[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 2nd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
245/21:58:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
9
246/10:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
9
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 3330)
---------------------------------------
Vector Time (GMT): 2017/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5000706
52 A = 6788125
60 meter
Y = 4202014
62 meter E =
0010703
Z = 1835599
01 I = 51
83051
XDOT = -4389
064557 Wp = 82
87955
YDOT = 2740
201080 meter/sec RA = 27
27769 deg
ZDOT = 5657
329391 TA = 297
24882
MA = 297
35782
Ha = 221
147 n
mi
Hp = 215
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16406517
45 X = 4944430
41
Y = 13786137
22 feet Y = 4257621
34 meter
Z = 6022306
47 Z = 1859753
95
XDOT = -14399
818102 XDOT = -4446
860422
YDOT = 8990
161025 feet/sec YDOT = 2690
796626 meter/sec
ZDOT = 18560
791965 ZDOT = 5635
868291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10011942
25 X = -3051640
00
Y = -18912995
83 feet Y = -5764681
13 meter
Z = 6128553
69 Z = 1867983
16
XDOT = 15452
739591 XDOT = 4709
995027
YDOT = -2168
567232 feet/sec YDOT = -660
979292 meter/sec
ZDOT = 18465
260034 ZDOT = 5628
211258
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 17242
56063421
00016717 00000-0 10270-3 0 9000
2 25544 51
6398 27
5636 0004825 206
9358 153
1545 15
54034441 33310
Satellite: ISS
Catalog Number: 25544
Epoch time: 17242
56063421 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 27
5636 deg
Eccentricity:
0004825
Arg of perigee: 206
9358 deg
Mean anomaly: 153
1545 deg
Mean motion: 15
54034441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3331
Checksum: 294
Coasting Arc #2 (Orbit 3345)
---------------------------------------
Vector Time (GMT): 2017/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3925848
67 A = 6784927
08 meter
Y = -4430339
71 meter E =
0004837
Z = -3313236
83 I = 51
79077
XDOT = 5816
667822 Wp = 151
54616
YDOT = -1629
414089 meter/sec RA = 22
31274 deg
ZDOT = -4720
348055 TA = 66
88591
MA = 66
83493
Ha = 220
974 n
mi
Hp = 215
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12880080
94 X = -3859921
68
Y = -14535235
28 feet Y = -4473872
72 meter
Z = -10870199
57 Z = -3332146
99
XDOT = 19083
555846 XDOT = 5857
385048
YDOT = -5345
846749 feet/sec YDOT = -1564
140645 meter/sec
ZDOT = -15486
706217 ZDOT = -4691
993716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6745480
57 X = 2056022
48
Y = 18161974
69 feet Y = 5535769
88 meter
Z = -10953171
04 Z = -3338526
53
XDOT = -18501
950462 XDOT = -5639
394501
YDOT = -2378
397802 feet/sec YDOT = -724
935650 meter/sec
ZDOT = -15360
842183 ZDOT = -4681
984697
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 17243
52523803
00016717 00000-0 10270-3 0 9013
2 25544 51
6404 22
7557 0004685 211
6727 148
4144 15
54016455 33467
Satellite: ISS
Catalog Number: 25544
Epoch time: 17243
52523803 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 22
7557 deg
Eccentricity:
0004685
Arg of perigee: 211
6727 deg
Mean anomaly: 148
4144 deg
Mean motion: 15
54016455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3346
Checksum: 294
Coasting Arc #3 (Orbit 3361)
---------------------------------------
Vector Time (GMT): 2017/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2535235
99 A = 6781152
47 meter
Y = 4456137
57 meter E =
0009161
Z = 4437316
17 I = 51
74870
XDOT = -6884
040281 Wp = 139
90493
YDOT = 596
175177 meter/sec RA = 17
33623 deg
ZDOT = 3323
791702 TA = 276
53906
MA = 276
64335
Ha = 220
798 n
mi
Hp = 215
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8317703
39 X = 2463663
74
Y = 14619873
93 feet Y = 4484088
29 meter
Z = 14558123
92 Z = 4449457
46
XDOT = -22585
