[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 1st 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
183/15:38:00
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
190/12:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (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 = -2999606
35 A = 6784033
52 meter
Y = 4904404
25 meter E =
0011562
Z = 3597652
89 I = 51
46521
XDOT = -6250
269631 Wp = 63
15492
YDOT = -580
847335 meter/sec RA = 331
34451 deg
ZDOT = -4403
376370 TA = 74
14477
MA = 74
01735
Ha = 221
296 n
mi
Hp = 215
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9841228
17 X = -3071701
27
Y = 16090565
12 feet Y = 4870457
23 meter
Z = 11803323
12 Z = 3582907
10
XDOT = -20506
133960 XDOT = -6221
920611
YDOT = -1905
667108 feet/sec YDOT = -650
583239 meter/sec
ZDOT = -14446
772868 ZDOT = -4433
669238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17299757
46 X = 5272966
08
Y = 7617671
91 feet Y = 2321866
40 meter
Z = 11737289
33 Z = 3577525
79
XDOT = 1465
757977 XDOT = 446
763032
YDOT = 19218
377456 feet/sec YDOT = 5857
761449 meter/sec
ZDOT = -14580
385011 ZDOT = -4444
101351
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
53973971
00016717 00000-0 10270-3 0 9009
2 25544 51
6393 331
7738 0004820 339
7641 20
3320 15
54084338 23824
Satellite: ISS
Catalog Number: 25544
Epoch time: 17181
53973971 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 331
7738 deg
Eccentricity:
0004820
Arg of perigee: 339
7641 deg
Mean anomaly: 20
3320 deg
Mean motion: 15
54084338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 307
Coasting Arc #2 (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 = 4174579
46 A = 6787420
79 meter
Y = -4875827
70 meter E =
0009723
Z = -2191058
37 I = 51
44927
XDOT = 5045
715686 Wp = 16
68941
YDOT = 1871
694089 meter/sec RA = 326
35373 deg
ZDOT = 5463
522407 TA = 318
91241
MA = 318
98559
Ha = 221
395 n
mi
Hp = 215
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13696126
83 X = 4239435
03
Y = -15996810
04 feet Y = -4828781
92 meter
Z = -7188511
71 Z = -2170622
49
XDOT = 16554
185322 XDOT = 4997
871889
YDOT = 6140
728639 feet/sec YDOT = 1927
850756 meter/sec
ZDOT = 17924
942281 ZDOT = 5487
916789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17924794
49 X = -5463477
36
Y = -11112403
96 feet Y = -3387060
73 meter
Z = -7097375
80 Z = -2163280
14
XDOT = 2724
716966 XDOT = 830
493731
YDOT = -15879
934340 feet/sec YDOT = -4840
203987 meter/sec
ZDOT = 18032
264673 ZDOT = 5496
234272
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
50428815
00016717 00000-0 10270-3 0 9010
2 25544 51
6400 326
9665 0004851 344
0468 16
0532 15
54101136 23977
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
50428815 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 326
9665 deg
Eccentricity:
0004851
Arg of perigee: 344
0468 deg
Mean anomaly: 16
0532 deg
Mean motion: 15
54101136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2397
Checksum: 291
Coasting Arc #3 (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 = -3749399
77 A = 6778162
69 meter
Y = -2365207
54 meter E =
0014504
Z = -5139863
78 I = 51
40817
XDOT = 5357
930822 Wp = 57
79844
YDOT = -5267
501811 meter/sec RA = 324
53209 deg
ZDOT = -1480
026894 TA = 197
86019
MA = 197
91121
Ha = 221
497 n
mi
Hp = 214
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12301180
33 X = -3697705
86
Y = -7759867
25 feet Y = -2406846
41 meter
Z = -16863070
16 Z = -5157951
80
XDOT = 17578
513197 XDOT = 5423
624427
YDOT = -17281
830090 feet/sec YDOT = -5207
218357 meter/sec
ZDOT = -4855
731280 ZDOT = -1453
840669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13536414
55 X = 4125899
15
Y = -5061245
91 feet Y = -1542667
75 meter
Z = -16942460
97 Z = -5164062
10
XDOT = 2828
516211 XDOT = 862
131741
YDOT = 23478
392200 feet/sec YDOT = 7156
213943 meter/sec
ZDOT = -4739
