[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 7th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25336 0914 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
008/21:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 212
4
015/23:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
8
000/00:00:00
000 0
0 0
0 212
0
Coasting Arc #1 (Orbit 3660)
---------------------------------------
Vector Time (GMT): 2017/006/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3800842
17 A = 6789674
83 meter
Y = -5620750
86 meter E =
0014876
Z = -145347
22 I = 51
97062
XDOT = 3846
478778 Wp = 108
13765
YDOT = 2743
943268 meter/sec RA = 123
10723 deg
ZDOT = -6035
922462 TA = 73
42033
MA = 73
25700
Ha = 223
599 n
mi
Hp = 212
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12469954
62 X = 3864118
39
Y = -18440783
65 feet Y = -5577893
48 meter
Z = -476860
95 Z = -126730
34
XDOT = 12619
681030 XDOT = 3844
829050
YDOT = 9002
438542 feet/sec YDOT = 2786
948150 meter/sec
ZDOT = -19802
895215 ZDOT = -6017
241327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22218135
50 X = 6772087
70
Y = 1410239
95 feet Y = 429841
14 meter
Z = -394137
60 Z = -120133
14
XDOT = -1198
147649 XDOT = -365
195403
YDOT = 13930
787824 feet/sec YDOT = 4246
104129 meter/sec
ZDOT = -19721
308182 ZDOT = -6011
054734
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 17006
57365116
00016717 00000-0 10270-3 0 9005
2 25544 51
6418 123
9690 0007015 56
3626 303
8195 15
54006317 36615
Satellite: ISS
Catalog Number: 25544
Epoch time: 17006
57365116 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 123
9690 deg
Eccentricity:
0007015
Arg of perigee: 56
3626 deg
Mean anomaly: 303
8195 deg
Mean motion: 15
54006317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3661
Checksum: 294
Coasting Arc #2 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2017/007/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4238635
67 A = 6788357
90 meter
Y = 4983661
82 meter E =
0021064
Z = 1771613
59 I = 51
98358
XDOT = -2722
520444 Wp = 63
14983
YDOT = -4357
265870 meter/sec RA = 118
16001 deg
ZDOT = 5700
836118 TA = 316
22614
MA = 316
39294
Ha = 223
677 n
mi
Hp = 212
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13906285
00 X = -4302654
90
Y = 16350596
53 feet Y = 4935904
51 meter
Z = 5812380
53 Z = 1750868
26
XDOT = -8932
153687 XDOT = -2701
286005
YDOT = -14295
491700 feet/sec YDOT = -4387
592464 meter/sec
ZDOT = 18703
530572 ZDOT = 5687
662276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21222934
70 X = -6468750
50
Y = -3372627
23 feet Y = -1027976
78 meter
Z = 5720399
02 Z = 1743577
62
XDOT = 7230
432325 XDOT = 2203
835773
YDOT = -13630
732554 feet/sec YDOT = -4154
647283 meter/sec
ZDOT = 18646
410446 ZDOT = 5683
425904
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 17007
60255895
00016717 00000-0 10270-3 0 9013
2 25544 51
6422 118
8414 0007140 59
2484 300
9371 15
54021756 36775
Satellite: ISS
Catalog Number: 25544
Epoch time: 17007
60255895 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 118
8414 deg
Eccentricity:
0007140
Arg of perigee: 59
2484 deg
Mean anomaly: 300
9371 deg
Mean motion: 15
54021756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3677
Checksum: 302
Coasting Arc #3 (Orbit 3691)
---------------------------------------
Vector Time (GMT): 2017/008/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4470384
66 A = 6785166
58 meter
Y = -3921793
35 meter E =
0011122
Z = -3279195
60 I = 51
98681
XDOT = 1579
007529 Wp = 76
92040
YDOT = 5779
066816 meter/sec RA = 113
20775 deg
ZDOT = -4770
091652 TA = 140
87794
MA = 140
79747
Ha = 223
643 n
mi
Hp = 212
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14666616
33 X = 4529835
68
Y = -12866776
09 feet Y = -3871469
