[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 5th 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) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
255/21:17:02
000 0
0 0
0 0
0
N/A 0
0 0
0 219
3
000/00:00:00
000 0
0 0
0 216
2
256/02:57:42
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
3
256/23:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
2
Coasting Arc #1 (Orbit 3407)
---------------------------------------
Vector Time (GMT): 2017/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2619031
66 A = 6779152
09 meter
Y = -3819947
47 meter E =
0010660
Z = -4959858
95 I = 51
64736
XDOT = 7063
128492 Wp = 126
38294
YDOT = 2013
833328 meter/sec RA = 2
35791 deg
ZDOT = 2175
735178 TA = 164
86801
MA = 164
83610
Ha = 220
415 n
mi
Hp = 215
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8592623
54 X = 2685644
93
Y = -12532636
05 feet Y = -3790287
62 meter
Z = -16272503
10 Z = -4946974
56
XDOT = 23172
993740 XDOT = 7029
515807
YDOT = 6607
064725 feet/sec YDOT = 2092
630281 meter/sec
ZDOT = 7138
238774 ZDOT = 2209
963431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11994645
51 X = -3655967
95
Y = 9428881
11 feet Y = 2873922
96 meter
Z = -16214782
86 Z = -4942265
81
XDOT = -19480
411919 XDOT = -5937
629553
YDOT = -12229
231872 feet/sec YDOT = -3727
469875 meter/sec
ZDOT = 7289
447028 ZDOT = 2221
823454
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 17247
51221155
00016717 00000-0 10270-3 0 9000
2 25544 51
6427 2
8847 0004419 228
1037 131
9740 15
54073479 34082
Satellite: ISS
Catalog Number: 25544
Epoch time: 17247
51221155 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 2
8847 deg
Eccentricity:
0004419
Arg of perigee: 228
1037 deg
Mean anomaly: 131
9740 deg
Mean motion: 15
54073479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3408
Checksum: 296
Coasting Arc #2 (Orbit 3423)
---------------------------------------
Vector Time (GMT): 2017/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4165728
16 A = 6782562
31 meter
Y = 3438358
99 meter E =
0007044
Z = 4095785
53 I = 51
62543
XDOT = -6046
790679 Wp = 93
07123
YDOT = -2757
685663 meter/sec RA = 357
36646 deg
ZDOT = -3829
691441 TA = 36
51116
MA = 36
46315
Ha = 220
468 n
mi
Hp = 216
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13667087
14 X = -4223762
30
Y = 11280705
34 feet Y = 3391450
89 meter
Z = 13437616
58 Z = 4075408
65
XDOT = -19838
552098 XDOT = -5996
901541
YDOT = -9047
525140 feet/sec YDOT = -2825
026431 meter/sec
ZDOT = -12564
604465 ZDOT = -3858
943099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16341755
24 X = 4980967
00
Y = -7030162
38 feet Y = -2142793
49 meter
Z = 13346796
46 Z = 4068103
56
XDOT = 15963
533085 XDOT = 4865
684884
YDOT = 12975
279072 feet/sec YDOT = 3954
865061 meter/sec
ZDOT = -12693
638817 ZDOT = -3869
021111
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 17248
54109168
00016717 00000-0 10270-3 0 9014
2 25544 51
6424 357
7566 0004345 230
9320 129
1446 15
54040232 34244
Satellite: ISS
Catalog Number: 25544
Epoch time: 17248
54109168 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 357
7566 deg
Eccentricity:
0004345
Arg of perigee: 230
9320 deg
Mean anomaly: 129
1446 deg
Mean motion: 15
54040232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3424
Checksum: 292
Coasting Arc #3 (Orbit 3438)
---------------------------------------
Vector Time (GMT): 2017/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5400007
03 A = 6786261
12 meter
Y = -2982914
01 meter E =
0000340
Z = -2827834
99 I = 51
60596
XDOT = 4572
791285 Wp = 79
68797
YDOT = 3455
