[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 15th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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
348/01:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 215
5
348/05:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
349/15:36:09
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
351/06:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
6
351/07:21:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
7
351/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
8
353/08:43:02
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
7
361/06:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
6
362/01:04:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2017/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4959580
49 A = 6789265
33 meter
Y = -4629330
37 meter E =
0009144
Z = -46650
96 I = 51
39844
XDOT = 3237
531411 Wp = 40
31287
YDOT = -3522
163774 meter/sec RA = 223
34199 deg
ZDOT = 5992
039252 TA = 319
18301
MA = 319
25147
Ha = 220
139 n
mi
Hp = 215
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16271589
54 X = -4907218
86
Y = -15188091
77 feet Y = -4684499
02 meter
Z = -153054
35 Z = -70616
37
XDOT = 10621
822215 XDOT = 3247
569909
YDOT = -11555
655425 feet/sec YDOT = -3485
903676 meter/sec
ZDOT = 19658
921431 ZDOT = 6007
790520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17427611
26 X = 5311935
91
Y = -13844767
35 feet Y = -4219885
09 meter
Z = -258778
38 Z = -78875
65
XDOT = 8865
375630 XDOT = 2702
166492
YDOT = 10815
006696 feet/sec YDOT = 3296
414041 meter/sec
ZDOT = 19729
345352 ZDOT = 6013
504463
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 17347
50015472
00016717 00000-0 10270-3 0 9003
2 25544 51
6413 224
4274 0002950 240
2437 119
8422 15
54148744 9633
Satellite: ISS
Catalog Number: 25544
Epoch time: 17347
50015472 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 224
4274 deg
Eccentricity:
0002950
Arg of perigee: 240
2437 deg
Mean anomaly: 119
8422 deg
Mean motion: 15
54148744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 963
Checksum: 290
Coasting Arc #2 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2645142
82 A = 6777392
56 meter
Y = 3310652
13 meter E =
0012454
Z = -5299939
01 I = 51
37117
XDOT = -5885
593096 Wp = 96
31177
YDOT = -4900
239557 meter/sec RA = 220
52830 deg
ZDOT = -125
136294 TA = 172
49924
MA = 172
48060
Ha = 220
243 n
mi
Hp = 215
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8678290
10 X = -2656222
07
Y = 10861719
59 feet Y = 3281010
71 meter
Z = -17388251
36 Z = -5312815
13
XDOT = -19309
688636 XDOT = -5829
752015
YDOT = -16076
901435 feet/sec YDOT = -4965
744049 meter/sec
ZDOT = -410
552147 ZDOT = -153
591642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12663202
76 X = 3859744
20
Y = 5561059
97 feet Y = 1695011
08 meter
Z = -17445883
89 Z = -5317505
41
XDOT = -10306
135281 XDOT = -3141
310034
YDOT = 21802
613039 feet/sec YDOT = 6645
436454 meter/sec
ZDOT = -536
178663 ZDOT = -163
427257
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 17348
07887164
00016717 00000-0 10270-3 0 9012
2 25544 51
6404 221
5409 0002956 236
8315 123
2555 15
54118817 9727
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
07887164 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 221
5409 deg
Eccentricity:
0002956
Arg of perigee: 236
8315 deg
Mean anomaly: 123
2555 deg
Mean motion: 15
54118817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 313
Coasting Arc #3 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2017/348/05:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -100195
00 A = 6780050
37 meter
Y = -4924219
74 meter E =
0006881
Z = 4657786
86 I = 51
38112
XDOT = 6641
