[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 14th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 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
317/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
318/09:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
323/23:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
5
328/13:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2017/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6519395
94 A = 6787844
77 meter
Y = -44541
16 meter E =
0018010
Z = 1858962
84 I = 51
74802
XDOT = -1585
709094 Wp = 113
18697
YDOT = -4950
555002 meter/sec RA = 13
38254 deg
ZDOT = -5643
275300 TA = 46
37601
MA = 46
22676
Ha = 222
417 n
mi
Hp = 213
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21389094
28 X = -6527443
41
Y = -146132
40 feet Y = -117490
44 meter
Z = 6098959
44 Z = 1827273
55
XDOT = -5202
457658 XDOT = -1502
820079
YDOT = -16241
978352 feet/sec YDOT = -4967
824188 meter/sec
ZDOT = -18514
682744 ZDOT = -5650
776842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13329350
28 X = 4062785
97
Y = -16779111
20 feet Y = -5114273
09 meter
Z = 5958344
02 Z = 1816103
26
XDOT = 14696
748595 XDOT = 4479
568972
YDOT = 5045
506437 feet/sec YDOT = 1537
870362 meter/sec
ZDOT = -18547
092678 ZDOT = -5653
153848
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 17317
53577000
00016717 00000-0 10270-3 0 9003
2 25544 51
6417 13
8016 0004058 112
0845 248
0739 15
54159665 4973
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
53577000 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 13
8016 deg
Eccentricity:
0004058
Arg of perigee: 112
0845 deg
Mean anomaly: 248
0739 deg
Mean motion: 15
54159665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 300
Coasting Arc #2 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2017/317/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4968192
23 A = 6782482
43 meter
Y = -2257050
40 meter E =
0011029
Z = -4039645
97 I = 51
71738
XDOT = 5082
147616 Wp = 108
36460
YDOT = 4175
055918 meter/sec RA = 11
31988 deg
ZDOT = 3923
017522 TA = 202
34831
MA = 202
39640
Ha = 222
426 n
mi
Hp = 213
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16299843
28 X = 5012684
91
Y = -7405021
01 feet Y = -2201244
03 meter
Z = -13253431
67 Z = -4015403
46
XDOT = 16673
712651 XDOT = 5016
026859
YDOT = 13697
690020 feet/sec YDOT = 4231
518378 meter/sec
ZDOT = 12870
792395 ZDOT = 3947
544750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12653499
69 X = 3856786
70
Y = -12777268
86 feet Y = -3894511
55 meter
Z = -13145456
40 Z = -4006735
11
XDOT = 19459
389270 XDOT = 5931
221850
YDOT = 5936
394897 feet/sec YDOT = 1809
413165 meter/sec
ZDOT = 12978
888206 ZDOT = 3955
965125
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 17317
92158266
00016717 00000-0 10270-3 0 9016
2 25544 51
6423 11
8800 0004088 110
8912 249
2679 15
54146336 5038
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
92158266 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 11
8800 deg
Eccentricity:
0004088
Arg of perigee: 110
8912 deg
Mean anomaly: 249
2679 deg
Mean motion: 15
54146336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 298
Coasting Arc #3 (Orbit 510)
---------------------------------------
Vector Time (GMT): 2017/318/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5290359
12 A = 6785729
56 meter
Y = -3127528
36 meter E =
0008736
Z = -2878331
50 I = 51
71178
XDOT = 4703
796144 Wp = 116
95224
YDOT = -3310
473688 meter/sec RA = 8
89188 deg
ZDOT = -5064
175806 TA = 95
75649
MA = 95
65689
Ha = 222
367 n
