[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 11th 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
255/21:17:02
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 216
1
256/02:57:42
000 0
0 0
0 0
0
N/A 0
0 0
0 219
4
000/00:00:00
000 0
0 0
0 216
2
256/23:24:00
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
0
260/08:47:00
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
0
261/05:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
9
Coasting Arc #1 (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 = -4759764
28 A = 6779997
29 meter
Y = -1353195
68 meter E =
0006449
Z = -4641237
99 I = 51
43160
XDOT = 4407
893770 Wp = 64
22052
YDOT = -5556
083335 meter/sec RA = 327
46217 deg
ZDOT = -2900
934604 TA = 176
82094
MA = 176
81684
Ha = 219
454 n
mi
Hp = 216
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15616024
53 X = -4721733
69
Y = -4439618
36 feet Y = -1406210
33 meter
Z = -15227158
76 Z = -4664267
15
XDOT = 14461
593734 XDOT = 4483
787194
YDOT = -18228
619867 feet/sec YDOT = -5506
367147 meter/sec
ZDOT = -9517
501982 ZDOT = -2879
337482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14488216
56 X = 4416008
41
Y = 7110199
57 feet Y = 2167188
83 meter
Z = -15328843
41 Z = -4672231
47
XDOT = -16995
185212 XDOT = -5180
132453
YDOT = 14322
698825 feet/sec YDOT = 4365
558602 meter/sec
ZDOT = -9420
978443 ZDOT = -2871
514229
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
52119098
00016717 00000-0 10270-3 0 9001
2 25544 51
6413 327
9490 0004237 259
4311 100
6365 15
54157674 35179
Satellite: ISS
Catalog Number: 25544
Epoch time: 17254
52119098 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 327
9490 deg
Eccentricity:
0004237
Arg of perigee: 259
4311 deg
Mean anomaly: 100
6365 deg
Mean motion: 15
54157674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3517
Checksum: 304
Coasting Arc #2 (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 = 3490867
80 A = 6777490
92 meter
Y = 2566227
98 meter E =
0002676
Z = 5213118
55 I = 51
39657
XDOT = -5465
692780 Wp = 204
23178
YDOT = 5271
762903 meter/sec RA = 322
44974 deg
ZDOT = 1062
702949 TA = 235
54031
MA = 235
56560
Ha = 219
242 n
mi
Hp = 216
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11452978
33 X = 3436589
17
Y = 8419383
13 feet Y = 2604962
07 meter
Z = 17103407
32 Z = 5229944
22
XDOT = -17932
062926 XDOT = -5529
398933
YDOT = 17295
810048 feet/sec YDOT = 5210
285663 meter/sec
ZDOT = 3486
558230 ZDOT = 1035
997090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9851521
21 X = -3002743
67
Y = -10122581
21 feet Y = -3085362
75 meter
Z = 17177431
30 Z = 5235681
06
XDOT = 19746
343984 XDOT = 6018
685646
YDOT = -13490
963737 feet/sec YDOT = -4112
045747 meter/sec
ZDOT = 3367
482492 ZDOT = 1026
408664
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
54999143
00016717 00000-0 10270-3 0 9012
2 25544 51
6413 322
8203 0004231 263
8940 96
1730 15
54199624 35330
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
54999143 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 322
8203 deg
Eccentricity:
0004231
Arg of perigee: 263
8940 deg
Mean anomaly: 96
1730 deg
Mean motion: 15
54199624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3533
Checksum: 306
Coasting Arc #3 (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 = 3087825
19 A = 6777156
57 meter
Y = 2920505
63 meter E =
0001864
Z = 5280306
13 I = 51
38470
XDOT = -5664
020573 Wp = 242
86505
YDOT = 5147
652422 meter/sec RA = 320
51207 deg
ZDOT = 464
370876 TA = 202
68549
MA = 202
69373
Ha = 219
213 n
mi
Hp = 216
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10130660
07 X = 3029288
56
Y = 9581711
39 feet Y = 2954708
79 meter
Z = 17323839
00 Z = 5295163
56
XDOT = -18582
744663 XDOT = -5723
