[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 13th 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
349/01:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
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
4
Coasting Arc #1 (Orbit 3271)
---------------------------------------
Vector Time (GMT): 2016/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 660387
70 A = 6784980
75 meter
Y = -5785379
72 meter E =
0009934
Z = 3470255
96 I = 51
29857
XDOT = 5242
514377 Wp = 59
78748
YDOT = 3311
192217 meter/sec RA = 247
99105 deg
ZDOT = 4517
760489 TA = 341
20715
MA = 341
24380
Ha = 221
413 n
mi
Hp = 216
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2166626
32 X = 708175
01
Y = -18980904
58 feet Y = -5777727
94 meter
Z = 11385354
21 Z = 3473579
55
XDOT = 17199
850317 XDOT = 5183
152542
YDOT = 10863
491527 feet/sec YDOT = 3369
485212 meter/sec
ZDOT = 14822
048849 ZDOT = 4543
083738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18397544
96 X = 5607571
70
Y = 5113153
20 feet Y = 1558489
10 meter
Z = 11400934
30 Z = 3475004
77
XDOT = -13097
330615 XDOT = -3992
066371
YDOT = 13795
227878 feet/sec YDOT = 4204
785457 meter/sec
ZDOT = 14932
341456 ZDOT = 4551
377676
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
55703061
00016717 00000-0 10270-3 0 9005
2 25544 51
6427 248
6461 0006445 325
1315 34
9414 15
53861808 32721
Satellite: ISS
Catalog Number: 25544
Epoch time: 16347
55703061 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 248
6461 deg
Eccentricity:
0006445
Arg of perigee: 325
1315 deg
Mean anomaly: 34
9414 deg
Mean motion: 15
53861808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3272
Checksum: 300
Coasting Arc #2 (Orbit 3286)
---------------------------------------
Vector Time (GMT): 2016/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1626836
50 A = 6781292
80 meter
Y = 4790438
60 meter E =
0010562
Z = -4525276
86 I = 51
30032
XDOT = -5189
343900 Wp = 32
36518
YDOT = -4700
713190 meter/sec RA = 242
98291 deg
ZDOT = -3105
202353 TA = 206
31193
MA = 206
36562
Ha = 221
536 n
mi
Hp = 215
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5337390
08 X = -1658301
49
Y = 15716662
07 feet Y = 4772070
79 meter
Z = -14846708
86 Z = -4533255
58
XDOT = -17025
406497 XDOT = -5121
309784
YDOT = -15422
287369 feet/sec YDOT = -4758
363174 meter/sec
ZDOT = -10187
671763 ZDOT = -3130
246358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14800040
41 X = -4511052
32
Y = -7442858
30 feet Y = -2268583
21 meter
Z = -14882494
01 Z = -4536184
17
XDOT = 17155
496984 XDOT = 5228
995481
YDOT = -13489
711833 feet/sec YDOT = -4111
664167 meter/sec
ZDOT = -10296
512684 ZDOT = -3138
377066
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
52171825
00016717 00000-0 10270-3 0 9011
2 25544 51
6434 243
8402 0006580 327
5594 32
5153 15
53898673 32876
Satellite: ISS
Catalog Number: 25544
Epoch time: 16348
52171825 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 243
8402 deg
Eccentricity:
0006580
Arg of perigee: 327
5594 deg
Mean anomaly: 32
5153 deg
Mean motion: 15
53898673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3287
Checksum: 321
Coasting Arc #3 (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 = 1447887
13 A = 6787768
86 meter
Y = 6219515
84 meter E =
0001601
Z = -2304234
54 I = 51
32922
XDOT = -5397
787478 Wp = 37
51580
YDOT = -739
036643 meter/sec RA = 240
11005 deg
ZDOT = -5387