88 meter
Z = -10758515
74 Z = -3257335
64
XDOT = 5180
470896 XDOT = 1537
437998
YDOT = 18960
192967 feet/sec YDOT = 5796
492223 meter/sec
ZDOT = -15649
906995 ZDOT = -4762
521887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18761881
69 X = 5718621
54
Y = 5543191
82 feet Y = 1689564
87 meter
Z = -10661802
96 Z = -3249717
54
XDOT = -12769
717964 XDOT = -3892
210035
YDOT = 13253
149249 feet/sec YDOT = 4039
559891 meter/sec
ZDOT = -15617
656977 ZDOT = -4760
261847
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 17008
56715417
00016717 00000-0 10270-3 0 9021
2 25544 51
6416 114
0341 0007027 63
1231 297
0639 15
54021625 36928
Satellite: ISS
Catalog Number: 25544
Epoch time: 17008
56715417 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 114
0341 deg
Eccentricity:
0007027
Arg of perigee: 63
1231 deg
Mean anomaly: 297
0639 deg
Mean motion: 15
54021625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3692
Checksum: 283
Coasting Arc #4 (Orbit 3697)
---------------------------------------
Vector Time (GMT): 2017/008/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3463948
56 A = 6777893
94 meter
Y = -2464281
30 meter E =
0010798
Z = 5271640
24 I = 51
96580
XDOT = 3432
856891 Wp = 60
62926
YDOT = -6803
080129 meter/sec RA = 111
36882 deg
ZDOT = -917
898338 TA = 38
14225
MA = 38
06588
Ha = 223
854 n
mi
Hp = 212
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11364660
64 X = -3461741
99
Y = -8084912
39 feet Y = -2503005
54 meter
Z = 17295407
60 Z = 5254818
59
XDOT = 11262
653842 XDOT = 3513
134259
YDOT = -22319
816695 feet/sec YDOT = -6764
242690 meter/sec
ZDOT = -3011
477486 ZDOT = -901
028050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10930263
34 X = -3331544
26
Y = 8808329
18 feet Y = 2684778
74 meter
Z = 17221937
29 Z = 5249246
49
XDOT = -17709
893550 XDOT = -5397
975554
YDOT = -16193
124900 feet/sec YDOT = -4935
664470 meter/sec
ZDOT = -2936
175620 ZDOT = -894
946329
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 17008
95299118
00016717 00000-0 10270-3 0 9030
2 25544 51
6401 112
1128 0007394 61
1525 299
0372 15
54030463 36987
Satellite: ISS
Catalog Number: 25544
Epoch time: 17008
95299118 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 112
1128 deg
Eccentricity:
0007394
Arg of perigee: 61
1525 deg
Mean anomaly: 299
0372 deg
Mean motion: 15
54030463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3698
Checksum: 301
Coasting Arc #5 (Orbit 3712)
---------------------------------------
Vector Time (GMT): 2017/009/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2715303
21 A = 6780038
12 meter
Y = 3993218
24 meter E =
0017151
Z = -4774150
95 I = 51
98459
XDOT = -3971
857935 Wp = 91
22416
YDOT = 5950
036225 meter/sec RA = 106
39559 deg
ZDOT = 2725
842203 TA = 205
60138
MA = 205
68640
Ha = 223
766 n
mi
Hp = 212
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8908475
08 X = 2693638
65
Y = 13101109
73 feet Y = 4023461
87 meter
Z = -15663224
89 Z = -4761013
14
XDOT = -13031
029971 XDOT = -4051
338361
YDOT = 19521
116224 feet/sec YDOT = 5905
175601 meter/sec
ZDOT = 8943
051848 ZDOT = 2706
355642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14984594
12 X = 4567304
29
Y = -5314587
12 feet Y = -1619886
16 meter
Z = -15606207
77 Z = -4756772
13
XDOT = 15083
866418 XDOT = 4597
562484
YDOT = 16600
801232 feet/sec YDOT = 5059
924216 meter/sec
ZDOT = 8856
383697 ZDOT = 2699
425751
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 17009
91757564
00016717 00000-0 10270-3 0 9042
2 25544 51
6408 107
3051 0007400 63
9375 296
2538 15
54034349 37134
Satellite: ISS
Catalog Number: 25544
Epoch time: 17009
91757564 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 107
3051 deg
Eccentricity:
0007400
Arg of perigee: 63
9375 deg
