[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 27th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19170 5245 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
306/03:16:48
099 0
7 1
4 1
4
N/A 1
3 -0
1 222
6
000/00:03:36
198 -0
0 0
0 213
4
307/05:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
4
310/13:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 232)
---------------------------------------
Vector Time (GMT): 2017/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2431869
70 A = 6787135
28 meter
Y = 5988368
84 meter E =
0019089
Z = 2041199
08 I = 52
02382
XDOT = -3919
974084 Wp = 67
59043
YDOT = -3508
032342 meter/sec RA = 97
82983 deg
ZDOT = 5587
036247 TA = 314
86983
MA = 315
02470
Ha = 222
588 n
mi
Hp = 212
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7978575
14 X = -2508567
82
Y = 19646879
39 feet Y = 5960745
22 meter
Z = 6696847
36 Z = 2029199
16
XDOT = -12860
807363 XDOT = -3907
594536
YDOT = -11509
292462 feet/sec YDOT = -3551
798810 meter/sec
ZDOT = 18330
171413 ZDOT = 5568
024058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4759259
28 X = -1450622
23
Y = -20681620
07 feet Y = -6303757
80 meter
Z = 6642690
58 Z = 2024692
09
XDOT = 15731
568006 XDOT = 4794
981928
YDOT = 2276
919792 feet/sec YDOT = 694
005153 meter/sec
ZDOT = 18246
311007 ZDOT = 5561
475595
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 17300
56030215
00016717 00000-0 10270-3 0 9000
2 25544 51
6376 98
4241 0005160 64
6969 295
4718 15
54287140 2331
Satellite: ISS
Catalog Number: 25544
Epoch time: 17300
56030215 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 98
4241 deg
Eccentricity:
0005160
Arg of perigee: 64
6969 deg
Mean anomaly: 295
4718 deg
Mean motion: 15
54287140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 233
Checksum: 295
Coasting Arc #2 (Orbit 247)
---------------------------------------
Vector Time (GMT): 2017/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3034818
17 A = 6783516
66 meter
Y = -4916390
80 meter E =
0010323
Z = -3565616
18 I = 52
01526
XDOT = 3256
260307 Wp = 76
02757
YDOT = 5270
136113 meter/sec RA = 92
87694 deg
ZDOT = -4503
603846 TA = 145
75658
MA = 145
68997
Ha = 222
597 n
mi
Hp = 212
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9956752
52 X = 3106889
30
Y = -16129891
07 feet Y = -4882050
54 meter
Z = -11698215
81 Z = -3550698
52
XDOT = 10683
268724 XDOT = 3218
962867
YDOT = 17290
472811 feet/sec YDOT = 5306
341137 meter/sec
ZDOT = -14775
603168 ZDOT = -4487
876472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1415897
00 X = 431565
40
Y = 18943802
55 feet Y = 5774071
02 meter
Z = -11631257
05 Z = -3545207
15
XDOT = -17522
942977 XDOT = -5340
993020
YDOT = -7702
785695 feet/sec YDOT = -2347
809080 meter/sec
ZDOT = -14706
591670 ZDOT = -4482
569141
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 17301
52473675
00016717 00000-0 10270-3 0 9019
2 25544 51
6375 93
6158 0005250 67
6626 292
5083 15
54296697 2483
Satellite: ISS
Catalog Number: 25544
Epoch time: 17301
52473675 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 93
6158 deg
Eccentricity:
0005250
Arg of perigee: 67
6626 deg
Mean anomaly: 292
5083 deg
Mean motion: 15
54296697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 248
Checksum: 326
Coasting Arc #3 (Orbit 263)
---------------------------------------
Vector Time (GMT): 2017/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514939
48 A = 6779636
28 meter
Y = 3439772
13 meter E =
0012398
Z = 4656923
16 I = 52
00360
XDOT = -2548
086883 Wp = 98
84752
YDOT = -6611
008793 meter/sec RA = 87
