[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 7th 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) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
160/01:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
6
165/09:20:13
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
7
167/11:41:08
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 216
6
167/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
4
Coasting Arc #1 (Orbit 2022)
---------------------------------------
Vector Time (GMT): 2017/158/10:33:06
005
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4189354
27 A = 6778058
45 meter
Y = 781670
93 meter E =
0010542
Z = -5279744
42 I = 51
99484
XDOT = -219
814101 Wp = 109
42935
YDOT = 7598
510355 meter/sec RA = 86
06058 deg
ZDOT = 948
677806 TA = 169
62382
MA = 169
60205
Ha = 219
889 n
mi
Hp = 216
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13744600
62 X = 4205948
80
Y = 2564537
17 feet Y = 828612
52 meter
Z = -17321996
13 Z = -5259353
16
XDOT = -721
174871 XDOT = -309
374572
YDOT = 24929
495915 feet/sec YDOT = 7595
551373 meter/sec
ZDOT = 3112
459993 ZDOT = 947
393342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10314928
28 X = 3143990
14
Y = -9602079
11 feet Y = -2926713
71 meter
Z = -17232085
72 Z = -5252339
73
XDOT = 18879
562919 XDOT = 5754
490778
YDOT = 14696
983131 feet/sec YDOT = 4479
640458 meter/sec
ZDOT = 3105
451376 ZDOT = 946
541580
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 17158
45412224
00016717 00000-0 10270-3 0 9003
2 25544 51
6400 86
8441 0004666 248
9342 111
1312 15
53988886 20231
Satellite: ISS
Catalog Number: 25544
Epoch time: 17158
45412224 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 86
8441 deg
Eccentricity:
0004666
Arg of perigee: 248
9342 deg
Mean anomaly: 111
1312 deg
Mean motion: 15
53988886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2023
Checksum: 298
Coasting Arc #2 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2017/159/10:33:06
005
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4149037
95 A = 6780236
20 meter
Y = -2476336
54 meter E =
0003350
Z = 4755404
77 I = 51
99910
XDOT = 1066
587655 Wp = 47
95653
YDOT = -7077
679096 meter/sec RA = 81
09039 deg
ZDOT = -2751
633521 TA = 69
15021
MA = 69
11435
Ha = 219
907 n
mi
Hp = 216
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13612329
22 X = -4144138
24
Y = -8124463
70 feet Y = -2522707
11 meter
Z = 15601721
68 Z = 4735261
36
XDOT = 3499
303331 XDOT = 1159
019094
YDOT = -23220
731943 feet/sec YDOT = -7065
234620 meter/sec
ZDOT = -9027
669033 ZDOT = -2746
228716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14586451
96 X = -4445950
56
Y = 6425884
02 feet Y = 1958609
45 meter
Z = 15513206
33 Z = 4728425
29
XDOT = -16345
715721 XDOT = -4982
174152
YDOT = -15343
045199 feet/sec YDOT = -4676
560177 meter/sec
ZDOT = -9002
537587 ZDOT = -2743
973456
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 17159
48304412
00016717 00000-0 10270-3 0 9017
2 25544 51
6401 81
7170 0004620 253
4044 106
6601 15
53993597 20397
Satellite: ISS
Catalog Number: 25544
Epoch time: 17159
48304412 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 81
7170 deg
Eccentricity:
0004620
Arg of perigee: 253
4044 deg
Mean anomaly: 106
6601 deg
Mean motion: 15
53993597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 288
Coasting Arc #3 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2017/160/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3525478
99 A = 6778597
70 meter
Y = 2688800
99 meter E =
0004528
Z = 5129005
57 I = 51
99204
XDOT = -2822
963719 Wp = 186
34857
YDOT = -6926
030445 meter/sec RA = 77
97301 deg
ZDOT = 1686
229680 TA = 247
41912
