[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 3rd 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) : 75 9 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
283/16:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
4
285/09:32:03
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
1
285/12:56:34
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
1
286/19:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
290/03:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
7
Coasting Arc #1 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2017/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3277123
22 A = 6777689
36 meter
Y = -2717924
15 meter E =
0005215
Z = 5273454
04 I = 51
36170
XDOT = 5370
977629 Wp = 6
34515
YDOT = 5448
839676 meter/sec RA = 222
27226 deg
ZDOT = -524
271628 TA = 88
70575
MA = 88
64601
Ha = 221
041 n
mi
Hp = 215
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10751716
59 X = 3281656
23
Y = -8917074
00 feet Y = -2681251
16 meter
Z = 17301358
41 Z = 5289384
69
XDOT = 17621
317679 XDOT = 5312
194736
YDOT = 17876
770591 feet/sec YDOT = 5508
572877 meter/sec
ZDOT = -1720
051272 ZDOT = -498
324383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8829502
78 X = -2691232
45
Y = 10709598
14 feet Y = 3264285
51 meter
Z = 17372248
25 Z = 5295061
27
XDOT = -19821
286397 XDOT = -6041
528094
YDOT = -13709
437290 feet/sec YDOT = -4178
636486 meter/sec
ZDOT = -1605
885144 ZDOT = -489
473792
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 17275
54741629
00016717 00000-0 10270-3 0 9007
2 25544 51
6383 223
1264 0004669 334
5151 25
5771 15
54038859 38449
Satellite: ISS
Catalog Number: 25544
Epoch time: 17275
54741629 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 223
1264 deg
Eccentricity:
0004669
Arg of perigee: 334
5151 deg
Mean anomaly: 25
5771 deg
Mean motion: 15
54038859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 320
Coasting Arc #2 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2017/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4485570
81 A = 6779396
40 meter
Y = 1476268
06 meter E =
0009733
Z = -4872356
75 I = 51
39314
XDOT = -4459
537542 Wp = 85
71025
YDOT = -5763
535170 meter/sec RA = 217
25653 deg
ZDOT = 2364
040460 TA = 207
52201
MA = 207
57358
Ha = 221
161 n
mi
Hp = 215
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14716439
68 X = -4478077
77
Y = 4843399
15 feet Y = 1426148
60 meter
Z = -15985422
40 Z = -4894128
40
XDOT = -14631
028682 XDOT = -4406
240145
YDOT = -18909
236121 feet/sec YDOT = -5813
106447 meter/sec
ZDOT = 7756
038256 ZDOT = 2342
507473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13350491
21 X = 4069229
72
Y = -7661527
70 feet Y = -2335233
64 meter
Z = -16082015
40 Z = -4901798
29
XDOT = 17602
186629 XDOT = 5365
146485
YDOT = 14623
496615 feet/sec YDOT = 4457
241768 meter/sec
ZDOT = 7661
439508 ZDOT = 2335
206762
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 17276
51199882
00016717 00000-0 10270-3 0 9014
2 25544 51
6391 218
3183 0004666 337
0010 23
0933 15
54045483 38593
Satellite: ISS
Catalog Number: 25544
Epoch time: 17276
51199882 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 218
3183 deg
Eccentricity:
0004666
Arg of perigee: 337
0010 deg
Mean anomaly: 23
0933 deg
Mean motion: 15
54045483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 311
Coasting Arc #3 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2017/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5501433
97 A = 6782750
39 meter
Y = -258623
40 meter E =
0011307
Z = 3955957
57 I = 51
43200
XDOT = 3147
167439 Wp = 54
70206
YDOT = 5744
454814 meter/sec RA = 212
25017 deg
ZDOT = -3986
645921 TA = 77
04050
MA = 76
91425
Ha = 221
254 n
mi
Hp = 215
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18049324
04 X = 5484700
77
Y = -848501
98 feet Y = -197195
63 meter
Z = 12978863
42 Z = 3982641
51
XDOT = 10325
352489 XDOT = 3102
062892
YDOT = 18846
636530 feet/sec YDOT = 5779
395844 meter/sec
