[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 25th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 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
328/20:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 217
7
332/03:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 217
7
336/14:51:52
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 217
6
338/15:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 217
5
338/16:38:45
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 217
6
Coasting Arc #1 (Orbit 2944)
---------------------------------------
Vector Time (GMT): 2016/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5688024
21 A = 6786126
35 meter
Y = -1855483
01 meter E =
0003963
Z = -3197253
12 I = 51
60798
XDOT = 4112
312731 Wp = 190
40372
YDOT = -4337
073494 meter/sec RA = 353
01545 deg
ZDOT = -4801
866287 TA = 26
56169
MA = 26
54139
Ha = 220
606 n
mi
Hp = 217
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18661496
76 X = -5651321
97
Y = -6087542
68 feet Y = -1918885
09 meter
Z = -10489675
58 Z = -3224795
21
XDOT = 13491
839669 XDOT = 4183
830950
YDOT = -14229
243746 feet/sec YDOT = -4290
686948 meter/sec
ZDOT = -15754
154484 ZDOT = -4781
715845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14555188
88 X = 4436421
57
Y = -13073624
12 feet Y = -3984840
63 meter
Z = -10609889
73 Z = -3233894
39
XDOT = 4594
408282 XDOT = 1400
375644
YDOT = 17820
440711 feet/sec YDOT = 5431
670329 meter/sec
ZDOT = -15665
048684 ZDOT = -4774
706839
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 16326
52548839
00016717 00000-0 10270-3 0 9009
2 25544 51
6436 353
4284 0006189 238
8539 121
2007 15
53704902 29457
Satellite: ISS
Catalog Number: 25544
Epoch time: 16326
52548839 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 353
4284 deg
Eccentricity:
0006189
Arg of perigee: 238
8539 deg
Mean anomaly: 121
2007 deg
Mean motion: 15
53704902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2945
Checksum: 320
Coasting Arc #2 (Orbit 2960)
---------------------------------------
Vector Time (GMT): 2016/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4617644
44 A = 6782688
16 meter
Y = 2502929
74 meter E =
0007015
Z = 4291792
73 I = 51
56239
XDOT = -5478
907611 Wp = 145
63014
YDOT = 4030
326242 meter/sec RA = 348
02973 deg
ZDOT = 3535
949541 TA = 268
25209
MA = 268
33245
Ha = 220
518 n
mi
Hp = 217
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15149752
09 X = 4568464
95
Y = 8211711
74 feet Y = 2554292
37 meter
Z = 14080684
81 Z = 4314104
86
XDOT = -17975
418672 XDOT = -5540
744841
YDOT = 13222
855124 feet/sec YDOT = 3968
711675 meter/sec
ZDOT = 11600
884321 ZDOT = 3509
183899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14475929
48 X = -4412263
30
Y = 9200462
85 feet Y = 2804301
08 meter
Z = 14177864
15 Z = 4321412
99
XDOT = -2162
531809 XDOT = -659
139695
YDOT = -21140
232329 feet/sec YDOT = -6443
542814 meter/sec
ZDOT = 11482
886005 ZDOT = 3499
983654
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 16327
55460915
00016717 00000-0 10270-3 0 9012
2 25544 51
6416 348
3016 0006051 242
2517 117
8022 15
53691470 29615
Satellite: ISS
Catalog Number: 25544
Epoch time: 16327
55460915 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 348
3016 deg
Eccentricity:
0006051
Arg of perigee: 242
2517 deg
Mean anomaly: 117
8022 deg
Mean motion: 15
53691470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2961
Checksum: 291
Coasting Arc #3 (Orbit 2975)
---------------------------------------