Mean anomaly: 296
2538 deg
Mean motion: 15
54034349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3713
Checksum: 310
Coasting Arc #6 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2017/010/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1917967
83 A = 6783572
79 meter
Y = -5306626
27 meter E =
0018931
Z = 3753044
54 I = 52
00515
XDOT = 4359
091473 Wp = 77
39712
YDOT = -4628
967734 meter/sec RA = 101
43130 deg
ZDOT = -4295
245533 TA = 57
95492
MA = 57
77118
Ha = 223
805 n
mi
Hp = 212
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6292545
36 X = -1876715
55
Y = -17410191
17 feet Y = -5327843
97 meter
Z = 12313138
27 Z = 3743827
41
XDOT = 14301
481211 XDOT = 4431
393864
YDOT = -15186
902015 feet/sec YDOT = -4579
816776 meter/sec
ZDOT = -14092
012902 ZDOT = -4273
895374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18433806
02 X = -5618624
08
Y = 1969306
19 feet Y = 600244
53 meter
Z = 12273584
91 Z = 3740988
68
XDOT = -11109
394254 XDOT = -3386
143369
YDOT = -16296
726691 feet/sec YDOT = -4967
242296 meter/sec
ZDOT = -13997
371634 ZDOT = -4266
398874
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 17010
94645914
00016717 00000-0 10270-3 0 9053
2 25544 51
6410 102
1772 0007500 67
1267 293
0676 15
54066023 37296
Satellite: ISS
Catalog Number: 25544
Epoch time: 17010
94645914 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 102
1772 deg
Eccentricity:
0007500
Arg of perigee: 67
1267 deg
Mean anomaly: 293
0676 deg
Mean motion: 15
54066023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 293
Coasting Arc #7 (Orbit 3743)
---------------------------------------
Vector Time (GMT): 2017/011/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1178823
96 A = 6787104
28 meter
Y = 6237043
39 meter E =
0012736
Z = -2401768
47 I = 52
02241
XDOT = -4577
015945 Wp = 60
48570
YDOT = 2934
489486 meter/sec RA = 96
47784 deg
ZDOT = 5401
519063 TA = 272
83718
MA = 272
98293
Ha = 223
793 n
mi
Hp = 212
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3867532
67 X = 1120658
59
Y = 20462740
79 feet Y = 6249900
78 meter
Z = -7879817
80 Z = -2396182
89
XDOT = -15016
456514 XDOT = -4635
727603
YDOT = 9627
590176 feet/sec YDOT = 2882
977460 meter/sec
ZDOT = 17721
519235 ZDOT = 5379
143263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20818794
07 X = 6345568
43
Y = 792443
28 feet Y = 241536
71 meter
Z = -7856395
16 Z = -2394629
25
XDOT = 6030
121193 XDOT = 1837
980940
YDOT = 15393
693406 feet/sec YDOT = 4691
997750 meter/sec
ZDOT = 17622
659505 ZDOT = 5371
386617
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 17011
91103169
00016717 00000-0 10270-3 0 9063
2 25544 51
6410 97
3703 0007426 70
8183 289
3773 15
54055437 37440
Satellite: ISS
Catalog Number: 25544
Epoch time: 17011
91103169 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 97
3703 deg
Eccentricity:
0007426
Arg of perigee: 70
8183 deg
Mean anomaly: 289
3773 deg
Mean motion: 15
54055437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3744
Checksum: 307
Coasting Arc #8 (Orbit 3759)
---------------------------------------
Vector Time (GMT): 2017/012/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -400174
61 A = 6789258
58 meter
Y = -6730822
96 meter E =
0018753
Z = 743212
07 I = 52
03370
XDOT = 4698
059637 Wp = 108
58079
YDOT = -953
210622 meter/sec RA = 91
53179 deg
ZDOT = -5985
733726 TA = 63
43090
MA = 63
23882
Ha = 223
788 n
mi
Hp = 212
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1312908
83 X = -328489
17
Y = -22082752
51 feet Y = -6734897
22 meter
Z = 2438359
82 Z = 741441
80
XDOT = 15413
581486 XDOT = 4737
444796
YDOT = -3127
331436 feet/sec YDOT = -900
453102 meter/sec
ZDOT = -19638
234009 ZDOT = -5962
816792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21874180