mi
Hp = 213
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17356821
25 X = -5241011
26
Y = -10260919
80 feet Y = -3186412
93 meter
Z = -9443344
81 Z = -2903910
99
XDOT = 15432
402047 XDOT = 4765
064927
YDOT = -10861
134146 feet/sec YDOT = -3257
530196 meter/sec
ZDOT = -16614
750019 ZDOT = -5041
176853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19781810
62 X = 6029495
88
Y = 3616594
42 feet Y = 1102337
98 meter
Z = -9556290
80 Z = -2912757
44
XDOT = -10537
528637 XDOT = -3211
838729
YDOT = 14141
336286 feet/sec YDOT = 4310
279300 meter/sec
ZDOT = -16512
108867 ZDOT = -5032
890783
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 17318
43599574
00016717 00000-0 10270-3 0 9025
2 25544 51
6417 9
3135 0004158 120
3942 239
7622 15
54128347 5114
Satellite: ISS
Catalog Number: 25544
Epoch time: 17318
43599574 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 9
3135 deg
Eccentricity:
0004158
Arg of perigee: 120
3942 deg
Mean anomaly: 239
7622 deg
Mean motion: 15
54128347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 511
Checksum: 303
Coasting Arc #4 (Orbit 526)
---------------------------------------
Vector Time (GMT): 2017/319/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4023440
24 A = 6781865
25 meter
Y = 3553375
43 meter E =
0014227
Z = 4136458
46 I = 51
66730
XDOT = -6165
498072 Wp = 109
39997
YDOT = 2569
690010 meter/sec RA = 3
91182 deg
ZDOT = 3774
374803 TA = 301
69014
MA = 301
82879
Ha = 222
216 n
mi
Hp = 213
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13200263
26 X = 3963313
06
Y = 11658055
89 feet Y = 3598032
19 meter
Z = 13571057
94 Z = 4155857
42
XDOT = -20228
012046 XDOT = -6212
109285
YDOT = 8430
741503 feet/sec YDOT = 2500
482659 meter/sec
ZDOT = 12383
119434 ZDOT = 3744
310762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16451314
57 X = -5014360
68
Y = -6097969
70 feet Y = -1858661
16 meter
Z = 13656494
62 Z = 4162499
56
XDOT = 15412
004566 XDOT = 4697
578992
YDOT = -14035
598330 feet/sec YDOT = -4278
050371 meter/sec
ZDOT = 12249
269621 ZDOT = 3733
577381
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 17319
46481854
00016717 00000-0 10270-3 0 9031
2 25544 51
6423 4
1848 0004068 123
7692 236
3849 15
54166129 5275
Satellite: ISS
Catalog Number: 25544
Epoch time: 17319
46481854 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 4
1848 deg
Eccentricity:
0004068
Arg of perigee: 123
7692 deg
Mean anomaly: 236
3849 deg
Mean motion: 15
54166129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 527
Checksum: 320
Coasting Arc #5 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2017/320/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2405441
12 A = 6778696
63 meter
Y = -3913834
09 meter E =
0015634
Z = -4998460
39 I = 51
62284
XDOT = 7157
922892 Wp = 86
02718
YDOT = -1769
527368 meter/sec RA = 358
91974 deg
ZDOT = -2063
617517 TA = 163
88933
MA = 163
83956
Ha = 222
308 n
mi
Hp = 213
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7891867
20 X = -2337216
12
Y = -12840663
03 feet Y = -3940351
95 meter
Z = -16399148
25 Z = -5009979
83
XDOT = 23483
998988 XDOT = 7187
202521
YDOT = -5805
535984 feet/sec YDOT = -1689
318887 meter/sec
ZDOT = -6770
398677 ZDOT = -2028
774531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12073797
76 X = 3680093
56
Y = 8929269
34 feet Y = 2721641
29 meter
Z = -16449553
64 Z = -5013823
95
XDOT = -18915
619622 XDOT = -5765
480861
YDOT = 13417
052069 feet/sec YDOT = 4089
517471 meter/sec
ZDOT = -6615
498391 ZDOT = -2016
403910
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 17320
42933787