91227 deg
ZDOT = 2951
361697 TA = 321
90248
MA = 321
99008
Ha = 222
610 n
mi
Hp = 212
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11531953
69 X = -3575764
09
Y = 11285341
65 feet Y = 3400125
82 meter
Z = 15278619
28 Z = 4639700
50
XDOT = -8359
865101 XDOT = -2488
307926
YDOT = -21689
661393 feet/sec YDOT = -6639
168850 meter/sec
ZDOT = 9682
945201 ZDOT = 2939
129214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2457723
47 X = 749114
11
Y = -16020321
44 feet Y = -4882993
98 meter
Z = 15201644
50 Z = 4633461
24
XDOT = 18641
773135 XDOT = 5682
012452
YDOT = 12024
140834 feet/sec YDOT = 3664
958126 meter/sec
ZDOT = 9629
658768 ZDOT = 2935
119992
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 17302
55346046
00016717 00000-0 10270-3 0 9025
2 25544 51
6380 88
4857 0005029 71
5302 288
6397 15
54322785 2646
Satellite: ISS
Catalog Number: 25544
Epoch time: 17302
55346046 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 88
4857 deg
Eccentricity:
0005029
Arg of perigee: 71
5302 deg
Mean anomaly: 288
6397 deg
Mean motion: 15
54322785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 264
Checksum: 315
Coasting Arc #4 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2017/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3941118
75 A = 6777160
59 meter
Y = -1677720
78 meter E =
0019533
Z = -5268998
84 I = 51
99412
XDOT = 1739
698146 Wp = 79
89002
YDOT = 7379
705824 meter/sec RA = 82
93905 deg
ZDOT = -1048
501803 TA = 180
09804
MA = 180
09842
Ha = 222
585 n
mi
Hp = 212
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12930179
61 X = 3985181
19
Y = -5504333
27 feet Y = -1633402
47 meter
Z = -17286741
61 Z = -5249746
66
XDOT = 5707
671082 XDOT = 1662
140197
YDOT = 24211
633280 feet/sec YDOT = 7398
726597 meter/sec
ZDOT = -3439
966544 ZDOT = -1040
239599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6861183
70 X = -2091288
79
Y = 12384167
72 feet Y = 3774694
32 meter
Z = -17201023
61 Z = -5242871
99
XDOT = -18552
791174 XDOT = -5654
890750
YDOT = -15007
525899 feet/sec YDOT = -4574
293894 meter/sec
ZDOT = -3404
433205 ZDOT = -1037
671241
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 17303
51788438
00016717 00000-0 10270-3 0 9038
2 25544 51
6390 83
6773 0005254 74
3738 285
7994 15
54320226 2790
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
51788438 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 83
6773 deg
Eccentricity:
0005254
Arg of perigee: 74
3738 deg
Mean anomaly: 285
7994 deg
Mean motion: 15
54320226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 332
Coasting Arc #5 (Orbit 294)
---------------------------------------
Vector Time (GMT): 2017/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4252177
81 A = 6777184
70 meter
Y = -202136
16 meter E =
0008758
Z = 5266708
98 I = 51
98866
XDOT = -841
945632 Wp = 69
89067
YDOT = -7567
234313 meter/sec RA = 77
96045 deg
ZDOT = -965
961128 TA = 29
32580
MA = 29
27667
Ha = 222
835 n
mi
Hp = 212
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13950714
59 X = -4275185
02
Y = -663176
38 feet Y = -249815
17 meter
Z = 17279228
95 Z = 5245996
96
XDOT = -2762
288818 XDOT = -752
571963
YDOT = -24826
884229 feet/sec YDOT = -7576
149876 meter/sec
ZDOT = -3169
163806 ZDOT = -969
833483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11329694
61 X = 3453290
92
Y = -8358706
01 feet Y = -2547733
59 meter
Z = 17187322
29 Z = 5238695
83
XDOT = 17179
727716 XDOT = 5236
381008
YDOT = 16707
939751 feet/sec YDOT = 5092
580036 meter/sec
ZDOT = -3185
168226 ZDOT = -970
839275
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 17304