Vector Time (GMT): 2016/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3275280
95 A = 6779805
66 meter
Y = -3174194
42 meter E =
0006882
Z = -5022401
34 I = 51
52248
XDOT = 6477
512765 Wp = 83
75226
YDOT = -3598
021343 meter/sec RA = 343
03417 deg
ZDOT = -1951
804268 TA = 167
26799
MA = 167
25060
Ha = 220
310 n
mi
Hp = 217
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10745672
42 X = -3215145
89
Y = -10414023
70 feet Y = -3210484
61 meter
Z = -16477694
69 Z = -5038165
96
XDOT = 21251
682301 XDOT = 6526
746483
YDOT = -11804
531965 feet/sec YDOT = -3525
310172 meter/sec
ZDOT = -6403
557310 ZDOT = -1920
218124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14188273
16 X = 4324585
66
Y = -4511793
32 feet Y = -1375194
60 meter
Z = -16546069
42 Z = -5043241
96
XDOT = 112
105949 XDOT = 34
169893
YDOT = 23307
669761 feet/sec YDOT = 7104
177743 meter/sec
ZDOT = -6264
552495 ZDOT = -1909
435600
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 16328
51940398
00016717 00000-0 10270-3 0 9028
2 25544 51
6427 343
4961 0006258 246
5629 113
4866 15
53699704 29764
Satellite: ISS
Catalog Number: 25544
Epoch time: 16328
51940398 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 343
4961 deg
Eccentricity:
0006258
Arg of perigee: 246
5629 deg
Mean anomaly: 113
4866 deg
Mean motion: 15
53699704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2976
Checksum: 346
Coasting Arc #4 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2016/328/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4605935
56 A = 6786909
78 meter
Y = -4023381
48 meter E =
0001772
Z = -2941508
20 I = 51
53725
XDOT = 5291
323642 Wp = 263
46968
YDOT = 2401
869330 meter/sec RA = 341
32428 deg
ZDOT = 4997
318897 TA = 62
91877
MA = 62
90070
Ha = 220
128 n
mi
Hp = 217
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15111337
13 X = 4664872
49
Y = -13200070
48 feet Y = -3971545
29 meter
Z = -9650617
46 Z = -2918990
24
XDOT = 17359
985701 XDOT = 5239
796901
YDOT = 7880
148721 feet/sec YDOT = 2460
752386 meter/sec
ZDOT = 16395
403204 ZDOT = 5022
898013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14464696
66 X = 4408839
54
Y = -13974096
34 feet Y = -4259304
56 meter
Z = -9551228
71 Z = -2911214
51
XDOT = 16621
769528 XDOT = 5066
315352
YDOT = 5916
617668 feet/sec YDOT = 1803
385065 meter/sec
ZDOT = 16506
897715 ZDOT = 5031
302424
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 16328
84100209
00016717 00000-0 10270-3 0 9034
2 25544 51
6441 341
8949 0006291 250
3289 109
7185 15
53725165 29819
Satellite: ISS
Catalog Number: 25544
Epoch time: 16328
84100209 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 341
8949 deg
Eccentricity:
0006291
Arg of perigee: 250
3289 deg
Mean anomaly: 109
7185 deg
Mean motion: 15
53725165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 317
Coasting Arc #5 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2016/329/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5476901
48 A = 6789693
30 meter
Y = 3707032
65 meter E =
0010499
Z = 1506918
44 I = 51
51535
XDOT = -3832
382037 Wp = 142
93518
YDOT = -3317
074051 meter/sec RA = 336
34435 deg
ZDOT = -5756
051169 TA = 20
57701
MA = 20
53476
Ha = 220
069 n
mi
Hp = 217
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17968836
88 X = -5525267
49
Y = 12162180
62 feet Y = 3645515
83 meter
Z = 4943958
12 Z = 1480195
10
XDOT = -12573
431880 XDOT = -3767
043953
YDOT = -10882
788882 feet/sec YDOT = -3359
564991 meter/sec
ZDOT = -18884
682313 ZDOT = -5774