00016717 00000-0 10270-3 0 9047
2 25544 51
6415 359
3772 0004022 125
6302 234
5225 15
54129903 5420
Satellite: ISS
Catalog Number: 25544
Epoch time: 17320
42933787 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 359
3772 deg
Eccentricity:
0004022
Arg of perigee: 125
6302 deg
Mean anomaly: 234
5225 deg
Mean motion: 15
54129903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 542
Checksum: 291
Coasting Arc #6 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2017/321/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 623136
49 A = 6777196
09 meter
Y = 4164644
96 meter E =
0006172
Z = 5305408
52 I = 51
58536
XDOT = -7614
373369 Wp = 115
60868
YDOT = 936
167657 meter/sec RA = 353
91892 deg
ZDOT = 156
702815 TA = 332
88170
MA = 332
91393
Ha = 222
180 n
mi
Hp = 213
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2044411
04 X = 550748
24
Y = 13663533
33 feet Y = 4171208
49 meter
Z = 17406195
93 Z = 5308259
82
XDOT = -24981
539924 XDOT = -7625
037131
YDOT = 3071
416199 feet/sec YDOT = 850
958906 meter/sec
ZDOT = 514
116847 ZDOT = 119
687675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7173469
03 X = -2186473
36
Y = -11789770
25 feet Y = -3593521
97 meter
Z = 17418096
21 Z = 5309035
73
XDOT = 20876
807612 XDOT = 6363
250960
YDOT = -12172
419030 feet/sec YDOT = -3710
153320 meter/sec
ZDOT = 349
739100 ZDOT = 106
600478
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 17321
45815280
00016717 00000-0 10270-3 0 9059
2 25544 51
6414 354
2490 0004005 128
7418 231
4094 15
54180067 5588
Satellite: ISS
Catalog Number: 25544
Epoch time: 17321
45815280 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 354
2490 deg
Eccentricity:
0004005
Arg of perigee: 128
7418 deg
Mean anomaly: 231
4094 deg
Mean motion: 15
54180067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 558
Checksum: 291
Coasting Arc #7 (Orbit 572)
---------------------------------------
Vector Time (GMT): 2017/322/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1195802
94 A = 6778389
78 meter
Y = -4343593
63 meter E =
0016823
Z = -5079806
03 I = 51
55555
XDOT = 7447
252308 Wp = 109
34047
YDOT = -24
523177 meter/sec RA = 348
91447 deg
ZDOT = 1773
434838 TA = 177
86711
MA = 177
85992
Ha = 222
233 n
mi
Hp = 213
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3923237
98 X = 1268961
14
Y = -14250635
25 feet Y = -4329812
14 meter
Z = -16666030
29 Z = -5073819
47
XDOT = 24433
242481 XDOT = 7438
358329
YDOT = -80
456619 feet/sec YDOT = 58
707304 meter/sec
ZDOT = 5818
355768 ZDOT = 1809
590636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2180556
86 X = 664633
73
Y = 14650191
72 feet Y = 4465378
44 meter
Z = -16638690
49 Z = -5071472
86
XDOT = -21138
220847 XDOT = -6442
929714
YDOT = 9938
895925 feet/sec YDOT = 3029
375478 meter/sec
ZDOT = 5978
748692 ZDOT = 1822
322601
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 17322
42266542
00016717 00000-0 10270-3 0 9069
2 25544 51
6404 349
4407 0004010 130
4436 229
7066 15
54152749 5739
Satellite: ISS
Catalog Number: 25544
Epoch time: 17322
42266542 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 349
4407 deg
Eccentricity:
0004010
Arg of perigee: 130
4436 deg
Mean anomaly: 229
7066 deg
Mean motion: 15
54152749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 573
Checksum: 292
Coasting Arc #8 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2017/323/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2881515
12 A = 6781360
93 meter
Y = 4379213
97 meter E =
0012307
Z = 4291417
80 I = 51
53468
XDOT = -6745
390478 Wp = 88
61256
YDOT = -972
036592 meter/sec RA = 343