54659747
00016717 00000-0 10270-3 0 9043
2 25544 51
6387 78
5469 0005332 77
9751 282
1999 15
54290193 2955
Satellite: ISS
Catalog Number: 25544
Epoch time: 17304
54659747 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 78
5469 deg
Eccentricity:
0005332
Arg of perigee: 77
9751 deg
Mean anomaly: 282
1999 deg
Mean motion: 15
54290193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 295
Checksum: 352
Coasting Arc #6 (Orbit 309)
---------------------------------------
Vector Time (GMT): 2017/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4461897
21 A = 6779498
89 meter
Y = 2003468
60 meter E =
0015391
Z = -4708908
61 I = 51
98933
XDOT = -169
501433 Wp = 100
31398
YDOT = 7098
417387 meter/sec RA = 72
98647 deg
ZDOT = 2864
768495 TA = 198
01040
MA = 198
06499
Ha = 222
590 n
mi
Hp = 212
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14638770
38 X = 4462036
37
Y = 6573059
70 feet Y = 2053365
01 meter
Z = -15449175
24 Z = -4687233
41
XDOT = -556
107063 XDOT = -262
781199
YDOT = 23288
770956 feet/sec YDOT = 7096
000559 meter/sec
ZDOT = 9398
846768 ZDOT = 2863
717998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15508021
56 X = -4726844
97
Y = 4466963
75 feet Y = 1361530
55 meter
Z = -15353280
75 Z = -4679679
97
XDOT = -14202
522498 XDOT = -4328
928857
YDOT = -17082
170604 feet/sec YDOT = -5206
645600 meter/sec
ZDOT = 9393
058280 ZDOT = 2863
004164
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 17305
51100890
00016717 00000-0 10270-3 0 9052
2 25544 51
6392 73
7387 0005177 81
6200 278
5539 15
54324134 3105
Satellite: ISS
Catalog Number: 25544
Epoch time: 17305
51100890 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 73
7387 deg
Eccentricity:
0005177
Arg of perigee: 81
6200 deg
Mean anomaly: 278
5539 deg
Mean motion: 15
54324134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 310
Checksum: 291
Coasting Arc #7 (Orbit 319)
---------------------------------------
Vector Time (GMT): 2017/306/03:18:36
198
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3936889
43 A = 6777500
47 meter
Y = -1413035
17 meter E =
0018874
Z = -5349021
62 I = 51
97624
XDOT = 2617
308913 Wp = 87
04218
YDOT = 7193
055599 meter/sec RA = 69
84604 deg
ZDOT = 27
204853 TA = 183
21025
MA = 183
22238
Ha = 222
550 n
mi
Hp = 213
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12916303
91 X = 3978381
37
Y = -4635942
14 feet Y = -1368778
55 meter
Z = -17549283
52 Z = -5329796
06
XDOT = 8586
971498 XDOT = 2536
547566
YDOT = 23599
263775 feet/sec YDOT = 7221
872573 meter/sec
ZDOT = 89
254768 ZDOT = 39
722601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4723246
42 X = -1439645
51
Y = -13000370
79 feet Y = -3962513
02 meter
Z = -17463720
14 Z = -5322941
90
XDOT = 22594
126382 XDOT = 6886
689721
YDOT = -8397
248458 feet/sec YDOT = -2559
481330 meter/sec
ZDOT = 143
667114 ZDOT = 43
789736
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 17306
15394788
00016717 00000-0 10270-3 0 9065
2 25544 51
6415 70
5367 0004104 75
8331 284
3277 15
54080606 3201
Satellite: ISS
Catalog Number: 25544
Epoch time: 17306
15394788 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 70
5367 deg
Eccentricity:
0004104
Arg of perigee: 75
8331 deg
Mean anomaly: 284
3277 deg
Mean motion: 15
54080606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 320
Checksum: 300
Coasting Arc #8 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2017/307/03:18:36
198
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4499869
18 A = 6778618
77 meter
Y = -282004
23 meter E =
0009640
Z = 5055441
71 I = 51
96875