417726
YDOT = 16888
623433 feet/sec YDOT = 5083
981400 meter/sec
ZDOT = 1523
526497 ZDOT = 436
712130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -791961
42 X = -241389
84
Y = 13840053
95 feet Y = 4218448
44 meter
Z = 17389093
36 Z = 5300195
66
XDOT = -23905
453974 XDOT = -7286
382371
YDOT = -3130
164064 feet/sec YDOT = -954
074007 meter/sec
ZDOT = 1400
257941 ZDOT = 426
798620
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
93579164
00016717 00000-0 10270-3 0 9023
2 25544 51
6404 320
8989 0004191 270
3858 89
6815 15
54215159 35394
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
93579164 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 320
8989 deg
Eccentricity:
0004191
Arg of perigee: 270
3858 deg
Mean anomaly: 89
6815 deg
Mean motion: 15
54215159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 341
Coasting Arc #4 (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 = 3080019
19 A = 6786240
25 meter
Y = -5434893
74 meter E =
0003026
Z = -2646363
79 I = 51
40746
XDOT = 5602
250895 Wp = 355
20691
YDOT = 647
659285 meter/sec RA = 319
30094 deg
ZDOT = 5192
697268 TA = 334
85518
MA = 334
86991
Ha = 219
361 n
mi
Hp = 216
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10105049
83 X = 3153419
49
Y = -17831016
22 feet Y = -5400040
60 meter
Z = -8682295
89 Z = -2631223
38
XDOT = 18380
088237 XDOT = 5569
368540
YDOT = 2124
866420 feet/sec YDOT = 710
123889 meter/sec
ZDOT = 17036
408361 ZDOT = 5219
831480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2209336
09 X = -673405
64
Y = -20404675
08 feet Y = -6219344
97 meter
Z = -8614377
64 Z = -2625662
31
XDOT = 14563
414759 XDOT = 4438
928818
YDOT = -8816
362492 feet/sec YDOT = -2687
227288 meter/sec
ZDOT = 17156
374927 ZDOT = 5229
263078
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
12869025
00016717 00000-0 10270-3 0 9034
2 25544 51
6392 319
9354 0004267 270
1469 89
9195 15
54184668 35423
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
12869025 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 319
9354 deg
Eccentricity:
0004267
Arg of perigee: 270
1469 deg
Mean anomaly: 89
9195 deg
Mean motion: 15
54184668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3542
Checksum: 341
Coasting Arc #5 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2017/256/23:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5078230
58 A = 6780489
49 meter
Y = 4839
30 meter E =
0005103
Z = 4490982
12 I = 51
37133
XDOT = -2816
741732 Wp = 125
90159
YDOT = 6388
184656 meter/sec RA = 315
08759 deg
ZDOT = 3172
707286 TA = 292
09344
MA = 292
14762
Ha = 219
301 n
mi
Hp = 216
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16660861
49 X = 5055984
03
Y = 15876
98 feet Y = 61503
37 meter
Z = 14734193
31 Z = 4515596
58
XDOT = -9241
278647 XDOT = -2903
378234
YDOT = 20958
611075 feet/sec YDOT = 6356
201668 meter/sec
ZDOT = 10409
144640 ZDOT = 3158
813684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15857978
62 X = 4833511
88
Y = 4784078
19 feet Y = 1458187
03 meter
Z = 14843116
92 Z = 4524182
04
XDOT = -14599
396830 XDOT = -4449
896154
YDOT = 16236
506448 feet/sec YDOT = 4948
887165 meter/sec
ZDOT = 10346
590440 ZDOT = 3153
640766
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
02888614
00016717 00000-0 10270-3 0 9040
2 25544 51
6428 315
4495 0004064 275
3902 84
6787 15
54181985 35567
Satellite: ISS
Catalog Number: 25544
Epoch time: 17257
02888614 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 315
4495 deg
Eccentricity:
0004064
Arg of perigee: 275
3902 deg
Mean anomaly: 84
6787 deg
Mean motion: 15
54181985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 341
Coasting Arc #6 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2017/257/23:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150096