91350 deg
ZDOT = -3528
291645 TA = 37
38778
MA = 37
30221
Ha = 222
149 n
mi
Hp = 213
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9453789
78 X = -2951116
63
Y = 14367499
90 feet Y = 4346601
54 meter
Z = 14079454
74 Z = 4277251
09
XDOT = -22130
546188 XDOT = -6716
880430
YDOT = -3189
096432 feet/sec YDOT = -1047
308584 meter/sec
ZDOT = -11575
759989 ZDOT = -3560
990282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2504651
97 X = 763417
92
Y = -17067913
67 feet Y = -5202300
09 meter
Z = 14015822
55 Z = 4272022
71
XDOT = 20063
007083 XDOT = 6115
204559
YDOT = -6705
050940 feet/sec YDOT = -2043
699527 meter/sec
ZDOT = -11720
630763 ZDOT = -3572
448256
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 17323
45147173
00016717 00000-0 10270-3 0 9072
2 25544 51
6411 344
3115 0003899 133
5986 226
5491 15
54201967 5896
Satellite: ISS
Catalog Number: 25544
Epoch time: 17323
45147173 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 344
3115 deg
Eccentricity:
0003899
Arg of perigee: 133
5986 deg
Mean anomaly: 226
5491 deg
Mean motion: 15
54201967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 322
Coasting Arc #9 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2017/323/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6508948
80 A = 6789115
27 meter
Y = 1848423
67 meter E =
0014783
Z = -467439
84 I = 51
54017
XDOT = -916
843246 Wp = 136
62559
YDOT = -4710
484172 meter/sec RA = 341
00088 deg
ZDOT = -5983
135323 TA = 48
42379
MA = 48
29716
Ha = 222
075 n
mi
Hp = 213
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21354818
91 X = -6526863
96
Y = 6064382
13 feet Y = 1775536
02 meter
Z = -1533595
27 Z = -499102
47
XDOT = -3008
015900 XDOT = -835
037381
YDOT = -15454
344395 feet/sec YDOT = -4720
279211 meter/sec
ZDOT = -19629
709066 ZDOT = -5987
390726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6184287
56 X = -1884970
85
Y = 21309809
58 feet Y = 6495229
96 meter
Z = -1674377
07 Z = -510350
13
XDOT = -13074
734049 XDOT = -3985
178938
YDOT = -5309
151942 feet/sec YDOT = -1618
229512 meter/sec
ZDOT = -19647
734318 ZDOT = -5988
629420
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 17324
03017497
00016717 00000-0 10270-3 0 9083
2 25544 51
6393 341
4267 0003788 132
9485 227
1986 15
54164205 5984
Satellite: ISS
Catalog Number: 25544
Epoch time: 17324
03017497 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 341
4267 deg
Eccentricity:
0003788
Arg of perigee: 132
9485 deg
Mean anomaly: 227
1986 deg
Mean motion: 15
54164205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 598
Checksum: 331
Coasting Arc #10 (Orbit 613)
---------------------------------------
Vector Time (GMT): 2017/324/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6366086
46 A = 6787149
95 meter
Y = -986790
46 meter E =
0015705
Z = 2119347
01 I = 51
50219
XDOT = -1028
981660 Wp = 83
31820
YDOT = 5245
406257 meter/sec RA = 336
02000 deg
ZDOT = 5499
887213 TA = 300
21633
MA = 300
37176
Ha = 221
979 n
mi
Hp = 213
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20886110
45 X = 6366352
91
Y = -3237501
51 feet Y = -915599
18 meter
Z = 6953238
23 Z = 2150272
73
XDOT = -3375
924081 XDOT = -1114
277037
YDOT = 17209
338113 feet/sec YDOT = 5233
422215 meter/sec
ZDOT = 18044
249387 ZDOT = 5494
681794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7978662
46 X = 2431896
32
Y = -19522371
81 feet Y = -5950418
93 meter
Z = 7090591
79 Z = 2161212
38
XDOT = 11517
190378 XDOT = 3510
439627
YDOT = 11290
891041 feet/sec YDOT = 3441
463589 meter/sec
ZDOT = 18020
214050 ZDOT = 5492
561242