27 X = -6667250
15
Y = -3305128
16 feet Y = -1007403
06 meter
Z = 2431800
13 Z = 741212
68
XDOT = -60
762756 XDOT = -18
520488
YDOT = -14256
680793 feet/sec YDOT = -4345
436306 meter/sec
ZDOT = -19537
343483 ZDOT = -5954
982294
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 17012
93990107
00016717 00000-0 10270-3 0 9073
2 25544 51
6423 92
2416 0007462 74
3456 285
8520 15
54073372 37608
Satellite: ISS
Catalog Number: 25544
Epoch time: 17012
93990107 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 92
2416 deg
Eccentricity:
0007462
Arg of perigee: 74
3456 deg
Mean anomaly: 285
8520 deg
Mean motion: 15
54073372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 305
Coasting Arc #9 (Orbit 3775)
---------------------------------------
Vector Time (GMT): 2017/013/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -327629
59 A = 6789107
25 meter
Y = 6708482
87 meter E =
0020654
Z = 930556
21 I = 52
03239
XDOT = -4718
437576 Wp = 62
95036
YDOT = -1069
121141 meter/sec RA = 86
58906 deg
ZDOT = 5954
143557 TA = 307
07475
MA = 307
26341
Ha = 223
821 n
mi
Hp = 212
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1074900
24 X = -407141
33
Y = 22009458
24 feet Y = 6704374
47 meter
Z = 3053005
95 Z = 928771
94
XDOT = -15480
438240 XDOT = -4735
053472
YDOT = -3507
615292 feet/sec YDOT = -1121
979094 meter/sec
ZDOT = 19534
591722 ZDOT = 5931
182866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21391859
65 X = 6520238
82
Y = 5292945
76 feet Y = 1613289
87 meter
Z = 3043940
53 Z = 927793
07
XDOT = -6046
221570 XDOT = -1842
888335
YDOT = 13085
873096 feet/sec YDOT = 3988
574120 meter/sec
ZDOT = 19433
870455 ZDOT = 5923
443715
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 17013
96876279
00016717 00000-0 10270-3 0 9081
2 25544 51
6415 87
1138 0007534 77
5391 282
6605 15
54081498 37760
Satellite: ISS
Catalog Number: 25544
Epoch time: 17013
96876279 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 87
1138 deg
Eccentricity:
0007534
Arg of perigee: 77
5391 deg
Mean anomaly: 282
6605 deg
Mean motion: 15
54081498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3776
Checksum: 345
Coasting Arc #10 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2017/014/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1123940
89 A = 6786608
07 meter
Y = -6180407
12 meter E =
0011601
Z = -2575142
76 I = 52
02215
XDOT = 4625
859816 Wp = 100
16033
YDOT = 3038
963688 meter/sec RA = 81
64253 deg
ZDOT = -5296
811854 TA = 108
60343
MA = 108
47741
Ha = 223
775 n
mi
Hp = 212
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3687470
12 X = 1205476
81
Y = -20276926
26 feet Y = -6167382
50 meter
Z = -8448631
09 Z = -2569485
23
XDOT = 15176
705433 XDOT = 4617
262368
YDOT = 9970
353308 feet/sec YDOT = 3090
645233 meter/sec
ZDOT = -17377
991647 ZDOT = -5274
362087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19311670
70 X = -5886197
23
Y = -7228360
50 feet Y = -2203204
28 meter
Z = -8422631
47 Z = -2567218
07
XDOT = 11960
170694 XDOT = 3645
460027
YDOT = -11903
755199 feet/sec YDOT = -3628
264585 meter/sec
ZDOT = -17279
874351 ZDOT = -5266
905702
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 17014
93331423
00016717 00000-0 10270-3 0 9097
2 25544 51
6422 82
3061 0007477 81
1170 279
0828 15
54101952 37914
Satellite: ISS
Catalog Number: 25544
Epoch time: 17014
93331423 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 82
3061 deg
Eccentricity:
0007477
Arg of perigee: 81
1170 deg
Mean anomaly: 279
0828 deg
Mean motion: 15
54101952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 295
Coasting Arc #11 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2017/015/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1900126
92 A = 6782971
06 meter
Y = 5202410