XDOT = -1722
256237 Wp = 64
73444
YDOT = -7224
728374 meter/sec RA = 64
87012 deg
ZDOT = -1929
129472 TA = 43
91623
MA = 43
83965
Ha = 222
631 n
mi
Hp = 213
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14763350
32 X = -4520938
88
Y = -925210
71 feet Y = -332442
38 meter
Z = 16586094
83 Z = 5033530
92
XDOT = -5650
446972 XDOT = -1631
968345
YDOT = -23703
177081 feet/sec YDOT = -7243
483091 meter/sec
ZDOT = -6329
164936 ZDOT = -1937
276228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -569684
56 X = -173639
85
Y = 14889699
13 feet Y = 4538380
30 meter
Z = 16488886
82 Z = 5025812
70
XDOT = -22477
755356 XDOT = -6851
219833
YDOT = 6212
776942 feet/sec YDOT = 1893
654412 meter/sec
ZDOT = -6364
151748 ZDOT = -1939
793453
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 17307
18281902
00016717 00000-0 10270-3 0 9073
2 25544 51
6421 65
4081 0004054 77
8390 282
3217 15
54119526 3368
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
18281902 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 65
4081 deg
Eccentricity:
0004054
Arg of perigee: 77
8390 deg
Mean anomaly: 282
3217 deg
Mean motion: 15
54119526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 295
Coasting Arc #9 (Orbit 336)
---------------------------------------
Vector Time (GMT): 2017/307/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4779268
61 A = 6782044
56 meter
Y = 2336323
45 meter E =
0011458
Z = -4217642
36 I = 51
97662
XDOT = -4
841355 Wp = 98
92437
YDOT = 6698
891277 meter/sec RA = 64
36359 deg
ZDOT = 3712
160595 TA = 209
01671
MA = 209
08045
Ha = 222
551 n
mi
Hp = 213
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15680015
14 X = 4773275
87
Y = 7665103
18 feet Y = 2389734
78 meter
Z = -13837409
31 Z = -4194440
13
XDOT = -15
883709 XDOT = -97
782189
YDOT = 21977
989753 feet/sec YDOT = 6698
317660 meter/sec
ZDOT = 12179
004577 ZDOT = 3711
910993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3501131
06 X = -1067144
75
Y = -17181031
09 feet Y = -5236778
28 meter
Z = -13734803
60 Z = -4186368
14
XDOT = 16257
405279 XDOT = 4955
257129
YDOT = -13029
135758 feet/sec YDOT = -3971
280579 meter/sec
ZDOT = 12176
806721 ZDOT = 3711
490689
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 17307
24712344
00016717 00000-0 10270-3 0 9080
2 25544 51
6403 65
0861 0004027 78
2948 281
8656 15
54082661 3375
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
24712344 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 65
0861 deg
Eccentricity:
0004027
Arg of perigee: 78
2948 deg
Mean anomaly: 281
8656 deg
Mean motion: 15
54082661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 337
Checksum: 309
Coasting Arc #10 (Orbit 352)
---------------------------------------
Vector Time (GMT): 2017/308/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4860648
23 A = 6785752
61 meter
Y = -3694219
72 meter E =
0017108
Z = 2945795
03 I = 51
97439
XDOT = 1231
386079 Wp = 93
80614
YDOT = -5655
300144 meter/sec RA = 59
40381 deg
ZDOT = -5036
287381 TA = 52
71256
MA = 52
55670
Ha = 222
533 n
mi
Hp = 213
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15947008
64 X = -4833286
92
Y = -12120143
45 feet Y = -3748421
75 meter
Z = 9664681
87 Z = 2922249
30
XDOT = 4039
980573 XDOT = 1318
998245
YDOT = -18554
134332 feet/sec YDOT = -5641
040208 meter/sec
ZDOT = -16523
252563 ZDOT = -5030
092542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 454441
30 X = 138513
71
Y = 20074758
31 feet Y = 6118786
33 meter
Z = 9560784
47 Z = 2914127
10
XDOT = -15651
564036 XDOT = -4770
596718
YDOT = 8248
036225 feet/sec YDOT = 2514
