[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 9th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
344/13:26:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 216
7
345/20:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 216
4
348/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 216
0
349/01:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 215
9
352/04:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 3224)
---------------------------------------
Vector Time (GMT): 2016/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1679329
87 A = 6789657
34 meter
Y = 6484502
12 meter E =
0007431
Z = 1090643
70 I = 51
29025
XDOT = -4461
744983 Wp = 114
87721
YDOT = 2144
618366 meter/sec RA = 262
97865 deg
ZDOT = -5852
585652 TA = 53
23790
MA = 53
16971
Ha = 221
020 n
mi
Hp = 216
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5509612
44 X = 1601395
76
Y = 21274613
25 feet Y = 6502845
72 meter
Z = 3578227
35 Z = 1098612
46
XDOT = -14638
270941 XDOT = -4456
965416
YDOT = 7036
149495 feet/sec YDOT = 2094
751044 meter/sec
ZDOT = -19201
396497 ZDOT = -5874
248240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21953810
19 X = -6691521
35
Y = 867656
16 feet Y = 264461
60 meter
Z = 3611938
51 Z = 1100918
86
XDOT = -3746
056701 XDOT = -1141
798082
YDOT = -14071
038694 feet/sec YDOT = -4288
852594 meter/sec
ZDOT = -19296
617776 ZDOT = -5881
609098
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 16344
53431104
00016717 00000-0 10270-3 0 9006
2 25544 51
6418 263
7075 0006369 312
7073 47
3542 15
53838484 32250
Satellite: ISS
Catalog Number: 25544
Epoch time: 16344
53431104 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 263
7075 deg
Eccentricity:
0006369
Arg of perigee: 312
7073 deg
Mean anomaly: 47
3542 deg
Mean motion: 15
53838484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3225
Checksum: 300
Coasting Arc #2 (Orbit 3225)
---------------------------------------
Vector Time (GMT): 2016/344/13:26:46
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3102520
32 A = 6786319
21 meter
Y = 5232253
00 meter E =
0008835
Z = 3004817
12 I = 51
27970
XDOT = -3356
794137 Wp = 71
85645
YDOT = 4824
976100 meter/sec RA = 262
66432 deg
ZDOT = -4921
068984 TA = 73
55693
MA = 73
45985
Ha = 221
007 n
mi
Hp = 216
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10178872
46 X = 3029185
08
Y = 17166184
38 feet Y = 5266537
33 meter
Z = 9858323
88 Z = 3019710
59
XDOT = -11013
104123 XDOT = -3386
594090
YDOT = 15829
974081 feet/sec YDOT = 4787
271709 meter/sec
ZDOT = -16145
239450 ZDOT = -4937
447848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15250134
18 X = -4648240
90
Y = 12823796
43 feet Y = 3908693
15 meter
Z = 9922576
94 Z = 3024401
45
XDOT = -16484
330699 XDOT = -5024
423997
YDOT = -7017
537016 feet/sec YDOT = -2138
945283 meter/sec
ZDOT = -16217
814973 ZDOT = -4943
190004
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 16344
59862517
00016717 00000-0 10270-3 0 9019
2 25544 51
6422 263
3881 0006288 312
7239 47
3383 15
53831250 32268
Satellite: ISS
Catalog Number: 25544
Epoch time: 16344
59862517 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 263
3881 deg
Eccentricity:
0006288
Arg of perigee: 312
7239 deg
Mean anomaly: 47
3383 deg
Mean motion: 15
53831250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3226
Checksum: 311
Coasting Arc #3 (Orbit 3240)
---------------------------------------
Vector Time (GMT): 2016/345/13:26:46