MA = 247
46704
Ha = 219
803 n
mi
Hp = 216
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11566532
11 X = -3580198
30
Y = 8821525
56 feet Y = 2649070
04 meter
Z = 16827446
09 Z = 5111747
16
XDOT = -9261
691993 XDOT = -2753
496185
YDOT = -22723
196997 feet/sec YDOT = -6957
210551 meter/sec
ZDOT = 5532
249606 ZDOT = 1672
684229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11347978
69 X = -3458863
90
Y = -9241368
09 feet Y = -2816768
99 meter
Z = 16750743
73 Z = 5105626
69
XDOT = 19183
760467 XDOT = 5847
210190
YDOT = -13609
976843 feet/sec YDOT = -4148
320942 meter/sec
ZDOT = 5473
674916 ZDOT = 1668
376114
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 17160
12611751
00016717 00000-0 10270-3 0 9028
2 25544 51
6418 78
5109 0004946 251
6310 108
4305 15
54017123 20493
Satellite: ISS
Catalog Number: 25544
Epoch time: 17160
12611751 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 78
5109 deg
Eccentricity:
0004946
Arg of perigee: 251
6310 deg
Mean anomaly: 108
4305 deg
Mean motion: 15
54017123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 275
Coasting Arc #4 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2017/161/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4059392
01 A = 6777788
88 meter
Y = -1007458
09 meter E =
0010192
Z = -5342077
62 I = 51
98085
XDOT = 2090
701793 Wp = 98
80539
YDOT = 7367
542558 meter/sec RA = 72
99894 deg
ZDOT = 198
069139 TA = 173
08232
MA = 173
06825
Ha = 219
636 n
mi
Hp = 216
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13318215
27 X = 4096305
37
Y = -3305308
70 feet Y = -961856
05 meter
Z = -17526501
39 Z = -5322268
68
XDOT = 6859
257851 XDOT = 2007
198484
YDOT = 24171
727551 feet/sec YDOT = 7390
455277 meter/sec
ZDOT = 649
833132 ZDOT = 208
023450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6618096
92 X = 2017195
94
Y = 12147679
36 feet Y = 3702612
67 meter
Z = -17438831
78 Z = -5315355
93
XDOT = -20743
855606 XDOT = -6322
727189
YDOT = 12301
047927 feet/sec YDOT = 3749
359408 meter/sec
ZDOT = 692
454028 ZDOT = 211
059988
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 17161
09072902
00016717 00000-0 10270-3 0 9035
2 25544 51
6414 73
7038 0004918 256
4367 103
6238 15
53984110 20648
Satellite: ISS
Catalog Number: 25544
Epoch time: 17161
09072902 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 73
7038 deg
Eccentricity:
0004918
Arg of perigee: 256
4367 deg
Mean anomaly: 103
6238 deg
Mean motion: 15
53984110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 297
Coasting Arc #5 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2017/162/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4506535
03 A = 6779037
40 meter
Y = -679925
01 meter E =
0002593
Z = 5018988
74 I = 51
97571
XDOT = -1200
873568 Wp = 5
24767
YDOT = -7286
569883 meter/sec RA = 68
02495 deg
ZDOT = -2062
779036 TA = 104
73582
MA = 104
70709
Ha = 219
593 n
mi
Hp = 216
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14785219
90 X = -4522976
89
Y = -2230725
08 feet Y = -730412
80 meter
Z = 16466498
48 Z = 4997057
24
XDOT = -3939
873911 XDOT = -1109
283964
YDOT = -23906
069171 feet/sec YDOT = -7299
486452 meter/sec
ZDOT = -6767
647757 ZDOT = -2068
391153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1893451
54 X = -577124
03
Y = -14938883
46 feet Y = -4553371
68 meter
Z = 16369759
82 Z = 4989502
79
XDOT = 20864
668676 XDOT = 6359
551012
YDOT = -10095
473490 feet/sec YDOT = -3077
100320 meter/sec
ZDOT = -6791
092560 ZDOT = -2069
925012
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 17162
11964228
00016717 00000-0 10270-3 0 9041
2 25544 51
6420 68
5761 0004895 261
3362 98
7236 15
54036081 20800
Satellite: ISS
Catalog Number: 25544