001441 meter/sec
ZDOT = -16494
821315 ZDOT = -5027
621537
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 17308
27598900
00016717 00000-0 10270-3 0 9095
2 25544 51
6404 59
9582 0004003 80
0034 280
1570 15
54120699 3538
Satellite: ISS
Catalog Number: 25544
Epoch time: 17308
27598900 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 59
9582 deg
Eccentricity:
0004003
Arg of perigee: 80
0034 deg
Mean anomaly: 280
1570 deg
Mean motion: 15
54120699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 297
Coasting Arc #11 (Orbit 367)
---------------------------------------
Vector Time (GMT): 2017/309/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4705235
97 A = 6788621
18 meter
Y = 4679785
42 meter E =
0011618
Z = -1415716
59 I = 51
96566
XDOT = -2530
791515 Wp = 51
90108
YDOT = 4294
557700 meter/sec RA = 54
45101 deg
ZDOT = 5824
152756 TA = 292
73865
MA = 292
86139
Ha = 222
522 n
mi
Hp = 213
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15437125
89 X = 4659432
73
Y = 15353626
72 feet Y = 4732146
48 meter
Z = -4644739
48 Z = -1392970
54
XDOT = -8303
121767 XDOT = -2606
918096
YDOT = 14089
756234 feet/sec YDOT = 4265
831016 meter/sec
ZDOT = 19108
112718 ZDOT = 5811
673652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2043596
15 X = 622888
11
Y = -21697532
81 feet Y = -6613408
00 meter
Z = -4544568
07 Z = -1385184
35
XDOT = 14656
102652 XDOT = 4467
180088
YDOT = -2582
426526 feet/sec YDOT = -787
123605 meter/sec
ZDOT = 19052
002653 ZDOT = 5807
050409
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 17309
24054663
00016717 00000-0 10270-3 0 9108
2 25544 51
6398 55
1500 0003914 85
7900 274
3699 15
54090385 3683
Satellite: ISS
Catalog Number: 25544
Epoch time: 17309
24054663 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 55
1500 deg
Eccentricity:
0003914
Arg of perigee: 85
7900 deg
Mean anomaly: 274
3699 deg
Mean motion: 15
54090385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 368
Checksum: 315
Coasting Arc #12 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2017/310/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4212418
21 A = 6789339
31 meter
Y = -5308885
23 meter E =
0014361
Z = -312249
85 I = 51
94859
XDOT = 3873
098452 Wp = 124
65186
YDOT = -2730
622614 meter/sec RA = 49
50245 deg
ZDOT = -6028
303598 TA = 58
69889
MA = 58
55835
Ha = 222
499 n
mi
Hp = 213
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13820269
72 X = -4151222
96
Y = -17417602
47 feet Y = -5355649
20 meter
Z = -1024441
77 Z = -332564
54
XDOT = 12707
015920 XDOT = 3932
628538
YDOT = -8958
735610 feet/sec YDOT = -2686
978002 meter/sec
ZDOT = -19777
898944 ZDOT = -6009
344203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4314254
17 X = -1314984
67
Y = 21807546
61 feet Y = 6646940
21 meter
Z = -1113702
73 Z = -339456
59
XDOT = -13552
628512 XDOT = -4130
841171
YDOT = -3655
401222 feet/sec YDOT = -1114
166293 meter/sec
ZDOT = -19693
282221 ZDOT = -6002
512421
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 17310
26939984
00016717 00000-0 10270-3 0 9111
2 25544 51
6400 50
0210 0004035 88
0165 272
1449 15
54107772 3849
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
26939984 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 50
0210 deg
Eccentricity:
0004035
Arg of perigee: 88
0165 deg
Mean anomaly: 272
1449 deg
Mean motion: 15
54107772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 284
Coasting Arc #13 (Orbit 388)
---------------------------------------
Vector Time (GMT): 2017/310/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5039447
74 A = 6780724
25 meter