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 17325
05897614
00016717 00000-0 10270-3 0 9094
2 25544 51
6382 336
2971 0003857 139
6481 220
4959 15
54198352 6148
Satellite: ISS
Catalog Number: 25544
Epoch time: 17325
05897614 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 336
2971 deg
Eccentricity:
0003857
Arg of perigee: 139
6481 deg
Mean anomaly: 220
4959 deg
Mean motion: 15
54198352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 614
Checksum: 336
Coasting Arc #11 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2017/325/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5758431
98 A = 6783566
81 meter
Y = -80214
29 meter E =
0008116
Z = -3589653
31 I = 51
46066
XDOT = 2825
428568 Wp = 104
74452
YDOT = -5586
877165 meter/sec RA = 331
02905 deg
ZDOT = -4418
040409 TA = 117
80871
MA = 117
72642
Ha = 221
948 n
mi
Hp = 213
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18892493
38 X = -5739669
93
Y = -263170
25 feet Y = -144503
86 meter
Z = -11777077
79 Z = -3617580
93
XDOT = 9269
778767 XDOT = 2909
153592
YDOT = -18329
649490 feet/sec YDOT = -5554
812855 meter/sec
ZDOT = -14494
883233 ZDOT = -4404
112128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9656617
57 X = -2943337
03
Y = 16149691
55 feet Y = 4922425
98 meter
Z = -11900938
03 Z = -3627405
91
XDOT = -9993
038238 XDOT = -3045
878055
YDOT = -16585
612097 feet/sec YDOT = -5055
294567 meter/sec
ZDOT = -14432
099590 ZDOT = -4398
903955
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 17326
02347632
00016717 00000-0 10270-3 0 9104
2 25544 51
6381 331
4878 0003820 140
1557 219
9877 15
54191950 6296
Satellite: ISS
Catalog Number: 25544
Epoch time: 17326
02347632 = yrday
fracday
Element set: 910
Inclination: 51
6381 deg
RA of node: 331
4878 deg
Eccentricity:
0003820
Arg of perigee: 140
1557 deg
Mean anomaly: 219
9877 deg
Mean motion: 15
54191950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 314
Coasting Arc #12 (Orbit 644)
---------------------------------------
Vector Time (GMT): 2017/326/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4779913
63 A = 6779935
62 meter
Y = 1242284
66 meter E =
0011578
Z = 4639915
77 I = 51
42015
XDOT = -4287
967038 Wp = 124
48013
YDOT = 5667
774422 meter/sec RA = 326
02575 deg
ZDOT = 2888
277762 TA = 296
67010
MA = 296
78861
Ha = 221
861 n
mi
Hp = 213
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15682131
34 X = 4743128
04
Y = 4075737
07 feet Y = 1295530
92 meter
Z = 15222820
76 Z = 4663046
20
XDOT = -14068
133326 XDOT = -4365
056965
YDOT = 18595
060440 feet/sec YDOT = 5619
392213 meter/sec
ZDOT = 9475
976911 ZDOT = 2867
260975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11137730
94 X = 3394780
39
Y = -11634626
83 feet Y = -3546234
26 meter
Z = 15325193
50 Z = 4671118
98
XDOT = 8533
020159 XDOT = 2600
864545
YDOT = 20576
007866 feet/sec YDOT = 6271
567198 meter/sec
ZDOT = 9381
744574 ZDOT = 2859
555746
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 17327
05227196
00016717 00000-0 10270-3 0 9111
2 25544 51
6381 326
3581 0003800 144
2496 215
8912 15
54172860 6457
Satellite: ISS
Catalog Number: 25544
Epoch time: 17327
05227196 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 326
3581 deg
Eccentricity:
0003800
Arg of perigee: 144
2496 deg
Mean anomaly: 215
8912 deg
Mean motion: 15
54172860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 645
Checksum: 302
Coasting Arc #13 (Orbit 659)
---------------------------------------
Vector Time (GMT): 2017/327/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3530925
79 A = 6777498
20 meter
Y = -2511598
21 meter E =