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2602295
75 A = 6789021
19 meter
Y = -6066641
61 meter E =
0011038
Z = -1555256
93 I = 51
29560
XDOT = 3998
263648 Wp = 2
36538
YDOT = -3178
867881 meter/sec RA = 257
66473 deg
ZDOT = 5722
200203 TA = 340
54546
MA = 340
58755
Ha = 221
044 n
mi
Hp = 216
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8537715
71 X = -2526708
73
Y = -19903679
81 feet Y = -6095319
52 meter
Z = -5102548
99 Z = -1567715
09
XDOT = 13117
662886 XDOT = 4005
717061
YDOT = -10429
356565 feet/sec YDOT = -3134
115202 meter/sec
ZDOT = 18773
622712 ZDOT = 5741
640975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18012716
46 X = 5490275
98
Y = -12001782
00 feet Y = -3658143
15 meter
Z = -5156000
43 Z = -1571548
93
XDOT = 11753
629336 XDOT = 3582
506222
YDOT = 9555
401388 feet/sec YDOT = 2912
486343 meter/sec
ZDOT = 18859
304217 ZDOT = 5748
315925
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 16345
56332608
00016717 00000-0 10270-3 0 9021
2 25544 51
6436 258
5804 0006469 315
9693 44
0943 15
53873998 32412
Satellite: ISS
Catalog Number: 25544
Epoch time: 16345
56332608 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 258
5804 deg
Eccentricity:
0006469
Arg of perigee: 315
9693 deg
Mean anomaly: 44
0943 deg
Mean motion: 15
53873998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3241
Checksum: 337
Coasting Arc #4 (Orbit 3245)
---------------------------------------
Vector Time (GMT): 2016/345/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4427812
23 A = 6779372
71 meter
Y = -1202259
67 meter E =
0008265
Z = -4997718
16 I = 51
26324
XDOT = -206
468273 Wp = 83
10574
YDOT = -7402
394146 meter/sec RA = 256
09643 deg
ZDOT = 1967
440545 TA = 206
09268
MA = 206
13436
Ha = 220
905 n
mi
Hp = 216
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14526943
01 X = -4389762
08
Y = -3944421
48 feet Y = -1251561
42 meter
Z = -16396713
12 Z = -5019135
30
XDOT = -677
389348 XDOT = -133
234563
YDOT = -24286
070032 feet/sec YDOT = -7404
293642 meter/sec
ZDOT = 6454
857432 ZDOT = 1966
615048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14230556
26 X = -4337473
55
Y = 4583148
45 feet Y = 1396943
65 meter
Z = -16490262
40 Z = -5026231
98
XDOT = -13550
032944 XDOT = -4130
050041
YDOT = -18900
431178 feet/sec YDOT = -5760
851423 meter/sec
ZDOT = 6452
570281 ZDOT = 1966
743422
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 16345
88489186
00016717 00000-0 10270-3 0 9031
2 25544 51
6413 256
9736 0006012 315
0477 45
0189 15
53873166 32463
Satellite: ISS
Catalog Number: 25544
Epoch time: 16345
88489186 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 256
9736 deg
Eccentricity:
0006012
Arg of perigee: 315
0477 deg
Mean anomaly: 45
0189 deg
Mean motion: 15
53873166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3246
Checksum: 328
Coasting Arc #5 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2016/346/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4528251
82 A = 6782480
05 meter
Y = 2764929
21 meter E =
0009233
Z = 4224974
87 I = 51
28179
XDOT = -741
904295 Wp = 38
13310
YDOT = 6729
128161 meter/sec RA = 251
07958 deg
ZDOT = -3597
189687 TA = 88
88937
MA = 88
78359
Ha = 221
116 n
mi
Hp = 216
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14856469
21 X = 4476473
74
Y = 9071290
06 feet Y = 2815277
34 meter
Z = 13861466
12 Z = 4246846
73
XDOT = -2434
069210 XDOT = -799
622162
YDOT = 22077
192129 feet/sec YDOT = 6720
509242 meter/sec
ZDOT = -11801
803435 ZDOT = -3600
