[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 22nd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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
182/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
183/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
9
Coasting Arc #1 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2017/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6285063
10 A = 6786746
35 meter
Y = 254376
06 meter E =
0009072
Z = 2539871
67 I = 51
76050
XDOT = -2348
317896 Wp = 91
86396
YDOT = -5027
027071 meter/sec RA = 16
23618 deg
ZDOT = -5291
552754 TA = 59
66619
MA = 59
57650
Ha = 220
225 n
mi
Hp = 216
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20620285
75 X = -6299778
05
Y = 834567
13 feet Y = 184009
61 meter
Z = 8332912
30 Z = 2509304
77
XDOT = -7704
455038 XDOT = -2266
225808
YDOT = -16492
870967 feet/sec YDOT = -5052
827836 meter/sec
ZDOT = -17360
737383 ZDOT = -5302
761555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 478662
10 X = 145896
21
Y = 20685635
99 feet Y = 6304981
85 meter
Z = 8197893
64 Z = 2498717
98
XDOT = -15114
456244 XDOT = -4606
886263
YDOT = 7270
358540 feet/sec YDOT = 2216
005283 meter/sec
ZDOT = -17409
242530 ZDOT = -5306
337123
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 17172
53717994
00016717 00000-0 10270-3 0 9000
2 25544 51
6406 16
6533 0005216 306
6420 53
4252 15
54106940 22429
Satellite: ISS
Catalog Number: 25544
Epoch time: 17172
53717994 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 16
6533 deg
Eccentricity:
0005216
Arg of perigee: 306
6420 deg
Mean anomaly: 53
4252 deg
Mean motion: 15
54106940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 283
Coasting Arc #2 (Orbit 2256)
---------------------------------------
Vector Time (GMT): 2017/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6691241
88 A = 6789174
55 meter
Y = 570940
28 meter E =
0011129
Z = -948041
34 I = 51
73522
XDOT = 422
635603 Wp = 11
24742
YDOT = 4850
760285 meter/sec RA = 11
27013 deg
ZDOT = 5926
587582 TA = 338
49730
MA = 338
54401
Ha = 220
368 n
mi
Hp = 216
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21952893
31 X = 6688965
32
Y = 1873163
64 feet Y = 645753
70 meter
Z = -3110371
85 Z = -915542
56
XDOT = 1386
599747 XDOT = 339
573058
YDOT = 15914
567863 feet/sec YDOT = 4855
021130 meter/sec
ZDOT = 19444
184981 ZDOT = 5928
439636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1873842
94 X = 571147
33
Y = -21972673
26 feet Y = -6697270
81 meter
Z = -2966988
80 Z = -904338
19
XDOT = 14314
094795 XDOT = 4362
936094
YDOT = -1395
440318 feet/sec YDOT = -425
330209 meter/sec
ZDOT = 19451
404456 ZDOT = 5928
788078
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 17173
50175103
00016717 00000-0 10270-3 0 9019
2 25544 51
6391 11
8448 0005115 307
7266 52
3422 15
54062325 22573
Satellite: ISS
Catalog Number: 25544
Epoch time: 17173
50175103 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 11
8448 deg
Eccentricity:
0005115
Arg of perigee: 307
7266 deg
Mean anomaly: 52
3422 deg
Mean motion: 15
54062325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2257
Checksum: 276
Coasting Arc #3 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2017/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6610551
71 A = 6789185
00 meter
Y = -1334130
27 meter E =
0005207
Z = -759853
19 I = 51
70360
XDOT = 1600
825238 Wp = 147
43430
YDOT = -4553
807519 meter/sec RA = 6
30555 deg
ZDOT = -5954
632870 TA = 40
76776
MA = 40
72881
Ha = 220
465 n
mi
Hp = 216
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21688161
79 X = -6591450
81
Y = -4377067
81 feet Y = -1407947
01 meter
Z = -2492956
66 Z = -791919
11
XDOT = 5252
051305 XDOT = 1680
552876
YDOT = -14940
313382 feet/sec YDOT = -4535
459215 meter/sec
ZDOT = -19536
197080 ZDOT = -5946
663662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4004815