269736 TA = 168
25234
MA = 168
24860
Ha = 221
575 n
mi
Hp = 215
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4750285
87 X = 1389424
33
Y = 20405235
69 feet Y = 6235380
47 meter
Z = -7559824
59 Z = -2297342
30
XDOT = -17709
276502 XDOT = -5362
953055
YDOT = -2424
660903 feet/sec YDOT = -799
202926 meter/sec
ZDOT = -17674
769474 ZDOT = -5413
406435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17815673
70 X = 5430217
34
Y = -11044438
94 feet Y = -3366344
99 meter
Z = -7530733
45 Z = -2295367
56
XDOT = 2494
771836 XDOT = 760
406456
YDOT = 16152
272225 feet/sec YDOT = 4923
212574 meter/sec
ZDOT = -17789
103526 ZDOT = -5422
118755
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
10052832
00016717 00000-0 10270-3 0 9023
2 25544 51
6420 240
9538 0006298 330
2723 29
8071 15
53896440 32968
Satellite: ISS
Catalog Number: 25544
Epoch time: 16349
10052832 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 240
9538 deg
Eccentricity:
0006298
Arg of perigee: 330
2723 deg
Mean anomaly: 29
8071 deg
Mean motion: 15
53896440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 305
Coasting Arc #4 (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 = -422340
86 A = 6784392
88 meter
Y = -5700535
84 meter E =
0010338
Z = 3641909
53 I = 51
33367
XDOT = 5873
174276 Wp = 62
38173
YDOT = 2343
868745 meter/sec RA = 235
11103 deg
ZDOT = 4345
082531 TA = 341
10481
MA = 341
14315
Ha = 221
697 n
mi
Hp = 215
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1385632
73 X = -376255
41
Y = -18702545
40 feet Y = -5705001
49 meter
Z = 11948522
09 Z = 3639969
17
XDOT = 19268
944476 XDOT = 5825
421525
YDOT = 7689
858088 feet/sec YDOT = 2409
279007 meter/sec
ZDOT = 14255
520116 ZDOT = 4373
497194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17134229
50 X = -5222513
15
Y = 7635618
76 feet Y = 2327336
60 meter
Z = 11941016
22 Z = 3639621
74
XDOT = 1389
224669 XDOT = 423
435679
YDOT = -19394
705276 feet/sec YDOT = -5911
506168 meter/sec
ZDOT = 14379
568995 ZDOT = 4382
892630
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
12951956
00016717 00000-0 10270-3 0 9033
2 25544 51
6409 235
8266 0006316 334
6792 25
4050 15
53892486 33125
Satellite: ISS
Catalog Number: 25544
Epoch time: 16350
12951956 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 235
8266 deg
Eccentricity:
0006316
Arg of perigee: 334
6792 deg
Mean anomaly: 25
4050 deg
Mean motion: 15
53892486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 312
Coasting Arc #5 (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 = -757518
76 A = 6780853
98 meter
Y = 4889928
19 meter E =
0011929
Z = -4647166
03 I = 51
34133
XDOT = -6071
811013 Wp = 38
76963
YDOT = -3677
403775 meter/sec RA = 230
10356 deg
ZDOT = -2874
654292 TA = 202
47465
MA = 202
52695
Ha = 221
818 n
mi
Hp = 215
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2485297
78 X = -789569
12
Y = 16043071
50 feet Y = 4881278
41 meter
Z = -15246607
71 Z = -4650923
16
XDOT = -19920
639805 XDOT = -6016
274333
YDOT = -12064
973016 feet/sec YDOT = -3744
992010 meter/sec
ZDOT = -9431
280485 ZDOT = -2904
014942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15859601
99 X = 4834006
69
Y = -3391459
08 feet Y = -1033716
73 meter
Z = -15263909
22 Z = -4652439
53
XDOT = -4581
751995 XDOT = -1396
518008
YDOT = 21672
813446 feet/sec YDOT = 6605
873538 meter/sec
ZDOT = -9559
265036 ZDOT = -2913
663983
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