Epoch time: 17162
11964228 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 68
5761 deg
Eccentricity:
0004895
Arg of perigee: 261
3362 deg
Mean anomaly: 98
7236 deg
Mean motion: 15
54036081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 305
Coasting Arc #6 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2017/163/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4829132
49 A = 6782225
90 meter
Y = 2237536
66 meter E =
0004120
Z = -4208193
15 I = 51
97211
XDOT = 139
928596 Wp = 137
56190
YDOT = 6697
657256 meter/sec RA = 63
05659 deg
ZDOT = 3720
943563 TA = 170
49749
MA = 170
48969
Ha = 219
507 n
mi
Hp = 216
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15843610
54 X = 4824194
23
Y = 7340999
54 feet Y = 2291512
29 meter
Z = -13806407
96 Z = -4184746
34
XDOT = 459
083321 XDOT = 46
948686
YDOT = 21973
941129 feet/sec YDOT = 6698
701612 meter/sec
ZDOT = 12207
820088 ZDOT = 3721
398428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2444714
79 X = -745149
07
Y = 17371559
68 feet Y = 5294851
39 meter
Z = -13703264
34 Z = -4176754
97
XDOT = -19669
803604 XDOT = -5995
356139
YDOT = 6864
581197 feet/sec YDOT = 2092
324349 meter/sec
ZDOT = 12208
584238 ZDOT = 3721
176476
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 17163
08424924
00016717 00000-0 10270-3 0 9053
2 25544 51
6409 63
7691 0004591 264
5882 95
4747 15
54029594 20959
Satellite: ISS
Catalog Number: 25544
Epoch time: 17163
08424924 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 63
7691 deg
Eccentricity:
0004591
Arg of perigee: 264
5882 deg
Mean anomaly: 95
4747 deg
Mean motion: 15
54029594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2095
Checksum: 336
Coasting Arc #7 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2017/164/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4950812
80 A = 6785907
68 meter
Y = -3559521
74 meter E =
0008509
Z = 2968406
61 I = 51
96912
XDOT = 1079
187015 Wp = 102
21875
YDOT = -5696
077460 meter/sec RA = 58
09633 deg
ZDOT = -5020
108797 TA = 44
02303
MA = 43
95530
Ha = 219
443 n
mi
Hp = 216
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16242824
14 X = -4925060
39
Y = -11678220
92 feet Y = -3614741
49 meter
Z = 9738866
84 Z = 2944419
18
XDOT = 3540
639812 XDOT = 1167
187046
YDOT = -18687
918176 feet/sec YDOT = -5683
516537 meter/sec
ZDOT = -16470
173217 ZDOT = -5014
653482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6164260
90 X = 1878866
72
Y = -19085377
92 feet Y = -5817223
19 meter
Z = 9633584
20 Z = 2936316
46
XDOT = 17521
790022 XDOT = 5340
641599
YDOT = -2658
911834 feet/sec YDOT = -810
436327 meter/sec
ZDOT = -16445
011079 ZDOT = -5012
439377
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 17164
11315798
00016717 00000-0 10270-3 0 9067
2 25544 51
6410 58
6409 0004797 270
0656 89
9947 15
54048135 21111
Satellite: ISS
Catalog Number: 25544
Epoch time: 17164
11315798 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 58
6409 deg
Eccentricity:
0004797
Arg of perigee: 270
0656 deg
Mean anomaly: 89
9947 deg
Mean motion: 15
54048135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 322
Coasting Arc #8 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2017/165/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4822663
78 A = 6788801
77 meter
Y = 4547161
92 meter E =
0007156
Z = -1446070
51 I = 51
96092
XDOT = -2396
076898 Wp = 4
35376
YDOT = 4387
399601 meter/sec RA = 53
14370 deg
ZDOT = 5814
031661 TA = 339
94404
MA = 339
97215
Ha = 219
533 n
mi
Hp = 216
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15822387
73 X = 4778482
08
Y = 14918510
24 feet Y = 4600845
36 meter
Z = -4744325
82 Z = -1422750
30
XDOT = -7861
144677 XDOT = -2473
201513
YDOT = 14394