433994 XDOT = -6906
340446
YDOT = 1955
955305 feet/sec YDOT = 519
068584 meter/sec
ZDOT = 10904
828418 ZDOT = 3290
297275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2718604
88 X = -828630
77
Y = -16552599
96 feet Y = -5045232
47 meter
Z = 14611108
70 Z = 4453465
93
XDOT = 20749
850531 XDOT = 6324
554442
YDOT = 6117
551096 feet/sec YDOT = 1864
629574 meter/sec
ZDOT = 10756
387265 ZDOT = 3278
546838
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 17244
55414166
00016717 00000-0 10270-3 0 9029
2 25544 51
6412 17
6274 0004664 215
8513 144
2327 15
54048451 33627
Satellite: ISS
Catalog Number: 25544
Epoch time: 17244
55414166 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 17
6274 deg
Eccentricity:
0004664
Arg of perigee: 215
8513 deg
Mean anomaly: 144
2327 deg
Mean motion: 15
54048451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3362
Checksum: 290
Coasting Arc #4 (Orbit 3376)
---------------------------------------
Vector Time (GMT): 2017/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -873155
06 A = 6778403
79 meter
Y = -4344248
18 meter E =
0010530
Z = -5138419
60 I = 51
70751
XDOT = 7487
122198 Wp = 93
83894
YDOT = 361
251926 meter/sec RA = 12
34935 deg
ZDOT = -1581
163909 TA = 160
93418
MA = 160
89474
Ha = 220
750 n
mi
Hp = 215
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2864681
95 X = -799551
98
Y = -14252782
75 feet Y = -4353601
10 meter
Z = -16858332
02 Z = -5142482
10
XDOT = 24564
049207 XDOT = 7490
206563
YDOT = 1185
209730 feet/sec YDOT = 444
995198 meter/sec
ZDOT = -5187
545634 ZDOT = -1544
786714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2046274
91 X = -623704
59
Y = 14372887
51 feet Y = 4380856
11 meter
Z = -16875557
50 Z = -5143669
93
XDOT = -21817
480617 XDOT = -6649
968092
YDOT = -8994
514405 feet/sec YDOT = -2741
527991 meter/sec
ZDOT = -5026
513769 ZDOT = -1532
081397
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 17245
51873675
00016717 00000-0 10270-3 0 9031
2 25544 51
6409 12
8207 0004563 219
2033 140
8789 15
54034000 33774
Satellite: ISS
Catalog Number: 25544
Epoch time: 17245
51873675 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 12
8207 deg
Eccentricity:
0004563
Arg of perigee: 219
2033 deg
Mean anomaly: 140
8789 deg
Mean motion: 15
54034000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3377
Checksum: 299
Coasting Arc #5 (Orbit 3383)
---------------------------------------
Vector Time (GMT): 2017/245/21:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2742332
05 A = 6780572
07 meter
Y = 4176765
23 meter E =
0008021
Z = 4582940
17 I = 51
69974
XDOT = -6932
090535 Wp = 144
01526
YDOT = 1191
490229 meter/sec RA = 10
29501 deg
ZDOT = 3053
064022 TA = 275
45038
MA = 275
54187
Ha = 220
469 n
mi
Hp = 215
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8997152
40 X = 2673161
12
Y = 13703298
01 feet Y = 4207045
34 meter
Z = 15035892
94 Z = 4596093
19
XDOT = -22743
079184 XDOT = -6959
729006
YDOT = 3909
088678 feet/sec YDOT = 1113
816494 meter/sec
ZDOT = 10016
614245 ZDOT = 3019
323277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4540461
04 X = -1383932
52
Y = 15696514
38 feet Y = 4784297
58 meter
Z = 15093404
33 Z = 4600469
64
XDOT = -16736
753388 XDOT = -5101
362433
YDOT = -14357
698026 feet/sec YDOT = -4376
226358 meter/sec
ZDOT = 9866
987626 ZDOT = 3007
457828
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 17245
96887827
00016717 00000-0 10270-3 0 9045
2 25544 51
6389 10
5808 0004318 225
2993 134
7809 15
54053466 33843
Satellite: ISS
Catalog Number: 25544
Epoch time: 17245
96887827 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 10
5808 deg
Eccentricity:
0004318
Arg of perigee: 225
2993 deg
Mean anomaly: 134
7809 deg
Mean motion: 15