509531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17114272
14 X = -5216430
15
Y = 13380942
84 feet Y = 4078511
38 meter
Z = 4826232
08 Z = 1471035
54
XDOT = -12199
403537 XDOT = -3718
378198
YDOT = -8747
431920 feet/sec YDOT = -2666
217249 meter/sec
ZDOT = -18964
815618 ZDOT = -5780
475800
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 16329
87011136
00016717 00000-0 10270-3 0 9049
2 25544 51
6435 336
7690 0006181 253
2438 106
8037 15
53688440 29979
Satellite: ISS
Catalog Number: 25544
Epoch time: 16329
87011136 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 336
7690 deg
Eccentricity:
0006181
Arg of perigee: 253
2438 deg
Mean anomaly: 106
8037 deg
Mean motion: 15
53688440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 322
Coasting Arc #6 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2016/330/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5975437
44 A = 6790480
47 meter
Y = -3214814
72 meter E =
0007708
Z = 52642
61 I = 51
48887
XDOT = 2219
242172 Wp = 20
12569
YDOT = 4227
356578 meter/sec RA = 331
36580 deg
ZDOT = 5999
140090 TA = 340
44238
MA = 340
47193
Ha = 219
695 n
mi
Hp = 217
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19604453
53 X = 6010686
49
Y = -10547292
38 feet Y = -3147796
27 meter
Z = 172711
98 Z = 81755
91
XDOT = 7280
978256 XDOT = 2142
664065
YDOT = 13869
280112 feet/sec YDOT = 4251
745395 meter/sec
ZDOT = 19682
218142 ZDOT = 6009
734859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18617634
74 X = 5674655
07
Y = -12202581
88 feet Y = -3719346
96 meter
Z = 300792
58 Z = 91681
58
XDOT = 7435
845126 XDOT = 2266
445595
YDOT = 11843
084262 feet/sec YDOT = 3609
772083 meter/sec
ZDOT = 19727
744547 ZDOT = 6013
016538
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 16330
89921442
00016717 00000-0 10270-3 0 9054
2 25544 51
6430 331
6418 0006312 258
8246 101
2197 15
53731445 30130
Satellite: ISS
Catalog Number: 25544
Epoch time: 16330
89921442 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 331
6418 deg
Eccentricity:
0006312
Arg of perigee: 258
8246 deg
Mean anomaly: 101
2197 deg
Mean motion: 15
53731445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 288
Coasting Arc #7 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2016/331/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6094589
82 A = 6789419
99 meter
Y = 2503202
32 meter E =
0007294
Z = -1618420
25 I = 51
45756
XDOT = -571
867609 Wp = 192
10182
YDOT = -5083
684155 meter/sec RA = 326
38595 deg
ZDOT = -5711
698293 TA = 5
65575
MA = 5
64752
Ha = 219
492 n
mi
Hp = 217
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19995373
41 X = -6114266
55
Y = 8212606
04 feet Y = 2434938
55 meter
Z = -5309777
73 Z = -1648074
57
XDOT = -1876
206065 XDOT = -487
232523
YDOT = -16678
753788 feet/sec YDOT = -5089
605796 meter/sec
ZDOT = -18739
167629 ZDOT = -5714
270894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19002535
55 X = -5791972
83
Y = 10235467
98 feet Y = 3119770
64 meter
Z = -5440076
60 Z = -1658135
35
XDOT = -2726
618171 XDOT = -831
073219
YDOT = -15023
314643 feet/sec YDOT = -4579
106303 meter/sec
ZDOT = -18749
408581 ZDOT = -5714
819735
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 16331
86399696
00016717 00000-0 10270-3 0 9063
2 25544 51
6434 326
8361 0006444 261
4460 98
5963 15
53696253 30283
Satellite: ISS
Catalog Number: 25544
Epoch time: 16331
86399696 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 326
8361 deg
Eccentricity:
0006444
Arg of perigee: 261
4460 deg
Mean anomaly: 98
5963 deg
Mean motion: 15