933401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17313201
60 X = 5277063
85
Y = -778326
62 feet Y = -237233
95 meter
Z = 13956736
08 Z = 4254013
16
XDOT = 10381
967177 XDOT = 3164
423596
YDOT = 18332
006916 feet/sec YDOT = 5587
595708 meter/sec
ZDOT = -11819
393885 ZDOT = -3602
551256
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 16346
91389758
00016717 00000-0 10270-3 0 9041
2 25544 51
6410 251
8458 0005922 318
9418 41
1288 15
53846779 32626
Satellite: ISS
Catalog Number: 25544
Epoch time: 16346
91389758 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 251
8458 deg
Eccentricity:
0005922
Arg of perigee: 318
9418 deg
Mean anomaly: 41
1288 deg
Mean motion: 15
53846779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 341
Coasting Arc #6 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2016/347/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4488017
64 A = 6786015
61 meter
Y = -4056458
46 meter E =
0006082
Z = -3067701
37 I = 51
30567
XDOT = 1771
056229 Wp = 5
93625
YDOT = -5643
883341 meter/sec RA = 246
07352 deg
ZDOT = 4878
746098 TA = 318
65075
MA = 318
69678
Ha = 221
190 n
mi
Hp = 216
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14724467
31 X = -4427421
99
Y = -13308590
74 feet Y = -4106307
37 meter
Z = -10064637
02 Z = -3089356
49
XDOT = 5810
551931 XDOT = 1810
336853
YDOT = -18516
677628 feet/sec YDOT = -5623
859053 meter/sec
ZDOT = 16006
384836 ZDOT = 4887
444388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19647331
88 X = -5988506
76
Y = -2451074
25 feet Y = -747087
43 meter
Z = -10158741
48 Z = -3096384
40
XDOT = -6164
879280 XDOT = -1879
055204
YDOT = -16993
989300 feet/sec YDOT = -5179
767939 meter/sec
ZDOT = 16045
472761 ZDOT = 4890
660098
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 16347
87858286
00016717 00000-0 10270-3 0 9055
2 25544 51
6415 247
0396 0006116 322
3078 37
7645 15
53868919 32770
Satellite: ISS
Catalog Number: 25544
Epoch time: 16347
87858286 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 247
0396 deg
Eccentricity:
0006116
Arg of perigee: 322
3078 deg
Mean anomaly: 37
7645 deg
Mean motion: 15
53868919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 349
Coasting Arc #7 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2016/348/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3881838
13 A = 6789320
05 meter
Y = -5411974
51 meter E =
0012656
Z = -1276380
23 I = 51
32500
XDOT = 3319
141128 Wp = 8
76328
YDOT = -3746
976859 meter/sec RA = 243
17322 deg
ZDOT = 5812
975592 TA = 337
28597
MA = 337
34192
Ha = 221
462 n
mi
Hp = 216
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12735689
41 X = -3814831
38
Y = -17755821
87 feet Y = -5455009
03 meter
Z = -4187599
17 Z = -1295075
22
XDOT = 10889
570630 XDOT = 3332
556945
YDOT = -12293
231164 feet/sec YDOT = -3709
785619 meter/sec
ZDOT = 19071
442231 ZDOT = 5829
131454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21431072
07 X = 6532190
77
Y = -4182337
47 feet Y = -1274776
46 meter
Z = -4268510
85 Z = -1301042
11
XDOT = 6402
639798 XDOT = 1951
524611
YDOT = 13336
390987 feet/sec YDOT = 4064
931973 meter/sec
ZDOT = 19142
851532 ZDOT = 5834
741147
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 16348
45739194
00016717 00000-0 10270-3 0 9067
2 25544 51
6419 244
1598 0006540 327
1130 32
9615 15
53884801 32861
Satellite: ISS
Catalog Number: 25544
Epoch time: 16348
45739194 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 244
1598 deg
Eccentricity:
0006540