ZDOT = -13079
546984 ZDOT = -3971
468141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17354462
45 X = -5289640
15
Y = 4715786
88 feet Y = 1437371
84 meter
Z = 13097058
32 Z = 3991983
38
XDOT = -13899
541731 XDOT = -4236
580320
YDOT = -14879
709734 feet/sec YDOT = -4535
335527 meter/sec
ZDOT = -13013
072122 ZDOT = -3966
384383
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 17277
54088022
00016717 00000-0 10270-3 0 9022
2 25544 51
6398 213
1899 0004778 341
5479 18
5500 15
54067721 38756
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
54088022 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 213
1899 deg
Eccentricity:
0004778
Arg of perigee: 341
5479 deg
Mean anomaly: 18
5500 deg
Mean motion: 15
54067721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 332
Coasting Arc #4 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2017/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6187644
38 A = 6786434
16 meter
Y = -805201
75 meter E =
0007868
Z = -2659958
54 I = 51
47198
XDOT = -1519
793317 Wp = 21
53796
YDOT = -5433
543987 meter/sec RA = 207
25613 deg
ZDOT = 5192
224522 TA = 308
37810
MA = 308
44875
Ha = 221
347 n
mi
Hp = 214
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20300670
53 X = -6165259
54
Y = -2641738
01 feet Y = -874271
41 meter
Z = -8726898
11 Z = -2689962
18
XDOT = -4986
198545 XDOT = -1484
142697
YDOT = -17826
587885 feet/sec YDOT = -5450
339316 meter/sec
ZDOT = 17034
857355 ZDOT = 5184
929051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20301035
27 X = 6187755
55
Y = -2151511
41 feet Y = -655780
68 meter
Z = -8859668
17 Z = -2700426
86
XDOT = 8957
594113 XDOT = 2730
274686
YDOT = 14664
339622 feet/sec YDOT = 4469
690717 meter/sec
ZDOT = 17003
239029 ZDOT = 5182
587256
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 17278
50545138
00016717 00000-0 10270-3 0 9036
2 25544 51
6394 208
3825 0004770 345
2347 14
8665 15
54059323 38901
Satellite: ISS
Catalog Number: 25544
Epoch time: 17278
50545138 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 208
3825 deg
Eccentricity:
0004770
Arg of perigee: 345
2347 deg
Mean anomaly: 14
8665 deg
Mean motion: 15
54059323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 321
Coasting Arc #5 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2017/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6472363
14 A = 6788969
66 meter
Y = 1741756
39 meter E =
0010841
Z = 1058133
66 I = 51
51126
XDOT = -351
705031 Wp = 105
39160
YDOT = 4907
426966 meter/sec RA = 202
27286 deg
ZDOT = -5879
127924 TA = 63
11692
MA = 63
00615
Ha = 221
485 n
mi
Hp = 214
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21234787
19 X = 6447265
31
Y = 5714423
85 feet Y = 1813994
57 meter
Z = 3471567
12 Z = 1089513
84
XDOT = -1153
887898 XDOT = -377
996557
YDOT = 16100
482172 feet/sec YDOT = 4903
346223 meter/sec
ZDOT = -19288
477441 ZDOT = -5880
900903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21966660
59 X = -6695438
15
Y = -232310
05 feet Y = -70808
10 meter
Z = 3610326
83 Z = 1100427
62
XDOT = -3045
555563 XDOT = -928
285336
YDOT = -14242
961378 feet/sec YDOT = -4341
254628 meter/sec
ZDOT = -19296
950244 ZDOT = -5881
710434
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 17279
53432043
00016717 00000-0 10270-3 0 9041
2 25544 51
6407 203
2543 0004733 348
4065 11
6978 15
54075447 39063
Satellite: ISS
Catalog Number: 25544
Epoch time: 17279
53432043 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 203
2543 deg
Eccentricity:
0004733
Arg of perigee: 348
4065 deg
Mean anomaly: 11
6978 deg
Mean motion: 15
54075447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 308
Coasting Arc #6 (Orbit 3921)
---------------------------------------
Vector Time (GMT): 2017/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6280600
83 A = 6789329
15 meter
Y = -2475774
25 meter E =
0016114
Z = 625311
38 I = 51
54288
XDOT = 2277
415850 Wp = 36
80259
YDOT = -4253
609203 meter/sec RA = 197
29530 deg
ZDOT = 5966
083940 TA = 329