46 X = -1220667
75
Y = 21743319
95 feet Y = 6627363
92 meter
Z = -2634275
65 Z = -802927
22
XDOT = -13446
622810 XDOT = -4098
530632
YDOT = -4830
429879 feet/sec YDOT = -1472
315027 meter/sec
ZDOT = -19500
107486 ZDOT = -5943
632762
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 17174
53062324
00016717 00000-0 10270-3 0 9024
2 25544 51
6392 6
7157 0005156 312
9318 47
1401 15
54082863 22731
Satellite: ISS
Catalog Number: 25544
Epoch time: 17174
53062324 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 6
7157 deg
Eccentricity:
0005156
Arg of perigee: 312
9318 deg
Mean anomaly: 47
1401 deg
Mean motion: 15
54082863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 289
Coasting Arc #4 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2017/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6022485
89 A = 6786978
08 meter
Y = 2016527
22 meter E =
0012166
Z = 2371853
19 I = 51
66281
XDOT = -3523
845510 Wp = 52
54282
YDOT = 4177
137820 meter/sec RA = 1
33490 deg
ZDOT = 5384
496285 TA = 333
94639
MA = 334
00757
Ha = 220
448 n
mi
Hp = 215
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19758811
97 X = 5987967
69
Y = 6615902
94 feet Y = 2083681
33 meter
Z = 7781670
57 Z = 2401024
96
XDOT = -11561
172934 XDOT = -3596
448600
YDOT = 13704
520407 feet/sec YDOT = 4137
324924 meter/sec
ZDOT = 17665
670226 ZDOT = 5367
202971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5935664
33 X = 1809190
49
Y = -19923198
09 feet Y = -6072590
78 meter
Z = 7910074
96 Z = 2410990
85
XDOT = 12646
324893 XDOT = 3854
599827
YDOT = 10765
812655 feet/sec YDOT = 3281
419697 meter/sec
ZDOT = 17588
485587 ZDOT = 5360
970407
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 17175
55949255
00016717 00000-0 10270-3 0 9035
2 25544 51
6382 1
5858 0004990 315
3983 44
6768 15
54090004 22892
Satellite: ISS
Catalog Number: 25544
Epoch time: 17175
55949255 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 1
5858 deg
Eccentricity:
0004990
Arg of perigee: 315
3983 deg
Mean anomaly: 44
6768 deg
Mean motion: 15
54090004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2289
Checksum: 331
Coasting Arc #5 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2017/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4985513
53 A = 6783359
41 meter
Y = -2664107
87 meter E =
0005916
Z = -3756737
52 I = 51
61772
XDOT = 5185
581072 Wp = 27
39425
YDOT = -3704
982076 meter/sec RA = 356
35509 deg
ZDOT = -4251
839410 TA = 197
52453
MA = 197
54495
Ha = 220
716 n
mi
Hp = 215
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16356671
69 X = -4937104
03
Y = -8740511
39 feet Y = -2719587
99 meter
Z = -12325254
33 Z = -3780838
23
XDOT = 17013
061260 XDOT = 5247
278911
YDOT = -12155
453004 feet/sec YDOT = -3646
647742 meter/sec
ZDOT = -13949
604364 ZDOT = -4226
500429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7891145
31 X = -2405221
09
Y = 16704661
65 feet Y = 5091580
87 meter
Z = -12431140
22 Z = -3789011
54
XDOT = -11803
959572 XDOT = -3597
846877
YDOT = -15879
166292 feet/sec YDOT = -4839
969886 meter/sec
ZDOT = -13836
991330 ZDOT = -4217
514957
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 17176
52405771
00016717 00000-0 10270-3 0 9044
2 25544 51
6377 356
7778 0004933 321
3425 38
7374 15
54090849 23049
Satellite: ISS
Catalog Number: 25544
Epoch time: 17176
52405771 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 356
7778 deg
Eccentricity:
0004933
Arg of perigee: 321
3425 deg
Mean anomaly: 38
7374 deg
Mean motion: 15
54090849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 327
Coasting Arc #6 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2017/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3573867
60 A = 6779846
29 meter
Y = 3264060
39 meter E =
0003657
Z = 4744252
96 I = 51
57372
XDOT = -6454
878405 Wp = 82
42978
YDOT = 3145
052490 meter/sec RA = 351
36211 deg