54053466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3384
Checksum: 342
Coasting Arc #6 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2017/246/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6669176
52 A = 6788961
79 meter
Y = -90856
03 meter E =
0004670
Z = -1254801
91 I = 51
71257
XDOT = 1163
152785 Wp = 33
48309
YDOT = 4817
130418 meter/sec RA = 7
76012 deg
ZDOT = 5847
454656 TA = 312
89269
MA = 312
93188
Ha = 220
653 n
mi
Hp = 215
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21880500
38 X = 6675791
96
Y = -298084
09 feet Y = -16239
84 meter
Z = -4116804
16 Z = -1222389
44
XDOT = 3816
118060 XDOT = 1080
796187
YDOT = 15804
233654 feet/sec YDOT = 4829
677456 meter/sec
ZDOT = 19184
562521 ZDOT = 5852
904500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14842518
88 X = -4523999
75
Y = -16115399
02 feet Y = -4911973
62 meter
Z = -3973257
51 Z = -1211048
89
XDOT = 8132
927393 XDOT = 2478
916269
YDOT = -12214
364219 feet/sec YDOT = -3722
938214 meter/sec
ZDOT = 19207
848826 ZDOT = 5854
552322
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 17246
41902137
00016717 00000-0 10270-3 0 9059
2 25544 51
6402 8
3329 0004499 222
0393 138
0415 15
54039350 33915
Satellite: ISS
Catalog Number: 25544
Epoch time: 17246
41902137 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 8
3329 deg
Eccentricity:
0004499
Arg of perigee: 222
0393 deg
Mean anomaly: 138
0415 deg
Mean motion: 15
54039350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 288
Coasting Arc #7 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2017/247/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6733876
59 A = 6789406
12 meter
Y = -676748
03 meter E =
0011949
Z = -439971
16 I = 51
68191
XDOT = 860
593774 Wp = 159
22184
YDOT = -4703
448753 meter/sec RA = 2
79405 deg
ZDOT = -5997
743797 TA = 25
52104
MA = 25
46210
Ha = 220
393 n
mi
Hp = 215
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22092770
98 X = -6723671
41
Y = -2220301
95 feet Y = -751993
81 meter
Z = -1443474
92 Z = -472656
99
XDOT = 2823
470387 XDOT = 942
258760
YDOT = -15431
262313 feet/sec YDOT = -4693
368870 meter/sec
ZDOT = -19677
637130 ZDOT = -5993
364627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13390460
74 X = 4081412
43
Y = 17699644
81 feet Y = 5394851
74 meter
Z = -1588088
38 Z = -484049
34
XDOT = -12031
516984 XDOT = -3667
206377
YDOT = 7354
824699 feet/sec YDOT = 2241
750568 meter/sec
ZDOT = -19657
422286 ZDOT = -5991
582313
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
44791163
00016717 00000-0 10270-3 0 9069
2 25544 51
6402 3
2040 0004348 227
6828 132
3956 15
54068384 34070
Satellite: ISS
Catalog Number: 25544
Epoch time: 17247
44791163 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 3
2040 deg
Eccentricity:
0004348
Arg of perigee: 227
6828 deg
Mean anomaly: 132
3956 deg
Mean motion: 15
54068384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 303
Coasting Arc #8 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2017/248/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6307088
11 A = 6787573
85 meter
Y = 1399252
12 meter E =
0009844
Z = 2069426
27 I = 51
64423
XDOT = -2820
053135 Wp = 78
43539
YDOT = 4491
988780 meter/sec RA = 357
82502 deg
ZDOT = 5537
140138 TA = 304
45781
MA = 304
55078
Ha = 220
336 n
mi
Hp = 215
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20692546
30 X = 6280920
40
Y = 4590722
18 feet Y = 1469636
17 meter
Z = 6789456
27 Z = 2100000
11
XDOT = -9252
142832 XDOT = -2896
970565
YDOT = 14737
495999 feet/sec YDOT = 4460
023496 meter/sec
ZDOT = 18166
470268 ZDOT = 5523
254091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10988734
78 X = -3349366
36
Y = -18073482
96 feet Y = -5508797
61 meter
Z = 6924582
34 Z = 2110612
70
XDOT = 15803
998709 XDOT = 4817