96143
MA = 330
05377
Ha = 221
593 n
mi
Hp = 214
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20605645
77 X = -6255486
80
Y = -8122618
94 feet Y = -2545867
73 meter
Z = 2051546
52 Z = 594862
73
XDOT = 7471
836777 XDOT = 2295
830595
YDOT = -13955
410772 feet/sec YDOT = -4228
037980 meter/sec
ZDOT = 19573
766206 ZDOT = 5977
192359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22037700
67 X = 6717091
16
Y = 2333090
18 feet Y = 711125
89 meter
Z = 1916992
09 Z = 584299
19
XDOT = -3188
355623 XDOT = -971
810794
YDOT = 13799
241252 feet/sec YDOT = 4206
008734 meter/sec
ZDOT = 19623
506440 ZDOT = 5981
244763
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 17280
56318095
00016717 00000-0 10270-3 0 9057
2 25544 51
6405 198
1258 0004842 352
5309 7
5771 15
54080889 39223
Satellite: ISS
Catalog Number: 25544
Epoch time: 17280
56318095 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 198
1258 deg
Eccentricity:
0004842
Arg of perigee: 352
5309 deg
Mean anomaly: 7
5771 deg
Mean motion: 15
54080889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3922
Checksum: 324
Coasting Arc #7 (Orbit 3936)
---------------------------------------
Vector Time (GMT): 2017/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5605876
46 A = 6787277
14 meter
Y = 3075915
18 meter E =
0003817
Z = -2279978
45 I = 51
56818
XDOT = -4125
168369 Wp = 84
06391
YDOT = 3503
838215 meter/sec RA = 192
31809 deg
ZDOT = -5423
138681 TA = 121
32372
MA = 121
28635
Ha = 221
662 n
mi
Hp = 214
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18391983
15 X = 5582139
40
Y = 10091585
22 feet Y = 3138470
99 meter
Z = -7480244
26 Z = -2252804
10
XDOT = -13534
016959 XDOT = -4137
699038
YDOT = 11495
532203 feet/sec YDOT = 3457
637235 meter/sec
ZDOT = -17792
449741 ZDOT = -5443
208694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20542888
36 X = -6261472
37
Y = -4458202
00 feet Y = -1358859
97 meter
Z = -7360255
66 Z = -2243405
93
XDOT = 9289
477446 XDOT = 2831
432726
YDOT = -13323
909373 feet/sec YDOT = -4061
127577 meter/sec
ZDOT = -17881
800012 ZDOT = -5450
372644
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 17281
52772992
00016717 00000-0 10270-3 0 9065
2 25544 51
6410 193
3183 0004805 356
0387 4
0727 15
54099389 39371
Satellite: ISS
Catalog Number: 25544
Epoch time: 17281
52772992 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 193
3183 deg
Eccentricity:
0004805
Arg of perigee: 356
0387 deg
Mean anomaly: 4
0727 deg
Mean motion: 15
54099389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3937
Checksum: 330
Coasting Arc #8 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2017/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4478758
55 A = 6783747
32 meter
Y = -3514660
18 meter E =
0012440
Z = 3675100
90 I = 51
58783
XDOT = 5710
287440 Wp = 72
14054
YDOT = -2732
595061 meter/sec RA = 187
33468 deg
ZDOT = 4337
345673 TA = 331
66029
MA = 331
72790
Ha = 221
810 n
mi
Hp = 214
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14694089
74 X = -4456976
06
Y = -11531037
35 feet Y = -3564622
68 meter
Z = 12057417
65 Z = 3653397
12
XDOT = 18734
538845 XDOT = 5719
350457
YDOT = -8965
206893 feet/sec YDOT = -2668
687772 meter/sec
ZDOT = 14230
136724 ZDOT = 4365
107311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17548192
91 X = 5348689
20
Y = 6575781
91 feet Y = 2004298
33 meter
Z = 11961706
98 Z = 3645928
29
XDOT = -14620
439048 XDOT = -4456
309822
YDOT = 12856
267898 feet/sec YDOT = 3918
590455 meter/sec
ZDOT = 14353
479272 ZDOT = 4374
940482
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 17282
55657651
00016717 00000-0 10270-3 0 9074
2 25544 51
6403 188
1899 0004803 359
8136
3014 15
54107206 39534
Satellite: ISS
Catalog Number: 25544
Epoch time: 17282
55657651 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 188
1899 deg
Eccentricity:
0004803
Arg of perigee: 359
8136 deg
Mean anomaly:
3014 deg
Mean motion: 15
54107206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 312