142232 ZDOT = -1444
490552
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
89010600
00016717 00000-0 10270-3 0 9022
2 25544 51
6398 325
0476 0005156 346
5389 13
5625 15
54090427 24034
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
89010600 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 325
0476 deg
Eccentricity:
0005156
Arg of perigee: 346
5389 deg
Mean anomaly: 13
5625 deg
Mean motion: 15
54090427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 300
Coasting Arc #4 (Orbit 2414)
---------------------------------------
Vector Time (GMT): 2017/183/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 466307
46 A = 6780703
09 meter
Y = -5045194
40 meter E =
0008030
Z = -4512285
87 I = 51
39808
XDOT = 6632
066145 Wp = 78
93675
YDOT = -2196
433356 meter/sec RA = 320
59593 deg
ZDOT = 3147
487706 TA = 222
74100
MA = 222
80348
Ha = 221
406 n
mi
Hp = 214
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1529880
11 X = 544607
94
Y = -16552475
06 feet Y = -5039541
62 meter
Z = -14804087
49 Z = -4509830
97
XDOT = 21758
747194 XDOT = 6640
845399
YDOT = -7206
146181 feet/sec YDOT = -2122
220290 meter/sec
ZDOT = 10326
403236 ZDOT = 3179
725323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8594074
10 X = -2619473
79
Y = 14241342
86 feet Y = 4340761
30 meter
Z = -14792295
77 Z = -4508691
75
XDOT = -21641
327069 XDOT = -6596
276491
YDOT = -2206
962995 feet/sec YDOT = -672
682321 meter/sec
ZDOT = 10469
111875 ZDOT = 3190
985299
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
66174305
00016717 00000-0 10270-3 0 9032
2 25544 51
6414 321
1996 0004975 346
9590 13
1433 15
54132899 24159
Satellite: ISS
Catalog Number: 25544
Epoch time: 17183
66174305 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 321
1996 deg
Eccentricity:
0004975
Arg of perigee: 346
9590 deg
Mean anomaly: 13
1433 deg
Mean motion: 15
54132899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2415
Checksum: 315
Coasting Arc #5 (Orbit 2430)
---------------------------------------
Vector Time (GMT): 2017/184/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1846459
65 A = 6784532
69 meter
Y = 5584204
58 meter E =
0012670
Z = 3377007
99 I = 51
38684
XDOT = -6073
612110 Wp = 66
75352
YDOT = 792
505484 meter/sec RA = 315
59166 deg
ZDOT = -4612
659034 TA = 73
65973
MA = 73
52044
Ha = 221
592 n
mi
Hp = 214
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6057938
49 X = -1925170
31
Y = 18320881
16 feet Y = 5563115
77 meter
Z = 11079422
55 Z = 3367847
86
XDOT = -19926
548916 XDOT = -6059
616680
YDOT = 2600
083610 feet/sec YDOT = 724
664959 meter/sec
ZDOT = -15133
395782 ZDOT = -4642
128688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13179096
43 X = 4016988
59
Y = -14127356
89 feet Y = -4306018
38 meter
Z = 11037939
75 Z = 3364364
04
XDOT = 18088
257102 XDOT = 5513
300765
YDOT = 4900
256395 feet/sec YDOT = 1493
598149 meter/sec
ZDOT = -15263
615624 ZDOT = -4652
350042
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
69058890
00016717 00000-0 10270-3 0 9047
2 25544 51
6420 316
0706 0005179 350
7756 9
3300 15
54128601 24316
Satellite: ISS
Catalog Number: 25544
Epoch time: 17184
69058890 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 316
0706 deg
Eccentricity:
0005179
Arg of perigee: 350
7756 deg
Mean anomaly: 9
3300 deg
Mean motion: 15
54128601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2431
Checksum: 297
Coasting Arc #6 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2017/185/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2948302
02 A = 6787920
20 meter
Y = -5797984
04 meter E =
0011439
Z = -1920126
95 I = 51
37451
XDOT = 5194
369763 Wp = 19
50556
YDOT = 798
065735 meter/sec RA = 310
59636 deg
ZDOT = 5586
196795 TA = 319
24700
MA = 319
33251
Ha = 221
769 n
mi
Hp = 214
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9672906
90 X = 3022244