53696253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 340
Coasting Arc #8 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2016/332/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4920519
55 A = 6781473
78 meter
Y = 989391
96 meter E =
0004966
Z = 4561585
50 I = 51
42228
XDOT = -3997
891647 Wp = 162
13758
YDOT = 5784
968518 meter/sec RA = 324
90386 deg
ZDOT = 3052
211093 TA = 257
21695
MA = 257
27245
Ha = 219
578 n
mi
Hp = 217
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16143436
85 X = 4886931
55
Y = 3246036
60 feet Y = 1044228
57 meter
Z = 14965831
71 Z = 4585407
09
XDOT = -13116
442413 XDOT = -4077
110140
YDOT = 18979
555505 feet/sec YDOT = 5739
818380 meter/sec
ZDOT = 10013
815923 ZDOT = 3032
597699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3312061
25 X = -1009516
27
Y = -16032835
31 feet Y = -4886808
20 meter
Z = 15069899
39 Z = 4593305
34
XDOT = 21462
007194 XDOT = 6541
619793
YDOT = 4913
889889 feet/sec YDOT = 1497
753638 meter/sec
ZDOT = 9926
809829 ZDOT = 3025
691636
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 16332
18558902
00016717 00000-0 10270-3 0 9077
2 25544 51
6421 325
2276 0006405 258
8134 101
2299 15
53755178 30334
Satellite: ISS
Catalog Number: 25544
Epoch time: 16332
18558902 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 325
2276 deg
Eccentricity:
0006405
Arg of perigee: 258
8134 deg
Mean anomaly: 101
2299 deg
Mean motion: 15
53755178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 305
Coasting Arc #9 (Orbit 3047)
---------------------------------------
Vector Time (GMT): 2016/333/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3857022
18 A = 6779083
00 meter
Y = -2135622
12 meter E =
0007682
Z = -5156461
78 I = 51
38826
XDOT = 4985
816628 Wp = 76
47723
YDOT = -5649
725230 meter/sec RA = 319
89645 deg
ZDOT = -1389
451768 TA = 180
10355
MA = 180
10371
Ha = 219
436 n
mi
Hp = 217
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12654272
25 X = -3807806
07
Y = -7006634
24 feet Y = -2178478
51 meter
Z = -16917525
53 Z = -5175079
16
XDOT = 16357
666101 XDOT = 5055
372238
YDOT = -18535
843930 feet/sec YDOT = -5593
581507 meter/sec
ZDOT = -4558
568792 ZDOT = -1365
062743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1275441
93 X = -388754
70
Y = 14312498
21 feet Y = 4362449
45 meter
Z = -16998583
54 Z = -5181168
26
XDOT = -22567
930514 XDOT = -6878
705221
YDOT = -7297
142225 feet/sec YDOT = -2224
168950 meter/sec
ZDOT = -4450
692754 ZDOT = -1356
571152
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 16333
15036548
00016717 00000-0 10270-3 0 9083
2 25544 51
6421 320
4221 0006258 263
1725 96
8715 15
53743271 30481
Satellite: ISS
Catalog Number: 25544
Epoch time: 16333
15036548 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 320
4221 deg
Eccentricity:
0006258
Arg of perigee: 263
1725 deg
Mean anomaly: 96
8715 deg
Mean motion: 15
53743271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3048
Checksum: 298
Coasting Arc #10 (Orbit 3063)
---------------------------------------
Vector Time (GMT): 2016/334/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2678463
70 A = 6778480
48 meter
Y = 3297674
82 meter E =
0003779
Z = 5285226
73 I = 51
36217
XDOT = -5620
644322 Wp = 277
66336
YDOT = 5197
356676 meter/sec RA = 314
88194 deg
ZDOT = -394
149277 TA = 176
11250
MA = 176
10956
Ha = 219
197 n
mi
Hp = 217
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8787610
56 X = 2615715
34
Y = 10819143
10 feet Y = 3327276
03 meter
Z = 17339982
73 Z = 5298086