Arg of perigee: 327
1130 deg
Mean anomaly: 32
9615 deg
Mean motion: 15
53884801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3286
Checksum: 322
Coasting Arc #8 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2016/349/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1438486
42 A = 6787705
51 meter
Y = 6218155
46 meter E =
0001577
Z = -2313551
99 I = 51
32905
XDOT = -5401
033118 Wp = 36
57465
YDOT = -752
813679 meter/sec RA = 240
11009 deg
ZDOT = -5382
177467 TA = 169
30576
MA = 169
30241
Ha = 221
533 n
mi
Hp = 215
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4719443
65 X = 1380084
79
Y = 20400772
51 feet Y = 6233915
31 meter
Z = -7590393
68 Z = -2306705
28
XDOT = -17719
924928 XDOT = -5366
069132
YDOT = -2469
861151 feet/sec YDOT = -813
015532 meter/sec
ZDOT = -17658
062557 ZDOT = -5408
329620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17821193
73 X = 5431899
85
Y = -11013967
97 feet Y = -3357057
44 meter
Z = -7561501
64 Z = -2304745
70
XDOT = 2457
569779 XDOT = 749
067269
YDOT = 16176
453700 feet/sec YDOT = 4930
583088 meter/sec
ZDOT = -17772
461866 ZDOT = -5417
046377
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 16349
10050785
00016717 00000-0 10270-3 0 9073
2 25544 51
6419 240
9537 0006282 329
8676 30
2115 15
53911936 32962
Satellite: ISS
Catalog Number: 25544
Epoch time: 16349
10050785 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 240
9537 deg
Eccentricity:
0006282
Arg of perigee: 329
8676 deg
Mean anomaly: 30
2115 deg
Mean motion: 15
53911936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 319
Coasting Arc #9 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2016/350/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -406309
03 A = 6784296
85 meter
Y = -5694098
32 meter E =
0010238
Z = 3653728
54 I = 51
33344
XDOT = 5874
622199 Wp = 62
60843
YDOT = 2363
747908 meter/sec RA = 235
11087 deg
ZDOT = 4332
302292 TA = 341
05516
MA = 341
09322
Ha = 221
646 n
mi
Hp = 215
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1333034
88 X = -360354
17
Y = -18681424
92 feet Y = -5698385
42 meter
Z = 11987298
35 Z = 3651865
73
XDOT = 19273
694879 XDOT = 5826
709127
YDOT = 7755
078438 feet/sec YDOT = 2429
173466 meter/sec
ZDOT = 14213
590198 ZDOT = 4360
723601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17131835
33 X = -5221783
41
Y = 7579222
82 feet Y = 2310147
11 meter
Z = 11980131
08 Z = 3651543
95
XDOT = 1444
890180 XDOT = 440
402527
YDOT = -19421
431798 feet/sec YDOT = -5919
652412 meter/sec
ZDOT = 14337
664728 ZDOT = 4370
120209
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 16350
12948715
00016717 00000-0 10270-3 0 9087
2 25544 51
6407 235
8265 0006297 334
2337 25
8502 15
53912771 33127
Satellite: ISS
Catalog Number: 25544
Epoch time: 16350
12948715 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 235
8265 deg
Eccentricity:
0006297
Arg of perigee: 334
2337 deg
Mean anomaly: 25
8502 deg
Mean motion: 15
53912771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 308
Coasting Arc #10 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2016/351/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -781600
28 A = 6780737
69 meter
Y = 4875210
43 meter E =
0011926
Z = -4658450
54 I = 51
34107
XDOT = -6068
002558 Wp = 38
97332
YDOT = -3702
070695 meter/sec RA = 230
10309 deg
ZDOT = -2851
128438 TA = 202
52780
MA = 202
58020
Ha = 221
760 n
mi
Hp = 215
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2564305
38 X = -813429
45
Y = 15994784