ZDOT = 2697
372758 TA = 340
89063
MA = 340
90435
Ha = 220
741 n
mi
Hp = 215
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11725287
41 X = 3514057
44
Y = 10708859
55 feet Y = 3303690
72 meter
Z = 15565134
38 Z = 4761468
68
XDOT = -21177
422589 XDOT = -6502
669821
YDOT = 10318
413681 feet/sec YDOT = 3072
602071 meter/sec
ZDOT = 8849
648156 ZDOT = 2665
901704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9886294
13 X = 3013342
45
Y = -12331718
47 feet Y = -3758707
79 meter
Z = 15640503
64 Z = 4767225
51
XDOT = 10854
638608 XDOT = 3308
493848
YDOT = 19754
675146 feet/sec YDOT = 6021
224985 meter/sec
ZDOT = 8710
076395 ZDOT = 2654
831285
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 17177
55292448
00016717 00000-0 10270-3 0 9054
2 25544 51
6381 351
6483 0005037 323
3440 36
7367 15
54071481 23205
Satellite: ISS
Catalog Number: 25544
Epoch time: 17177
55292448 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 351
6483 deg
Eccentricity:
0005037
Arg of perigee: 323
3440 deg
Mean anomaly: 36
7367 deg
Mean motion: 15
54071481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 303
Coasting Arc #7 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2017/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1937619
45 A = 6777687
16 meter
Y = -3828005
12 meter E =
0013272
Z = -5257875
65 I = 51
53557
XDOT = 7203
650955 Wp = 63
96887
YDOT = -2454
265804 meter/sec RA = 346
35982 deg
ZDOT = -863
839801 TA = 197
72602
MA = 197
77237
Ha = 220
926 n
mi
Hp = 215
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6357019
18 X = -1869129
84
Y = -12559071
90 feet Y = -3849289
33 meter
Z = -17250248
20 Z = -5267121
98
XDOT = 23634
025444 XDOT = 7234
755868
YDOT = -8052
053162 feet/sec YDOT = -2373
535677 meter/sec
ZDOT = -2834
120083 ZDOT = -828
771890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11978099
28 X = -3650924
66
Y = 7299514
73 feet Y = 2224892
09 meter
Z = -17290322
88 Z = -5270090
41
XDOT = -9521
079285 XDOT = -2902
024966
YDOT = -21999
861920 feet/sec YDOT = -6705
557913 meter/sec
ZDOT = -2678
811727 ZDOT = -816
501814
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 17178
51748448
00016717 00000-0 10270-3 0 9068
2 25544 51
6392 346
8406 0004808 329
2144 30
8726 15
54091333 23357
Satellite: ISS
Catalog Number: 25544
Epoch time: 17178
51748448 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 346
8406 deg
Eccentricity:
0004808
Arg of perigee: 329
2144 deg
Mean anomaly: 30
8726 deg
Mean motion: 15
54091333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 319
Coasting Arc #8 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2017/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 186674
18 A = 6778002
12 meter
Y = 4319101
31 meter E =
0006433
Z = 5220465
24 I = 51
50343
XDOT = -7421
357213 Wp = 8
81250
YDOT = 1612
692073 meter/sec RA = 341
35166 deg
ZDOT = -1062
467715 TA = 91
42098
MA = 91
34729
Ha = 221
129 n
mi
Hp = 215
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 612448
11 X = 113004
83
Y = 14170279
87 feet Y = 4320776
41 meter
Z = 17127510
62 Z = 5221193
51
XDOT = -24348
284820 XDOT = -7433
678308
YDOT = 5290
984493 feet/sec YDOT = 1529
632635 meter/sec
ZDOT = -3485
786468 ZDOT = -1098
547713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14044910
59 X = 4280888
75
Y = -1957296
25 feet Y = -596583
90 meter
Z = 17129886
81 Z = 5221189
50
XDOT = 7624
958202 XDOT = 2324
087260
YDOT = 22626
587614 feet/sec YDOT = 6896
583905 meter/sec
ZDOT = -3645
388707 ZDOT = -1111
114478
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 17179
54634780
00016717 00000-0 10270-3 0 9076
2 25544 51
6379 341
7115 0004763 332
9903 27
1001 15
54045483 23515
Satellite: ISS
Catalog Number: 25544
Epoch time: 17179
54634780 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 341
7115 deg
Eccentricity:
0004763
Arg of perigee: 332
9903 deg
Mean anomaly: 27