351274 Wp = 136
84092
YDOT = 2566
591636 meter/sec RA = 219
76956 deg
ZDOT = 2848
843128 TA = 284
73167
MA = 284
80791
Ha = 220
117 n
mi
Hp = 215
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -328723
75 X = -67749
08
Y = -16155576
58 feet Y = -4925159
07 meter
Z = 15281452
95 Z = 4657378
63
XDOT = 21789
210216 XDOT = 6598
318935
YDOT = 8420
576234 feet/sec YDOT = 2640
618976 meter/sec
ZDOT = 9346
598188 ZDOT = 2881
000728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4899952
59 X = -1493505
55
Y = 15399194
18 feet Y = 4693674
39 meter
Z = 15280340
36 Z = 4657447
74
XDOT = -16633
421860 XDOT = -5069
866983
YDOT = -14732
611471 feet/sec YDOT = -4490
499976 meter/sec
ZDOT = 9488
994902 ZDOT = 2892
245646
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 17348
27177629
00016717 00000-0 10270-3 0 9023
2 25544 51
6374 220
5800 0003001 241
2274 118
8577 15
54154450 9753
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
27177629 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 220
5800 deg
Eccentricity:
0003001
Arg of perigee: 241
2274 deg
Mean anomaly: 118
8577 deg
Mean motion: 15
54154450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 300
Coasting Arc #4 (Orbit 989)
---------------------------------------
Vector Time (GMT): 2017/349/05:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1437799
03 A = 6777720
67 meter
Y = 4081121
75 meter E =
0011608
Z = -5226926
95 I = 51
39945
XDOT = -6663
114702 Wp = 86
44492
YDOT = -3640
805634 meter/sec RA = 214
75495 deg
ZDOT = -1011
078653 TA = 173
83853
MA = 173
82424
Ha = 220
129 n
mi
Hp = 215
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4717188
42 X = -1457938
27
Y = 13389507
07 feet Y = 4064931
12 meter
Z = -17148710
46 Z = -5233959
99
XDOT = -21860
612541 XDOT = -6616
995646
YDOT = -11944
900375 feet/sec YDOT = -3715
059189 meter/sec
ZDOT = -3317
187183 ZDOT = -1043
334600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8552983
73 X = 2606949
44
Y = -11282085
23 feet Y = -3438779
58 meter
Z = -17180513
93 Z = -5236620
64
XDOT = 16196
231936 XDOT = 4936
611494
YDOT = 17540
992140 feet/sec YDOT = 5346
494404 meter/sec
ZDOT = -3459
887364 ZDOT = -1054
573668
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 17349
23630300
00016717 00000-0 10270-3 0 9031
2 25544 51
6379 215
7712 0002848 244
7616 115
3242 15
54129556 9909
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
23630300 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 215
7712 deg
Eccentricity:
0002848
Arg of perigee: 244
7616 deg
Mean anomaly: 115
3242 deg
Mean motion: 15
54129556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 990
Checksum: 304
Coasting Arc #5 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2017/349/15:36:09
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6149898
41 A = 6787376
62 meter
Y = 1990117
30 meter E =
0011849
Z = 2048982
73 I = 51
44316
XDOT = 129
196484 Wp = 121
27418
YDOT = 5313
406899 meter/sec RA = 212
56655 deg
ZDOT = -5530
871849 TA = 35
99432
MA = 35
91458
Ha = 219
918 n
mi
Hp = 215
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20176832
04 X = 6117234
26
Y = 6529256
22 feet Y = 2058706
85 meter
Z = 6722384
28 Z = 2078778
15
XDOT = 423
872980 XDOT = 96
637456
YDOT = 17432
437332 feet/sec YDOT = 5314
670096 meter/sec
ZDOT = -18145
905017 ZDOT = -5530
322865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10479912
64 X = 3194277
37
Y = 18387898
31 feet Y = 5604631
40 meter
Z = 6854401
16 Z = 2089221
47
XDOT = -9999
943080 XDOT = -3047
982651
YDOT = 12484
068959 feet/sec YDOT = 3805
144219 meter/sec
ZDOT = -18144
217203 ZDOT = -5530
357403
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 17349
68641247
00016717 00000-0 10270-3 0 9043