777090 meter/sec RA = 352
38315 deg
ZDOT = 5087
446846 TA = 248
19419
MA = 248
19780
Ha = 220
144 n
mi
Hp = 216
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17716558
50 X = 5446697
55
Y = -9786463
28 feet Y = -2922266
70 meter
Z = -9277673
84 Z = -2801489
91
XDOT = 15002
596081 XDOT = 4509
095890
YDOT = 11337
851345 feet/sec YDOT = 3506
557589 meter/sec
ZDOT = 16691
098576 ZDOT = 5109
504769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19712479
34 X = -6008363
70
Y = 4819704
95 feet Y = 1469046
07 meter
Z = -9160520
89 Z = -2792126
77
XDOT = -11074
312274 XDOT = -3375
450381
YDOT = -13389
112497 feet/sec YDOT = -4081
001489 meter/sec
ZDOT = 16788
154865 ZDOT = 5117
029603
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 17249
50566088
00016717 00000-0 10270-3 0 9020
2 25544 51
6430 352
9496 0004415 238
1915 121
8808 15
54046572 34398
Satellite: ISS
Catalog Number: 25544
Epoch time: 17249
50566088 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 352
9496 deg
Eccentricity:
0004415
Arg of perigee: 238
1915 deg
Mean anomaly: 121
8808 deg
Mean motion: 15
54046572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3439
Checksum: 322
Coasting Arc #4 (Orbit 3454)
---------------------------------------
Vector Time (GMT): 2017/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6214224
23 A = 6788895
55 meter
Y = 2407814
27 meter E =
0012285
Z = 1254564
60 I = 51
58262
XDOT = -2781
439254 Wp = 139
50257
YDOT = -4123
945888 meter/sec RA = 347
40643 deg
ZDOT = -5839
450947 TA = 26
83991
MA = 26
77640
Ha = 220
089 n
mi
Hp = 216
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20387874
78 X = -6246781
23
Y = 7899653
12 feet Y = 2338140
69 meter
Z = 4116025
58 Z = 1224298
59
XDOT = -9125
456870 XDOT = -2706
752402
YDOT = -13530
006195 feet/sec YDOT = -4154
632936 meter/sec
ZDOT = -19158
303633 ZDOT = -5852
780363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21724412
91 X = 6621601
05
Y = -2684799
39 feet Y = -818326
85 meter
Z = 3981627
83 Z = 1213600
16
XDOT = 5233
486140 XDOT = 1595
166575
YDOT = 13733
175136 feet/sec YDOT = 4185
871781 meter/sec
ZDOT = -19216
598942 ZDOT = -5857
219357
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 17250
53453068
00016717 00000-0 10270-3 0 9039
2 25544 51
6429 347
8217 0004370 239
9292 120
1427 15
54063800 34557
Satellite: ISS
Catalog Number: 25544
Epoch time: 17250
53453068 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 347
8217 deg
Eccentricity:
0004370
Arg of perigee: 239
9292 deg
Mean anomaly: 120
1427 deg
Mean motion: 15
54063800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3455
Checksum: 300
Coasting Arc #5 (Orbit 3470)
---------------------------------------
Vector Time (GMT): 2017/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6550038
37 A = 6789378
78 meter
Y = -1715089
41 meter E =
0008946
Z = 430725
98 I = 51
55312
XDOT = 837
758286 Wp = 41
95800
YDOT = 4718
999739 meter/sec RA = 342
43189 deg
ZDOT = 5985
172609 TA = 322
69160
MA = 322
75370
Ha = 219
885 n
mi
Hp = 216
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21489627
21 X = 6566637
89
Y = -5626933
75 feet Y = -1641749
55 meter
Z = 1413142
99 Z = 462584
56
XDOT = 2748
550807 XDOT = 755
853870
YDOT = 15482
282609 feet/sec YDOT = 4727
910884 meter/sec
ZDOT = 19636
393074 ZDOT = 5989
042681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22196492
23 X = -6765490
83
Y = 602354
14 feet Y = 183597
54 meter
Z = 1554457
02 Z = 473798
50
XDOT = 1008
546505 XDOT = 307
404975
YDOT = -14055
714199 feet/sec YDOT = -4284
181688 meter/sec
ZDOT = 19652