85 A = 6777668
48 meter
Y = -1478670
00 meter E =
0010189
Z = -5159481
27 I = 51
33936
XDOT = 3972
136389 Wp = 71
35858
YDOT = -6408
697109 meter/sec RA = 310
07161 deg
ZDOT = -1357
365488 TA = 185
52114
MA = 185
53238
Ha = 219
409 n
mi
Hp = 215
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13615803
32 X = -4108191
38
Y = -4851279
54 feet Y = -1524845
18 meter
Z = -16927432
00 Z = -5179539
23
XDOT = 13031
943533 XDOT = 4050
098322
YDOT = -21025
909150 feet/sec YDOT = -6363
842133 meter/sec
ZDOT = -4453
298846 ZDOT = -1337
880444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11681312
87 X = -3560464
16
Y = -8334713
39 feet Y = -2540420
64 meter
Z = -17015946
92 Z = -5186460
62
XDOT = 17668
022722 XDOT = 5385
213326
YDOT = -15842
057999 feet/sec YDOT = -4828
659278 meter/sec
ZDOT = -4366
009409 ZDOT = -1330
759668
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
99337396
00016717 00000-0 10270-3 0 9053
2 25544 51
6423 310
6413 0004133 280
4002 79
6685 15
54221990 35713
Satellite: ISS
Catalog Number: 25544
Epoch time: 17257
99337396 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 310
6413 deg
Eccentricity:
0004133
Arg of perigee: 280
4002 deg
Mean anomaly: 79
6685 deg
Mean motion: 15
54221990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 310
Coasting Arc #7 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2017/258/23:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3059084
06 A = 6777187
47 meter
Y = 2978809
81 meter E =
0002596
Z = 5264407
32 I = 51
31699
XDOT = -4775
163404 Wp = 326
72509
YDOT = 5969
302860 meter/sec RA = 305
04975 deg
ZDOT = -600
886870 TA = 129
04798
MA = 129
02487
Ha = 219
318 n
mi
Hp = 216
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10036365
04 X = 2999975
11
Y = 9772998
08 feet Y = 3012688
44 meter
Z = 17271677
55 Z = 5279123
54
XDOT = -15666
546600 XDOT = -4838
640040
YDOT = 19584
326967 feet/sec YDOT = 5915
548767 meter/sec
ZDOT = -1971
413617 ZDOT = -624
237572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7105785
27 X = 2165843
35
Y = 11979611
42 feet Y = 3651385
56 meter
Z = 17336311
20 Z = 5284107
65
XDOT = -19251
933513 XDOT = -5867
989335
YDOT = 14432
711425 feet/sec YDOT = 4399
090442 meter/sec
ZDOT = -2075
723010 ZDOT = -632
680374
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
02215785
00016717 00000-0 10270-3 0 9067
2 25544 51
6418 305
5127 0004185 282
9342 77
1344 15
54229326 35876
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
02215785 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 305
5127 deg
Eccentricity:
0004185
Arg of perigee: 282
9342 deg
Mean anomaly: 77
1344 deg
Mean motion: 15
54229326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 317
Coasting Arc #8 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2017/259/23:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1923244
42 A = 6779177
31 meter
Y = -4376910
10 meter E =
0007295
Z = -4813280
40 I = 51
30542
XDOT = 5214
097330 Wp = 108
07700
YDOT = -5031
194718 meter/sec RA = 300
02803 deg
ZDOT = 2492
568699 TA = 186
55013
MA = 186
55967
Ha = 219
466 n
mi
Hp = 215
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6309857
03 X = -1850777
33
Y = -14359941
26 feet Y = -4398012
36 meter
Z = -15791602
35 Z = -4822446
45
XDOT = 17106
618537 XDOT = 5257
862377
YDOT = -16506
544351 feet/sec YDOT = -4972
642200 meter/sec
ZDOT = 8177
718829 ZDOT = 2518
003722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2609016
27 X = -795228
16
Y = -15425787
70 feet Y = -4701780
09 meter
Z = -15831456
71 Z = -4825428
00
XDOT = 19366
798498 XDOT = 5903
000182
YDOT = -11781
676637 feet/sec YDOT = -3591
055039 meter/sec
ZDOT = 8291
084413 ZDOT = 2527
122529