87 feet Y = 4866292
59 meter
Z = -15283630
38 Z = -4662324
11
XDOT = -19908
144874 XDOT = -6012
304607
YDOT = -12145
901231 feet/sec YDOT = -3769
615442 meter/sec
ZDOT = -9354
095926 ZDOT = -2880
470199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15842004
12 X = 4828642
86
Y = -3300760
27 feet Y = -1006071
73 meter
Z = -15301439
46 Z = -4663878
75
XDOT = -4655
125474 XDOT = -1418
882244
YDOT = 21691
245673 feet/sec YDOT = 6611
491681 meter/sec
ZDOT = -9481
993479 ZDOT = -2890
111612
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 16351
09414837
00016717 00000-0 10270-3 0 9098
2 25544 51
6409 231
0196 0006279 336
9421 23
1449 15
53919515 33273
Satellite: ISS
Catalog Number: 25544
Epoch time: 16351
09414837 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 231
0196 deg
Eccentricity:
0006279
Arg of perigee: 336
9421 deg
Mean anomaly: 23
1449 deg
Mean motion: 15
53919515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 315
Coasting Arc #11 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2016/352/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2074352
56 A = 6778296
98 meter
Y = -3813267
39 meter E =
0004110
Z = 5204165
73 I = 51
35395
XDOT = 5943
855102 Wp = 17
97653
YDOT = 4722
372818 meter/sec RA = 225
08797 deg
ZDOT = 1094
660112 TA = 61
51501
MA = 61
47362
Ha = 221
810 n
mi
Hp = 215
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6805618
62 X = 2091559
98
Y = -12510719
80 feet Y = -3789974
84 meter
Z = 17074034
54 Z = 5214283
77
XDOT = 19500
836949 XDOT = 5885
289223
YDOT = 15493
349141 feet/sec YDOT = 4788
513441 meter/sec
ZDOT = 3591
404568 ZDOT = 1123
391764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14092799
71 X = -4295485
35
Y = -1639993
52 feet Y = -499870
03 meter
Z = 17119013
64 Z = 5217875
36
XDOT = 7150
526372 XDOT = 2179
480438
YDOT = -22774
813167 feet/sec YDOT = -6941
763053 meter/sec
ZDOT = 3716
479589 ZDOT = 1132
782979
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 16352
12311047
00016717 00000-0 10270-3 0 9104
2 25544 51
6402 225
8915 0006377 342
0370 18
0556 15
53946968 33438
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
12311047 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 225
8915 deg
Eccentricity:
0006377
Arg of perigee: 342
0370 deg
Mean anomaly: 18
0556 deg
Mean motion: 15
53946968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 296
Coasting Arc #12 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2016/352/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2658483
38 A = 6777981
68 meter
Y = -3309713
69 meter E =
0005379
Z = 5283155
90 I = 51
35355
XDOT = 5674
706105 Wp = 5
22757
YDOT = 5145
509887 meter/sec RA = 224
43265 deg
ZDOT = 373
201843 TA = 81
23070
MA = 81
16978
Ha = 221
853 n
mi
Hp = 215
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8722058
32 X = 2669632
83
Y = -10858640
71 feet Y = -3279922
86 meter
Z = 17333188
64 Z = 5296096
81
XDOT = 18617
802183 XDOT = 5614
933102
YDOT = 16881
594117 feet/sec YDOT = 5208
634021 meter/sec
ZDOT = 1224
415495 ZDOT = 400
623133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12002109
04 X = -3658242
84
Y = 6924265
16 feet Y = 2110516
02 meter
Z = 17390449
63 Z = 5300609
05
XDOT = -10581
207451 XDOT = -3225
152031
YDOT = -21672
567268 feet/sec YDOT = -6605
798503 meter/sec
ZDOT = 1343
680773 ZDOT = 409
553900
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 16352
25173072
00016717 00000-0 10270-3 0 9113
2 25544 51
6380 225
2508 0006508 341
7576 18