058807
YDOT = -2647
398198 feet/sec YDOT = -806
926971 meter/sec
ZDOT = 18104
204580 ZDOT = 5518
161556
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
47679575
00016717 00000-0 10270-3 0 9076
2 25544 51
6410 358
0764 0004475 229
6460 130
4302 15
54083462 34234
Satellite: ISS
Catalog Number: 25544
Epoch time: 17248
47679575 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 358
0764 deg
Eccentricity:
0004475
Arg of perigee: 229
6460 deg
Mean anomaly: 130
4302 deg
Mean motion: 15
54083462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 314
Coasting Arc #9 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2017/249/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5400073
46 A = 6784195
75 meter
Y = -2127579
77 meter E =
0002602
Z = -3511894
78 I = 51
60003
XDOT = 4577
463730 Wp = 142
20286
YDOT = -4178
062294 meter/sec RA = 352
84638 deg
ZDOT = -4511
173280 TA = 79
14040
MA = 79
11112
Ha = 220
162 n
mi
Hp = 215
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17716776
44 X = -5358822
03
Y = -6980248
58 feet Y = -2187736
81 meter
Z = -11521964
52 Z = -3538026
01
XDOT = 15017
925623 XDOT = 4645
756609
YDOT = -13707
553459 feet/sec YDOT = -4126
492629 meter/sec
ZDOT = -14800
437271 ZDOT = -4488
771235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7483365
85 X = 2280929
91
Y = 17433775
51 feet Y = 5313814
78 meter
Z = -11637285
38 Z = -3547044
58
XDOT = -19106
742158 XDOT = -5823
735010
YDOT = -1603
126049 feet/sec YDOT = -488
632820 meter/sec
ZDOT = -14700
532693 ZDOT = -4480
722365
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
44137155
00016717 00000-0 10270-3 0 9088
2 25544 51
6409 353
2692 0004429 234
4540 125
6200 15
54059124 34388
Satellite: ISS
Catalog Number: 25544
Epoch time: 17249
44137155 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 353
2692 deg
Eccentricity:
0004429
Arg of perigee: 234
4540 deg
Mean anomaly: 125
6200 deg
Mean motion: 15
54059124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 300
Coasting Arc #10 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2017/250/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4119832
30 A = 6780418
73 meter
Y = 2832221
57 meter E =
0006943
Z = 4579875
60 I = 51
55677
XDOT = -5960
464963 Wp = 145
75104
YDOT = 3748
007128 meter/sec RA = 347
85490 deg
ZDOT = 3036
091087 TA = 273
84115
MA = 273
92053
Ha = 219
947 n
mi
Hp = 216
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13516510
17 X = 4065608
76
Y = 9292065
52 feet Y = 2877989
71 meter
Z = 15025838
60 Z = 4599756
34
XDOT = -19555
331244 XDOT = -6016
680957
YDOT = 12296
611313 feet/sec YDOT = 3681
039184 meter/sec
ZDOT = 9960
928762 ZDOT = 3007
000147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3142437
68 X = -957815
00
Y = -16016423
45 feet Y = -4881805
87 meter
Z = 15113358
98 Z = 4606551
82
XDOT = 21471
976492 XDOT = 6544
658435
YDOT = 5088
542578 feet/sec YDOT = 1550
987778 meter/sec
ZDOT = 9831
500273 ZDOT = 2996
641283
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
47024375
00016717 00000-0 10270-3 0 9093
2 25544 51
6422 348
1408 0004451 239
3651 120
7063 15
54097954 34547
Satellite: ISS
Catalog Number: 25544
Epoch time: 17250
47024375 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 348
1408 deg
Eccentricity:
0004451
Arg of perigee: 239
3651 deg
Mean anomaly: 120
7063 deg
Mean motion: 15
54097954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 304
Coasting Arc #11 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2017/251/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2556958
81 A = 6777942
65 meter
Y = -3534278
20 meter E =
0010147
Z = -5196472
34 I = 51
51643
XDOT = 6871
861853 Wp = 87
62849
YDOT = -3151
475819 meter/sec RA = 342
85338 deg
ZDOT = -1239
616447 TA = 170