51
Y = -19022257
34 feet Y = -5764600
47 meter
Z = -6299629
09 Z = -1905626
09
XDOT = 17041
895548 XDOT = 5157
924531
YDOT = 2618
325901 feet/sec YDOT = 855
948278 meter/sec
ZDOT = 18327
417305 ZDOT = 5611
341004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16499692
71 X = -5029106
34
Y = 13564194
26 feet Y = 4134366
41 meter
Z = -6234541
17 Z = -1900288
15
XDOT = -13480
224207 XDOT = -4108
772338
YDOT = -7953
534907 feet/sec YDOT = -2424
237440 meter/sec
ZDOT = 18438
244731 ZDOT = 5619
976994
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
65512920
00016717 00000-0 10270-3 0 9054
2 25544 51
6413 311
2629 0005332 353
7983 6
3103 15
54085385 24460
Satellite: ISS
Catalog Number: 25544
Epoch time: 17185
65512920 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 311
2629 deg
Eccentricity:
0005332
Arg of perigee: 353
7983 deg
Mean anomaly: 6
3103 deg
Mean motion: 15
54085385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2446
Checksum: 298
Coasting Arc #7 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2017/186/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3798797
41 A = 6789315
87 meter
Y = 5619482
21 meter E =
0009675
Z = 229204
72 I = 51
35864
XDOT = -4084
619467 Wp = 109
07350
YDOT = -2508
943322 meter/sec RA = 305
60691 deg
ZDOT = -5981
046271 TA = 68
44839
MA = 68
34530
Ha = 221
807 n
mi
Hp = 214
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12463246
09 X = -3862466
97
Y = 18436621
41 feet Y = 5576645
45 meter
Z = 751984
00 Z = 210597
44
XDOT = -13400
982504 XDOT = -4027
207282
YDOT = -8231
441345 feet/sec YDOT = -2554
298534 meter/sec
ZDOT = -19622
855220 ZDOT = -6000
748935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18582866
95 X = 5664057
85
Y = -12248948
44 feet Y = -3733479
48 meter
Z = 668812
72 Z = 203854
12
XDOT = 8209
220132 XDOT = 2502
170296
YDOT = 11336
914481 feet/sec YDOT = 3455
491534 meter/sec
ZDOT = -19709
347818 ZDOT = -6007
409215
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
68397056
00016717 00000-0 10270-3 0 9060
2 25544 51
6408 306
1347 0005234 359
3669
7476 15
54125832 24629
Satellite: ISS
Catalog Number: 25544
Epoch time: 17186
68397056 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 306
1347 deg
Eccentricity:
0005234
Arg of perigee: 359
3669 deg
Mean anomaly:
7476 deg
Mean motion: 15
54125832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 323
Coasting Arc #8 (Orbit 2477)
---------------------------------------
Vector Time (GMT): 2017/187/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4319517
86 A = 6788495
29 meter
Y = -5017770
94 meter E =
0017333
Z = 1452277
87 I = 51
33778
XDOT = 2890
981421 Wp = 45
94064
YDOT = 4165
030334 meter/sec RA = 300
61595 deg
ZDOT = 5760
940869 TA = 329
98492
MA = 330
08417
Ha = 221
936 n
mi
Hp = 214
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14171646
54 X = 4368252
44
Y = -16462503
08 feet Y = -4969194
87 meter
Z = 4764691
16 Z = 1473378
36
XDOT = 9484
847183 XDOT = 2816
208373
YDOT = 13664
797685 feet/sec YDOT = 4196
940383 meter/sec
ZDOT = 18900
724637 ZDOT = 5774
803268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19199303
46 X = -5851947
70
Y = 10115887
00 feet Y = 3083322
36 meter
Z = 4858747
96 Z = 1480946
38
XDOT = -2947
800792 XDOT = -898
489681
YDOT = -14749
855779 feet/sec YDOT = -4495
756041 meter/sec
ZDOT = 18961
139057 ZDOT = 5779
355185
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 17187
71280880
00016717 00000-0 10270-3 0 9072
2 25544 51
6411 301
0058 0005401 3
4612 356
6577 15
54097648 24782
Satellite: ISS
Catalog Number: 25544
Epoch time: 17187
71280880 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 301
0058 deg
Eccentricity:
0005401
Arg of perigee: 3
4612 deg
Mean anomaly: 356
6577 deg
Mean motion: 15
54097648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2478
Checksum: 308