712613 ZDOT = 5990
146804
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 17251
56339401
00016717 00000-0 10270-3 0 9048
2 25544 51
6432 342
6936 0004224 246
8636 113
2072 15
54078952 34710
Satellite: ISS
Catalog Number: 25544
Epoch time: 17251
56339401 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 342
6936 deg
Eccentricity:
0004224
Arg of perigee: 246
8636 deg
Mean anomaly: 113
2072 deg
Mean motion: 15
54078952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3471
Checksum: 302
Coasting Arc #6 (Orbit 3485)
---------------------------------------
Vector Time (GMT): 2017/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6396303
41 A = 6787523
30 meter
Y = 855058
75 meter E =
0006271
Z = -2091527
29 I = 51
51485
XDOT = 1105
684100 Wp = 177
74105
YDOT = -5208
425571 meter/sec RA = 337
45403 deg
ZDOT = -5517
409313 TA = 25
45512
MA = 25
42424
Ha = 219
717 n
mi
Hp = 216
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20985247
42 X = -6395229
86
Y = 2805310
84 feet Y = 783536
69 meter
Z = -6861966
17 Z = -2122596
17
XDOT = 3627
572506 XDOT = 1190
644909
YDOT = -17088
010404 feet/sec YDOT = -5195
586634 meter/sec
ZDOT = -18101
736590 ZDOT = -5511
831275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21061391
65 X = 6419512
18
Y = 1661323
24 feet Y = 506371
32 meter
Z = -6999624
60 Z = -2133485
58
XDOT = -7134
933126 XDOT = -2174
727617
YDOT = 14383
794645 feet/sec YDOT = 4384
180608 meter/sec
ZDOT = -18076
155864 ZDOT = -5509
612307
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 17252
52794996
00016717 00000-0 10270-3 0 9050
2 25544 51
6418 337
8867 0004300 249
1318 110
9374 15
54085173 34869
Satellite: ISS
Catalog Number: 25544
Epoch time: 17252
52794996 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 337
8867 deg
Eccentricity:
0004300
Arg of perigee: 249
1318 deg
Mean anomaly: 110
9374 deg
Mean motion: 15
54085173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3486
Checksum: 333
Coasting Arc #7 (Orbit 3501)
---------------------------------------
Vector Time (GMT): 2017/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5794455
94 A = 6783998
58 meter
Y = 139645
33 meter E =
0008124
Z = 3520006
04 I = 51
47411
XDOT = -2864
276311 Wp = 101
96979
YDOT = 5520
757545 meter/sec RA = 332
46514 deg
ZDOT = 4485
576013 TA = 299
59792
MA = 299
67885
Ha = 219
553 n
mi
Hp = 216
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19010682
23 X = 5775365
15
Y = 458153
97 feet Y = 204336
49 meter
Z = 11548576
24 Z = 3548107
52
XDOT = -9397
231990 XDOT = -2947
586894
YDOT = 18112
721605 feet/sec YDOT = 5488
261879 meter/sec
ZDOT = 14716
456734 ZDOT = 4471
459256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18488125
90 X = -5635180
77
Y = -4113108
20 feet Y = -1253675
38 meter
Z = 11672921
61 Z = 3557906
51
XDOT = 12518
188564 XDOT = 3815
543874
YDOT = -14587
226259 feet/sec YDOT = -4446
186564 meter/sec
ZDOT = 14653
037059 ZDOT = 4466
245696
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 17253
55680306
00016717 00000-0 10270-3 0 9064
2 25544 51
6423 332
7577 0004314 254
2258 105
8419 15
54116106 35025
Satellite: ISS
Catalog Number: 25544
Epoch time: 17253
55680306 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 332
7577 deg
Eccentricity:
0004314
Arg of perigee: 254
2258 deg
Mean anomaly: 105
8419 deg
Mean motion: 15
54116106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3502
Checksum: 293
Coasting Arc #8 (Orbit 3516)
---------------------------------------
Vector Time (GMT): 2017/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4819561
94 A = 6780345
07 meter