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
98663973
00016717 00000-0 10270-3 0 9079
2 25544 51
6416 300
7041 0004268 287
3983 72
6703 15
54227592 36028
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
98663973 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 300
7041 deg
Eccentricity:
0004268
Arg of perigee: 287
3983 deg
Mean anomaly: 72
6703 deg
Mean motion: 15
54227592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 331
Coasting Arc #9 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2017/260/08:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 351771
76 A = 6784931
02 meter
Y = -6003373
74 meter E =
0002050
Z = -3139696
95 I = 51
31808
XDOT = 5542
659867 Wp = 8
61926
YDOT = -2194
531840 meter/sec RA = 298
06216 deg
ZDOT = 4819
535564 TA = 315
01962
MA = 315
03622
Ha = 219
454 n
mi
Hp = 216
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1154106
83 X = 434127
94
Y = -19696108
07 feet Y = -5998979
81 meter
Z = -10300843
00 Z = -3137787
55
XDOT = 18184
579616 XDOT = 5543
376992
YDOT = -7199
907612 feet/sec YDOT = -2132
545562 meter/sec
ZDOT = 15812
124554 ZDOT = 4846
461843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16396500
56 X = -4997653
37
Y = 10982587
57 feet Y = 3347492
69 meter
Z = -10291430
51 Z = -3136828
02
XDOT = -15893
130256 XDOT = -4844
226102
YDOT = -8806
083358 feet/sec YDOT = -2684
094208 meter/sec
ZDOT = 15931
628152 ZDOT = 4855
960261
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 17260
37243091
00016717 00000-0 10270-3 0 9080
2 25544 51
6416 298
7779 0004199 283
3312 76
7372 15
54205557 36087
Satellite: ISS
Catalog Number: 25544
Epoch time: 17260
37243091 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 298
7779 deg
Eccentricity:
0004199
Arg of perigee: 283
3312 deg
Mean anomaly: 76
7372 deg
Mean motion: 15
54205557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 331
Coasting Arc #10 (Orbit 3621)
---------------------------------------
Vector Time (GMT): 2017/261/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1655348
15 A = 6781030
36 meter
Y = 4919697
90 meter E =
0006727
Z = 4361216
46 I = 51
29041
XDOT = -5027
845700 Wp = 51
89729
YDOT = 4698
374271 meter/sec RA = 293
72970 deg
ZDOT = -3384
006563 TA = 72
57774
MA = 72
50421
Ha = 219
588 n
mi
Hp = 215
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5430932
26 X = 1579027
23
Y = 16140741
15 feet Y = 4937782
89 meter
Z = 14308452
96 Z = 4369071
65
XDOT = -16495
556759 XDOT = -5063
572744
YDOT = 15414
613750 feet/sec YDOT = 4641
949324 meter/sec
ZDOT = -11102
383738 ZDOT = -3408
517440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16845581
36 X = 5134533
20
Y = -2295941
86 feet Y = -699803
08 meter
Z = 14342434
10 Z = 4371573
91
XDOT = 11984
120980 XDOT = 3652
760075
YDOT = 17735
168782 feet/sec YDOT = 5405
679445 meter/sec
ZDOT = -11211
588197 ZDOT = -3417
292082
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
27260958
00016717 00000-0 10270-3 0 9092
2 25544 51
6397 294
2876 0003828 285
7620 74
3110 15
54194495 36228
Satellite: ISS
Catalog Number: 25544
Epoch time: 17261
27260958 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 294
2876 deg
Eccentricity:
0003828
Arg of perigee: 285
7620 deg
Mean anomaly: 74
3110 deg
Mean motion: 15
54194495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3622
Checksum: 334
Coasting Arc #11 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2017/262/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -652548
10 A = 6784846
52 meter
Y = -5966955
75 meter E =
0002460
Z = -3160721
55 I = 51
29078
XDOT = 5111
360538 Wp = 16
43110
YDOT = -3099
474969 meter/sec RA = 288
71965 deg
ZDOT = 4799
298949 TA = 306
90788
MA = 306
93042
Ha = 219
633 n
mi
Hp = 215
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2140905