Y = 255278
82 meter E =
0013644
Z = -4542823
09 I = 51
91417
XDOT = 2530
160077 Wp = 105
05166
YDOT = 6491
683470 meter/sec RA = 47
77507 deg
ZDOT = 3176
051960 TA = 196
72800
MA = 196
77305
Ha = 222
531 n
mi
Hp = 213
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16533621
18 X = 5058286
01
Y = 837528
94 feet Y = 311738
82 meter
Z = -14904275
24 Z = -4518296
58
XDOT = 8301
050121 XDOT = 2441
952162
YDOT = 21298
174114 feet/sec YDOT = 6519
484161 meter/sec
ZDOT = 10420
117979 ZDOT = 3188
128958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5358941
10 X = -1633405
25
Y = 15766282
63 feet Y = 4805562
95 meter
Z = -14795458
32 Z = -4509655
70
XDOT = -21589
629546 XDOT = -6580
519086
YDOT = 2475
501207 feet/sec YDOT = 754
532768 meter/sec
ZDOT = 10472
609404 ZDOT = 3192
051346
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 17310
59091538
00016717 00000-0 10270-3 0 9122
2 25544 51
6415 48
4186 0004163 93
6631 266
4998 15
54129652 3891
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
59091538 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 48
4186 deg
Eccentricity:
0004163
Arg of perigee: 93
6631 deg
Mean anomaly: 266
4998 deg
Mean motion: 15
54129652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 389
Checksum: 327
Coasting Arc #14 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2017/311/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5642936
64 A = 6784479
90 meter
Y = -1597515
96 meter E =
0016550
Z = 3396156
98 I = 51
90404
XDOT = -1112
096715 Wp = 91
67345
YDOT = -6000
651110 meter/sec RA = 42
80703 deg
ZDOT = -4651
423780 TA = 48
77513
MA = 48
63260
Ha = 222
541 n
mi
Hp = 213
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18513571
64 X = -5641150
62
Y = -5241194
10 feet Y = -1660609
27 meter
Z = 11142247
31 Z = 3368749
01
XDOT = -3648
611269 XDOT = -1022
318334
YDOT = -19687
175557 feet/sec YDOT = -6012
585184 meter/sec
ZDOT = -15260
576705 ZDOT = -4656
608278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9845711
04 X = 3000972
73
Y = -16612478
85 feet Y = -5063483
55 meter
Z = 11020873
20 Z = 3359162
15
XDOT = 18727
203513 XDOT = 5708
051631
YDOT = 918
561938 feet/sec YDOT = 279
977679 meter/sec
ZDOT = -15282
548466 ZDOT = -4658
120772
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 17311
61975898
00016717 00000-0 10270-3 0 9137
2 25544 51
6414 43
2903 0004040 95
7319 264
4298 15
54149837 4057
Satellite: ISS
Catalog Number: 25544
Epoch time: 17311
61975898 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 43
2903 deg
Eccentricity:
0004040
Arg of perigee: 95
7319 deg
Mean anomaly: 264
4298 deg
Mean motion: 15
54149837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 318
Coasting Arc #15 (Orbit 419)
---------------------------------------
Vector Time (GMT): 2017/312/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5926441
01 A = 6787843
60 meter
Y = 2680730
31 meter E =
0009733
Z = -1937011
60 I = 51
88960
XDOT = -515
736972 Wp = 59
94252
YDOT = 5183
625266 meter/sec RA = 37
84723 deg
ZDOT = 5621
773954 TA = 278
78929
MA = 278
89949
Ha = 222
531 n
mi
Hp = 213
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19443704
12 X = 5905433
12
Y = 8795046
96 feet Y = 2746886
43 meter
Z = -6355024
93 Z = -1908273
21
XDOT = -1692
050432 XDOT = -600
971622
YDOT = 17006
644575 feet/sec YDOT = 5177
381175 meter/sec
ZDOT = 18444
140268 ZDOT = 5619
061772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13224567
83 X = -4030848
27
Y = 16796440
98 feet Y = 5119555
21 meter
Z = -6227936
95 Z = -1898275
18
XDOT = -14847
411215 XDOT = -4525