09419471
00016717 00000-0 10270-3 0 9042
2 25544 51
6411 231
0198 0006299 337
4166 22
6708 15
53895149 33270
Satellite: ISS
Catalog Number: 25544
Epoch time: 16351
09419471 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 231
0198 deg
Eccentricity:
0006299
Arg of perigee: 337
4166 deg
Mean anomaly: 22
6708 deg
Mean motion: 15
53895149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 316
Coasting Arc #6 (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 = 2041969
33 A = 6778408
10 meter
Y = -3838923
63 meter E =
0004120
Z = 5198151
38 I = 51
35415
XDOT = 5958
147746 Wp = 19
35633
YDOT = 4695
773728 meter/sec RA = 225
08882 deg
ZDOT = 1130
952867 TA = 59
78170
MA = 59
74090
Ha = 221
877 n
mi
Hp = 215
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6699374
44 X = 2059495
27
Y = -12594893
80 feet Y = -3815991
42 meter
Z = 17054302
41 Z = 5208112
88
XDOT = 19547
728826 XDOT = 5899
701950
YDOT = 15406
081785 feet/sec YDOT = 4762
074849 meter/sec
ZDOT = 3710
475284 ZDOT = 1159
754237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14132188
91 X = -4307491
18
Y = -1510401
00 feet Y = -460370
22 meter
Z = 17098600
06 Z = 5211653
30
XDOT = 7061
886090 XDOT = 2152
462880
YDOT = -22782
841007 feet/sec YDOT = -6944
209939 meter/sec
ZDOT = 3835
860288 ZDOT = 1169
170216
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
12317459
00016717 00000-0 10270-3 0 9051
2 25544 51
6403 225
8919 0006400 342
5189 17
5742 15
53918279 33438
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
12317459 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 225
8919 deg
Eccentricity:
0006400
Arg of perigee: 342
5189 deg
Mean anomaly: 17
5742 deg
Mean motion: 15
53918279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 313
Coasting Arc #7 (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 = 2626366
96 A = 6778078
14 meter
Y = -3338751
24 meter E =
0005349
Z = 5280986
78 I = 51
35369
XDOT = 5693
761475 Wp = 5
97116
YDOT = 5121
516234 meter/sec RA = 224
43356 deg
ZDOT = 411
466908 TA = 80
12004
MA = 80
05966
Ha = 221
921 n
mi
Hp = 215
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8616689
48 X = 2637854
03
Y = -10953908
27 feet Y = -3309317
67 meter
Z = 17326072
10 Z = 5293772
49
XDOT = 18680
319800 XDOT = 5634
069485
YDOT = 16802
874782 feet/sec YDOT = 5184
853907 meter/sec
ZDOT = 1349
957046 ZDOT = 438
980958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11939266
10 X = -3639088
31
Y = 7051619
78 feet Y = 2149333
71 meter
Z = 17382658
08 Z = 5298234
18
XDOT = -10658
267612 XDOT = -3248
639968
YDOT = -21626
690503 feet/sec YDOT = -6591
815265 meter/sec
ZDOT = 1469
632812 ZDOT = 447
944081
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
25179729
00016717 00000-0 10270-3 0 9062
2 25544 51
6382 225
2512 0006532 342
2432 17
8491 15
53899868 33459
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
25179729 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 225
2512 deg
Eccentricity:
0006532
Arg of perigee: 342
2432 deg
Mean anomaly: 17
8491 deg
Mean motion: 15
53899868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 325
Coasting Arc #8 (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 = -3860780
87 A = 6778672
41 meter
Y = 2151546
21 meter E =
0012641
Z = -5149260
01 I = 51
37945
XDOT = -5021
289829 Wp = 72
46435
YDOT = -5605
250020 meter/sec RA = 219
41762 deg
ZDOT = 1429
396506 TA = 211