Y = -1277186
36 meter E =
0006192
Z = -4601146
33 I = 51
43236
XDOT = 4324
525626 Wp = 63
59893
YDOT = -5578
817178 meter/sec RA = 327
46476 deg
ZDOT = -2981
662297 TA = 176
55676
MA = 176
55250
Ha = 219
553 n
mi
Hp = 216
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15812211
09 X = -4782571
61
Y = -4190243
97 feet Y = -1330875
53 meter
Z = -15095624
44 Z = -4624468
50
XDOT = 14188
076200 XDOT = 4401
071600
YDOT = -18303
205963 feet/sec YDOT = -5530
029626 meter/sec
ZDOT = -9782
356617 ZDOT = -2960
468568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14726191
27 X = 4488543
10
Y = 6899515
91 feet Y = 2102972
45 meter
Z = -15198618
76 Z = -4632539
00
XDOT = -16756
212333 XDOT = -5107
293519
YDOT = 14426
759102 feet/sec YDOT = 4397
276174 meter/sec
ZDOT = -9687
614406 ZDOT = -2952
784871
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 17254
52135017
00016717 00000-0 10270-3 0 9077
2 25544 51
6414 327
9502 0004254 259
2410 100
8264 15
54092012 35175
Satellite: ISS
Catalog Number: 25544
Epoch time: 17254
52135017 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 327
9502 deg
Eccentricity:
0004254
Arg of perigee: 259
2410 deg
Mean anomaly: 100
8264 deg
Mean motion: 15
54092012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3517
Checksum: 276
Coasting Arc #9 (Orbit 3532)
---------------------------------------
Vector Time (GMT): 2017/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3585384
44 A = 6777774
04 meter
Y = 2474109
88 meter E =
0002818
Z = 5193784
09 I = 51
39709
XDOT = -5387
143245 Wp = 199
75534
YDOT = 5327
508169 meter/sec RA = 322
45337 deg
ZDOT = 1178
639220 TA = 238
88701
MA = 238
91465
Ha = 219
343 n
mi
Hp = 216
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11763072
30 X = 3532222
79
Y = 8117158
39 feet Y = 2513907
16 meter
Z = 17039974
04 Z = 5211071
61
XDOT = -17674
354479 XDOT = -5452
041760
YDOT = 17478
701343 feet/sec YDOT = 5266
902664 meter/sec
ZDOT = 3866
926575 ZDOT = 1152
312034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10206274
00 X = -3110872
31
Y = -9873772
95 feet Y = -3009525
99 meter
Z = 17116057
50 Z = 5216974
32
XDOT = 19541
738610 XDOT = 5956
321928
YDOT = -13686
398797 feet/sec YDOT = -4171
614353 meter/sec
ZDOT = 3749
517123 ZDOT = 1142
852819
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 17255
55019512
00016717 00000-0 10270-3 0 9083
2 25544 51
6414 322
8218 0004251 263
6900 96
3769 15
54131176 35335
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
55019512 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 322
8218 deg
Eccentricity:
0004251
Arg of perigee: 263
6900 deg
Mean anomaly: 96
3769 deg
Mean motion: 15
54131176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3533
Checksum: 302
Coasting Arc #10 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2017/255/21:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3194093
70 A = 6777397
82 meter
Y = 2822793
83 meter E =
0001950
Z = 5270514
60 I = 51
38509
XDOT = -5588
387428 Wp = 234
90532
YDOT = 5216
595250 meter/sec RA = 320
51605 deg
ZDOT = 591
874178 TA = 209
41966
MA = 209
43063
Ha = 219
310 n
mi
Hp = 216
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10479310
04 X = 3136689
37
Y = 9261134
61 feet Y = 2858191
69 meter
Z = 17291714
55 Z = 5285891
01
XDOT = -18334
604422 XDOT = -5649
180490
YDOT = 17114
813813 feet/sec YDOT = 5153
762212 meter/sec
ZDOT = 1941
844415 ZDOT = 564
579442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -321671
71 X = -98045
54
Y = 13897474
55 feet Y = 4235950
24 meter
Z = 17359282
07 Z = 5291109
17
XDOT = -23914