Coasting Arc #9 (Orbit 3967)
---------------------------------------
Vector Time (GMT): 2017/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2990841
11 A = 6779950
16 meter
Y = 3861431
07 meter E =
0013306
Z = -4715082
25 I = 51
60901
XDOT = -6870
858385 Wp = 51
15466
YDOT = 1923
504563 meter/sec RA = 182
34321 deg
ZDOT = -2780
157172 TA = 191
23588
MA = 191
26562
Ha = 221
746 n
mi
Hp = 214
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9812470
82 X = 2970343
28
Y = 12668737
10 feet Y = 3894761
85 meter
Z = -15469429
96 Z = -4700603
36
XDOT = -22542
186302 XDOT = -6878
351956
YDOT = 6310
710507 feet/sec YDOT = 1846
627900 meter/sec
ZDOT = -9121
250563 ZDOT = -2813
552631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13407705
09 X = -4086668
51
Y = -8887103
38 feet Y = -2708789
11 meter
Z = -15405764
65 Z = -4695677
07
XDOT = 18689
309370 XDOT = 5696
501496
YDOT = -12111
051081 feet/sec YDOT = -3691
448370 meter/sec
ZDOT = -9269
472977 ZDOT = -2825
335363
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 17283
52111123
00016717 00000-0 10270-3 0 9082
2 25544 51
6412 183
3821 0004877 2
1449 357
9724 15
54147512 39681
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
52111123 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 183
3821 deg
Eccentricity:
0004877
Arg of perigee: 2
1449 deg
Mean anomaly: 357
9724 deg
Mean motion: 15
54147512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3968
Checksum: 307
Coasting Arc #10 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2017/283/16:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 998679
22 A = 6777697
48 meter
Y = 4185328
57 meter E =
0015888
Z = -5250130
82 I = 51
60365
XDOT = -7572
882003 Wp = 65
60767
YDOT = 588
458468 meter/sec RA = 181
34895 deg
ZDOT = -967
300162 TA = 195
09276
MA = 195
14022
Ha = 221
748 n
mi
Hp = 214
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3276506
62 X = 977306
58
Y = 13731392
94 feet Y = 4196376
73 meter
Z = -17224838
66 Z = -5245331
56
XDOT = -24845
413397 XDOT = -7574
200708
YDOT = 1930
638017 feet/sec YDOT = 503
765915 meter/sec
ZDOT = -3173
556963 ZDOT = -1004
090810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13774099
67 X = -4198345
58
Y = 3205409
85 feet Y = 977008
92 meter
Z = -17204105
33 Z = -5243811
30
XDOT = -1364
251329 XDOT = -415
823805
YDOT = -23843
243071 feet/sec YDOT = -7267
420488 meter/sec
ZDOT = -3336
658661 ZDOT = -1017
013560
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 17283
71401659
00016717 00000-0 10270-3 0 9090
2 25544 51
6371 182
4171 0004731 2
6842 357
4335 15
54130816 39710
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
71401659 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 182
4171 deg
Eccentricity:
0004731
Arg of perigee: 2
6842 deg
Mean anomaly: 357
4335 deg
Mean motion: 15
54130816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 304
Coasting Arc #11 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2017/284/16:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 841305
68 A = 6777700
85 meter
Y = -4211147
22 meter E =
0007363
Z = 5241472
50 I = 51
63588
XDOT = 7602
352646 Wp = 28
92476
YDOT = 291
418568 meter/sec RA = 176
34750 deg
ZDOT = -979
234956 TA = 70
48523
MA = 70
40572
Ha = 221
820 n
mi
Hp = 214
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2760189
23 X = 862872
44
Y = -13816099
81 feet Y = -4201618
36 meter
Z = 17196432
09 Z = 5245611
93
XDOT = 24942
101856 XDOT = 7603
285615
YDOT = 956
097663 feet/sec YDOT = 376
438438 meter/sec
ZDOT = -3212
713109 ZDOT = -942
302281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13824687
67 X = 4213764
80
Y = 2594509
88 feet Y = 790806
61 meter
Z = 17215314
82 Z = 5247227
96
XDOT = -671
292792 XDOT = -204
610043
YDOT = 23958
001559 feet/sec YDOT = 7302
398875 meter/sec
ZDOT = -3049
068909 ZDOT = -929
356204
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 17284
74284725
00016717 00000-0 10270-3 0 9109
2 25544 51
6367 177
2880 0004704 6