3342 15
53929318 33453
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
25173072 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 225
2508 deg
Eccentricity:
0006508
Arg of perigee: 341
7576 deg
Mean anomaly: 18
3342 deg
Mean motion: 15
53929318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 300
Coasting Arc #13 (Orbit 3359)
---------------------------------------
Vector Time (GMT): 2016/353/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3897676
95 A = 6778623
88 meter
Y = 2110046
20 meter E =
0012479
Z = -5138417
49 I = 51
37949
XDOT = -4984
932409 Wp = 72
73616
YDOT = -5625
298681 meter/sec RA = 219
41641 deg
ZDOT = 1477
880589 TA = 211
52276
MA = 211
59759
Ha = 222
057 n
mi
Hp = 215
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12787654
03 X = -3896022
40
Y = 6922723
74 feet Y = 2066469
34 meter
Z = -16858325
10 Z = -5157347
07
XDOT = -16354
765121 XDOT = -4928
837213
YDOT = -18455
704335 feet/sec YDOT = -5680
729995 meter/sec
ZDOT = 4848
689596 ZDOT = 1453
801176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14303139
13 X = 4359596
81
Y = -2013167
79 feet Y = -613613
54 meter
Z = -16941626
00 Z = -5163807
61
XDOT = 8690
281699 XDOT = 2648
797862
YDOT = 22000
444260 feet/sec YDOT = 6705
735410 meter/sec
ZDOT = 4744
123880 ZDOT = 1446
008959
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 16353
21637487
00016717 00000-0 10270-3 0 9126
2 25544 51
6380 220
4436 0006614 345
6330 14
4633 15
53929005 33609
Satellite: ISS
Catalog Number: 25544
Epoch time: 16353
21637487 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 220
4436 deg
Eccentricity:
0006614
Arg of perigee: 345
6330 deg
Mean anomaly: 14
4633 deg
Mean motion: 15
53929005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3360
Checksum: 289
Coasting Arc #14 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2016/354/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5017367
82 A = 6781208
69 meter
Y = -890087
58 meter E =
0012075
Z = 4473550
71 I = 51
41362
XDOT = 3896
846737 Wp = 35
40969
YDOT = 5771
450208 meter/sec RA = 214
40595 deg
ZDOT = -3208
218498 TA = 87
02371
MA = 86
88553
Ha = 222
081 n
mi
Hp = 214
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16461180
52 X = 5005217
74
Y = -2920234
85 feet Y = -834048
15 meter
Z = 14677003
63 Z = 4497894
03
XDOT = 12784
930238 XDOT = 3847
603266
YDOT = 18935
204096 feet/sec YDOT = 5814
752185 meter/sec
ZDOT = -10525
651241 ZDOT = -3189
408105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16394812
64 X = -4997138
89
Y = -2749746
51 feet Y = -838122
74 meter
Z = 14783831
83 Z = 4506111
94
XDOT = -5944
231410 XDOT = -1811
801734
YDOT = -20956
549866 feet/sec YDOT = -6387
556399 meter/sec
ZDOT = -10444
178592 ZDOT = -3183
385635
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 16354
24532401
00016717 00000-0 10270-3 0 9131
2 25544 51
6376 215
3156 0006674 348
5673 11
5327 15
53960996 33763
Satellite: ISS
Catalog Number: 25544
Epoch time: 16354
24532401 = yrday
fracday
Element set: 913
Inclination: 51
6376 deg
RA of node: 215
3156 deg
Eccentricity:
0006674
Arg of perigee: 348
5673 deg
Mean anomaly: 11
5327 deg
Mean motion: 15
53960996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 318
Coasting Arc #15 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2016/355/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5868890
95 A = 6784863
96 meter
Y = -202633
94 meter E =
0007710
Z = -3395149
03 I = 51
45373
XDOT = -2466
940192 Wp = 31