2 25544 51
6371 213
5244 0003113 247
2915 112
7909 15
54164177 9979
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
68641247 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 213
5244 deg
Eccentricity:
0003113
Arg of perigee: 247
2915 deg
Mean anomaly: 112
7909 deg
Mean motion: 15
54164177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 316
Coasting Arc #6 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2017/350/15:36:09
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6141299
71 A = 6789200
90 meter
Y = -2857244
98 meter E =
0008559
Z = -390706
51 I = 51
47673
XDOT = 1708
682343 Wp = 34
94150
YDOT = -4480
843725 meter/sec RA = 207
58224 deg
ZDOT = 5982
594565 TA = 320
83734
MA = 320
89925
Ha = 220
080 n
mi
Hp = 215
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20148621
10 X = -6106994
92
Y = -9374163
31 feet Y = -2925729
34 meter
Z = -1281845
50 Z = -420456
24
XDOT = 5605
913198 XDOT = 1729
600617
YDOT = -14700
930856 feet/sec YDOT = -4461
619718 meter/sec
ZDOT = 19627
934926 ZDOT = 5990
945231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8920636
26 X = -2719009
93
Y = -20344756
16 feet Y = -6201081
68 meter
Z = -1413557
00 Z = -430852
17
XDOT = 12340
634266 XDOT = 3761
425324
YDOT = -6762
546037 feet/sec YDOT = -2061
224032 meter/sec
ZDOT = 19665
648526 ZDOT = 5994
089671
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 17350
65093719
00016717 00000-0 10270-3 0 9058
2 25544 51
6367 208
7158 0002931 244
4617 115
6233 15
54144599 10126
Satellite: ISS
Catalog Number: 25544
Epoch time: 17350
65093719 = yrday
fracday
Element set: 905
Inclination: 51
6367 deg
RA of node: 208
7158 deg
Eccentricity:
0002931
Arg of perigee: 244
4617 deg
Mean anomaly: 115
6233 deg
Mean motion: 15
54144599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 308
Coasting Arc #7 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2017/351/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -30337
41 A = 6778205
84 meter
Y = 4461137
03 meter E =
0010629
Z = -5112621
71 I = 51
45964
XDOT = -7246
764127 Wp = 78
33863
YDOT = -1891
793694 meter/sec RA = 204
48102 deg
ZDOT = -1608
464522 TA = 176
09361
MA = 176
08531
Ha = 219
988 n
mi
Hp = 215
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -99532
19 X = -55386
03
Y = 14636276
35 feet Y = 4460658
28 meter
Z = -16773693
26 Z = -5112829
43
XDOT = -23775
472858 XDOT = -7217
257809
YDOT = -6206
672226 feet/sec YDOT = -1972
666809 meter/sec
ZDOT = -5277
114572 ZDOT = -1643
595812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1086375
72 X = -331127
32
Y = -14594462
58 feet Y = -4448392
19 meter
Z = -16775241
50 Z = -5113093
61
XDOT = 23067
988280 XDOT = 7031
122828
YDOT = 4524
780385 feet/sec YDOT = 1379
153061 meter/sec
ZDOT = -5432
875379 ZDOT = -1655
940416
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 17351
29395221
00016717 00000-0 10270-3 0 9063
2 25544 51
6381 205
5142 0002822 256
0703 104
0136 15
54148171 10229
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
29395221 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 205
5142 deg
Eccentricity:
0002822
Arg of perigee: 256
0703 deg
Mean anomaly: 104
0136 deg
Mean motion: 15
54148171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 266
Coasting Arc #8 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2017/351/07:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -552379
28 A = 6778774
25 meter
Y = -4585970
78 meter E =
0004824
Z = 4960691
01 I = 51
46314
XDOT = 7233
025336 Wp = 150
17527
YDOT = 1421
758459 meter/sec RA = 204
32950 deg
ZDOT = 2114
778076 TA = 279
15431
MA = 279
20888
Ha = 219
921 n
mi
Hp = 215
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1812267
99 X = -525153
42