6940 353
4274 15
54106093 39872
Satellite: ISS
Catalog Number: 25544
Epoch time: 17284
74284725 = yrday
fracday
Element set: 910
Inclination: 51
6367 deg
RA of node: 177
2880 deg
Eccentricity:
0004704
Arg of perigee: 6
6940 deg
Mean anomaly: 353
4274 deg
Mean motion: 15
54106093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 325
Coasting Arc #12 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2017/285/09:32:03
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3376142
71 A = 6779543
17 meter
Y = -3396709
71 meter E =
0007409
Z = 4791776
77 I = 51
66766
XDOT = 6611
436654 Wp = 81
40365
YDOT = -2898
112225 meter/sec RA = 172
88531 deg
ZDOT = 2601
506714 TA = 342
97594
MA = 343
00079
Ha = 221
912 n
mi
Hp = 214
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11076583
70 X = -3361185
26
Y = -11144060
74 feet Y = -3434380
19 meter
Z = 15721052
41 Z = 4775412
81
XDOT = 21691
065137 XDOT = 6630
715744
YDOT = -9508
242208 feet/sec YDOT = -2824
070714 meter/sec
ZDOT = 8535
127016 ZDOT = 2633
670368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7505342
66 X = 2287628
44
Y = 13885687
80 feet Y = 4232357
64 meter
Z = 15648954
94 Z = 4769801
47
XDOT = -22441
761556 XDOT = -6840
248922
YDOT = 2341
208222 feet/sec YDOT = 713
600266 meter/sec
ZDOT = 8678
057650 ZDOT = 2645
071972
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 17285
45016422
00016717 00000-0 10270-3 0 9116
2 25544 51
6390 173
7650 0004798 8
5593 351
5641 15
54168850 39980
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
45016422 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 173
7650 deg
Eccentricity:
0004798
Arg of perigee: 8
5593 deg
Mean anomaly: 351
5641 deg
Mean motion: 15
54168850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 330
Coasting Arc #13 (Orbit 3999)
---------------------------------------
Vector Time (GMT): 2017/285/12:56:34
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4748088
64 A = 6784081
68 meter
Y = -3402610
30 meter E =
0014045
Z = 3443719
81 I = 51
68927
XDOT = 5419
817154 Wp = 68
76689
YDOT = 2905
468408 meter/sec RA = 172
13340 deg
ZDOT = -4581
850719 TA = 70
90039
MA = 70
74836
Ha = 221
838 n
mi
Hp = 214
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15577718
65 X = 4769056
56
Y = -11163419
61 feet Y = -3349396
53 meter
Z = 11298293
34 Z = 3466835
91
XDOT = 17781
552343 XDOT = 5409
181259
YDOT = 9532
376668 feet/sec YDOT = 2966
016818 meter/sec
ZDOT = -15032
318631 ZDOT = -4555
548596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6433264
23 X = -1960858
94
Y = 17987904
22 feet Y = 5482713
21 meter
Z = 11401188
58 Z = 3475082
28
XDOT = -18819
366606 XDOT = -5736
142941
YDOT = 2764
854469 feet/sec YDOT = 842
727642 meter/sec
ZDOT = -14916
106403 ZDOT = -4546
429232
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 17285
57876683
00016717 00000-0 10270-3 0 9123
2 25544 51
6406 173
1248 0005011 8
9742 351
1499 15
54172941 40002
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
57876683 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 173
1248 deg
Eccentricity:
0005011
Arg of perigee: 8
9742 deg
Mean anomaly: 351
1499 deg
Mean motion: 15
54172941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4000
Checksum: 309
Coasting Arc #14 (Orbit 4014)
---------------------------------------
Vector Time (GMT): 2017/286/12:56:34
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5785768
06 A = 6787525
47 meter
Y = 2927926
46 meter E =
0011273
Z = -1988954
63 I = 51
73308
XDOT = -3766
089906 Wp = 28
15084
YDOT = -3661
931802 meter/sec RA = 167
15975 deg
ZDOT = 5587
253692 TA = 309
91787
MA = 310
01689
Ha = 221
903 n
mi
Hp = 214
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18982178
67 X = -5808417
45
Y = 9606057
95 feet Y = 2863099
29 meter
Z = -6525441
70 Z = -2017115
53
XDOT = -12355
938011 XDOT = -3752
001679
YDOT = -12014
211950 feet/sec YDOT = -3703
967677 meter/sec
ZDOT = 18330
884816 ZDOT = 5568
993479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9823428