168591 XDOT = -7289
038587
YDOT = -2830
948419 feet/sec YDOT = -862
873078 meter/sec
ZDOT = 1820
175032 ZDOT = 554
789350
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 17255
93601235
00016717 00000-0 10270-3 0 9095
2 25544 51
6406 320
9005 0004211 270
0881 89
9789 15
54146614 35394
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
93601235 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 320
9005 deg
Eccentricity:
0004211
Arg of perigee: 270
0881 deg
Mean anomaly: 89
9789 deg
Mean motion: 15
54146614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 313
Coasting Arc #11 (Orbit 3541)
---------------------------------------
Vector Time (GMT): 2017/256/02:57:42
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2968658
85 A = 6786208
08 meter
Y = -5446410
53 meter E =
0002625
Z = -2748553
67 I = 51
40691
XDOT = 5678
567884 Wp = 354
66110
YDOT = 510
313492 meter/sec RA = 319
30342 deg
ZDOT = 5124
262849 TA = 334
11931
MA = 334
13243
Ha = 219
462 n
mi
Hp = 216
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9739694
39 X = 3042692
60
Y = -17868800
96 feet Y = -5412799
16 meter
Z = -9017564
54 Z = -2733952
68
XDOT = 18630
472060 XDOT = 5647
548117
YDOT = 1674
256862 feet/sec YDOT = 573
641935 meter/sec
ZDOT = 16811
885986 ZDOT = 5151
772317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2525810
75 X = -769867
12
Y = -20222600
69 feet Y = -6163848
69 meter
Z = -8952031
41 Z = -2728579
17
XDOT = 14516
848651 XDOT = 4424
735469
YDOT = -9306
035319 feet/sec YDOT = -2836
479565 meter/sec
ZDOT = 16933
536367 ZDOT = 5161
341885
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 17256
12891958
00016717 00000-0 10270-3 0 9102
2 25544 51
6393 319
9371 0004286 269
8981 90
1681 15
54115513 35425
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
12891958 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 319
9371 deg
Eccentricity:
0004286
Arg of perigee: 269
8981 deg
Mean anomaly: 90
1681 deg
Mean motion: 15
54115513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3542
Checksum: 331
Coasting Arc #12 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2017/256/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2059374
57 A = 6785070
49 meter
Y = -5630141
88 meter E =
0001324
Z = -3176430
91 I = 51
38645
XDOT = 5956
756035 Wp = 12
50416
YDOT = -525
807265 meter/sec RA = 315
12681 deg
ZDOT = 4795
565360 TA = 310
68397
MA = 310
69548
Ha = 219
490 n
mi
Hp = 216
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6756478
26 X = 2137608
82
Y = -18471594
08 feet Y = -5606675
26 meter
Z = -10421361
25 Z = -3166236
81
XDOT = 19543
162845 XDOT = 5938
898506
YDOT = -1725
089451 feet/sec YDOT = -459
294377 meter/sec
ZDOT = 15733
482153 ZDOT = 4824
458113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13435932
12 X = 4095272
11
Y = -14397337
43 feet Y = -4388308
45 meter
Z = -10375305
28 Z = -3162393
05
XDOT = 17544
460201 XDOT = 5347
551469
YDOT = 4946
416133 feet/sec YDOT = 1507
667637 meter/sec
ZDOT = 15861
427117 ZDOT = 4834
562985
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 17256
96485342
00016717 00000-0 10270-3 0 9111
2 25544 51
6428 315
7719 0004155 274
5760 85
4918 15
54134394 35559
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
96485342 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 315
7719 deg
Eccentricity:
0004155
Arg of perigee: 274
5760 deg
Mean anomaly: 85
4918 deg
Mean motion: 15
54134394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 334
Coasting Arc #13 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2017/257/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3147659