Y = -15045835
88 feet Y = -4591996
17 meter
Z = 16275232
96 Z = 4958073
33
XDOT = 23730
398084 XDOT = 7206
316662
YDOT = 4664
561874 feet/sec YDOT = 1502
493524 meter/sec
ZDOT = 6938
248282 ZDOT = 2149
849369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5868860
00 X = 1788828
53
Y = 13984825
51 feet Y = 4262574
82 meter
Z = 16264250
31 Z = 4957343
50
XDOT = -23049
921035 XDOT = -7025
615932
YDOT = 1404
007737 feet/sec YDOT = 427
941558 meter/sec
ZDOT = 7093
809294 ZDOT = 2162
193073
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 17351
35825259
00016717 00000-0 10270-3 0 9070
2 25544 51
6386 205
1945 0002985 255
3333 104
7489 15
54171803 10239
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
35825259 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 205
1945 deg
Eccentricity:
0002985
Arg of perigee: 255
3333 deg
Mean anomaly: 104
7489 deg
Mean motion: 15
54171803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1023
Checksum: 313
Coasting Arc #9 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2017/351/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5207178
68 A = 6787911
66 meter
Y = 3914907
93 meter E =
0006536
Z = -1893292
28 I = 51
49871
XDOT = -4287
019537 Wp = 166
97144
YDOT = 2995
547500 meter/sec RA = 203
57039 deg
ZDOT = -5606
606258 TA = 33
92006
MA = 33
87828
Ha = 220
005 n
mi
Hp = 215
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17083919
54 X = 5172210
85
Y = 12844186
14 feet Y = 3972942
86 meter
Z = -6211588
83 Z = -1868081
77
XDOT = -14065
024727 XDOT = -4292
963642
YDOT = 9827
911744 feet/sec YDOT = 2947
574501 meter/sec
ZDOT = -18394
377488 ZDOT = -5627
445495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17844817
26 X = -5439100
30
Y = 11822338
97 feet Y = 3603448
92 meter
Z = -6100168
72 Z = -1859331
43
XDOT = -3716
120212 XDOT = -1132
673441
YDOT = -15131
131309 feet/sec YDOT = -4611
968823 meter/sec
ZDOT = -18487
351615 ZDOT = -5634
944772
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 17351
48685591
00016717 00000-0 10270-3 0 9088
2 25544 51
6397 204
5543 0003081 255
6042 104
4769 15
54111157 10252
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
48685591 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 204
5543 deg
Eccentricity:
0003081
Arg of perigee: 255
6042 deg
Mean anomaly: 104
4769 deg
Mean motion: 15
54111157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1025
Checksum: 304
Coasting Arc #10 (Orbit 1040)
---------------------------------------
Vector Time (GMT): 2017/352/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110826
85 A = 6784565
33 meter
Y = -4208923
87 meter E =
0009540
Z = 3370697
73 I = 51
51806
XDOT = 5794
842740 Wp = 90
85686
YDOT = -1938
747141 meter/sec RA = 198
58314 deg
ZDOT = 4634
883040 TA = 308
56631
MA = 308
65175
Ha = 219
943 n
mi
Hp = 215
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13486964
73 X = -4079829
24
Y = -13808805
33 feet Y = -4254721
01 meter
Z = 11058719
58 Z = 3350803
36
XDOT = 19011
951247 XDOT = 5793
577610
YDOT = -6360
718965 feet/sec YDOT = -1873
952862 meter/sec
ZDOT = 15206
309186 ZDOT = 4663
029359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17414352
54 X = 5307894
65
Y = -8441297
73 feet Y = -2572907
55 meter
Z = 10970935
21 Z = 3343941
05
XDOT = -626
900143 XDOT = -191
079163
YDOT = 18682
232260 feet/sec YDOT = 5694
344393 meter/sec
ZDOT = 15331
607106 ZDOT = 4673
073846
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 17352
51567756
00016717 00000-0 10270-3 0 9096
2 25544 51
6396 199
4247 0003030 264
1255 95
9552 15
54136365 10419
Satellite: ISS
Catalog Number: 25544
Epoch time: 17352
51567756 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 199
4247 deg
Eccentricity:
0003030