14 X = 2994180
90
Y = -18826839
73 feet Y = -5738420
75 meter
Z = -6650654
94 Z = -2027119
63
XDOT = 15762
108409 XDOT = 4804
290643
YDOT = 1802
985632 feet/sec YDOT = 549
550021 meter/sec
ZDOT = 18250
402748 ZDOT = 5562
722758
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 17286
54328536
00016717 00000-0 10270-3 0 9131
2 25544 51
6409 168
3163 0004998 10
6450 349
4808 15
54148188 40152
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
54328536 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 168
3163 deg
Eccentricity:
0004998
Arg of perigee: 10
6450 deg
Mean anomaly: 349
4808 deg
Mean motion: 15
54148188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4015
Checksum: 327
Coasting Arc #15 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2017/286/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 234851
56 A = 6777694
77 meter
Y = -4312057
36 meter E =
0007760
Z = 5221014
75 I = 51
70828
XDOT = 7522
665416 Wp = 35
05540
YDOT = -978
922362 meter/sec RA = 165
77290 deg
ZDOT = -1139
830306 TA = 65
89783
MA = 65
81668
Ha = 221
905 n
mi
Hp = 214
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 770510
37 X = 257691
34
Y = -14147169
83 feet Y = -4309303
04 meter
Z = 17129313
48 Z = 5222211
35
XDOT = 24680
660813 XDOT = 7538
589668
YDOT = -3211
687540 feet/sec YDOT = -894
709820 meter/sec
ZDOT = -3739
600742 ZDOT = -1103
248489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10247032
82 X = 3123295
60
Y = -9774139
52 feet Y = -2979157
73 meter
Z = 17135168
38 Z = 5222799
32
XDOT = 19369
738329 XDOT = 5903
896243
YDOT = 13994
942022 feet/sec YDOT = 4265
658328 meter/sec
ZDOT = -3577
299406 ZDOT = -1090
360859
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 17286
86479192
00016717 00000-0 10270-3 0 9142
2 25544 51
6401 166
7080 0004482 16
0406 344
0888 15
54144784 40206
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
86479192 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 166
7080 deg
Eccentricity:
0004482
Arg of perigee: 16
0406 deg
Mean anomaly: 344
0888 deg
Mean motion: 15
54144784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 312
Coasting Arc #16 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2017/287/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1948939
97 A = 6780037
80 meter
Y = 4553137
26 meter E =
0011368
Z = -4639796
31 I = 51
74800
XDOT = -7063
955114 Wp = 87
03890
YDOT = -11
476545 meter/sec RA = 160
78369 deg
ZDOT = 2962
780091 TA = 212
43294
MA = 212
50286
Ha = 221
926 n
mi
Hp = 213
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6394160
00 X = -1977171
48
Y = 14938114
37 feet Y = 4531184
64 meter
Z = -15222428
83 Z = -4649332
68
XDOT = -23175
705754 XDOT = -7077
693621
YDOT = -37
652708 feet/sec YDOT = -90
547082 meter/sec
ZDOT = 9720
407123 ZDOT = 2928
431947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14755670
72 X = -4497528
43
Y = 6707899
98 feet Y = 2044567
91 meter
Z = -15265292
08 Z = -4652861
02
XDOT = -16563
469733 XDOT = -5048
545575
YDOT = -14711
984392 feet/sec YDOT = -4484
212843 meter/sec
ZDOT = 9568
115710 ZDOT = 2916
361668
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 17287
82930284
00016717 00000-0 10270-3 0 9154
2 25544 51
6402 161
9009 0004463 19
5042 340
6281 15
54171723 40356
Satellite: ISS
Catalog Number: 25544
Epoch time: 17287
82930284 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 161
9009 deg
Eccentricity:
0004463
Arg of perigee: 19
5042 deg
Mean anomaly: 340
6281 deg
Mean motion: 15
54171723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 294
Coasting Arc #17 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2017/288/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3482563
80 A = 6783890
73 meter
Y = -4617772
78 meter E =
0014605
Z = 3537620
34 I = 51
79092
XDOT = 6104
759112 Wp = 72
16454
YDOT = 1141
016648 meter/sec RA = 155
80407 deg
ZDOT = -4500
708076 TA = 66
22611
MA = 66
07302
Ha = 221
988 n
mi
Hp = 213