45162
MA = 170
43232
Ha = 219
928 n
mi
Hp = 216
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8388972
47 X = -2492005
62
Y = -11595400
92 feet Y = -3562509
31 meter
Z = -17048793
75 Z = -5208735
06
XDOT = 22545
478521 XDOT = 6912
613211
YDOT = -10339
487595 feet/sec YDOT = -3074
402269 meter/sec
ZDOT = -4066
983093 ZDOT = -1206
135725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1906558
47 X = -581119
02
Y = 14119497
89 feet Y = 4303622
96 meter
Z = -17102466
61 Z = -5212831
82
XDOT = -22501
561558 XDOT = -6858
475963
YDOT = -7777
745528 feet/sec YDOT = -2370
656837 meter/sec
ZDOT = -3918
240666 ZDOT = -1194
279755
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
43480741
00016717 00000-0 10270-3 0 9105
2 25544 51
6420 343
3342 0004268 243
4957 116
5758 15
54088023 34697
Satellite: ISS
Catalog Number: 25544
Epoch time: 17251
43480741 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 343
3342 deg
Eccentricity:
0004268
Arg of perigee: 243
4957 deg
Mean anomaly: 116
5758 deg
Mean motion: 15
54088023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 306
Coasting Arc #12 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2017/252/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 874012
15 A = 6777602
91 meter
Y = 4172712
35 meter E =
0001217
Z = 5269839
07 I = 51
48402
XDOT = -7259
553996 Wp = 260
10254
YDOT = 2374
622478 meter/sec RA = 337
84421 deg
ZDOT = -676
578762 TA = 196
37046
MA = 196
37439
Ha = 219
758 n
mi
Hp = 216
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2867493
94 X = 801688
42
Y = 13690001
13 feet Y = 4182082
36 meter
Z = 17289498
27 Z = 5273908
63
XDOT = -23817
434371 XDOT = -7282
281609
YDOT = 7790
756160 feet/sec YDOT = 2293
314041 meter/sec
ZDOT = -2219
746593 ZDOT = -711
899033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7161018
07 X = 2182678
31
Y = -11989997
85 feet Y = -3654551
34 meter
Z = 17306795
63 Z = 5275111
31
XDOT = 21987
873299 XDOT = 6701
903782
YDOT = 9703
541495 feet/sec YDOT = 2957
639448 meter/sec
ZDOT = -2376
483214 ZDOT = -724
352084
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
46366909
00016717 00000-0 10270-3 0 9119
2 25544 51
6416 338
2055 0004269 247
8281 112
2419 15
54100410 34855
Satellite: ISS
Catalog Number: 25544
Epoch time: 17252
46366909 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 338
2055 deg
Eccentricity:
0004269
Arg of perigee: 247
8281 deg
Mean anomaly: 112
2419 deg
Mean motion: 15
54100410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 298
Coasting Arc #13 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2017/253/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 796736
98 A = 6779578
67 meter
Y = -4716899
10 meter E =
0008451
Z = -4811979
94 I = 51
46141
XDOT = 7099
615696 Wp = 125
55283
YDOT = -1380
552569 meter/sec RA = 332
83634 deg
ZDOT = 2527
101962 TA = 169
39809
MA = 169
38027
Ha = 219
709 n
mi
Hp = 216
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2613966
48 X = 872797
79
Y = -15475390
76 feet Y = -4707564
65 meter
Z = -15787335
77 Z = -4807924
40
XDOT = 23292
702416 XDOT = 7102
250235
YDOT = -4529
371944 feet/sec YDOT = -1301
144843 meter/sec
ZDOT = 8291
016935 ZDOT = 2561
596466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12245078
24 X = -3732299
85
Y = 9847355
64 feet Y = 3001474
00 meter
Z = -15768581
31 Z = -4806263
58
XDOT = -19742
011451 XDOT = -6017
365090
YDOT = -11018
878615 feet/sec YDOT = -3358
554202 meter/sec
ZDOT = 8443
916418 ZDOT = 2573
705724
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
42822146
00016717 00000-0 10270-3 0 9127
2 25544 51
6421 333
3986 0004257 250
9572 109
1119 15
54118077 35003
Satellite: ISS
Catalog Number: 25544
Epoch time: 17253
42822146 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 333