85605
YDOT = -5606
884237 meter/sec RA = 209
40637 deg
ZDOT = 4610
223614 TA = 288
35452
MA = 288
43837
Ha = 222
218 n
mi
Hp = 214
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19254891
57 X = -5849696
82
Y = -664809
51 feet Y = -268156
37 meter
Z = -11138940
37 Z = -3423611
80
XDOT = -8093
635801 XDOT = -2426
453531
YDOT = -18395
289493 feet/sec YDOT = -5634
245024 meter/sec
ZDOT = 15125
405559 ZDOT = 4598
338049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17962205
05 X = 5474880
10
Y = 6764475
16 feet Y = 2061812
03 meter
Z = -11263653
02 Z = -3433161
44
XDOT = 2373
349270 XDOT = 723
396858
YDOT = 18737
722659 feet/sec YDOT = 5711
257866 meter/sec
ZDOT = 15074
238609 ZDOT = 4594
627928
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 16355
20995878
00016717 00000-0 10270-3 0 9140
2 25544 51
6384 210
5083 0006720 352
3781 7
7269 15
53944063 33919
Satellite: ISS
Catalog Number: 25544
Epoch time: 16355
20995878 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 210
5083 deg
Eccentricity:
0006720
Arg of perigee: 352
3781 deg
Mean anomaly: 7
7269 deg
Mean motion: 15
53944063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 323
Coasting Arc #16 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2016/356/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6388787
04 A = 6788089
94 meter
Y = 1197747
68 meter E =
0012566
Z = 1948757
45 I = 51
49423
XDOT = 734
967048 Wp = 83
06446
YDOT = 5206
862755 meter/sec RA = 204
41784 deg
ZDOT = -5577
307816 TA = 75
40624
MA = 75
26692
Ha = 222
386 n
mi
Hp = 214
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20960587
40 X = 6365452
51
Y = 3929618
36 feet Y = 1269060
85 meter
Z = 6393561
18 Z = 1979735
79
XDOT = 2411
309214 XDOT = 703
779965
YDOT = 17082
883053 feet/sec YDOT = 5214
907477 meter/sec
ZDOT = -18298
253991 ZDOT = -5573
813108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18740077
34 X = -5711975
57
Y = -10091850
45 feet Y = -3075996
02 meter
Z = 6529150
40 Z = 1990085
04
XDOT = 2035
882087 XDOT = 620
536860
YDOT = -15677
091083 feet/sec YDOT = -4778
377362 meter/sec
ZDOT = -18283
789077 ZDOT = -5572
898911
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 16356
23889623
00016717 00000-0 10270-3 0 9155
2 25544 51
6392 205
3797 0006816 356
1096 4
0002 15
53977942 34074
Satellite: ISS
Catalog Number: 25544
Epoch time: 16356
23889623 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 205
3797 deg
Eccentricity:
0006816
Arg of perigee: 356
1096 deg
Mean anomaly: 4
0002 deg
Mean motion: 15
53977942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 323
Coasting Arc #17 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2016/357/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6470644
20 A = 6789690
67 meter
Y = -1994764
84 meter E =
0016929
Z = -342782
80 I = 51
52870
XDOT = 1124
426993 Wp = 27
07377
YDOT = -4655
109896 meter/sec RA = 199
43889 deg
ZDOT = 5995
287826 TA = 329
22361
MA = 329
32276
Ha = 222
436 n
mi
Hp = 214
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21229147
63 X = -6446192
23
Y = -6544504
08 feet Y = -2066987
20 meter
Z = -1124615
50 Z = -374156
18
XDOT = 3689
064939 XDOT = 1147
275614
YDOT = -15272
670261 feet/sec YDOT = -4642
408288 meter/sec
ZDOT = 19669
579483 ZDOT = 6000
805303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18450662
94 X = 5623762
06
Y = 12359322
21 feet Y = 3767121
41 meter
Z = -1261821
90 Z = -384603
32
XDOT = -6892
559740 XDOT = -2100
852209
YDOT = 12261