84 X = -570422
32
Y = -19576626
48 feet Y = -5973794
21 meter
Z = -10369821
35 Z = -3163691
17
XDOT = 16769
555572 XDOT = 5122
327231
YDOT = -10168
881132 feet/sec YDOT = -3042
254307 meter/sec
ZDOT = 15745
731461 ZDOT = 4824
155316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19650091
93 X = -5989348
02
Y = -1203436
55 feet Y = -366807
46 meter
Z = -10382032
78 Z = -3164443
59
XDOT = -7349
872171 XDOT = -2240
241038
YDOT = -16688
757970 feet/sec YDOT = -5086
733429 meter/sec
ZDOT = 15856
201057 ZDOT = 4832
970082
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 17262
23708015
00016717 00000-0 10270-3 0 9102
2 25544 51
6394 289
4795 0003992 290
6266 69
4458 15
54209162 36378
Satellite: ISS
Catalog Number: 25544
Epoch time: 17262
23708015 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 289
4795 deg
Eccentricity:
0003992
Arg of perigee: 290
6266 deg
Mean anomaly: 69
4458 deg
Mean motion: 15
54209162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 334
Coasting Arc #12 (Orbit 3652)
---------------------------------------
Vector Time (GMT): 2017/263/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -290102
22 A = 6787967
36 meter
Y = 6585941
71 meter E =
0009983
Z = 1597291
17 I = 51
29203
XDOT = -4990
557333 Wp = 118
59355
YDOT = 1168
992016 meter/sec RA = 283
71845 deg
ZDOT = -5703
869401 TA = 43
84269
MA = 43
76349
Ha = 219
685 n
mi
Hp = 215
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -951778
94 X = -371485
28
Y = 21607420
30 feet Y = 6582242
77 meter
Z = 5240456
60 Z = 1595683
36
XDOT = -16373
219597 XDOT = -4975
551771
YDOT = 3835
275643 feet/sec YDOT = 1113
267303 meter/sec
ZDOT = -18713
482287 ZDOT = -5728
075720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21220155
03 X = 6467903
25
Y = 4192445
41 feet Y = 1277857
36 meter
Z = 5232332
45 Z = 1594814
93
XDOT = 1677
143039 XDOT = 511
193198
YDOT = 15092
431026 feet/sec YDOT = 4600
172977 meter/sec
ZDOT = -18820
769302 ZDOT = -5736
570483
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 17263
26584526
00016717 00000-0 10270-3 0 9116
2 25544 51
6396 284
3500 0003949 292
8495 67
2240 15
54226367 36537
Satellite: ISS
Catalog Number: 25544
Epoch time: 17263
26584526 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 284
3500 deg
Eccentricity:
0003949
Arg of perigee: 292
8495 deg
Mean anomaly: 67
2240 deg
Mean motion: 15
54226367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3653
Checksum: 327
Coasting Arc #13 (Orbit 3668)
---------------------------------------
Vector Time (GMT): 2017/264/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1125322
68 A = 6789005
19 meter
Y = -6686688
91 meter E =
0011847
Z = 122579
96 I = 51
28983
XDOT = 4712
619375 Wp = 28
18328
YDOT = 906
954210 meter/sec RA = 278
72281 deg
ZDOT = 5983
778345 TA = 333
14400
MA = 333
20528
Ha = 219
820 n
mi
Hp = 215
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3692003
53 X = 1199415
94
Y = -21937955
75 feet Y = -6673690
49 meter
Z = 402165
23 Z = 128227
37
XDOT = 15461
349656 XDOT = 4673
060902
YDOT = 2975
571554 feet/sec YDOT = 959
433599 meter/sec
ZDOT = 19631
818716 ZDOT = 6006
574695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21259871
18 X = -6480008
74
Y = -6549891
73 feet Y = -1996407
00 meter
Z = 428164
78 Z = 130504
63
XDOT = 4495
337789 XDOT = 1370
178958
YDOT = -13255
510022 feet/sec YDOT = -4040
279455 meter/sec
ZDOT = 19732
548208 ZDOT = 6014
480694
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 17264
29460492
00016717 00000-0 10270-3 0 9126
2 25544 51
6406 279
2205 0003921 300
4068 59
6697 15
54238592 36697
Satellite: ISS
Catalog Number: 25544
Epoch time: 17264
29460492 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 279
2205 deg