56 A = 6788288
88 meter
Y = 5777575
66 meter E =
0010218
Z = 1648884
02 I = 51
37411
XDOT = -5018
762248 Wp = 123
56881
YDOT = -1103
901296 meter/sec RA = 310
13330 deg
ZDOT = -5692
678144 TA = 38
30157
MA = 38
22904
Ha = 219
617 n
mi
Hp = 216
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10326967
07 X = -3220041
45
Y = 18955300
73 feet Y = 5741971
76 meter
Z = 5409724
47 Z = 1633417
60
XDOT = -16465
755406 XDOT = -4978
392971
YDOT = -3621
723412 feet/sec YDOT = -1159
799101 meter/sec
ZDOT = -18676
765565 ZDOT = -5716
959550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16650950
98 X = -5075209
86
Y = 13763777
69 feet Y = 4195199
44 meter
Z = 5340322
89 Z = 1627730
42
XDOT = -12831
642463 XDOT = -3911
084623
YDOT = -8209
370556 feet/sec YDOT = -2502
216146 meter/sec
ZDOT = -18784
032138 ZDOT = -5725
372996
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 17257
99369044
00016717 00000-0 10270-3 0 9126
2 25544 51
6424 310
6439 0004004 277
8419 82
2279 15
54100420 35714
Satellite: ISS
Catalog Number: 25544
Epoch time: 17257
99369044 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 310
6439 deg
Eccentricity:
0004004
Arg of perigee: 277
8419 deg
Mean anomaly: 82
2279 deg
Mean motion: 15
54100420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 304
Coasting Arc #14 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2017/258/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3926486
84 A = 6789295
64 meter
Y = -5530703
05 meter E =
0010544
Z = 33936
43 I = 51
35724
XDOT = 3885
899706 Wp = 26
27964
YDOT = 2799
854963 meter/sec RA = 305
14340 deg
ZDOT = 5990
179174 TA = 334
08739
MA = 334
14015
Ha = 219
554 n
mi
Hp = 216
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12882174
69 X = 3987875
97
Y = -18145351
20 feet Y = -5486451
14 meter
Z = 111340
01 Z = 53159
45
XDOT = 12749
014782 XDOT = 3825
204999
YDOT = 9185
875863 feet/sec YDOT = 2842
970786 meter/sec
ZDOT = 19652
818811 ZDOT = 6008
907945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18479488
57 X = 5632548
12
Y = -12397022
28 feet Y = -3778612
39 meter
Z = 197312
03 Z = 60140
71
XDOT = 7636
826521 XDOT = 2327
704723
YDOT = 11718
653733 feet/sec YDOT = 3571
845658 meter/sec
ZDOT = 19735
237785 ZDOT = 6015
300477
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 17259
02252215
00016717 00000-0 10270-3 0 9134
2 25544 51
6420 305
5151 0004205 283
3815 76
6868 15
54140297 35873
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
02252215 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 305
5151 deg
Eccentricity:
0004205
Arg of perigee: 283
3815 deg
Mean anomaly: 76
6868 deg
Mean motion: 15
54140297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 301
Coasting Arc #15 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2017/259/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4419338
41 A = 6788078
18 meter
Y = 4848439
37 meter E =
0004792
Z = -1732092
60 I = 51
33514
XDOT = -2655
951684 Wp = 173
84383
YDOT = -4439
783078 meter/sec RA = 300
15297 deg
ZDOT = -5657
373500 TA = 25
23919
MA = 25
21578
Ha = 219
616 n
mi
Hp = 216
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14499141
75 X = -4464812
90
Y = 15906953
31 feet Y = 4798764
90 meter
Z = -5682718
50 Z = -1753671
09
XDOT = -8713
752243 XDOT = -2578
626907
YDOT = -14566
217448 feet/sec YDOT = -4469
051891 meter/sec
ZDOT = -18560
936681 ZDOT = -5670
086994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18992638
04 X = -5788956
07
Y = 10071372
72 feet Y = 3069754
41 meter
Z = -5778989
23 Z = -1761435