31611
MA = 211
39146
Ha = 222
131 n
mi
Hp = 215
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12666603
91 X = -3859540
46
Y = 7058878
63 feet Y = 2108379
63 meter
Z = -16893897
68 Z = -5168011
37
XDOT = -16474
047995 XDOT = -4965
180608
YDOT = -18389
927887 feet/sec YDOT = -5661
087825 meter/sec
ZDOT = 4689
621084 ZDOT = 1405
140515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14237576
35 X = 4339613
27
Y = -2183306
77 feet Y = -665471
90 meter
Z = -16976424
60 Z = -5174414
22
XDOT = 8811
706268 XDOT = 2685
808071
YDOT = 21985
317898 feet/sec YDOT = 6701
124895 meter/sec
ZDOT = 4584
278267 ZDOT = 1397
288016
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
21646071
00016717 00000-0 10270-3 0 9079
2 25544 51
6381 220
4442 0006636 346
1212 13
9757 15
53896656 33602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16353
21646071 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 220
4442 deg
Eccentricity:
0006636
Arg of perigee: 346
1212 deg
Mean anomaly: 13
9757 deg
Mean motion: 15
53896656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3360
Checksum: 305
Coasting Arc #9 (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 = 4981088
43 A = 6781199
89 meter
Y = -943417
32 meter E =
0012074
Z = 4503064
98 I = 51
41335
XDOT = 3955
868743 Wp = 34
75793
YDOT = 5760
619412 meter/sec RA = 214
40728 deg
ZDOT = -3155
001221 TA = 87
07528
MA = 86
93711
Ha = 222
157 n
mi
Hp = 214
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16342153
65 X = 4969394
03
Y = -3095201
17 feet Y = -887781
04 meter
Z = 14773835
23 Z = 4527233
17
XDOT = 12978
571991 XDOT = 3906
483495
YDOT = 18899
669986 feet/sec YDOT = 5804
580617 meter/sec
ZDOT = -10351
053876 ZDOT = -3135
904461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16340902
90 X = -4980707
20
Y = -2544757
03 feet Y = -775641
94 meter
Z = 14879904
83 Z = 4535394
99
XDOT = -6122
529522 XDOT = -1866
146998
YDOT = -20991
710608 feet/sec YDOT = -6398
273393 meter/sec
ZDOT = -10268
324481 ZDOT = -3129
785302
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
24543236
00016717 00000-0 10270-3 0 9083
2 25544 51
6377 215
3163 0006696 349
0774 11
0232 15
53925448 33767
Satellite: ISS
Catalog Number: 25544
Epoch time: 16354
24543236 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 215
3163 deg
Eccentricity:
0006696
Arg of perigee: 349
0774 deg
Mean anomaly: 11
0232 deg
Mean motion: 15
53925448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 314
Coasting Arc #10 (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 = -5840566
36 A = 6784823
61 meter
Y = -139191
68 meter E =
0007660
Z = -3447156
36 I = 51
45333
XDOT = -2551
467093 Wp = 33
58948
YDOT = -5609
325592 meter/sec RA = 209
40766 deg
ZDOT = 4560
597412 TA = 285
88723
MA = 285
97165
Ha = 222
300 n
mi
Hp = 214
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19161963
12 X = -5821831
13
Y = -456665
63 feet Y = -204399
94 meter
Z = -11309568
11 Z = -3475482
65
XDOT = -8370
955031 XDOT = -2510
705789
YDOT = -18403
299187 feet/sec YDOT = -5637
630077 meter/sec
ZDOT = 14962
589933 ZDOT = 4548
301906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17939657
44 X = 5468007
59
Y = 6537205
74 feet Y = 1992540
31 meter
Z = -11433693
06 Z = -3484989
64
XDOT = 2615
963534 XDOT = 797
345685
YDOT = 18835
304622 feet/sec YDOT = 5741
000849 meter/sec
ZDOT = 14909
626710 ZDOT = 4544
454221