Arg of perigee: 264
1255 deg
Mean anomaly: 95
9552 deg
Mean motion: 15
54136365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1041
Checksum: 319
Coasting Arc #11 (Orbit 1054)
---------------------------------------
Vector Time (GMT): 2017/353/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1785074
76 A = 6779415
25 meter
Y = -4405370
06 meter E =
0005144
Z = 4832455
98 I = 51
53009
XDOT = 7254
081104 Wp = 138
31022
YDOT = -214
092167 meter/sec RA = 194
05928 deg
ZDOT = 2479
151511 TA = 287
27491
MA = 287
33119
Ha = 219
977 n
mi
Hp = 215
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5856544
50 X = -1759153
74
Y = -14453313
85 feet Y = -4425187
62 meter
Z = 15854514
37 Z = 4823847
09
XDOT = 23799
478688 XDOT = 7243
893513
YDOT = -702
402122 feet/sec YDOT = -133
029327 meter/sec
ZDOT = 8133
699184 ZDOT = 2514
364793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13598842
50 X = 4144927
19
Y = 7711083
59 feet Y = 2350338
28 meter
Z = 15816880
01 Z = 4820985
03
XDOT = -17709
082233 XDOT = -5397
728265
YDOT = 14190
426187 feet/sec YDOT = 4325
241902 meter/sec
ZDOT = 8290
171033 ZDOT = 2526
844131
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 17353
41589527
00016717 00000-0 10270-3 0 9108
2 25544 51
6403 194
9366 0002849 265
1888 94
8939 15
54146019 10559
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
41589527 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 194
9366 deg
Eccentricity:
0002849
Arg of perigee: 265
1888 deg
Mean anomaly: 94
8939 deg
Mean motion: 15
54146019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1055
Checksum: 341
Coasting Arc #12 (Orbit 1069)
---------------------------------------
Vector Time (GMT): 2017/354/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5568
03 A = 6777368
45 meter
Y = 4251826
36 meter E =
0011740
Z = -5287965
75 I = 51
55495
XDOT = -7601
580945 Wp = 84
10535
YDOT = -731
931274 meter/sec RA = 189
05487 deg
ZDOT = -596
480718 TA = 180
18841
MA = 180
18885
Ha = 219
853 n
mi
Hp = 215
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18267
81 X = -16291
22
Y = 13949561
55 feet Y = 4251767
00 meter
Z = -17348968
99 Z = -5287991
31
XDOT = -24939
570028 XDOT = -7589
933930
YDOT = -2401
349323 feet/sec YDOT = -816
872158 meter/sec
ZDOT = -1956
957735 ZDOT = -633
378487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8883885
33 X = -2707808
25
Y = -10753735
79 feet Y = -3277738
67 meter
Z = -17349670
73 Z = -5288179
64
XDOT = 20094
345607 XDOT = 6124
756541
YDOT = -13178
523827 feet/sec YDOT = -4016
814063 meter/sec
ZDOT = -2120
808911 ZDOT = -646
422556
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 17354
38041187
00016717 00000-0 10270-3 0 9111
2 25544 51
6396 190
1287 0002936 270
5103 89
5714 15
54171603 10703
Satellite: ISS
Catalog Number: 25544
Epoch time: 17354
38041187 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 190
1287 deg
Eccentricity:
0002936
Arg of perigee: 270
5103 deg
Mean anomaly: 89
5714 deg
Mean motion: 15
54171603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1070
Checksum: 298
Coasting Arc #13 (Orbit 1085)
---------------------------------------
Vector Time (GMT): 2017/355/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1807976
77 A = 6777723
29 meter
Y = -3985736
49 meter E =
0002629
Z = 5175363
84 I = 51
58951
XDOT = 7379
124980 Wp = 8
84553
YDOT = 1593
818669 meter/sec RA = 184
05042 deg
ZDOT = -1347
754046 TA = 94
13058
MA = 94
10054
Ha = 219
698 n
mi
Hp = 215
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5931682
30 X = 1827272
77
Y = -13076563
30 feet Y = -3965411
11 meter
Z = 16979540
14 Z = 5184192
82
XDOT = 24209
727626 XDOT = 7367
300724
YDOT = 5229
063874 feet/sec YDOT = 1676
271115 meter/sec
