893648
YDOT = -23940
644169 feet/sec YDOT = -7322
941062 meter/sec
ZDOT = 957
948513 ZDOT = 280
761712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1696205
36 X = 517003
39
Y = 13717835
33 feet Y = 4181196
21 meter
Z = 17405474
31 Z = 5305188
57
XDOT = -24077
281592 XDOT = -7338
755429
YDOT = 1829
060487 feet/sec YDOT = 557
497637 meter/sec
ZDOT = 910
496843 ZDOT = 277
519438
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 16093
73202652
00016717 00000-0 10270-3 0 9137
2 25544 51
6420 74
3801 0002551 15
4177 344
7053 15
54344936 33243
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
73202652 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 74
3801 deg
Eccentricity:
0002551
Arg of perigee: 15
4177 deg
Mean anomaly: 344
7053 deg
Mean motion: 15
54344936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 284
Coasting Arc #15 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2016/093/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4177317
68 A = 6776838
05 meter
Y = 512549
57 meter E =
0004963
Z = 5309063
26 I = 51
97848
XDOT = -1702
891242 Wp = 41
69789
YDOT = -7454
708865 meter/sec RA = 73
51987 deg
ZDOT = -616
248197 TA = 54
17774
MA = 54
13164
Ha = 221
225 n
mi
Hp = 214
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13705110
48 X = -4208527
75
Y = 1681593
06 feet Y = 465662
05 meter
Z = 17418186
54 Z = 5288695
08
XDOT = -5586
913522 XDOT = -1616
410807
YDOT = -24457
706251 feet/sec YDOT = -7473
268248 meter/sec
ZDOT = -2021
811671 ZDOT = -624
309600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4138490
87 X = 1261412
02
Y = 13289488
38 feet Y = 4050636
06 meter
Z = 17329553
45 Z = 5282047
89
XDOT = -22089
160120 XDOT = -6732
776004
YDOT = 9576
120296 feet/sec YDOT = 2918
801466 meter/sec
ZDOT = -2055
499416 ZDOT = -626
516222
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 16093
79632062
00016717 00000-0 10270-3 0 9146
2 25544 51
6434 74
0598 0002540 14
9485 345
1742 15
54347241 33255
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
79632062 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 74
0598 deg
Eccentricity:
0002540
Arg of perigee: 14
9485 deg
Mean anomaly: 345
1742 deg
Mean motion: 15
54347241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 305
Coasting Arc #16 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2016/094/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4575145
87 A = 6778936
56 meter
Y = 1280418
12 meter E =
0011840
Z = -4846130
60 I = 51
97449
XDOT = 683
774974 Wp = 95
17664
YDOT = 7190
329735 meter/sec RA = 68
54330 deg
ZDOT = 2549
635611 TA = 199
79694
MA = 199
84293
Ha = 221
216 n
mi
Hp = 214
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15010321
09 X = 4584028
25
Y = 4200846
84 feet Y = 1331629
55 meter
Z = -15899378
61 Z = -4823884
31
XDOT = 2243
356214 XDOT = 590
935090
YDOT = 23590
320653 feet/sec YDOT = 7197
457357 meter/sec
ZDOT = 8364
946231 ZDOT = 2552
730887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1146656
78 X = 349500
99
Y = -15642900
62 feet Y = -4767956
11 meter
Z = -15802908
98 Z = -4816726
66
XDOT = 21559
612117 XDOT = 6571
369773
YDOT = -6868
049621 feet/sec YDOT = -2093
381524 meter/sec
ZDOT = 8377
085470 ZDOT = 2553
335651
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 16094
76073836
00016717 00000-0 10270-3 0 9153
2 25544 51
6427 69
2511 0002616 19
2720 340
8531 15
54325224 33404
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
76073836 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 69
2511 deg
Eccentricity:
0002616
Arg of perigee: 19
2720 deg
Mean anomaly: 340
8531 deg
Mean motion: 15
54325224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 291
Coasting Arc #17 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2016/094/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1591371
91 A = 6788286
43 meter
Y = -6491608
29 meter E =
0008163
Z = -1173129
06 I = 52
00427
XDOT = 4898
163672 Wp = 127
09887
YDOT = -141
458832 meter/sec RA = 68
34542 deg
ZDOT = -5894
624251 TA = 65
57310
MA = 65
48795
Ha = 221
217 n
mi
Hp = 214
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5221036
45 X = -1512964
31
Y = -21297927
46 feet Y = -6508965
80 meter
Z = -3848848
63 Z = -1180668
34
XDOT = 16070
090789 XDOT = 4928
014951
YDOT = -464
103780 feet/sec YDOT = -86
518083 meter/sec
ZDOT = -19339
318408 ZDOT = -5870
757727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16380824
25 X = -4992875
23
Y = 14570017
34 feet Y = 4440941
29 meter
Z = -3880433
34 Z = -1182756
08
XDOT = -6936
999742 XDOT = -2114
397521
YDOT = -12893
601482 feet/sec YDOT = -3929
969732 meter/sec
ZDOT = -19235
545400 ZDOT = -5862
994238
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 16094
82503288
00016717 00000-0 10270-3 0 9160
2 25544 51
6421 68
9304 0002469 19