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
21009007
00016717 00000-0 10270-3 0 9095
2 25544 51
6385 210
5091 0006743 352
8777 7
2279 15
53905795 33919
Satellite: ISS
Catalog Number: 25544
Epoch time: 16355
21009007 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 210
5091 deg
Eccentricity:
0006743
Arg of perigee: 352
8777 deg
Mean anomaly: 7
2279 deg
Mean motion: 15
53905795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 318
Coasting Arc #11 (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 = 6378206
87 A = 6788080
82 meter
Y = 1127392
11 meter E =
0012738
Z = 2023915
19 I = 51
49390
XDOT = 845
027995 Wp = 81
96832
YDOT = 5226
879341 meter/sec RA = 204
41898 deg
ZDOT = -5542
891863 TA = 75
62785
MA = 75
48649
Ha = 222
471 n
mi
Hp = 214
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20925875
55 X = 6355294
78
Y = 3698793
00 feet Y = 1198589
32 meter
Z = 6640141
69 Z = 2054843
15
XDOT = 2772
401557 XDOT = 813
441724
YDOT = 17148
554269 feet/sec YDOT = 5236
152605 meter/sec
ZDOT = -18185
340758 ZDOT = -5538
863477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18775504
59 X = -5722773
80
Y = -9860910
35 feet Y = -3005605
47 meter
Z = 6775521
65 Z = 2065179
00
XDOT = 1729
286118 XDOT = 527
086409
YDOT = -15846
427191 feet/sec YDOT = -4829
991008 meter/sec
ZDOT = -18168
539893 ZDOT = -5537
770959
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
23905383
00016717 00000-0 10270-3 0 9102
2 25544 51
6393 205
3808 0006839 356
6346 3
4759 15
53936799 34073
Satellite: ISS
Catalog Number: 25544
Epoch time: 16356
23905383 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 205
3808 deg
Eccentricity:
0006839
Arg of perigee: 356
6346 deg
Mean anomaly: 3
4759 deg
Mean motion: 15
53936799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 339
Coasting Arc #12 (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 = -6487531
10 A = 6789783
25 meter
Y = -1920660
25 meter E =
0016805
Z = -437963
52 I = 51
52869
XDOT = 992
733555 Wp = 26
58153
YDOT = -4694
860246 meter/sec RA = 199
44001 deg
ZDOT = 5987
287452 TA = 328
68580
MA = 328
78578
Ha = 222
525 n
mi
Hp = 214
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21284550
87 X = -6463444
19
Y = -6301378
77 feet Y = -1993073
49 meter
Z = -1436888
18 Z = -469419
81
XDOT = 3256
999851 XDOT = 1016
075324
YDOT = -15403
084796 feet/sec YDOT = -4683
628565 meter/sec
ZDOT = 19643
331534 ZDOT = 5992
166392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18571554
73 X = 5660609
88
Y = 12141767
84 feet Y = 3700810
84 meter
Z = -1574470
15 Z = -479898
50
XDOT = -6532
130512 XDOT = -1990
993380
YDOT = 12501
158217 feet/sec YDOT = 3810
353024 meter/sec
ZDOT = 19665
485420 ZDOT = 5994
039956
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
20370478
00016717 00000-0 10270-3 0 9112
2 25544 51
6386 200
5742 0006810
3043 359
8112 15
53939724 34224
Satellite: ISS
Catalog Number: 25544
Epoch time: 16357
20370478 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 200
5742 deg
Eccentricity:
0006810
Arg of perigee:
3043 deg
Mean anomaly: 359
8112 deg
Mean motion: 15
53939724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 290
Coasting Arc #13 (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 = 6153105
60 A = 6789248
88 meter
Y = 2594599
48 meter E =
0006055
Z = -1228883
74 I = 51
55881
XDOT = -2867
671145 Wp = 94
14200
YDOT = 4047
005747 meter/sec RA = 194
46444 deg
ZDOT = -5839