ZDOT = -4421
765243 ZDOT = -1311
937340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3946869
44 X = 1203005
81
Y = 13756849
82 feet Y = 4193087
82 meter
Z = 17019325
80 Z = 5187490
50
XDOT = -20924
889320 XDOT = -6377
906265
YDOT = 11287
806135 feet/sec YDOT = 3440
523310 meter/sec
ZDOT = -4262
810442 ZDOT = -1299
304623
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 17355
40922807
00016717 00000-0 10270-3 0 9123
2 25544 51
6402 185
0000 0003118 273
6361 86
4435 15
54191927 10864
Satellite: ISS
Catalog Number: 25544
Epoch time: 17355
40922807 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 185
0000 deg
Eccentricity:
0003118
Arg of perigee: 273
6361 deg
Mean anomaly: 86
4435 deg
Mean motion: 15
54191927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1086
Checksum: 291
Coasting Arc #14 (Orbit 1100)
---------------------------------------
Vector Time (GMT): 2017/356/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3495920
56 A = 6780429
95 meter
Y = 3645300
49 meter E =
0006858
Z = -4530707
71 I = 51
63139
XDOT = -6565
696017 Wp = 115
78992
YDOT = -2384
366337 meter/sec RA = 179
05190 deg
ZDOT = 3148
522413 TA = 185
81490
MA = 185
82286
Ha = 219
810 n
mi
Hp = 215
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11469555
65 X = -3514415
71
Y = 11959647
27 feet Y = 3606103
71 meter
Z = -14864526
62 Z = -4547734
26
XDOT = -21540
997430 XDOT = -6553
839261
YDOT = -7822
724203 feet/sec YDOT = -2457
722430 meter/sec
ZDOT = 10329
797944 ZDOT = 3116
657152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 740199
07 X = 225612
68
Y = -16485310
03 feet Y = -5024722
50 meter
Z = -14940705
47 Z = -4553927
03
XDOT = 20239
334626 XDOT = 6168
949194
YDOT = -8322
753651 feet/sec YDOT = -2536
775313 meter/sec
ZDOT = 10188
489498 ZDOT = 3105
451599
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 17356
37374297
00016717 00000-0 10270-3 0 9135
2 25544 51
6404 180
1911 0003113 279
0945 80
9855 15
54168208 11015
Satellite: ISS
Catalog Number: 25544
Epoch time: 17356
37374297 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 180
1911 deg
Eccentricity:
0003113
Arg of perigee: 279
0945 deg
Mean anomaly: 80
9855 deg
Mean motion: 15
54168208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1101
Checksum: 304
Coasting Arc #15 (Orbit 1116)
---------------------------------------
Vector Time (GMT): 2017/357/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4917722
10 A = 6784173
88 meter
Y = -3206890
85 meter E =
0009475
Z = 3392222
61 I = 51
67665
XDOT = 5247
562847 Wp = 85
08577
YDOT = 3135
153113 meter/sec RA = 174
06558 deg
ZDOT = -4631
617737 TA = 55
29376
MA = 55
20454
Ha = 219
796 n
mi
Hp = 215
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16134258
86 X = 4936739
32
Y = -10521295
45 feet Y = -3151791
45 meter
Z = 11129339
28 Z = 3416157
11
XDOT = 17216
413541 XDOT = 5234
612629
YDOT = 10285
935411 feet/sec YDOT = 3193
762893 meter/sec
ZDOT = -15195
596249 ZDOT = -4606
158155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4904439
73 X = -1494873
23
Y = 18562569
35 feet Y = 5657871
14 meter
Z = 11236175
94 Z = 3424786
43
XDOT = -18398
303081 XDOT = -5607
802779
YDOT = 4292
287753 feet/sec YDOT = 1308
289307 meter/sec
ZDOT = -15082
844685 ZDOT = -4597
251060
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 17357
40255608
00016717 00000-0 10270-3 0 9145
2 25544 51
6401 175
0622 0003072 285
9391 74
1423 15
54190904 11170
Satellite: ISS
Catalog Number: 25544
Epoch time: 17357
40255608 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 175
0622 deg
Eccentricity:
0003072
Arg of perigee: 285
9391 deg
Mean anomaly: 74
1423 deg
Mean motion: 15
54190904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1117