355647 feet/sec YDOT = 4360
173095 meter/sec
ZDOT = 19074
907023 ZDOT = 5802
205509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9050038
04 X = -2758451
60
Y = 19798118
71 feet Y = 6034466
58 meter
Z = -4642180
09 Z = -1414936
49
XDOT = -14752
363899 XDOT = -4496
520516
YDOT = -2290
315214 feet/sec YDOT = -698
088077 meter/sec
ZDOT = 19021
845571 ZDOT = 5797
858530
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 17165
07775873
00016717 00000-0 10270-3 0 9078
2 25544 51
6414 53
8332 0004650 274
5213 85
5409 15
54017114 21267
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
07775873 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 53
8332 deg
Eccentricity:
0004650
Arg of perigee: 274
5213 deg
Mean anomaly: 85
5409 deg
Mean motion: 15
54017114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 299
Coasting Arc #9 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025120
72 A = 6781131
21 meter
Y = 647883
79 meter E =
0004970
Z = -4511969
02 I = 51
92874
XDOT = 2042
113178 Wp = 122
08923
YDOT = 6643
071717 meter/sec RA = 51
57569 deg
ZDOT = 3228
285152 TA = 180
26344
MA = 180
26371
Ha = 219
541 n
mi
Hp = 216
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16486616
52 X = 5039419
30
Y = 2125603
00 feet Y = 704158
59 meter
Z = -14803047
96 Z = -4487523
79
XDOT = 6699
846383 XDOT = 1951
995450
YDOT = 21794
854714 feet/sec YDOT = 6665
403745 meter/sec
ZDOT = 10591
486720 ZDOT = 3237
986994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13735438
25 X = 4186561
58
Y = -9531306
60 feet Y = -2905142
25 meter
Z = -14695198
94 Z = -4479096
64
XDOT = 18828
409123 XDOT = 5738
899101
YDOT = 10739
601713 feet/sec YDOT = 3273
430602 meter/sec
ZDOT = 10633
084591 ZDOT = 3240
964183
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 17165
39929216
00016717 00000-0 10270-3 0 9086
2 25544 51
6410 52
2313 0004699 277
9274 82
1345 15
54024863 21319
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
39929216 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 52
2313 deg
Eccentricity:
0004699
Arg of perigee: 277
9274 deg
Mean anomaly: 82
1345 deg
Mean motion: 15
54024863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2131
Checksum: 309
Coasting Arc #10 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5529290
46 A = 6784871
06 meter
Y = -1983467
47 meter E =
0007934
Z = 3389208
26 I = 51
92016
XDOT = -693
119713 Wp = 84
27353
YDOT = -6049
406827 meter/sec RA = 46
61013 deg
ZDOT = -4660
953596 TA = 56
31563
MA = 56
24000
Ha = 219
636 n
mi
Hp = 216
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18140716
73 X = -5523162
92
Y = -6507439
19 feet Y = -2045265
83 meter
Z = 11119449
68 Z = 3362363
42
XDOT = -2274
014808 XDOT = -602
781578
YDOT = -19847
135259 feet/sec YDOT = -6056
652157 meter/sec
ZDOT = -15291
842508 ZDOT = -4664
101772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17751764
58 X = -5410737
84
Y = 7676047
67 feet Y = 2339659
33 meter
Z = 11001257
92 Z = 3353183
41
XDOT = -14576
686055 XDOT = -4442
973910
YDOT = -11727
733123 feet/sec YDOT = -3574
613056 meter/sec
ZDOT = -15304
599786 ZDOT = -4664
842015
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 17166
42819554
00016717 00000-0 10270-3 0 9095
2 25544 51
6409 47
1039 0004735 281
9479 78
1143 15
54022408 21479
Satellite: ISS
Catalog Number: 25544
Epoch time: 17166
42819554 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 47
1039 deg
Eccentricity:
0004735
Arg of perigee: 281
9479 deg
Mean anomaly: 78
1143 deg
Mean motion: 15
54022408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2147
Checksum: 318
Coasting Arc #11 (Orbit 2161)
---------------------------------------