Eccentricity:
0003921
Arg of perigee: 300
4068 deg
Mean anomaly: 59
6697 deg
Mean motion: 15
54238592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3669
Checksum: 327
Coasting Arc #14 (Orbit 3683)
---------------------------------------
Vector Time (GMT): 2017/265/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1894353
55 A = 6787499
97 meter
Y = 6247227
25 meter E =
0003674
Z = -1851381
24 I = 51
28033
XDOT = -4308
842412 Wp = 160
96472
YDOT = -2965
263986 meter/sec RA = 273
72683 deg
ZDOT = -5603
578195 TA = 39
50419
MA = 39
47741
Ha = 219
888 n
mi
Hp = 215
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6215070
69 X = -1955077
73
Y = 20496152
39 feet Y = 6225703
51 meter
Z = -6074085
44 Z = -1860731
84
XDOT = -14136
622088 XDOT = -4248
144114
YDOT = -9728
556385 feet/sec YDOT = -3013
109777 meter/sec
ZDOT = -18384
442897 ZDOT = -5624
361571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19651302
43 X = 5989716
98
Y = 8487045
41 feet Y = 2586851
44 meter
Z = -6116392
19 Z = -1864276
34
XDOT = -10655
777604 XDOT = -3247
881014
YDOT = 11373
157956 feet/sec YDOT = 3466
538545 meter/sec
ZDOT = -18475
958581 ZDOT = -5631
472176
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 17265
25906286
00016717 00000-0 10270-3 0 9130
2 25544 51
6399 274
4121 0003912 302
5207 57
5567 15
54249843 36841
Satellite: ISS
Catalog Number: 25544
Epoch time: 17265
25906286 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 274
4121 deg
Eccentricity:
0003912
Arg of perigee: 302
5207 deg
Mean anomaly: 57
5567 deg
Mean motion: 15
54249843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3684
Checksum: 325
Coasting Arc #15 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2017/266/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2577589
70 A = 6784048
93 meter
Y = -5293175
60 meter E =
0009636
Z = 3360044
08 I = 51
26884
XDOT = 3812
214044 Wp = 75
46174
YDOT = 4793
899800 meter/sec RA = 268
72310 deg
ZDOT = 4618
746434 TA = 323
98821
MA = 324
05309
Ha = 219
848 n
mi
Hp = 215
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8456659
12 X = 2620266
19
Y = -17366061
68 feet Y = -5264112
20 meter
Z = 11023766
66 Z = 3372669
66
XDOT = 12507
263923 XDOT = 3735
888177
YDOT = 15728
017718 feet/sec YDOT = 4836
104384 meter/sec
ZDOT = 15153
367564 ZDOT = 4637
079226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16463056
00 X = -5017939
47
Y = -10040460
48 feet Y = -3060332
35 meter
Z = 11080413
05 Z = 3377309
90
XDOT = 16133
956441 XDOT = 4917
629923
YDOT = -9611
196422 feet/sec YDOT = -2929
492669 meter/sec
ZDOT = 15233
775101 ZDOT = 4643
254651
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 17266
28781289
00016717 00000-0 10270-3 0 9149
2 25544 51
6408 269
2827 0003905 306
2381 53
8410 15
54280164 37009
Satellite: ISS
Catalog Number: 25544
Epoch time: 17266
28781289 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 269
2827 deg
Eccentricity:
0003905
Arg of perigee: 306
2381 deg
Mean anomaly: 53
8410 deg
Mean motion: 15
54280164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 312
Coasting Arc #16 (Orbit 3714)
---------------------------------------
Vector Time (GMT): 2017/267/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3214845
75 A = 6780253
98 meter
Y = 3912814
19 meter E =
0008554
Z = -4516981
07 I = 51
25786
XDOT = -3199
607453 Wp = 45
46546
YDOT = -6225
690230 meter/sec RA = 263
70905 deg
ZDOT = -3113
500371 TA = 193
12012
MA = 193
14238
Ha = 220
086 n
mi
Hp = 215
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10547394
19 X = -3236419
37
Y = 12837316
89 feet Y = 3876742
48 meter
Z = -14819491
70 Z = -4532650
82
XDOT = -10497
399781 XDOT = -3114
628268
YDOT = -20425
492880 feet/sec YDOT = -6260
995612 meter/sec
ZDOT = -10214