Checksum: 289
Coasting Arc #16 (Orbit 1131)
---------------------------------------
Vector Time (GMT): 2017/358/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5930598
22 A = 6787652
48 meter
Y = 2681089
76 meter E =
0006443
Z = -1913797
36 I = 51
71975
XDOT = -3542
049880 Wp = 12
67216
YDOT = -3832
190861 meter/sec RA = 169
09172 deg
ZDOT = 5617
432299 TA = 326
26616
MA = 326
30714
Ha = 219
874 n
mi
Hp = 215
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19457343
24 X = -5950841
91
Y = 8796226
24 feet Y = 2614656
68 meter
Z = -6278862
75 Z = -1942655
13
XDOT = -11620
898557 XDOT = -3526
220532
YDOT = -12572
804663 feet/sec YDOT = -3871
712326 meter/sec
ZDOT = 18429
895993 ZDOT = 5600
264476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8214995
25 X = 2503930
55
Y = -19668333
30 feet Y = -5994907
99 meter
Z = -6407529
77 Z = -1953015
07
XDOT = 15725
991600 XDOT = 4793
282240
YDOT = 599
175697 feet/sec YDOT = 182
628752 meter/sec
ZDOT = 18354
088539 ZDOT = 5594
326187
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 17358
36706841
00016717 00000-0 10270-3 0 9152
2 25544 51
6396 170
2539 0003191 288
1805 71
9000 15
54147866 11326
Satellite: ISS
Catalog Number: 25544
Epoch time: 17358
36706841 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 170
2539 deg
Eccentricity:
0003191
Arg of perigee: 288
1805 deg
Mean anomaly: 71
9000 deg
Mean motion: 15
54147866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1132
Checksum: 312
Coasting Arc #17 (Orbit 1147)
---------------------------------------
Vector Time (GMT): 2017/359/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6475258
88 A = 6789277
02 meter
Y = -2012659
13 meter E =
0009746
Z = 209258
52 I = 51
75778
XDOT = 1591
244124 Wp = 139
66179
YDOT = 4478
252602 meter/sec RA = 164
12721 deg
ZDOT = -6017
781683 TA = 38
08742
MA = 38
01857
Ha = 219
982 n
mi
Hp = 215
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21244287
66 X = 6496267
25
Y = -6603212
38 feet Y = -1940130
90 meter
Z = 686543
69 Z = 240764
03
XDOT = 5220
617204 XDOT = 1570
280067
YDOT = 14692
429796 feet/sec YDOT = 4495
930071 meter/sec
ZDOT = -19743
378224 ZDOT = -6010
102654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10710090
84 X = -3264435
69
Y = 19493683
35 feet Y = 5941674
68 meter
Z = 826908
76 Z = 252041
79
XDOT = -12625
749562 XDOT = -3848
328466
YDOT = -6083
422735 feet/sec YDOT = -1854
227250 meter/sec
ZDOT = -19709
841637 ZDOT = -6007
559731
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 17359
39587985
00016717 00000-0 10270-3 0 9163
2 25544 51
6404 165
1249 0003136 289
5918 70
4896 15
54137128 11480
Satellite: ISS
Catalog Number: 25544
Epoch time: 17359
39587985 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 165
1249 deg
Eccentricity:
0003136
Arg of perigee: 289
5918 deg
Mean anomaly: 70
4896 deg
Mean motion: 15
54137128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1148
Checksum: 347
Coasting Arc #18 (Orbit 1163)
---------------------------------------
Vector Time (GMT): 2017/360/08:43:02
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6501811
04 A = 6788251
39 meter
Y = 1213434
29 meter E =
0012211
Z = 1496797
95 I = 51
78471
XDOT = 399
098346 Wp = 49
67953
YDOT = -5023
693714 meter/sec RA = 159
16460 deg
ZDOT = 5782
936867 TA = 326
63612
MA = 326
71302
Ha = 219
977 n
mi
Hp = 215
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21331401
05 X = -6522167
44
Y = 3981083
64 feet Y = 1140612
71 meter
Z = 4910754
42 Z = 1465164
91
XDOT = 1309
377776 XDOT = 427
154423
YDOT = -16481
934757 feet/sec YDOT = -5019
074116 meter/sec
ZDOT = 18972
889982 ZDOT = 5784
943469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12312481
61 X = 3752844
39
Y = -17906532