1001 deg
Mean motion: 15
54045483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 305
Coasting Arc #9 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2017/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1479977
83 A = 6780267
76 meter
Y = -4700439
63 meter E =
0007928
Z = -4663397
84 I = 51
48253
XDOT = 7079
687068 Wp = 83
54393
YDOT = -609
976460 meter/sec RA = 336
34618 deg
ZDOT = 2866
706084 TA = 214
99582
MA = 215
04795
Ha = 221
136 n
mi
Hp = 215
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4855570
32 X = 1555081
67
Y = -15421389
87 feet Y = -4683469
20 meter
Z = -15299861
68 Z = -4656026
61
XDOT = 23227
319778 XDOT = 7072
056893
YDOT = -2001
235104 feet/sec YDOT = -530
849496 meter/sec
ZDOT = 9405
203689 ZDOT = 2901
078103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15906214
81 X = -4848214
27
Y = -3067661
86 feet Y = -935023
34 meter
Z = -15266413
36 Z = -4653202
79
XDOT = -4991
340567 XDOT = -1521
360605
YDOT = -21597
590395 feet/sec YDOT = -6582
945552 meter/sec
ZDOT = 9557
061009 ZDOT = 2912
992195
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 17180
51090333
00016717 00000-0 10270-3 0 9086
2 25544 51
6396 336
9041 0004794 335
5540 24
5384 15
54090224 23662
Satellite: ISS
Catalog Number: 25544
Epoch time: 17180
51090333 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 336
9041 deg
Eccentricity:
0004794
Arg of perigee: 335
5540 deg
Mean anomaly: 24
5384 deg
Mean motion: 15
54090224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 302
Coasting Arc #10 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2017/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2988143
71 A = 6784024
20 meter
Y = 4905418
23 meter E =
0011537
Z = 3605796
79 I = 51
46510
XDOT = -6257
319079 Wp = 63
01325
YDOT = -569
400678 meter/sec RA = 331
34578 deg
ZDOT = -4394
845683 TA = 74
16655
MA = 74
03939
Ha = 221
297 n
mi
Hp = 215
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9803621
11 X = -3060290
38
Y = 16093891
81 feet Y = 4871599
10 meter
Z = 11830041
97 Z = 3591106
56
XDOT = -20529
262069 XDOT = -6229
138971
YDOT = -1868
112461 feet/sec YDOT = -639
216360 meter/sec
ZDOT = -14418
785049 ZDOT = -4425
173204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17297921
70 X = 5272406
54
Y = 7580137
49 feet Y = 2310425
91 meter
Z = 11764253
23 Z = 3585744
38
XDOT = 1503
420027 XDOT = 458
242424
YDOT = 19236
451085 feet/sec YDOT = 5863
270291 meter/sec
ZDOT = -14552
552362 ZDOT = -4435
617960
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 17181
53976122
00016717 00000-0 10270-3 0 9099
2 25544 51
6392 331
7747 0004810 339
5422 20
5537 15
54078951 23823
Satellite: ISS
Catalog Number: 25544
Epoch time: 17181
53976122 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 331
7747 deg
Eccentricity:
0004810
Arg of perigee: 339
5422 deg
Mean anomaly: 20
5537 deg
Mean motion: 15
54078951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 316
Coasting Arc #11 (Orbit 2396)
---------------------------------------
Vector Time (GMT): 2017/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4163839
80 A = 6787415
72 meter
Y = -4879764
90 meter E =
0009664
Z = -2202798
22 I = 51
44917
XDOT = 5057
130516 Wp = 16
64883
YDOT = 1858
387286 meter/sec RA = 326
35497 deg
ZDOT = 5457
452039 TA = 318
81375
MA = 318
88663
Ha = 221
396 n
mi
Hp = 215
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13660891
72 X = 4228797
22
Y = -16009727
37 feet Y = -4832838
65 meter
Z = -7227028
27 Z = -2182414
26
XDOT = 16591
635550 XDOT = 5009
464157
YDOT = 6097
071147 feet/sec YDOT = 1914
672594 meter/sec
ZDOT = 17905
026375 ZDOT = 5481
902301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17932167
92 X = -5465724
78
Y = -11075847
79 feet Y = -3375918
41 meter
Z = -7136120
80 Z = -2175089
62
XDOT = 2678
452091 XDOT = 816
392197
YDOT = -15909
796614 feet/sec YDOT = -4849