08
XDOT = -18440
434127 XDOT = -5676
430112
YDOT = 17051
695131 feet/sec YDOT = 5134
190964 meter/sec
ZDOT = -1293
140674 ZDOT = -421
588659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6122431
36 X = 1866117
08
Y = -12444260
81 feet Y = -3793010
70 meter
Z = 17395607
63 Z = 5302181
20
XDOT = 22350
015057 XDOT = 6812
284589
YDOT = 9017
809182 feet/sec YDOT = 2748
628239 meter/sec
ZDOT = -1414
272212 ZDOT = -431
070170
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 16334
17945494
00016717 00000-0 10270-3 0 9096
2 25544 51
6420 315
2946 0006280 267
1182 92
9251 15
53761315 30641
Satellite: ISS
Catalog Number: 25544
Epoch time: 16334
17945494 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 315
2946 deg
Eccentricity:
0006280
Arg of perigee: 267
1182 deg
Mean anomaly: 92
9251 deg
Mean motion: 15
53761315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3064
Checksum: 311
Coasting Arc #11 (Orbit 3078)
---------------------------------------
Vector Time (GMT): 2016/335/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1477022
61 A = 6779960
18 meter
Y = -4402744
48 meter E =
0006622
Z = -4945925
81 I = 51
34598
XDOT = 5902
186277 Wp = 120
42178
YDOT = -4390
714728 meter/sec RA = 309
86848 deg
ZDOT = 2144
775250 TA = 170
58786
MA = 170
57544
Ha = 219
269 n
mi
Hp = 217
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4845874
71 X = -1403654
64
Y = -14444699
73 feet Y = -4418850
95 meter
Z = -16226790
72 Z = -4952923
06
XDOT = 19364
128205 XDOT = 5940
427142
YDOT = -14405
232047 feet/sec YDOT = -4324
498859 meter/sec
ZDOT = 7036
664207 ZDOT = 2173
539631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10893119
70 X = -3320222
89
Y = 10606855
13 feet Y = 3232969
44 meter
Z = -16256541
97 Z = -4954993
99
XDOT = -20655
226073 XDOT = -6295
712907
YDOT = -10227
971154 feet/sec YDOT = -3117
485608 meter/sec
ZDOT = 7163
430402 ZDOT = 2183
413586
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 16335
14422228
00016717 00000-0 10270-3 0 9101
2 25544 51
6429 310
4892 0006226 270
3386 89
7053 15
53774937 30793
Satellite: ISS
Catalog Number: 25544
Epoch time: 16335
14422228 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 310
4892 deg
Eccentricity:
0006226
Arg of perigee: 270
3386 deg
Mean anomaly: 89
7053 deg
Mean motion: 15
53774937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3079
Checksum: 318
Coasting Arc #12 (Orbit 3094)
---------------------------------------
Vector Time (GMT): 2016/336/03:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 324685
91 A = 6783128
88 meter
Y = 5350613
60 meter E =
0004990
Z = 4155162
04 I = 51
33654
XDOT = -5874
608743 Wp = 52
12063
YDOT = 3241
666752 meter/sec RA = 304
85831 deg
ZDOT = -3709
195275 TA = 76
19475
MA = 76
13922
Ha = 219
427 n
mi
Hp = 217
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1065242
48 X = 244645
58
Y = 17554506
55 feet Y = 5353796
58 meter
Z = 13632421
40 Z = 4156545
34
XDOT = -19273
650731 XDOT = -5892
403360
YDOT = 10635
389607 feet/sec YDOT = 3175
873743 meter/sec
ZDOT = -12169
275836 ZDOT = -3737
775999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15190277
03 X = 4629996
44
Y = -8855203
34 feet Y = -2699065
98 meter
Z = 13637419
58 Z = 4156685
49
XDOT = 17555
371643 XDOT = 5350
877277
YDOT = 11149
102318 feet/sec YDOT = 3398
246387 meter/sec
ZDOT = -12295
007923 ZDOT = -3747
518415
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 16336
17330239
00016717 00000-0 10270-3 0 9116
2 25544 51
6432 305
3620 0006094 274
6942 85
3514 15