89 feet Y = -5457911
22 meter
Z = 4769914
39 Z = 1453869
91
XDOT = 9494
881651 XDOT = 2894
039927
YDOT = 11606
158906 feet/sec YDOT = 3537
557234 meter/sec
ZDOT = 18982
498063 ZDOT = 5785
865409
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 17360
42468656
00016717 00000-0 10270-3 0 9173
2 25544 51
6390 159
9949 0003183 294
3338 65
7482 15
54192183 11642
Satellite: ISS
Catalog Number: 25544
Epoch time: 17360
42468656 = yrday
fracday
Element set: 917
Inclination: 51
6390 deg
RA of node: 159
9949 deg
Eccentricity:
0003183
Arg of perigee: 294
3338 deg
Mean anomaly: 65
7482 deg
Mean motion: 15
54192183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1164
Checksum: 339
Coasting Arc #19 (Orbit 1177)
---------------------------------------
Vector Time (GMT): 2017/361/06:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 659662
79 A = 6778771
99 meter
Y = -4608876
99 meter E =
0005691
Z = 4926375
02 I = 51
78255
XDOT = 7180
843733 Wp = 28
52323
YDOT = -1421
507204 meter/sec RA = 154
57097 deg
ZDOT = -2285
469422 TA = 83
80129
MA = 83
73646
Ha = 219
959 n
mi
Hp = 215
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2164248
01 X = 687221
59
Y = -15120987
50 feet Y = -4601346
33 meter
Z = 16162647
69 Z = 4929646
16
XDOT = 23559
198600 XDOT = 7207
307387
YDOT = -4663
737547 feet/sec YDOT = -1341
058020 meter/sec
ZDOT = -7498
259257 ZDOT = -2250
522949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2209547
52 X = 673470
08
Y = 15098185
58 feet Y = 4601926
97 meter
Z = 16177827
56 Z = 4931001
84
XDOT = -20292
188902 XDOT = -6185
059177
YDOT = 10858
327473 feet/sec YDOT = 3309
618214 meter/sec
ZDOT = -7342
638806 ZDOT = -2238
036308
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 17361
32489396
00016717 00000-0 10270-3 0 9188
2 25544 51
6404 155
5089 0003238 299
1988 60
8841 15
54210671 11783
Satellite: ISS
Catalog Number: 25544
Epoch time: 17361
32489396 = yrday
fracday
Element set: 918
Inclination: 51
6404 deg
RA of node: 155
5089 deg
Eccentricity:
0003238
Arg of perigee: 299
1988 deg
Mean anomaly: 60
8841 deg
Mean motion: 15
54210671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1178
Checksum: 335
Coasting Arc #20 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2017/362/01:04:30
000
Vector Time (MET): N/A
Weight (LBS) : 926477
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3860231
67 A = 6778461
81 meter
Y = -2382045
02 meter E =
0002741
Z = 5035698
03 I = 51
80138
XDOT = 5577
216325 Wp = 127
88440
YDOT = -4885
348594 meter/sec RA = 150
80217 deg
ZDOT = 1962
050152 TA = 303
10481
MA = 303
13112
Ha = 220
152 n
mi
Hp = 215
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12664802
05 X = -3857769
06
Y = -7815108
34 feet Y = -2425199
28 meter
Z = 16521318
99 Z = 5016952
06
XDOT = 18297
953821 XDOT = 5621
900415
YDOT = -16028
046569 feet/sec YDOT = -4822
730609 meter/sec
ZDOT = 6437
172415 ZDOT = 1989
250818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2471498
31 X = -753312
69
Y = 14768283
33 feet Y = 4501372
76 meter
Z = 16438266
76 Z = 5010383
71
XDOT = -20613
361042 XDOT = -6282
952446
YDOT = -10758
879638 feet/sec YDOT = -3279
306514 meter/sec
ZDOT = 6558
832114 ZDOT = 1999
132028
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 17362
09649978
00016717 00000-0 10270-3 0 9198
2 25544 51
6381 151
6609 0003172 300
6089 59
4751 15
54200791 11909
Satellite: ISS
Catalog Number: 25544
Epoch time: 17362
09649978 = yrday
fracday
Element set: 919
Inclination: 51
6381 deg
RA of node: 151
6609 deg
Eccentricity:
0003172
Arg of perigee: 300
6089 deg
Mean anomaly: 59
4751 deg
Mean motion: 15
54200791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 321
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