Vector Time (GMT): 2017/167/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5733299
94 A = 6788081
72 meter
Y = 3062358
19 meter E =
0006724
Z = -1941847
81 I = 51
90838
XDOT = -846
113322 Wp = 357
84331
YDOT = 5145
213779 meter/sec RA = 41
65151 deg
ZDOT = 5621
936339 TA = 340
82847
MA = 340
85376
Ha = 219
696 n
mi
Hp = 216
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18810039
16 X = 5708062
27
Y = 10047106
93 feet Y = 3126330
91 meter
Z = -6370891
77 Z = -1914058
25
XDOT = -2775
962342 XDOT = -930
894148
YDOT = 16880
622635 feet/sec YDOT = 5135
277401 meter/sec
ZDOT = 18444
673027 ZDOT = 5617
620750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20536448
45 X = 6259509
49
Y = -5878583
23 feet Y = -1791792
17 meter
Z = -6248738
86 Z = -1904615
60
XDOT = 9222
299325 XDOT = 2810
956834
YDOT = 12653
748836 feet/sec YDOT = 3856
862645 meter/sec
ZDOT = 18424
632027 ZDOT = 5615
827842
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 17167
39279013
00016717 00000-0 10270-3 0 9104
2 25544 51
6414 42
2959 0004832 285
2786 74
7833 15
54027708 21621
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
39279013 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 42
2959 deg
Eccentricity:
0004832
Arg of perigee: 285
2786 deg
Mean anomaly: 74
7833 deg
Mean motion: 15
54027708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2162
Checksum: 319
Coasting Arc #12 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2017/167/11:41:08
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5605984
98 A = 6789089
24 meter
Y = -3614529
75 meter E =
0009271
Z = 1237327
80 I = 51
91049
XDOT = 1688
313520 Wp = 130
27575
YDOT = -4635
860304 meter/sec RA = 41
17262 deg
ZDOT = -5870
106903 TA = 36
32485
MA = 36
26195
Ha = 219
662 n
mi
Hp = 216
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18392339
16 X = -5571160
03
Y = -11858693
39 feet Y = -3677025
07 meter
Z = 4059474
40 Z = 1210179
93
XDOT = 5539
086352 XDOT = 1768
541524
YDOT = -15209
515433 feet/sec YDOT = -4616
531311 meter/sec
ZDOT = -19258
880914 ZDOT = -5861
711174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15056787
00 X = -4589308
68
Y = 15910800
89 feet Y = 4849612
11 meter
Z = 3940261
62 Z = 1200991
74
XDOT = -12742
692817 XDOT = -3883
972771
YDOT = -7279
412441 feet/sec YDOT = -2218
764912 meter/sec
ZDOT = -19220
916207 ZDOT = -5858
535260
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 17167
52140263
00016717 00000-0 10270-3 0 9114
2 25544 51
6427 41
6562 0004767 284
6743 75
3881 15
54000906 21644
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
52140263 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 41
6562 deg
Eccentricity:
0004767
Arg of perigee: 284
6743 deg
Mean anomaly: 75
3881 deg
Mean motion: 15
54000906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 302
Coasting Arc #13 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3172497
70 A = 6786557
40 meter
Y = -5387883
53 meter E =
0001805
Z = -2635764
29 I = 51
89439
XDOT = 5545
277851 Wp = 194
79620
YDOT = -699
526046 meter/sec RA = 40
20399 deg
ZDOT = -5245
466041 TA = 14
78518
MA = 14
77990
Ha = 219
591 n
mi
Hp = 216
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10408457
03 X = -3099209
94
Y = -17676783
23 feet Y = -5422950
53 meter
Z = -8647520
64 Z = -2650997
78
XDOT = 18193
168801 XDOT = 5578
167891
YDOT = -2295
032960 feet/sec YDOT = -637
330614 meter/sec
ZDOT = -17209
534255 ZDOT = -5218
448983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 758271
36 X = 231121
11
Y = 20471430
08 feet Y = 6239691
89 meter
Z = -8713772
49 Z = -2655957
86
XDOT = -15721
282266 XDOT = -4791
846835
YDOT = -6690
898594 feet/sec YDOT = -2039
385892 meter/sec
ZDOT = -17090