3986 deg
Eccentricity:
0004257
Arg of perigee: 250
9572 deg
Mean anomaly: 109
1119 deg
Mean motion: 15
54118077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 294
Coasting Arc #14 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2017/254/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2318084
54 A = 6783216
82 meter
Y = 5079318
48 meter E =
0007326
Z = 3846234
52 I = 51
44451
XDOT = -6462
779762 Wp = 85
94652
YDOT = 180
148712 meter/sec RA = 327
83299 deg
ZDOT = -4125
648301 TA = 47
54746
MA = 47
48555
Ha = 219
734 n
mi
Hp = 216
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7605264
24 X = -2393393
81
Y = 16664430
72 feet Y = 5052975
31 meter
Z = 12618879
67 Z = 3834790
57
XDOT = -21203
345675 XDOT = -6444
273370
YDOT = 591
039080 feet/sec YDOT = 107
980644 meter/sec
ZDOT = -13535
591540 ZDOT = -4156
997790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16635562
53 X = 5070519
46
Y = -7752335
20 feet Y = -2362911
77 meter
Z = 12567369
56 Z = 3830534
24
XDOT = 15930
848445 XDOT = 4855
722606
YDOT = 11979
039013 feet/sec YDOT = 3651
211091 meter/sec
ZDOT = -13674
359090 ZDOT = -4167
944650
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
45707205
00016717 00000-0 10270-3 0 9130
2 25544 51
6420 328
2697 0004115 255
0320 105
0377 15
54089900 35164
Satellite: ISS
Catalog Number: 25544
Epoch time: 17254
45707205 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 328
2697 deg
Eccentricity:
0004115
Arg of perigee: 255
0320 deg
Mean anomaly: 105
0377 deg
Mean motion: 15
54089900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 288
Coasting Arc #15 (Orbit 3530)
---------------------------------------
Vector Time (GMT): 2017/255/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3570625
85 A = 6786860
28 meter
Y = -5202418
12 meter E =
0002986
Z = -2494371
17 I = 51
42967
XDOT = 5420
028383 Wp = 356
27110
YDOT = 1184
920459 meter/sec RA = 322
83857 deg
ZDOT = 5289
844268 TA = 335
68106
MA = 335
69515
Ha = 219
566 n
mi
Hp = 216
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11714651
74 X = 3640651
80
Y = -17068300
90 feet Y = -5162097
56 meter
Z = -8183632
44 Z = -2476855
66
XDOT = 17782
245351 XDOT = 5380
679824
YDOT = 3887
534315 feet/sec YDOT = 1245
311229 meter/sec
ZDOT = 17355
132114 ZDOT = 5316
077607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19914173
66 X = -6069840
13
Y = 5767373
96 feet Y = 1757895
58 meter
Z = -8105238
19 Z = -2470476
60
XDOT = -10797
321986 XDOT = -3291
023741
YDOT = -12740
939766 feet/sec YDOT = -3883
438441 meter/sec
ZDOT = 17471
022283 ZDOT = 5325
167592
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
42161399
00016717 00000-0 10270-3 0 9147
2 25544 51
6421 323
4621 0004255 262
0199 98
0470 15
54086797 35319
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
42161399 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 323
4621 deg
Eccentricity:
0004255
Arg of perigee: 262
0199 deg
Mean anomaly: 98
0470 deg
Mean motion: 15
54086797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3531
Checksum: 310
Coasting Arc #16 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2017/255/21:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 909986
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3205199
64 A = 6777398
29 meter
Y = 2812443
49 meter E =
0002028
Z = 5269328
99 I = 51
38502
XDOT = -5580
329060 Wp = 232
45288
YDOT = 5223
651422 meter/sec RA = 320
51695 deg
ZDOT = 605
256944 TA = 211
74283
MA = 211
75505
Ha = 219
299 n
mi
Hp = 216
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10515746
85 X = 3147915
98
Y = 9227176
81 feet Y = 2847966
22 meter
Z = 17287824
76 Z = 5284759
64
XDOT = -18308
166206 XDOT = -5641
266632
YDOT = 17137
963982 feet/sec YDOT = 5160