0016548
Z = -5225522
83 I = 51
38501
XDOT = 5345
840784 Wp = 94
79011
YDOT = -5384
084691 meter/sec RA = 321
01200 deg
ZDOT = -1028
590008 TA = 165
33384
MA = 165
28577
Ha = 221
991 n
mi
Hp = 213
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11584402
19 X = -3477194
65
Y = -8240151
62 feet Y = -2550782
68 meter
Z = -17144103
77 Z = -5242544
84
XDOT = 17538
847717 XDOT = 5410
646194
YDOT = -17664
319852 feet/sec YDOT = -5323
941434 meter/sec
ZDOT = -3374
639135 ZDOT = -1002
464177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12673512
92 X = -3862886
74
Y = 6237101
15 feet Y = 1901068
43 meter
Z = -17219158
13 Z = -5248399
40
XDOT = -6855
747509 XDOT = -2089
631841
YDOT = -22886
963001 feet/sec YDOT = -6975
946323 meter/sec
ZDOT = -3257
805621 ZDOT = -992
979153
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 17328
01676482
00016717 00000-0 10270-3 0 9125
2 25544 51
6376 321
5496 0004074 146
6383 213
5027 15
54192349 6601
Satellite: ISS
Catalog Number: 25544
Epoch time: 17328
01676482 = yrday
fracday
Element set: 912
Inclination: 51
6376 deg
RA of node: 321
5496 deg
Eccentricity:
0004074
Arg of perigee: 146
6383 deg
Mean anomaly: 213
5027 deg
Mean motion: 15
54192349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 310
Coasting Arc #14 (Orbit 668)
---------------------------------------
Vector Time (GMT): 2017/328/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5422173
60 A = 6782072
37 meter
Y = 514369
34 meter E =
0009033
Z = -4048512
55 I = 51
38706
XDOT = 2294
522002 Wp = 95
01569
YDOT = -6201
786168 meter/sec RA = 318
16370 deg
ZDOT = -3869
243009 TA = 134
75585
MA = 134
68231
Ha = 221
853 n
mi
Hp = 213
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17789283
47 X = -5407856
52
Y = 1687563
46 feet Y = 453815
18 meter
Z = -13282521
50 Z = -4074817
29
XDOT = 7527
959323 XDOT = 2382
496599
YDOT = -20347
067479 feet/sec YDOT = -6175
635136 meter/sec
ZDOT = -12694
366826 ZDOT = -3857
883483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1327291
41 X = -404558
42
Y = -17732155
94 feet Y = -5404761
13 meter
Z = -13399283
47 Z = -4084101
60
XDOT = 18896
646839 XDOT = 5759
697957
YDOT = 8118
869901 feet/sec YDOT = 2474
631546 meter/sec
ZDOT = -12642
889076 ZDOT = -3853
552590
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 17328
59545942
00016717 00000-0 10270-3 0 9135
2 25544 51
6387 318
6670 0003800 147
3141 212
8247 15
54193993 6691
Satellite: ISS
Catalog Number: 25544
Epoch time: 17328
59545942 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 318
6670 deg
Eccentricity:
0003800
Arg of perigee: 147
3141 deg
Mean anomaly: 212
8247 deg
Mean motion: 15
54193993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 669
Checksum: 330
Coasting Arc #15 (Orbit 684)
---------------------------------------
Vector Time (GMT): 2017/329/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4573913
92 A = 6778611
65 meter
Y = 875629
73 meter E =
0009695
Z = 4921866
52 I = 51
35309
XDOT = -3600
305585 Wp = 133
67653
YDOT = 6408
120372 meter/sec RA = 313
15339 deg
ZDOT = 2196
444141 TA = 294
76718
MA = 294
86803
Ha = 221
595 n
mi
Hp = 213
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15006279
26 X = 4539874
19
Y = 2872800
97 feet Y = 926587
81 meter
Z = 16147856
04 Z = 4944002
77
XDOT = -11812
026197 XDOT = -3682
364678
YDOT = 21024
016968 feet/sec YDOT = 6367
400374 meter/sec
ZDOT = 7206
181566 ZDOT = 2178
755774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2919877
20 X = -889978
57
Y = 14890944
89 feet Y = 4538760
00 meter
Z = 16245883
63 Z = 4951745
33