Coasting Arc #9 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2017/188/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4591086
39 A = 6785390
44 meter
Y = 3991802
76 meter E =
0006391
Z = -3014174
12 I = 51
31227
XDOT = -1668
282404 Wp = 51
69085
YDOT = -5630
135227 meter/sec RA = 295
61889 deg
ZDOT = -4918
395367 TA = 162
97208
MA = 162
95063
Ha = 222
053 n
mi
Hp = 214
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15062619
38 X = -4620741
28
Y = 13096465
76 feet Y = 3940296
74 meter
Z = -9889022
70 Z = -3036547
52
XDOT = -5473
367468 XDOT = -1581
309767
YDOT = -18471
572268 feet/sec YDOT = -5648
304109 meter/sec
ZDOT = -16136
467740 ZDOT = -4926
288863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18642455
90 X = 5682220
56
Y = -6991518
17 feet Y = -2131014
74 meter
Z = -9988503
37 Z = -3044495
83
XDOT = -1974
562889 XDOT = -601
846768
YDOT = 17821
785533 feet/sec YDOT = 5432
080231 meter/sec
ZDOT = -16170
277563 ZDOT = -4928
700601
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 17188
67734019
00016717 00000-0 10270-3 0 9087
2 25544 51
6413 296
1979 0005419 8
0094 352
1144 15
54132420 24930
Satellite: ISS
Catalog Number: 25544
Epoch time: 17188
67734019 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 296
1979 deg
Eccentricity:
0005419
Arg of perigee: 8
0094 deg
Mean anomaly: 352
1144 deg
Mean motion: 15
54132420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 311
Coasting Arc #10 (Orbit 2508)
---------------------------------------
Vector Time (GMT): 2017/189/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4604480
05 A = 6781559
58 meter
Y = -2602352
48 meter E =
0010832
Z = 4233768
57 I = 51
28553
XDOT = 524
125960 Wp = 76
80904
YDOT = 6765
949626 meter/sec RA = 290
61140 deg
ZDOT = 3583
460022 TA = 336
40786
MA = 336
45751
Ha = 221
960 n
mi
Hp = 214
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15106561
86 X = 4612672
66
Y = -8537901
85 feet Y = -2550816
84 meter
Z = 13890316
83 Z = 4256155
03
XDOT = 1719
573359 XDOT = 431
021855
YDOT = 22197
997459 feet/sec YDOT = 6771
289684 meter/sec
ZDOT = 11756
758604 ZDOT = 3585
780845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17008113
12 X = -5184072
88
Y = 3009999
41 feet Y = 917447
82 meter
Z = 13989598
72 Z = 4264029
69
XDOT = 6112
548032 XDOT = 1863
104640
YDOT = -20225
250236 feet/sec YDOT = -6164
656272 meter/sec
ZDOT = 11765
778468 ZDOT = 3586
209277
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 17189
70617152
00016717 00000-0 10270-3 0 9091
2 25544 51
6404 291
0699 0005402 11
3110 348
8164 15
54143503 25097
Satellite: ISS
Catalog Number: 25544
Epoch time: 17189
70617152 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 291
0699 deg
Eccentricity:
0005402
Arg of perigee: 11
3110 deg
Mean anomaly: 348
8164 deg
Mean motion: 15
54143503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2509
Checksum: 292
Coasting Arc #11 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2017/190/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3298937
97 A = 6787582
01 meter
Y = 5587360
69 meter E =
0005514
Z = -1996992
14 I = 51
29748
XDOT = -3451
565374 Wp = 91
00470
YDOT = -4012
952765 meter/sec RA = 286
28283 deg
ZDOT = -5539
365634 TA = 111
13870
MA = 111
07976
Ha = 222
080 n
mi
Hp = 213
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10823287
29 X = -3351471
83
Y = 18331235
85 feet Y = 5550176
26 meter
Z = -6551811
48 Z = -2013144
02
XDOT = -11324
033380 XDOT = -3379
527763
YDOT = -13165
855527 feet/sec YDOT = -4051
146989 meter/sec
ZDOT = -18173
771766 ZDOT = -5555
957634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21021295
10 X = 6407290
75
Y = 3214088
56 feet Y = 979654
19 meter
Z = -6624105
71 Z = -2019027
42
XDOT = -7839
207349 XDOT = -2389
390400
YDOT = 13755
974477 feet/sec YDOT = 4192
821021 meter/sec
ZDOT = -18246