53 meter E =
0018552
Z = 3900627
26 I = 52
00426
XDOT = -4427
935001 Wp = 93
14075
YDOT = -4722
612269 meter/sec RA = 76
68687 deg
ZDOT = 4123
899889 TA = 313
80109
MA = 313
95437
Ha = 223
827 n
mi
Hp = 211
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6234012
21 X = -1977107
41
Y = 17068276
03 feet Y = 5180731
59 meter
Z = 12797333
54 Z = 3891210
25
XDOT = -14527
345803 XDOT = -4394
827980
YDOT = -15494
134740 feet/sec YDOT = -4771
943325 meter/sec
ZDOT = 13529
855278 ZDOT = 4102
471113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15858806
58 X = 4833764
25
Y = 8931369
72 feet Y = 2722281
49 meter
Z = 12754982
92 Z = 3887718
80
XDOT = -16953
675272 XDOT = -5167
480223
YDOT = 10830
791380 feet/sec YDOT = 3301
225213 meter/sec
ZDOT = 13436
537635 ZDOT = 4095
456671
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 17015
96216227
00016717 00000-0 10270-3 0 9107
2 25544 51
6421 77
1776 0007478 84
8872 275
3134 15
54107510 38071
Satellite: ISS
Catalog Number: 25544
Epoch time: 17015
96216227 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 77
1776 deg
Eccentricity:
0007478
Arg of perigee: 84
8872 deg
Mean anomaly: 275
3134 deg
Mean motion: 15
54107510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 312
Coasting Arc #12 (Orbit 3807)
---------------------------------------
Vector Time (GMT): 2017/015/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3683534
09 A = 6785259
57 meter
Y = -4746587
36 meter E =
0020355
Z = 3134976
59 I = 52
01253
XDOT = 2635
622691 Wp = 91
13055
YDOT = -5293
492559 meter/sec RA = 76
23364 deg
ZDOT = -4891
028578 TA = 52
92909
MA = 52
74315
Ha = 223
809 n
mi
Hp = 211
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12085085
60 X = -3645410
68
Y = -15572793
17 feet Y = -4787565
97 meter
Z = 10285356
27 Z = 3117176
01
XDOT = 8647
056072 XDOT = 2718
377820
YDOT = -17367
101571 feet/sec YDOT = -5263
556525 meter/sec
ZDOT = -16046
681687 ZDOT = -4878
024777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10366348
23 X = -3159662
94
Y = 16813253
12 feet Y = 5124679
55 meter
Z = 10207990
93 Z = 3111395
63
XDOT = -18102
736068 XDOT = -5517
713954
YDOT = -1400
102662 feet/sec YDOT = -426
751291 meter/sec
ZDOT = -15988
548278 ZDOT = -4873
309515
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 17016
02646438
00016717 00000-0 10270-3 0 9117
2 25544 51
6433 76
8581 0007465 84
7021 275
4983 15
54116485 38080
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
02646438 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 76
8581 deg
Eccentricity:
0007465
Arg of perigee: 84
7021 deg
Mean anomaly: 275
4983 deg
Mean motion: 15
54116485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3808
Checksum: 321
Coasting Arc #13 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2017/016/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3281303
62 A = 6788193
41 meter
Y = 5711736
92 meter E =
0013902
Z = -1632493
13 I = 52
01391
XDOT = -3509
127904 Wp = 61
67194
YDOT = 3648
466442 meter/sec RA = 71
28207 deg
ZDOT = 5755
393050 TA = 280
55746
MA = 280
71404
Ha = 223
713 n
mi
Hp = 211
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10765431
81 X = 3225119
37
Y = 18739294
37 feet Y = 5748116
51 meter
Z = -5355948
60 Z = -1616690
32
XDOT = -11512
886823 XDOT = -3577
621671
YDOT = 11970
034258 feet/sec YDOT = 3608
842094 meter/sec
ZDOT = 18882
523131 ZDOT = 5738
180645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13517335
92 X = 4120083
99
Y = -16883877
26 feet Y = -5146205
79 meter
Z = -5287549
46 Z = -1611645
08
XDOT = 14156
391291 XDOT = 4314
868065
YDOT = 5489
441765 feet/sec YDOT = 1673
181850 meter/sec
ZDOT = 18806
190296 ZDOT = 5732
126802
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 17016
99100069