92
XDOT = -2418
297859 XDOT = -737
097187
YDOT = -15231
281985 feet/sec YDOT = -4642
494749 meter/sec
ZDOT = -18616
478428 ZDOT = -5674
302625
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 17259
98705111
00016717 00000-0 10270-3 0 9148
2 25544 51
6422 300
7079 0004288 284
9782 75
0895 15
54105551 36027
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
98705111 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 300
7079 deg
Eccentricity:
0004288
Arg of perigee: 284
9782 deg
Mean anomaly: 75
0895 deg
Mean motion: 15
54105551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 319
Coasting Arc #16 (Orbit 3617)
---------------------------------------
Vector Time (GMT): 2017/260/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4625252
41 A = 6784806
53 meter
Y = -3757981
60 meter E =
0009019
Z = 3233050
41 I = 51
30836
XDOT = 1441
404190 Wp = 75
47410
YDOT = 5857
515450 meter/sec RA = 295
15299 deg
ZDOT = 4737
581801 TA = 322
18352
MA = 322
24685
Ha = 219
661 n
mi
Hp = 216
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15174712
62 X = 4651226
93
Y = -12329335
95 feet Y = -3706113
29 meter
Z = 10607120
78 Z = 3255581
80
XDOT = 4729
016372 XDOT = 1352
784066
YDOT = 19217
570373 feet/sec YDOT = 5873
139224 meter/sec
ZDOT = 15543
247378 ZDOT = 4744
367770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18272302
52 X = 5569397
81
Y = -6802172
05 feet Y = -2073302
04 meter
Z = 10707420
57 Z = 3263621
79
XDOT = -2310
311956 XDOT = -704
183084
YDOT = 18352
114428 feet/sec YDOT = 5593
724478 meter/sec
ZDOT = 15572
344730 ZDOT = 4746
450674
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 17261
01587675
00016717 00000-0 10270-3 0 9159
2 25544 51
6416 295
5781 0004293 293
0763 66
9937 15
54130379 36186
Satellite: ISS
Catalog Number: 25544
Epoch time: 17261
01587675 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 295
5781 deg
Eccentricity:
0004293
Arg of perigee: 293
0763 deg
Mean anomaly: 66
9937 deg
Mean motion: 15
54130379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3618
Checksum: 339
Coasting Arc #17 (Orbit 3632)
---------------------------------------
Vector Time (GMT): 2017/261/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4611956
43 A = 6780942
98 meter
Y = 2310891
97 meter E =
0006934
Z = -4408258
94 I = 51
28083
XDOT = -293
927540 Wp = 42
49978
YDOT = -6903
851995 meter/sec RA = 290
14267 deg
ZDOT = -3309
657211 TA = 193
87305
MA = 193
89211
Ha = 219
817 n
mi
Hp = 215
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15131090
64 X = -4616041
59
Y = 7581666
58 feet Y = 2259294
53 meter
Z = -14462791
79 Z = -4430672
51
XDOT = -964
329198 XDOT = -200
628354
YDOT = -22650
433053 feet/sec YDOT = -6906
617642 meter/sec
ZDOT = -10858
455418 ZDOT = -3310
857537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16634224
82 X = -5070111
73
Y = 2616289
65 feet Y = 797445
09 meter
Z = -14562331
93 Z = -4438598
77
XDOT = 6271
261247 XDOT = 1911
480428
YDOT = -20625
234470 feet/sec YDOT = -6286
571466 meter/sec
ZDOT = -10862
687302 ZDOT = -3310
947090
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 17261
98039732
00016717 00000-0 10270-3 0 9162
2 25544 51
6398 290
7699 0004346 295
4977 64
5726 15
54143466 36330
Satellite: ISS
Catalog Number: 25544
Epoch time: 17261
98039732 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 290
7699 deg
Eccentricity:
0004346
Arg of perigee: 295
4977 deg
Mean anomaly: 64
5726 deg
Mean motion: 15
54143466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3633
Checksum: 356
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