291103 ZDOT = -5561
469528
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 17190
54209594
00016717 00000-0 10270-3 0 9104
2 25544 51
6416 286
9017 0005130 13
5219 346
6070 15
54133459 25225
Satellite: ISS
Catalog Number: 25544
Epoch time: 17190
54209594 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 286
9017 deg
Eccentricity:
0005130
Arg of perigee: 13
5219 deg
Mean anomaly: 346
6070 deg
Mean motion: 15
54133459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 293
Coasting Arc #12 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2017/191/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3713842
02 A = 6784132
32 meter
Y = -4499864
85 meter E =
0014639
Z = 3444767
85 I = 51
27852
XDOT = 2589
884171 Wp = 70
71041
YDOT = 5620
762459 meter/sec RA = 281
28012 deg
ZDOT = 4539
111588 TA = 329
95554
MA = 330
03945
Ha = 222
057 n
mi
Hp = 213
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12184521
07 X = 3747151
93
Y = -14763336
13 feet Y = -4458148
32 meter
Z = 11301731
79 Z = 3462888
65
XDOT = 8496
995312 XDOT = 2504
790384
YDOT = 18440
821716 feet/sec YDOT = 5649
247965 meter/sec
ZDOT = 14892
098385 ZDOT = 4551
486264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18297239
31 X = -5576998
54
Y = -5458681
13 feet Y = -1663806
01 meter
Z = 11382513
91 Z = 3469390
24
XDOT = 13360
596354 XDOT = 4072
309769
YDOT = -13543
987017 feet/sec YDOT = -4128
207243 meter/sec
ZDOT = 14945
731177 ZDOT = 4555
458863
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 17191
57092112
00016717 00000-0 10270-3 0 9115
2 25544 51
6422 281
7730 0005276 17
1889 342
9442 15
54158222 25385
Satellite: ISS
Catalog Number: 25544
Epoch time: 17191
57092112 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 281
7730 deg
Eccentricity:
0005276
Arg of perigee: 17
1889 deg
Mean anomaly: 342
9442 deg
Mean motion: 15
54158222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 304
Coasting Arc #13 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2017/192/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4012802
42 A = 6780442
36 meter
Y = 3036757
22 meter E =
0014075
Z = -4558360
61 I = 51
25902
XDOT = -1704
567208 Wp = 53
12947
YDOT = -6817
518243 meter/sec RA = 276
26754 deg
ZDOT = -3039
482509 TA = 186
26726
MA = 186
28488
Ha = 222
280 n
mi
Hp = 213
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13165362
26 X = -4024320
07
Y = 9963114
25 feet Y = 2991819
42 meter
Z = -14955251
35 Z = -4577880
91
XDOT = -5592
412100 XDOT = -1613
441156
YDOT = -22367
185836 feet/sec YDOT = -6836
070034 meter/sec
ZDOT = -9972
055476 ZDOT = -3047
542026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14379234
42 X = 4382790
65
Y = 7951563
73 feet Y = 2423636
63 meter
Z = -15041948
13 Z = -4584785
79
XDOT = -17670
895937 XDOT = -5386
089081
YDOT = 13015
221547 feet/sec YDOT = 3967
039528 meter/sec
ZDOT = -10006
449264 ZDOT = -3049
965736
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 17192
53544485
00016717 00000-0 10270-3 0 9128
2 25544 51
6407 276
9659 0005303 20
3315 339
8048 15
54128689 25533
Satellite: ISS
Catalog Number: 25544
Epoch time: 17192
53544485 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 276
9659 deg
Eccentricity:
0005303
Arg of perigee: 20
3315 deg
Mean anomaly: 339
8048 deg
Mean motion: 15
54128689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 325
Coasting Arc #14 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2017/193/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4178244
67 A = 6777726
34 meter
Y = -1306550
40 meter E =
0006069
Z = 5168992
41 I = 51
24782
XDOT = 827
917995 Wp = 64
97382
YDOT = 7527
905733 meter/sec RA = 271
24463 deg
ZDOT = 1234
960768 TA = 13
12420
MA = 13
10842
Ha = 222
125 n
mi
Hp = 213
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13708151
79 X = 4167436
29
Y = -4286582
67 feet Y = -1259887
32 meter