53742364 30958
Satellite: ISS
Catalog Number: 25544
Epoch time: 16336
17330239 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 305
3620 deg
Eccentricity:
0006094
Arg of perigee: 274
6942 deg
Mean anomaly: 85
3514 deg
Mean motion: 15
53742364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3095
Checksum: 298
Coasting Arc #13 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2016/336/14:51:52
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1903091
97 A = 6788532
49 meter
Y = -6157179
60 meter E =
0006388
Z = -2119680
91 I = 51
34419
XDOT = 5349
871791 Wp = 342
69710
YDOT = -235
053998 meter/sec RA = 302
42906 deg
ZDOT = 5487
713362 TA = 353
71849
MA = 353
72650
Ha = 219
679 n
mi
Hp = 217
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6243740
07 X = 1982098
31
Y = -20200720
46 feet Y = -6135456
01 meter
Z = -6954333
69 Z = -2110244
67
XDOT = 17552
072804 XDOT = 5325
445345
YDOT = -771
174533 feet/sec YDOT = -175
365180 meter/sec
ZDOT = 18004
308932 ZDOT = 5513
642665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21052553
15 X = 6416818
20
Y = -2105442
09 feet Y = -641738
75 meter
Z = -6911821
30 Z = -2106723
13
XDOT = 7367
863050 XDOT = 2245
724658
YDOT = 14212
759349 feet/sec YDOT = 4332
049050 meter/sec
ZDOT = 18117
843601 ZDOT = 5522
318729
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 16336
62352281
00016717 00000-0 10270-3 0 9128
2 25544 51
6415 303
1221 0006245 281
9560 78
0892 15
53754812 31025
Satellite: ISS
Catalog Number: 25544
Epoch time: 16336
62352281 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 303
1221 deg
Eccentricity:
0006245
Arg of perigee: 281
9560 deg
Mean anomaly: 78
0892 deg
Mean motion: 15
53754812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3102
Checksum: 287
Coasting Arc #14 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2016/337/14:51:52
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700701
54 A = 6790266
68 meter
Y = 6198390
83 meter E =
0007754
Z = 574051
71 I = 51
33441
XDOT = -4610
098241 Wp = 147
94319
YDOT = -1454
689881 meter/sec RA = 297
43875 deg
ZDOT = -5951
020707 TA = 25
83667
MA = 25
79796
Ha = 219
844 n
mi
Hp = 217
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8860569
37 X = -2772601
34
Y = 20335927
93 feet Y = 6167787
71 meter
Z = 1883371
75 Z = 560758
15
XDOT = -15124
994229 XDOT = -4564
581152
YDOT = -4772
604597 feet/sec YDOT = -1505
988090 meter/sec
ZDOT = -19524
346150 ZDOT = -5973
305171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22186793
97 X = -6762534
80
Y = 161325
80 feet Y = 49172
10 meter
Z = 1823976
69 Z = 555948
10
XDOT = -1723
600929 XDOT = -525
353563
YDOT = -14025
789979 feet/sec YDOT = -4275
060786 meter/sec
ZDOT = -19621
600094 ZDOT = -5980
663709
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 16337
65259608
00016717 00000-0 10270-3 0 9132
2 25544 51
6424 297
9958 0006244 285
1288 74
9174 15
53760767 31185
Satellite: ISS
Catalog Number: 25544
Epoch time: 16337
65259608 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 297
9958 deg
Eccentricity:
0006244
Arg of perigee: 285
1288 deg
Mean anomaly: 74
9174 deg
Mean motion: 15
53760767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3118
Checksum: 351
Coasting Arc #15 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2016/338/14:51:52
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3293073
82 A = 6789927
74 meter
Y = -5842234
50 meter E =
0011017
Z = 1015056
74 I = 51
31936
XDOT = 3785
434671 Wp = 28
74561
YDOT = 3157
633638 meter/sec RA = 292