306008 meter/sec
ZDOT = 18012
597964 ZDOT = 5490
239859
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 17182
50431307
00016717 00000-0 10270-3 0 9100
2 25544 51
6399 326
9674 0004840 343
8291 16
2707 15
54095400 23975
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
50431307 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 326
9674 deg
Eccentricity:
0004840
Arg of perigee: 343
8291 deg
Mean anomaly: 16
2707 deg
Mean motion: 15
54095400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2397
Checksum: 309
Coasting Arc #12 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2017/182/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3761507
17 A = 6778193
93 meter
Y = -2353322
93 meter E =
0014471
Z = -5136488
18 I = 51
40820
XDOT = 5347
199729 Wp = 57
69144
YDOT = -5274
205146 meter/sec RA = 324
53354 deg
ZDOT = -1494
906727 TA = 197
82026
MA = 197
87106
Ha = 221
498 n
mi
Hp = 214
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12340902
78 X = -3709961
66
Y = -7720875
74 feet Y = -2395098
02 meter
Z = -16851995
35 Z = -5154635
37
XDOT = 17543
306198 XDOT = 5413
041368
YDOT = -17303
822659 feet/sec YDOT = -5214
040866 meter/sec
ZDOT = -4904
549628 ZDOT = -1468
772271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13529237
62 X = 4123711
63
Y = -5116495
06 feet Y = -1559507
69 meter
Z = -16931649
62 Z = -5160766
80
XDOT = 2863
054456 XDOT = 872
658998
YDOT = 23464
302241 feet/sec YDOT = 7151
919323 meter/sec
ZDOT = -4788
187810 ZDOT = -1459
439645
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 17182
89013236
00016717 00000-0 10270-3 0 9110
2 25544 51
6397 325
0486 0005145 346
3440 13
7573 15
54084655 24038
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
89013236 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 325
0486 deg
Eccentricity:
0005145
Arg of perigee: 346
3440 deg
Mean anomaly: 13
7573 deg
Mean motion: 15
54084655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 302
Coasting Arc #13 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2017/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5003653
19 A = 6789273
07 meter
Y = 4552341
92 meter E =
0009501
Z = 542265
85 I = 51
42829
XDOT = -3584
974606 Wp = 111
12947
YDOT = -3220
619241 meter/sec RA = 321
36924 deg
ZDOT = -5961
264083 TA = 63
00446
MA = 62
90749
Ha = 221
423 n
mi
Hp = 214
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16416185
00 X = -5056820
85
Y = 14935504
99 feet Y = 4496090
35 meter
Z = 1779087
45 Z = 517830
95
XDOT = -11761
727710 XDOT = -3519
737496
YDOT = -10566
336093 feet/sec YDOT = -3260
343569 meter/sec
ZDOT = -19557
953028 ZDOT = -5978
520591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17526593
34 X = 5342105
65
Y = 13629159
11 feet Y = 4154167
70 meter
Z = 1670371
01 Z = 509129
08
XDOT = -7427
446011 XDOT = -2263
885544
YDOT = 11992
441720 feet/sec YDOT = 3655
296236 meter/sec
ZDOT = -19633
510415 ZDOT = -5984
293974
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 17183
53316666
00016717 00000-0 10270-3 0 9126
2 25544 51
6392 321
8386 0004908 346
3989 13
7030 15
54109198 24139
Satellite: ISS
Catalog Number: 25544
Epoch time: 17183
53316666 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 321
8386 deg
Eccentricity:
0004908
Arg of perigee: 346
3989 deg
Mean anomaly: 13
7030 deg
Mean motion: 15
54109198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 319
Coasting Arc #14 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2017/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5422041
91 A = 6788775
10 meter
Y = -3905030
10 meter E =
0016247
Z = 1144004
32 I = 51
40371
XDOT = 2019
907315 Wp = 41
48301
YDOT = 4530
271317 meter/sec RA = 316
38362 deg
ZDOT = 5854
778289 TA = 330
98644
MA = 331
07664
Ha = 221
475 n
mi
Hp = 214
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17788851
40 X = 5459748
99
Y = -12811778