Z = 16958636
51 Z = 5189262
34
XDOT = 2716
266388 XDOT = 737
678699
YDOT = 24697
853456 feet/sec YDOT = 7536
659408 meter/sec
ZDOT = 4051
708556 ZDOT = 1238
763959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9579050
33 X = -2919694
54
Y = -10558381
21 feet Y = -3218194
59 meter
Z = 17048341
55 Z = 5196334
50
XDOT = 20539
432260 XDOT = 6260
418953
YDOT = -12074
397684 feet/sec YDOT = -3680
276414 meter/sec
ZDOT = 4067
211788 ZDOT = 1239
686153
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 17193
56426629
00016717 00000-0 10270-3 0 9132
2 25544 51
6407 271
8373 0005319 23
5336 336
6059 15
54170979 25698
Satellite: ISS
Catalog Number: 25544
Epoch time: 17193
56426629 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 271
8373 deg
Eccentricity:
0005319
Arg of perigee: 23
5336 deg
Mean anomaly: 336
6059 deg
Mean motion: 15
54170979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 334
Coasting Arc #15 (Orbit 2583)
---------------------------------------
Vector Time (GMT): 2017/194/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263582
31 A = 6777503
21 meter
Y = -511693
85 meter E =
0017388
Z = -5257972
52 I = 51
24624
XDOT = 58
796827 Wp = 78
31319
YDOT = -7624
010291 meter/sec RA = 266
21728 deg
ZDOT = 699
704496 TA = 198
38528
MA = 198
44820
Ha = 222
424 n
mi
Hp = 213
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13988130
95 X = -4232003
26
Y = -1678785
59 feet Y = -559195
17 meter
Z = -17250566
01 Z = -5278606
72
XDOT = 192
902976 XDOT = 140
647377
YDOT = -25013
157123 feet/sec YDOT = -7622
895181 meter/sec
ZDOT = 2295
618426 ZDOT = 700
188362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4505007
82 X = 1373126
38
Y = 13230378
25 feet Y = 4032619
29 meter
Z = -17341572
95 Z = -5285711
43
XDOT = -21649
268708 XDOT = -6598
697102
YDOT = 10361
886839 feet/sec YDOT = 3158
303108 meter/sec
ZDOT = 2299
035909 ZDOT = 700
746145
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 17194
52878585
00016717 00000-0 10270-3 0 9142
2 25544 51
6400 267
0292 0005494 26
7655 333
3780 15
54134169 25844
Satellite: ISS
Catalog Number: 25544
Epoch time: 17194
52878585 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 267
0292 deg
Eccentricity:
0005494
Arg of perigee: 26
7655 deg
Mean anomaly: 333
3780 deg
Mean motion: 15
54134169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2584
Checksum: 330
Coasting Arc #16 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2017/195/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227906
30 A = 6779398
53 meter
Y = 2306290
44 meter E =
0012468
Z = 4766819
47 I = 51
25641
XDOT = -984
024375 Wp = 47
83747
YDOT = 7158
061610 meter/sec RA = 261
19203 deg
ZDOT = -2577
871362 TA = 67
74930
MA = 67
61711
Ha = 222
333 n
mi
Hp = 213
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13871083
66 X = 4178647
93
Y = 7566569
69 feet Y = 2353294
05 meter
Z = 15639171
50 Z = 4787237
59
XDOT = -3228
426428 XDOT = -1051
472685
YDOT = 23484
454102 feet/sec YDOT = 7146
680610 meter/sec
ZDOT = -8457
583209 ZDOT = -2582
814782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 576017
53 X = 175570
14
Y = -15700717
62 feet Y = -4785578
73 meter
Z = 15728931
75 Z = 4794178
40
XDOT = 21261
170473 XDOT = 6480
404760
YDOT = -7756
921632 feet/sec YDOT = -2364
309714 meter/sec
ZDOT = -8480
591933 ZDOT = -2584
884421
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 17195
55760232
00016717 00000-0 10270-3 0 9156
2 25544 51
6402 261
9002 0005549 30
1066 330
0405 15
54187204 26009
Satellite: ISS
Catalog Number: 25544
Epoch time: 17195
55760232 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 261
9002 deg
Eccentricity:
0005549
Arg of perigee: 30
1066 deg
Mean anomaly: 330
0405 deg
Mean motion: 15
54187204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 269
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