077575 ZDOT = -5209
055645
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 17167
71431997
00016717 00000-0 10270-3 0 9123
2 25544 51
6393 40
6891 0004654 284
4440 75
6196 15
54052859 21676
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
71431997 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 40
6891 deg
Eccentricity:
0004654
Arg of perigee: 284
4440 deg
Mean anomaly: 75
6196 deg
Mean motion: 15
54052859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 333
Coasting Arc #14 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1937177
07 A = 6782904
59 meter
Y = 5162208
41 meter E =
0006389
Z = 3945574
42 I = 51
85647
XDOT = -6474
323059 Wp = 95
94178
YDOT = -674
603243 meter/sec RA = 35
23835 deg
ZDOT = 4055
072812 TA = 311
78497
MA = 311
83955
Ha = 219
616 n
mi
Hp = 216
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6355567
80 X = 1860142
21
Y = 16936379
28 feet Y = 5183440
17 meter
Z = 12944797
98 Z = 3954797
99
XDOT = -21241
217386 XDOT = -6485
995889
YDOT = -2213
265233 feet/sec YDOT = -747
069127 meter/sec
ZDOT = 13304
044660 ZDOT = 4023
594061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2179033
35 X = 664169
36
Y = -17929178
60 feet Y = -5464813
64 meter
Z = 12984542
67 Z = 3957688
60
XDOT = 16641
293144 XDOT = 5072
266150
YDOT = 11571
748293 feet/sec YDOT = 3527
068880 meter/sec
ZDOT = 13165
152386 ZDOT = 4012
738447
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 17168
74321661
00016717 00000-0 10270-3 0 9134
2 25544 51
6391 35
5600 0004657 285
8988 74
1651 15
54053056 21838
Satellite: ISS
Catalog Number: 25544
Epoch time: 17168
74321661 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 35
5600 deg
Eccentricity:
0004657
Arg of perigee: 285
8988 deg
Mean anomaly: 74
1651 deg
Mean motion: 15
54053056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 316
Coasting Arc #15 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -456069
36 A = 6779506
53 meter
Y = -4701356
98 meter E =
0008753
Z = -4871304
00 I = 51
81843
XDOT = 7015
648370 Wp = 53
69496
YDOT = 1861
568897 meter/sec RA = 30
26331 deg
ZDOT = -2451
467153 TA = 192
27316
MA = 192
29449
Ha = 219
793 n
mi
Hp = 216
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1496290
55 X = -379801
11
Y = -15424399
54 feet Y = -4706030
19 meter
Z = -15981968
50 Z = -4873334
62
XDOT = 23017
219063 XDOT = 7006
218494
YDOT = 6107
509504 feet/sec YDOT = 1939
970123 meter/sec
ZDOT = -8042
871237 ZDOT = -2417
409844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5576934
89 X = -1699849
76
Y = 14449604
19 feet Y = 4404239
36 meter
Z = -15990029
38 Z = -4873760
96
XDOT = -16932
794018 XDOT = -5161
115617
YDOT = -15276
810269 feet/sec YDOT = -4656
371770 meter/sec
ZDOT = -7892
829298 ZDOT = -2405
734370
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 17169
70780700
00016717 00000-0 10270-3 0 9145
2 25544 51
6396 30
7538 0004529 290
7697 69
2970 15
54048233 21986
Satellite: ISS
Catalog Number: 25544
Epoch time: 17169
70780700 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 30
7538 deg
Eccentricity:
0004529
Arg of perigee: 290
7697 deg
Mean anomaly: 69
2970 deg
Mean motion: 15
54048233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 335
Coasting Arc #16 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1163450
19 A = 6777754
65 meter
Y = 4064550
49 meter E =
0001802
Z = 5298850
14 I = 51
78400
XDOT = -7102
489570 Wp = 296
18121
YDOT = -2824
392653 meter/sec RA = 25
27646 deg
ZDOT = 607
953035 TA = 148
03230
MA = 148
02137
Ha = 219
993 n
mi
Hp = 216
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3817093
81 X = -1234554
03
Y = 13335139
40 feet Y = 4051141
91 meter
Z = 17384678
95 Z = 5293026