907690 meter/sec
ZDOT = 1985
751130 ZDOT = 578
001002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -272174
13 X = -82958
68
Y = 13903182
94 feet Y = 4237690
16 meter
Z = 17355634
06 Z = 5289997
26
XDOT = -23914
401713 XDOT = -7289
109642
YDOT = -2799
636663 feet/sec YDOT = -853
329255 meter/sec
ZDOT = 1864
252225 ZDOT = 568
224078
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
93603514
00016717 00000-0 10270-3 0 9154
2 25544 51
6405 320
9010 0004236 268
8872 91
1795 15
54148200 35396
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
93603514 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 320
9010 deg
Eccentricity:
0004236
Arg of perigee: 268
8872 deg
Mean anomaly: 91
1795 deg
Mean motion: 15
54148200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 304
Coasting Arc #17 (Orbit 3541)
---------------------------------------
Vector Time (GMT): 2017/256/02:57:42
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2957693
55 A = 6786179
49 meter
Y = -5447387
56 meter E =
0002502
Z = -2758517
30 I = 51
40674
XDOT = 5685
907001 Wp = 353
94322
YDOT = 496
828025 meter/sec RA = 319
30415 deg
ZDOT = 5117
355061 TA = 334
71135
MA = 334
72359
Ha = 219
450 n
mi
Hp = 216
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9703719
00 X = 3031787
45
Y = -17872006
42 feet Y = -5413898
47 meter
Z = -9050253
60 Z = -2743969
43
XDOT = 18654
550527 XDOT = 5655
071041
YDOT = 1630
013207 feet/sec YDOT = 560
239568 meter/sec
ZDOT = 16789
222642 ZDOT = 5144
900628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2556672
98 X = -779273
93
Y = -20204253
67 feet Y = -6158256
52 meter
Z = -8984955
37 Z = -2738614
40
XDOT = 14511
904102 XDOT = 4423
228370
YDOT = -9353
836007 feet/sec YDOT = -2851
049215 meter/sec
ZDOT = 16911
035047 ZDOT = 5154
483482
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
12894216
00016717 00000-0 10270-3 0 9168
2 25544 51
6393 319
9376 0004311 268
7301 91
3357 15
54117362 35420
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
12894216 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 319
9376 deg
Eccentricity:
0004311
Arg of perigee: 268
7301 deg
Mean anomaly: 91
3357 deg
Mean motion: 15
54117362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3542
Checksum: 312
Coasting Arc #18 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2017/256/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2048486
51 A = 6785039
19 meter
Y = -5629165
54 meter E =
0001203
Z = -3185251
23 I = 51
38629
XDOT = 5961
576572 Wp = 13
02424
YDOT = -538
989855 meter/sec RA = 315
12754 deg
ZDOT = 4788
025230 TA = 310
04481
MA = 310
05537
Ha = 219
471 n
mi
Hp = 216
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6720756
26 X = 2126753
49
Y = -18468390
87 feet Y = -5605820
50 meter
Z = -10450299
31 Z = -3175109
94
XDOT = 19558
978254 XDOT = 5943
902722
YDOT = -1768
339418 feet/sec YDOT = -472
422034 meter/sec
ZDOT = 15708
744192 ZDOT = 4816
941846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13401926
21 X = 4084907
11
Y = -14408123
04 feet Y = -4391595
90 meter
Z = -10404477
20 Z = -3171284
65
XDOT = 17575
130985 XDOT = 5356
899924
YDOT = 4915
184627 feet/sec YDOT = 1498
148274 meter/sec
ZDOT = 15836
796971 ZDOT = 4827
055717
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
96487479
00016717 00000-0 10270-3 0 9170
2 25544 51
6427 315
7724 0004177 273
3752 86
6923 15
54136968 35554
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
96487479 = yrday
fracday
Element set: 917
Inclination: 51
6427 deg
RA of node: 315
7724 deg
Eccentricity:
0004177
Arg of perigee: 273
3752 deg
Mean anomaly: 86
6923 deg
Mean motion: 15
54136968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 358
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