896229 ZDOT = -3128
836197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11952578
63 X = 3643145
97
Y = 11450031
69 feet Y = 3489969
66 meter
Z = -14889398
97 Z = -4538288
81
XDOT = -20365
210761 XDOT = -6207
316240
YDOT = 7879
243437 feet/sec YDOT = 2401
593400 meter/sec
ZDOT = -10281
842457 ZDOT = -3133
905581
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 17267
25226265
00016717 00000-0 10270-3 0 9156
2 25544 51
6410 264
4744 0004039 310
2324 49
8475 15
54250732 37158
Satellite: ISS
Catalog Number: 25544
Epoch time: 17267
25226265 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 264
4744 deg
Eccentricity:
0004039
Arg of perigee: 310
2324 deg
Mean anomaly: 49
8475 deg
Mean motion: 15
54250732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3715
Checksum: 298
Coasting Arc #17 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2017/268/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3781246
05 A = 6777399
78 meter
Y = -2226085
82 meter E =
0000798
Z = 5164619
89 I = 51
25361
XDOT = 2471
297132 Wp = 51
42778
YDOT = 7148
160159 meter/sec RA = 258
68519 deg
ZDOT = 1272
053340 TA = 26
29600
MA = 26
29195
Ha = 220
009 n
mi
Hp = 215
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12405662
89 X = 3780770
18
Y = -7303431
17 feet Y = -2183803
52 meter
Z = 16944290
99 Z = 5182987
31
XDOT = 8107
930223 XDOT = 2385
001736
YDOT = 23451
969027 feet/sec YDOT = 7175
313502 meter/sec
ZDOT = 4173
403348 ZDOT = 1283
848021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6507911
17 X = -1983611
33
Y = -12732470
79 feet Y = -3880857
10 meter
Z = 17025887
81 Z = 5189490
60
XDOT = 22988
950915 XDOT = 7007
032239
YDOT = -6102
739845 feet/sec YDOT = -1860
115105 meter/sec
ZDOT = 4224
558668 ZDOT = 1287
645482
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 17268
28100224
00016717 00000-0 10270-3 0 9167
2 25544 51
6412 259
3451 0004060 315
6118 44
4709 15
54298588 37312
Satellite: ISS
Catalog Number: 25544
Epoch time: 17268
28100224 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 259
3451 deg
Eccentricity:
0004060
Arg of perigee: 315
6118 deg
Mean anomaly: 44
4709 deg
Mean motion: 15
54298588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 303
Coasting Arc #18 (Orbit 3745)
---------------------------------------
Vector Time (GMT): 2017/269/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4272241
56 A = 6777084
28 meter
Y = 413739
39 meter E =
0012036
Z = -5254756
70 I = 51
25886
XDOT = -1592
822479 Wp = 81
76468
YDOT = -7459
025740 meter/sec RA = 253
65783 deg
ZDOT = 710
802161 TA = 195
04981
MA = 195
08565
Ha = 220
272 n
mi
Hp = 215
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14016540
54 X = -4251025
23
Y = 1357412
71 feet Y = 366082
47 meter
Z = -17240015
41 Z = -5275458
68
XDOT = -5225
795535 XDOT = -1512
748058
YDOT = -24471
869225 feet/sec YDOT = -7476
389985 meter/sec
ZDOT = 2332
028088 ZDOT = 703
259736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 711907
21 X = 216989
32
Y = 13950986
00 feet Y = 4252260
53 meter
Z = -17331684
48 Z = -5282697
43
XDOT = -23670
449720 XDOT = -7214
753075
YDOT = 4052
339980 feet/sec YDOT = 1235
153226 meter/sec
ZDOT = 2299
720274 ZDOT = 700
954740
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 17269
24544338
00016717 00000-0 10270-3 0 9173
2 25544 51
6403 254
5373 0004102 319
7921 40
2928 15
54277005 37460
Satellite: ISS
Catalog Number: 25544
Epoch time: 17269
24544338 = yrday
fracday
Element set: 917
Inclination: 51
6403 deg
RA of node: 254
5373 deg
Eccentricity:
0004102
Arg of perigee: 319
7921 deg
Mean anomaly: 40
2928 deg
Mean motion: 15
54277005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3746
Checksum: 307
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