11
XDOT = -23302
131136 XDOT = -7073
331760
YDOT = -9266
380095 feet/sec YDOT = -2903
654534 meter/sec
ZDOT = 1994
596573 ZDOT = 573
521581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9248526
61 X = 2818950
91
Y = -10381802
71 feet Y = -3164373
47 meter
Z = 17358172
09 Z = 5290770
85
XDOT = 16369
502903 XDOT = 4989
424485
YDOT = 17659
096973 feet/sec YDOT = 5382
492757 meter/sec
ZDOT = 1843
100111 ZDOT = 561
776914
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 17170
73670143
00016717 00000-0 10270-3 0 9150
2 25544 51
6400 25
6244 0004641 294
6525 65
4144 15
54024789 22147
Satellite: ISS
Catalog Number: 25544
Epoch time: 17170
73670143 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 25
6244 deg
Eccentricity:
0004641
Arg of perigee: 294
6525 deg
Mean anomaly: 65
4144 deg
Mean motion: 15
54024789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 291
Coasting Arc #17 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2790147
19 A = 6778158
58 meter
Y = -3341357
79 meter E =
0009704
Z = -5203976
51 I = 51
75660
XDOT = 6663
893031 Wp = 91
30047
YDOT = 3551
242256 meter/sec RA = 20
28775 deg
ZDOT = 1294
587457 TA = 191
11330
MA = 191
13475
Ha = 220
028 n
mi
Hp = 216
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9154026
20 X = 2852582
38
Y = -10962459
94 feet Y = -3309806
77 meter
Z = -17073413
75 Z = -5190271
44
XDOT = 21863
166111 XDOT = 6617
398298
YDOT = 11651
057269 feet/sec YDOT = 3625
502304 meter/sec
ZDOT = 4247
334175 ZDOT = 1326
846402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12955162
95 X = -3948733
67
Y = 6182271
53 feet Y = 1884356
36 meter
Z = -17012244
19 Z = -5185332
03
XDOT = -14658
681890 XDOT = -4467
966240
YDOT = -18656
926046 feet/sec YDOT = -5686
631059 meter/sec
ZDOT = 4389
084460 ZDOT = 1337
792943
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 17171
70128606
00016717 00000-0 10270-3 0 9161
2 25544 51
6409 20
8177 0004578 298
4106 61
6585 15
54055055 22297
Satellite: ISS
Catalog Number: 25544
Epoch time: 17171
70128606 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 20
8177 deg
Eccentricity:
0004578
Arg of perigee: 298
4106 deg
Mean anomaly: 61
6585 deg
Mean motion: 15
54055055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 312
Coasting Arc #18 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4297646
39 A = 6780893
85 meter
Y = 2565170
43 meter E =
0007165
Z = 4574405
39 I = 51
73381
XDOT = -5717
369067 Wp = 35
48986
YDOT = -4079
361469 meter/sec RA = 15
29967 deg
ZDOT = -3075
776897 TA = 85
27637
MA = 85
19454
Ha = 220
273 n
mi
Hp = 216
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14099889
72 X = -4348231
81
Y = 8415913
48 feet Y = 2516827
76 meter
Z = 15007891
69 Z = 4553406
04
XDOT = -18757
772529 XDOT = -5656
386891
YDOT = -13383
731854 feet/sec YDOT = -4142
955565 meter/sec
ZDOT = -10091
131553 ZDOT = -3103
402823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16369329
64 X = 4989371
68
Y = -2114030
30 feet Y = -644356
44 meter
Z = 14914664
78 Z = 4545989
82
XDOT = 11717
546805 XDOT = 3571
508266
YDOT = 18493
395848 feet/sec YDOT = 5636
787055 meter/sec
ZDOT = -10212
311433 ZDOT = -3112
712525
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 17172
73017622
00016717 00000-0 10270-3 0 9171
2 25544 51
6402 15
6889 0004517 302
0702 58
0012 15
54015687 22459
Satellite: ISS
Catalog Number: 25544
Epoch time: 17172
73017622 = yrday
fracday
Element set: 917
Inclination: 51
6402 deg
RA of node: 15
6889 deg
Eccentricity:
0004517
Arg of perigee: 302
0702 deg
Mean anomaly: 58
0012 deg
Mean motion: 15
54015687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 284
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