490938
YDOT = -4887
983614 feet/sec YDOT = -1489
857405 meter/sec
ZDOT = 18431
196536 ZDOT = 5617
828704
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 17312
58429391
00016717 00000-0 10270-3 0 9147
2 25544 51
6407 38
4825 0004048 99
2566 260
9045 15
54111912 4200
Satellite: ISS
Catalog Number: 25544
Epoch time: 17312
58429391 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 38
4825 deg
Eccentricity:
0004048
Arg of perigee: 99
2566 deg
Mean anomaly: 260
9045 deg
Mean motion: 15
54111912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 301
Coasting Arc #16 (Orbit 435)
---------------------------------------
Vector Time (GMT): 2017/313/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5786206
49 A = 6789223
02 meter
Y = -3531777
71 meter E =
0016186
Z = 225015
21 I = 51
86898
XDOT = 2289
402312 Wp = 124
27803
YDOT = -4153
897202 meter/sec RA = 32
89207 deg
ZDOT = -6027
308326 TA = 53
30479
MA = 53
15617
Ha = 222
475 n
mi
Hp = 213
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18983617
11 X = -5747376
20
Y = -11587197
20 feet Y = -3596265
91 meter
Z = 738238
89 Z = 197001
46
XDOT = 7511
162441 XDOT = 2364
960257
YDOT = -13628
271661 feet/sec YDOT = -4127
872937 meter/sec
ZDOT = -19774
633614 ZDOT = -6016
003538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15544161
12 X = 4737860
31
Y = -15911859
53 feet Y = -4849934
79 meter
Z = 614520
57 Z = 187305
87
XDOT = 10412
952050 XDOT = 3173
867785
YDOT = 9364
960268 feet/sec YDOT = 2854
439890 meter/sec
ZDOT = -19723
727720 ZDOT = -6011
792209
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 17313
61312171
00016717 00000-0 10270-3 0 9150
2 25544 51
6414 33
3532 0004226 100
5067 259
6562 15
54160421 4362
Satellite: ISS
Catalog Number: 25544
Epoch time: 17313
61312171 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 33
3532 deg
Eccentricity:
0004226
Arg of perigee: 100
5067 deg
Mean anomaly: 259
6562 deg
Mean motion: 15
54160421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 266
Coasting Arc #17 (Orbit 451)
---------------------------------------
Vector Time (GMT): 2017/314/13:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 919890
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5223693
60 A = 6788413
42 meter
Y = 4070207
14 meter E =
0017378
Z = 1461596
01 I = 51
83704
XDOT = -4001
344487 Wp = 70
59118
YDOT = 3035
312865 meter/sec RA = 27
93650 deg
ZDOT = 5797
606976 TA = 305
31808
MA = 305
48044
Ha = 222
559 n
mi
Hp = 213
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17138102
37 X = 5170691
42
Y = 13353697
97 feet Y = 4128325
69 meter
Z = 4795262
50 Z = 1486842
68
XDOT = -13127
770627 XDOT = -4063
151044
YDOT = 9958
375541 feet/sec YDOT = 2990
221484 meter/sec
ZDOT = 19021
020261 ZDOT = 5778
019350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16607116
51 X = -5061849
11
Y = 13969943
18 feet Y = 4258038
68 meter
Z = 4906598
97 Z = 1495531
37
XDOT = -5980
943859 XDOT = -1822
991688
YDOT = -13816
714169 feet/sec YDOT = -4211
334479 meter/sec
ZDOT = 18933
548173 ZDOT = 5770
945483
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 17314
64194350
00016717 00000-0 10270-3 0 9162
2 25544 51
6405 28
2249 0004300 102
5468 257
6166 15
54119048 4525
Satellite: ISS
Catalog Number: 25544
Epoch time: 17314
64194350 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 28
2249 deg
Eccentricity:
0004300
Arg of perigee: 102
5468 deg
Mean anomaly: 257
6166 deg
Mean motion: 15
54119048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 452
Checksum: 291
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