44859 deg
ZDOT = 5876
045052 TA = 342
30659
MA = 342
34493
Ha = 219
995 n
mi
Hp = 217
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10804047
96 X = 3353227
70
Y = -19167436
01 feet Y = -5805072
87 meter
Z = 3330238
64 Z = 1031199
40
XDOT = 12419
405089 XDOT = 3721
300412
YDOT = 10359
690412 feet/sec YDOT = 3199
605850 meter/sec
ZDOT = 19278
363030 ZDOT = 5894
278322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21927305
89 X = 6683442
84
Y = 1681672
71 feet Y = 512573
84 meter
Z = 3402025
61 Z = 1036937
41
XDOT = -4079
461514 XDOT = -1243
419869
YDOT = 13920
293227 feet/sec YDOT = 4242
905376 meter/sec
ZDOT = 19357
560880 ZDOT = 5900
184556
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 16338
68166400
00016717 00000-0 10270-3 0 9144
2 25544 51
6424 292
8687 0006320 289
6132 70
4338 15
53766984 31348
Satellite: ISS
Catalog Number: 25544
Epoch time: 16338
68166400 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 292
8687 deg
Eccentricity:
0006320
Arg of perigee: 289
6132 deg
Mean anomaly: 70
4338 deg
Mean motion: 15
53766984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 326
Coasting Arc #16 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2016/338/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4559271
56 A = 6784810
22 meter
Y = -3511190
98 meter E =
0006124
Z = 3587776
11 I = 51
30253
XDOT = 1272
118051 Wp = 77
84511
YDOT = 6151
587187 meter/sec RA = 292
43626 deg
ZDOT = 4398
583165 TA = 324
83343
MA = 324
87383
Ha = 219
888 n
mi
Hp = 217
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14958240
04 X = 4580767
78
Y = -11519655
46 feet Y = -3460086
24 meter
Z = 11770918
98 Z = 3609975
96
XDOT = 4173
615652 XDOT = 1181
868343
YDOT = 20182
372661 feet/sec YDOT = 6165
307902 meter/sec
ZDOT = 14431
047128 ZDOT = 4404
544109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17020975
90 X = 5187993
45
Y = 8026497
57 feet Y = 2446476
46 meter
Z = 11868768
12 Z = 3617600
52
XDOT = -15543
442959 XDOT = -4737
641414
YDOT = 11560
821789 feet/sec YDOT = 3523
738481 meter/sec
ZDOT = 14455
949454 ZDOT = 4406
173394
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 16338
68166368
00016717 00000-0 10270-3 0 9158
2 25544 51
6426 292
8689 0006277 289
2428 70
8045 15
53774372 31346
Satellite: ISS
Catalog Number: 25544
Epoch time: 16338
68166368 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 292
8689 deg
Eccentricity:
0006277
Arg of perigee: 289
2428 deg
Mean anomaly: 70
8045 deg
Mean motion: 15
53774372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 348
Coasting Arc #17 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2016/338/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4619595
64 A = 6780247
39 meter
Y = -1037748
32 meter E =
0001453
Z = 4853881
48 I = 51
28781
XDOT = -877
085585 Wp = 183
21470
YDOT = 7235
068225 meter/sec RA = 292
08670 deg
ZDOT = 2380
199823 TA = 243
33310
MA = 243
34799
Ha = 219
893 n
mi
Hp = 217
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15156153
68 X = 4607278
49
Y = -3404686
07 feet Y = -986158
14 meter
Z = 15924808
00 Z = 4876292
44
XDOT = -2877
577378 XDOT = -969
486830
YDOT = 23737
100477 feet/sec YDOT = 7224
743232 meter/sec
ZDOT = 7809
054538 ZDOT = 2375
715273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13929971
21 X = 4245855
22
Y = 6642022
34 feet Y = 2024488
41 meter
Z = 16023103
10 Z = 4883841
83
XDOT = -16505
925013 XDOT = -5031
005944
YDOT = 15818
375400 feet/sec YDOT = 4821
440822 meter/sec
ZDOT = 7788
027726 ZDOT = 2373
790851