55 feet Y = -3844186
43 meter
Z = 3753295
00 Z = 1170434
11
XDOT = 6626
992504 XDOT = 1940
658871
YDOT = 14863
094871 feet/sec YDOT = 4552
415599 meter/sec
ZDOT = 19208
590187 ZDOT = 5864
398344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15923446
91 X = -4853466
62
Y = -15037744
43 feet Y = -4583504
50 meter
Z = 3870685
70 Z = 1179785
00
XDOT = 12280
441259 XDOT = 3743
078496
YDOT = -8019
481116 feet/sec YDOT = -2444
337844 meter/sec
ZDOT = 19250
195734 ZDOT = 5867
459660
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 17184
56201733
00016717 00000-0 10270-3 0 9139
2 25544 51
6409 316
7098 0004889 351
1183 8
9882 15
54118219 24291
Satellite: ISS
Catalog Number: 25544
Epoch time: 17184
56201733 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 316
7098 deg
Eccentricity:
0004889
Arg of perigee: 351
1183 deg
Mean anomaly: 8
9882 deg
Mean motion: 15
54118219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 324
Coasting Arc #15 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2017/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5486053
64 A = 6786101
17 meter
Y = 2911934
04 meter E =
0004432
Z = -2740853
88 I = 51
37156
XDOT = -454
819033 Wp = 55
26774
YDOT = -5676
788738 meter/sec RA = 311
39241 deg
ZDOT = -5124
208957 TA = 155
85005
MA = 155
82926
Ha = 221
657 n
mi
Hp = 214
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17998863
63 X = -5504894
19
Y = 9553589
37 feet Y = 2850480
23 meter
Z = -8992302
76 Z = -2767548
86
XDOT = -1492
188428 XDOT = -366
414996
YDOT = -18624
634968 feet/sec YDOT = -5681
379955 meter/sec
ZDOT = -16811
709177 ZDOT = -5126
204251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13026271
63 X = 3970407
59
Y = 15601397
22 feet Y = 4755305
87 meter
Z = -9110670
85 Z = -2776932
47
XDOT = -16809
941381 XDOT = -5123
670133
YDOT = 4219
874820 feet/sec YDOT = 1286
217845 meter/sec
ZDOT = -16819
450733 ZDOT = -5126
568583
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 17185
52656281
00016717 00000-0 10270-3 0 9149
2 25544 51
6406 311
9020 0004970 355
2546 4
8559 15
54114322 24443
Satellite: ISS
Catalog Number: 25544
Epoch time: 17185
52656281 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 311
9020 deg
Eccentricity:
0004970
Arg of perigee: 355
2546 deg
Mean anomaly: 4
8559 deg
Mean motion: 15
54114322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2444
Checksum: 296
Coasting Arc #16 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2017/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5200587
98 A = 6782280
31 meter
Y = -1623992
85 meter E =
0010545
Z = 4028460
40 I = 51
33862
XDOT = -967
247044 Wp = 75
32904
YDOT = 6547
830070 meter/sec RA = 306
39039 deg
ZDOT = 3882
399230 TA = 334
25793
MA = 334
31038
Ha = 221
521 n
mi
Hp = 214
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17062296
52 X = 5198793
12
Y = -5328060
53 feet Y = -1565846
89 meter
Z = 13216733
61 Z = 4053718
66
XDOT = -3173
382691 XDOT = -1059
253482
YDOT = 21482
382118 feet/sec YDOT = 6536
498730 meter/sec
ZDOT = 12737
530281 ZDOT = 3877
478002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8958207
32 X = -2730461
59
Y = -15371838
43 feet Y = -4685336
35 meter
Z = 13328516
19 Z = 4062531
73
XDOT = 20549
912388 XDOT = 6263
613296
YDOT = -934
675294 feet/sec YDOT = -284
889030 meter/sec
ZDOT = 12714
589637 ZDOT = 3875
406921
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 17186
55540773
00016717 00000-0 10270-3 0 9152
2 25544 51
6409 306
7736 0004924 357
9045 2
2086 15
54141780 24607
Satellite: ISS
Catalog Number: 25544
Epoch time: 17186
55540773 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 306
7736 deg
Eccentricity:
0004924
Arg of perigee: 357
9045 deg
Mean anomaly: 2
2086 deg
Mean motion: 15
54141780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 313
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