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11425734
24 X = 3516757
94
Y = -15150173
15 feet Y = -4578636
82 meter
Z = 11606365
95 Z = 3554621
24
XDOT = 20028
737244 XDOT = 6113
408689
YDOT = 3743
492938 feet/sec YDOT = 1209
332144 meter/sec
ZDOT = -14766
102612 ZDOT = -4471
031867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18552749
05 X = 5654877
91
Y = -3755163
26 feet Y = -1144573
76 meter
Z = 11682342
72 Z = 3560778
06
XDOT = 12257
783486 XDOT = 3736
172407
YDOT = 14833
134880 feet/sec YDOT = 4521
139511 meter/sec
ZDOT = -14634
655890 ZDOT = -4460
643115
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 17288
85811165
00016717 00000-0 10270-3 0 9165
2 25544 51
6399 156
7719 0004396 24
2472 335
8886 15
54150161 40514
Satellite: ISS
Catalog Number: 25544
Epoch time: 17288
85811165 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 156
7719 deg
Eccentricity:
0004396
Arg of perigee: 24
2472 deg
Mean anomaly: 335
8886 deg
Mean motion: 15
54150161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 333
Coasting Arc #18 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2017/289/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4644388
72 A = 6787338
27 meter
Y = 4478029
47 meter E =
0010841
Z = -2095742
46 I = 51
83308
XDOT = -4749
527208 Wp = 35
04026
YDOT = -2341
241280 meter/sec RA = 150
83736 deg
ZDOT = 5545
714560 TA = 301
82104
MA = 301
92656
Ha = 222
063 n
mi
Hp = 213
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15237495
82 X = -4683937
84
Y = 14691697
73 feet Y = 4425871
38 meter
Z = -6875795
49 Z = -2118400
31
XDOT = -15582
438348 XDOT = -4749
932543
YDOT = -7681
237796 feet/sec YDOT = -2394
355389 meter/sec
ZDOT = 18194
601576 ZDOT = 5522
641807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21098367
49 X = -6430782
41
Y = 1219126
11 feet Y = 371589
64 meter
Z = -6976850
68 Z = -2126544
09
XDOT = -6797
851618 XDOT = -2071
985173
YDOT = -14526
614754 feet/sec YDOT = -4427
712177 meter/sec
ZDOT = 18092
581633 ZDOT = 5514
618882
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 17289
82261376
00016717 00000-0 10270-3 0 9177
2 25544 51
6412 151
9641 0004597 24
9196 335
2178 15
54152142 40669
Satellite: ISS
Catalog Number: 25544
Epoch time: 17289
82261376 = yrday
fracday
Element set: 917
Inclination: 51
6412 deg
RA of node: 151
9641 deg
Eccentricity:
0004597
Arg of perigee: 24
9196 deg
Mean anomaly: 335
2178 deg
Mean motion: 15
54152142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 320
Coasting Arc #19 (Orbit 4070)
---------------------------------------
Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2238192
64 A = 6777271
61 meter
Y = 3552510
66 meter E =
0017760
Z = -5334798
13 I = 51
80522
XDOT = -6544
550101 Wp = 75
16486
YDOT = 3971
314746 meter/sec RA = 149
32148 deg
ZDOT = -97
029663 TA = 193
88666
MA = 193
93557
Ha = 222
245 n
mi
Hp = 213
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7343151
71 X = 2224215
37
Y = 11655218
71 feet Y = 3577460
91 meter
Z = -17502618
53 Z = -5323959
88
XDOT = -21471
621067 XDOT = -6588
000667
YDOT = 13029
247855 feet/sec YDOT = 3897
886159 meter/sec
ZDOT = -318
338789 ZDOT = -128
927490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13449899
59 X = 4099529
39
Y = -3245070
34 feet Y = -989097
44 meter
Z = -17455010
03 Z = -5320287
06
XDOT = 5070
507677 XDOT = 1545
490740
YDOT = 23565
409181 feet/sec YDOT = 7182
736718 meter/sec
ZDOT = -460
310022 ZDOT = -140
302495
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 17290
14411328
00016717 00000-0 10270-3 0 9189
2 25544 51
6382 150
3643 0004939 27
4706 332
6707 15
54161307 40713
Satellite: ISS
Catalog Number: 25544
Epoch time: 17290
14411328 = yrday
fracday
Element set: 918
Inclination: 51
6382 deg
RA of node: 150
3643 deg
Eccentricity:
0004939
Arg of perigee: 27
4706 deg
Mean anomaly: 332
6707 deg
Mean motion: 15
54161307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4071
Checksum: 296
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