4027 340
7219 15
54281684 33416
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
82503288 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 68
9304 deg
Eccentricity:
0002469
Arg of perigee: 19
4027 deg
Mean anomaly: 340
7219 deg
Mean motion: 15
54281684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 310
Coasting Arc #18 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2016/095/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 619731
97 A = 6785410
25 meter
Y = 6137659
64 meter E =
0014885
Z = 2807293
48 I = 51
98221
XDOT = -5401
852113 Wp = 71
10088
YDOT = -1813
176416 meter/sec RA = 63
39359 deg
ZDOT = 5139
221003 TA = 320
61835
MA = 320
72648
Ha = 221
221 n
mi
Hp = 213
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2033241
38 X = 537416
45
Y = 20136678
62 feet Y = 6144130
01 meter
Z = 9210280
44 Z = 2810103
24
XDOT = -17722
611920 XDOT = -5406
139373
YDOT = -5948
741521 feet/sec YDOT = -1873
606817 meter/sec
ZDOT = 16860
961297 ZDOT = 5112
969985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16670365
54 X = 5081127
42
Y = -11467978
78 feet Y = -3495439
93 meter
Z = 9221363
12 Z = 2810671
48
XDOT = 2582
958678 XDOT = 787
285805
YDOT = 17267
106102 feet/sec YDOT = 5263
013940 meter/sec
ZDOT = 16747
185533 ZDOT = 5104
542150
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 16095
85373816
00016717 00000-0 10270-3 0 9177
2 25544 51
6419 63
8004 0002627 20
3398 339
7859 15
54324418 33570
Satellite: ISS
Catalog Number: 25544
Epoch time: 16095
85373816 = yrday
fracday
Element set: 917
Inclination: 51
6419 deg
RA of node: 63
8004 deg
Eccentricity:
0002627
Arg of perigee: 20
3398 deg
Mean anomaly: 339
7859 deg
Mean motion: 15
54324418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 331
Coasting Arc #19 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2016/096/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 543334
61 A = 6781418
71 meter
Y = -5335480
91 meter E =
0009607
Z = -4160855
17 I = 51
95373
XDOT = 5646
253881 Wp = 58
63020
YDOT = 3527
330536 meter/sec RA = 58
43037 deg
ZDOT = -3787
380330 TA = 172
48213
MA = 172
46772
Ha = 221
205 n
mi
Hp = 213
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1782593
87 X = 623168
63
Y = -17504858
62 feet Y = -5328959
19 meter
Z = -13651099
62 Z = -4158021
11
XDOT = 18524
454991 XDOT = 5624
788287
YDOT = 11572
606745 feet/sec YDOT = 3590
350148 meter/sec
ZDOT = -12425
788483 ZDOT = -3760
004774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16106790
21 X = -4909349
66
Y = 7108601
93 feet Y = 2166701
87 meter
Z = -13637790
33 Z = -4156798
49
XDOT = 1271
160720 XDOT = 387
449788
YDOT = -20721
612209 feet/sec YDOT = -6315
947401 meter/sec
ZDOT = -12307
450040 ZDOT = -3751
310772
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 16096
81814347
00016717 00000-0 10270-3 0 9184
2 25544 51
6418 58
9905 0002602 22
2498 337
8767 15
54333577 33729
Satellite: ISS
Catalog Number: 25544
Epoch time: 16096
81814347 = yrday
fracday
Element set: 918
Inclination: 51
6418 deg
RA of node: 58
9905 deg
Eccentricity:
0002602
Arg of perigee: 22
2498 deg
Mean anomaly: 337
8767 deg
Mean motion: 15
54333577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 337
Coasting Arc #20 (Orbit 3387)
---------------------------------------
Vector Time (GMT): 2016/097/19:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 917037
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1805122
70 A = 6778116
33 meter
Y = 4172312
41 meter E =
0006311
Z = 5022440
61 I = 51
92470
XDOT = -5580
158045 Wp = 98
15509
YDOT = -4859
932058 meter/sec RA = 53
45590 deg
ZDOT = 2028
693966 TA = 332
20248
MA = 332
23619
Ha = 221
437 n
mi
Hp = 213
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5922318
58 X = -1876041
45
Y = 13688688
99 feet Y = 4151730
50 meter
Z = 16477823
53 Z = 5013498
86
XDOT = -18307
605134 XDOT = -5535
252952
YDOT = -15944
658982 feet/sec YDOT = -4922
081733 meter/sec
ZDOT = 6655
820098 ZDOT = 2001
696477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14842821
14 X = 4524091
88
Y = -1857344
78 feet Y = -566118
69 meter
Z = 16438177
00 Z = 5010356
35
XDOT = -4393
916066 XDOT = -1339
265617
YDOT = 22850
932938 feet/sec YDOT = 6964
964359 meter/sec
ZDOT = 6539
386481 ZDOT = 1993
204999
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 16097
84683849
00016717 00000-0 10270-3 0 9190
2 25544 51
6416 53
8607 0002704 30
1334 329
9973 15
54315309 33881
Satellite: ISS
Catalog Number: 25544
Epoch time: 16097
84683849 = yrday
fracday
Element set: 919
Inclination: 51
6416 deg
RA of node: 53
8607 deg
Eccentricity:
0002704
Arg of perigee: 30
1334 deg
Mean anomaly: 329
9973 deg
Mean motion: 15
54315309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3388
Checksum: 335
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