XDOT = -19902
279323 XDOT = -6066
214738
YDOT = -11710
650184 feet/sec YDOT = -3569
406176 meter/sec
ZDOT = 7126
609587 ZDOT = 2172
190602
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 17329
62424470
00016717 00000-0 10270-3 0 9143
2 25544 51
6396 313
5389 0003705 154
1038 206
0300 15
54232903 6855
Satellite: ISS
Catalog Number: 25544
Epoch time: 17329
62424470 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 313
5389 deg
Eccentricity:
0003705
Arg of perigee: 154
1038 deg
Mean anomaly: 206
0300 deg
Mean motion: 15
54232903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 685
Checksum: 292
Coasting Arc #16 (Orbit 699)
---------------------------------------
Vector Time (GMT): 2017/330/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3519481
84 A = 6777175
25 meter
Y = -2379551
23 meter E =
0016648
Z = -5294408
78 I = 51
32583
XDOT = 4554
608805 Wp = 99
49322
YDOT = -6148
814150 meter/sec RA = 308
13215 deg
ZDOT = -267
550425 TA = 167
96136
MA = 167
92152
Ha = 221
747 n
mi
Hp = 213
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11546856
42 X = -3466893
57
Y = -7806926
62 feet Y = -2418614
27 meter
Z = -17370107
56 Z = -5311377
86
XDOT = 14942
942273 XDOT = 4624
327626
YDOT = -20173
274771 feet/sec YDOT = -6097
491572 meter/sec
ZDOT = -877
790109 ZDOT = -245
256174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7646042
33 X = 2330513
70
Y = -11541669
25 feet Y = -3517900
79 meter
Z = -17444957
45 Z = -5317223
03
XDOT = 19540
974802 XDOT = 5956
089120
YDOT = 14104
206780 feet/sec YDOT = 4298
962227 meter/sec
ZDOT = -777
849107 ZDOT = -237
088408
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 17330
58872903
00016717 00000-0 10270-3 0 9159
2 25544 51
6393 308
7296 0003660 154
7238 205
4094 15
54197893 7002
Satellite: ISS
Catalog Number: 25544
Epoch time: 17330
58872903 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 308
7296 deg
Eccentricity:
0003660
Arg of perigee: 154
7238 deg
Mean anomaly: 205
4094 deg
Mean motion: 15
54197893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 700
Checksum: 325
Coasting Arc #17 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2017/331/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2364740
46 A = 6778095
82 meter
Y = 3814107
74 meter E =
0005648
Z = 5074692
44 I = 51
30939
XDOT = -5150
810613 Wp = 93
88013
YDOT = 5432
609321 meter/sec RA = 303
11058 deg
ZDOT = -1681
660420 TA = 12
43461
MA = 12
42068
Ha = 221
594 n
mi
Hp = 213
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7758334
83 X = 2297263
66
Y = 12513476
84 feet Y = 3840174
49 meter
Z = 16649253
40 Z = 5086015
94
XDOT = -16898
984951 XDOT = -5203
007905
YDOT = 17823
521394 feet/sec YDOT = 5374
717618 meter/sec
ZDOT = -5517
258595 ZDOT = -1706
808434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12269103
30 X = -3739622
68
Y = 8037097
34 feet Y = 2449707
27 meter
Z = 16698822
46 Z = 5089801
09
XDOT = -17756
542562 XDOT = -5412
194173
YDOT = -15400
979109 feet/sec YDOT = -4694
218433 meter/sec
ZDOT = -5629
719382 ZDOT = -1715
938468
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 17331
61750838
00016717 00000-0 10270-3 0 9167
2 25544 51
6391 303
6015 0003651 158
2681 201
8627 15
54204991 7161
Satellite: ISS
Catalog Number: 25544
Epoch time: 17331
61750838 = yrday
fracday
Element set: 916
Inclination: 51
6391 deg
RA of node: 303
6015 deg
Eccentricity:
0003651
Arg of perigee: 158
2681 deg
Mean anomaly: 201
8627 deg
Mean motion: 15
54204991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 302
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