300037 TA = 99
21824
MA = 99
14974
Ha = 222
668 n
mi
Hp = 214
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20187354
34 X = 6129604
19
Y = 8512465
50 feet Y = 2663276
31 meter
Z = -4031770
79 Z = -1199050
47
XDOT = -9408
369899 XDOT = -2884
347897
YDOT = 13277
577911 feet/sec YDOT = 4014
844564 meter/sec
ZDOT = -19157
808519 ZDOT = -5853
270758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17157701
46 X = -5229667
40
Y = -13661584
67 feet Y = -4164051
01 meter
Z = -3901397
81 Z = -1189146
05
XDOT = 11532
069489 XDOT = 3514
974780
YDOT = -9019
067885 feet/sec YDOT = -2749
011891 meter/sec
ZDOT = -19219
717991 ZDOT = -5858
170044
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
23266299
00016717 00000-0 10270-3 0 9122
2 25544 51
6397 195
4462 0006880 3
2371 356
8825 15
53947675 34389
Satellite: ISS
Catalog Number: 25544
Epoch time: 16358
23266299 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 195
4462 deg
Eccentricity:
0006880
Arg of perigee: 3
2371 deg
Mean anomaly: 356
8825 deg
Mean motion: 15
53947675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 345
Coasting Arc #14 (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 = -5360864
39 A = 6786714
10 meter
Y = -3104252
79 meter E =
0016970
Z = 2746445
55 I = 51
58186
XDOT = 4593
367926 Wp = 56
45369
YDOT = -3368
983008 meter/sec RA = 189
48676 deg
ZDOT = 5144
314948 TA = 334
69753
MA = 334
78055
Ha = 222
806 n
mi
Hp = 214
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17588137
78 X = -5339094
46
Y = -10184556
41 feet Y = -3164080
03 meter
Z = 9010648
14 Z = 2720456
50
XDOT = 15070
104743 XDOT = 4605
710509
YDOT = -11053
093857 feet/sec YDOT = -3317
548181 meter/sec
ZDOT = 16877
673715 ZDOT = 5166
658153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14483062
27 X = 4414437
38
Y = 14329701
26 feet Y = 4367692
94 meter
Z = 8897197
80 Z = 2711865
89
XDOT = -16230
667866 XDOT = -4947
107566
YDOT = 5835
697322 feet/sec YDOT = 1778
720544 meter/sec
ZDOT = 16976
191390 ZDOT = 5174
343136
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
26161662
00016717 00000-0 10270-3 0 9135
2 25544 51
6397 190
3186 0006868 7
1776 352
9473 15
53955614 34540
Satellite: ISS
Catalog Number: 25544
Epoch time: 16359
26161662 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 190
3186 deg
Eccentricity:
0006868
Arg of perigee: 7
1776 deg
Mean anomaly: 352
9473 deg
Mean motion: 15
53955614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 339
Coasting Arc #15 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2016/360/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4176347
60 A = 6783035
20 meter
Y = 3530186
01 meter E =
0012006
Z = -4026802
19 I = 51
60147
XDOT = -6019
963300 Wp = 41
91464
YDOT = 2644
742962 meter/sec RA = 184
50252 deg
ZDOT = -3922
997824 TA = 187
25041
MA = 187
26779
Ha = 222
890 n
mi
Hp = 214
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13701927
82 X = 4156122
22
Y = 11581975
10 feet Y = 3576775
95 meter
Z = -13211293
27 Z = -4006563
40
XDOT = -19750
535761 XDOT = -6030
033853
YDOT = 8676
978221 feet/sec YDOT = 2577
367666 meter/sec
ZDOT = -12870
727770 ZDOT = -3952
265559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10647324
21 X = -3245304
42
Y = -14520385
51 feet Y = -4425813
50 meter
Z = -13123114
53 Z = -3999925
31
XDOT = 20104
241223 XDOT = 6127
772725
YDOT = -2987
347589 feet/sec YDOT = -910
543545 meter/sec
ZDOT = -12999