102418 feet/sec YDOT = 3737
184017 meter/sec
ZDOT = 19694
526041 ZDOT = 6002
891537
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 16357
20352089
00016717 00000-0 10270-3 0 9165
2 25544 51
6385 200
5729 0006785 359
7555
3593 15
53983691 34221
Satellite: ISS
Catalog Number: 25544
Epoch time: 16357
20352089 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 200
5729 deg
Eccentricity:
0006785
Arg of perigee: 359
7555 deg
Mean anomaly:
3593 deg
Mean motion: 15
53983691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 330
Coasting Arc #18 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2016/358/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6099052
68 A = 6788999
26 meter
Y = 2668144
35 meter E =
0005757
Z = -1335794
01 I = 51
55833
XDOT = -3011
065906 Wp = 92
25271
YDOT = 3985
520633 meter/sec RA = 194
46301 deg
ZDOT = -5809
257652 TA = 102
29464
MA = 102
23017
Ha = 222
573 n
mi
Hp = 214
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20010015
35 X = 6075252
21
Y = 8753754
43 feet Y = 2736215
05 meter
Z = -4382526
29 Z = -1306224
04
XDOT = -9878
825152 XDOT = -3027
190391
YDOT = 13075
855094 feet/sec YDOT = 3951
758999 meter/sec
ZDOT = -19059
244265 ZDOT = -5823
923611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16923918
91 X = -5158410
48
Y = -13846505
28 feet Y = -4220414
81 meter
Z = -4253319
63 Z = -1296411
82
XDOT = 11917
560100 XDOT = 3632
472319
YDOT = -8714
512313 feet/sec YDOT = -2656
183353 meter/sec
ZDOT = -19124
191796 ZDOT = -5829
053659
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 16358
23244931
00016717 00000-0 10270-3 0 9176
2 25544 51
6396 195
4448 0006862 2
6877 357
4311 15
53994696 34388
Satellite: ISS
Catalog Number: 25544
Epoch time: 16358
23244931 = yrday
fracday
Element set: 917
Inclination: 51
6396 deg
RA of node: 195
4448 deg
Eccentricity:
0006862
Arg of perigee: 2
6877 deg
Mean anomaly: 357
4311 deg
Mean motion: 15
53994696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 348
Coasting Arc #19 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2016/359/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5262776
63 A = 6786312
76 meter
Y = -3174014
04 meter E =
0016634
Z = 2853765
20 I = 51
58093
XDOT = 4736
389216 Wp = 57
44130
YDOT = -3284
574044 meter/sec RA = 189
48458 deg
ZDOT = 5068
696564 TA = 335
07485
MA = 335
15509
Ha = 222
706 n
mi
Hp = 214
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17266327
54 X = -5240755
21
Y = -10413431
89 feet Y = -3232742
99 meter
Z = 9362746
71 Z = 2828253
24
XDOT = 15539
334698 XDOT = 4748
144608
YDOT = -10776
161562 feet/sec YDOT = -3231
543135 meter/sec
ZDOT = 16629
581904 ZDOT = 5091
733110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14115919
12 X = 4302532
15
Y = 14469937
39 feet Y = 4410436
92 meter
Z = 9251399
66 Z = 2819826
62
XDOT = -16605
555245 XDOT = -5061
373239
YDOT = 5475
109163 feet/sec YDOT = 1668
813273 meter/sec
ZDOT = 16731
125975 ZDOT = 5099
647197
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 16359
26137131
00016717 00000-0 10270-3 0 9184
2 25544 51
6397 190
3169 0006841 6
5962 353
5279 15
54006165 34542
Satellite: ISS
Catalog Number: 25544
Epoch time: 16359
26137131 = yrday
fracday
Element set: 918
Inclination: 51
6397 deg
RA of node: 190
3169 deg
Eccentricity:
0006841
Arg of perigee: 6
5962 deg
Mean anomaly: 353
5279 deg
Mean motion: 15
54006165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 320
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