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 16338
74597958
00016717 00000-0 10270-3 0 9169
2 25544 51
6440 292
5491 0006299 289
3572 70
6899 15
53773699 31352
Satellite: ISS
Catalog Number: 25544
Epoch time: 16338
74597958 = yrday
fracday
Element set: 916
Inclination: 51
6440 deg
RA of node: 292
5491 deg
Eccentricity:
0006299
Arg of perigee: 289
3572 deg
Mean anomaly: 70
6899 deg
Mean motion: 15
53773699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 375
Coasting Arc #18 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2016/339/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4246565
03 A = 6778400
59 meter
Y = -549048
12 meter E =
0009559
Z = -5262674
83 I = 51
27020
XDOT = 1749
929650 Wp = 66
37555
YDOT = -7431
917990 meter/sec RA = 287
06718 deg
ZDOT = -633
848268 TA = 197
52011
MA = 197
55311
Ha = 220
156 n
mi
Hp = 217
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13932299
97 X = -4214545
94
Y = -1801338
97 feet Y = -596356
67 meter
Z = -17265993
54 Z = -5283225
91
XDOT = 5741
239010 XDOT = 1835
984175
YDOT = -24382
933039 feet/sec YDOT = -7411
867899 meter/sec
ZDOT = -2079
554685 ZDOT = -625
139010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9910012
46 X = -3020571
80
Y = -9799726
20 feet Y = -2986956
55 meter
Z = -17355845
03 Z = -5290061
57
XDOT = 18624
093362 XDOT = 5676
623657
YDOT = -15204
271111 feet/sec YDOT = -4634
261835 meter/sec
ZDOT = -2040
012709 ZDOT = -621
795874
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 16339
71072326
00016717 00000-0 10270-3 0 9175
2 25544 51
6435 287
7427 0006396 293
7950 66
2531 15
53812773 31506
Satellite: ISS
Catalog Number: 25544
Epoch time: 16339
71072326 = yrday
fracday
Element set: 917
Inclination: 51
6435 deg
RA of node: 287
7427 deg
Eccentricity:
0006396
Arg of perigee: 293
7950 deg
Mean anomaly: 66
2531 deg
Mean motion: 15
53812773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 325
Coasting Arc #19 (Orbit 3165)
---------------------------------------
Vector Time (GMT): 2016/340/16:38:45
000
Vector Time (MET): N/A
Weight (LBS) : 911335
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3789252
66 A = 6778698
90 meter
Y = 2176066
48 meter E =
0005682
Z = 5185397
12 I = 51
26202
XDOT = -2491
556917 Wp = 334
55081
YDOT = 7153
294901 meter/sec RA = 282
04516 deg
ZDOT = -1176
622486 TA = 126
82411
MA = 126
77198
Ha = 220
278 n
mi
Hp = 217
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12431931
30 X = 3739449
23
Y = 7139325
73 feet Y = 2218161
70 meter
Z = 17012457
73 Z = 5203683
55
XDOT = -8174
399335 XDOT = -2565
646182
YDOT = 23468
815291 feet/sec YDOT = 7125
018444 meter/sec
ZDOT = -3860
309992 ZDOT = -1188
905434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5711452
99 X = 1740850
87
Y = 13045546
36 feet Y = 3976282
53 meter
Z = 17092092
64 Z = 5209669
84
XDOT = -19500
404884 XDOT = -5943
723409
YDOT = 13686
898363 feet/sec YDOT = 4171
766621 meter/sec
ZDOT = -3915
426708 ZDOT = -1193
422060
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 16340
73977789
00016717 00000-0 10270-3 0 9187
2 25544 51
6428 282
6161 0006446 296
7903 63
2590 15
53827873 31660
Satellite: ISS
Catalog Number: 25544
Epoch time: 16340
73977789 = yrday
fracday
Element set: 918
Inclination: 51
6428 deg
RA of node: 282
6161 deg
Eccentricity:
0006446
Arg of perigee: 296
7903 deg
Mean anomaly: 63
2590 deg
Mean motion: 15
53827873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3166
Checksum: 351
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