507442 ZDOT = -3962
249868
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 16360
22625813
00016717 00000-0 10270-3 0 9147
2 25544 51
6395 185
5112 0007053 11
2090 348
9219 15
53966505 34695
Satellite: ISS
Catalog Number: 25544
Epoch time: 16360
22625813 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 185
5112 deg
Eccentricity:
0007053
Arg of perigee: 11
2090 deg
Mean anomaly: 348
9219 deg
Mean motion: 15
53966505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 306
Coasting Arc #16 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2016/361/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2665482
27 A = 6779627
67 meter
Y = -3852505
08 meter E =
0008085
Z = 4893103
84 I = 51
62260
XDOT = 7054
723138 Wp = 67
52816
YDOT = -1911
651329 meter/sec RA = 179
51162 deg
ZDOT = 2337
841721 TA = 359
60337
MA = 359
60401
Ha = 222
897 n
mi
Hp = 213
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8745020
58 X = -2645973
02
Y = -12639452
35 feet Y = -3882203
63 meter
Z = 16053490
28 Z = 4880202
66
XDOT = 23145
417120 XDOT = 7064
219184
YDOT = -6271
821947 feet/sec YDOT = -1832
707780 meter/sec
ZDOT = 7670
084386 ZDOT = 2372
134649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5845605
84 X = 1781740
66
Y = 14277725
86 feet Y = 4351850
84 meter
Z = 15997535
04 Z = 4876048
68
XDOT = -22868
237934 XDOT = -6970
238922
YDOT = 599
674727 feet/sec YDOT = 182
780857 meter/sec
ZDOT = 7820
803910 ZDOT = 2383
781032
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 16361
25520508
00016717 00000-0 10270-3 0 9157
2 25544 51
6394 180
3840 0006854 13
3788 346
7545 15
53989148 34854
Satellite: ISS
Catalog Number: 25544
Epoch time: 16361
25520508 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 180
3840 deg
Eccentricity:
0006854
Arg of perigee: 13
3788 deg
Mean anomaly: 346
7545 deg
Mean motion: 15
53989148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 335
Coasting Arc #17 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2016/362/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 987534
94 A = 6777923
53 meter
Y = 4121401
88 meter E =
0018534
Z = -5304678
05 I = 51
64983
XDOT = -7552
818242 Wp = 65
43607
YDOT = 1136
324295 meter/sec RA = 174
51452 deg
ZDOT = -517
104175 TA = 199
58708
MA = 199
65837
Ha = 223
033 n
mi
Hp = 213
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3239944
03 X = 967142
71
Y = 13521659
71 feet Y = 4132331
65 meter
Z = -17403799
37 Z = -5299930
00
XDOT = -24779
587408 XDOT = -7562
451712
YDOT = 3728
098080 feet/sec YDOT = 1051
809790 meter/sec
ZDOT = -1696
536007 ZDOT = -553
817025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -529688
38 X = -161449
02
Y = -13919520
21 feet Y = -4242669
76 meter
Z = -17383645
72 Z = -5298535
22
XDOT = 23993
208069 XDOT = 7313
129820
YDOT = 1432
095328 feet/sec YDOT = 436
502656 meter/sec
ZDOT = -1857
767548 ZDOT = -566
247549
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 16362
21984141
00016717 00000-0 10270-3 0 9162
2 25544 51
6401 175
5759 0007043 17
6813 342
4583 15
53972077 35001
Satellite: ISS
Catalog Number: 25544
Epoch time: 16362
21984141 = yrday
fracday
Element set: 916
Inclination: 51
6401 deg
RA of node: 175
5759 deg
Eccentricity:
0007043
Arg of perigee: 17
6813 deg
Mean anomaly: 342
4583 deg
Mean motion: 15
53972077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 307
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