00016717 00000-0 10270-3 0 9129
2 25544 51
6432 72
0495 0007387 87
7753 272
4245 15
54138003 38234
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
99100069 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 72
0495 deg
Eccentricity:
0007387
Arg of perigee: 87
7753 deg
Mean anomaly: 272
4245 deg
Mean motion: 15
54138003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 307
Coasting Arc #14 (Orbit 3838)
---------------------------------------
Vector Time (GMT): 2017/017/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2647640
19 A = 6789422
99 meter
Y = -6244768
28 meter E =
0018033
Z = -104139
44 I = 52
00560
XDOT = 4378
189983 Wp = 119
13222
YDOT = -1768
737290 meter/sec RA = 66
33700 deg
ZDOT = -6042
509375 TA = 61
98397
MA = 61
80166
Ha = 223
765 n
mi
Hp = 212
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8686483
56 X = -2577106
95
Y = -20488084
89 feet Y = -6273981
60 meter
Z = -341664
84 Z = -116829
32
XDOT = 14364
140364 XDOT = 4426
994279
YDOT = -5802
943865 feet/sec YDOT = -1719
504614 meter/sec
ZDOT = -19824
505825 ZDOT = -6021
123169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15647374
42 X = -4769319
72
Y = 15822009
86 feet Y = 4822548
60 meter
Z = -396272
76 Z = -120783
94
XDOT = -9725
542934 XDOT = -2964
345486
YDOT = -10056
059257 feet/sec YDOT = -3065
086862 meter/sec
ZDOT = -19730
175282 ZDOT = -6013
757426
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 17018
01983515
00016717 00000-0 10270-3 0 9130
2 25544 51
6425 66
9210 0007407 92
9416 267
2584 15
54094061 38390
Satellite: ISS
Catalog Number: 25544
Epoch time: 17018
01983515 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 66
9210 deg
Eccentricity:
0007407
Arg of perigee: 92
9416 deg
Mean anomaly: 267
2584 deg
Mean motion: 15
54094061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3839
Checksum: 314
Coasting Arc #15 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2017/018/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1850668
08 A = 6787904
75 meter
Y = 6278473
43 meter E =
0020553
Z = 1767757
14 I = 51
98745
XDOT = -5133
304918 Wp = 75
18963
YDOT = -105
997423 meter/sec RA = 61
38972 deg
ZDOT = 5700
533645 TA = 304
13538
MA = 304
33016
Ha = 223
599 n
mi
Hp = 211
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6071745
67 X = 1771736
20
Y = 20598666
09 feet Y = 6298727
52 meter
Z = 5799728
15 Z = 1776555
27
XDOT = -16841
551568 XDOT = -5159
428262
YDOT = -347
760574 feet/sec YDOT = -163
547516 meter/sec
ZDOT = 18702
538205 ZDOT = 5675
534414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16524573
02 X = 5036689
86
Y = -13699394
60 feet Y = -4175575
47 meter
Z = 5837213
47 Z = 1779182
66
XDOT = 5401
904034 XDOT = 1646
500350
YDOT = 14507
574392 feet/sec YDOT = 4421
908675 meter/sec
ZDOT = 18592
680379 ZDOT = 5667
048979
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 17019
04865983
00016717 00000-0 10270-3 0 9143
2 25544 51
6427 61
7920 0007233 95
2850 264
9128 15
54158993 38559
Satellite: ISS
Catalog Number: 25544
Epoch time: 17019
04865983 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 61
7920 deg
Eccentricity:
0007233
Arg of perigee: 95
2850 deg
Mean anomaly: 264
9128 deg
Mean motion: 15
54158993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 336
Coasting Arc #16 (Orbit 3869)
---------------------------------------
Vector Time (GMT): 2017/019/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -788573
09 A = 6784629
97 meter
Y = -5873993
37 meter E =
0011879
Z = -3310995
79 I = 51
95973
XDOT = 5710
080911 Wp = 96
71832
YDOT = 1896
709680 meter/sec RA = 56
43458 deg
ZDOT = -4740
796201 TA = 121
54344
MA = 121
42737
Ha = 223
598 n
mi
Hp = 212
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2587182
04 X = -706746
89
Y = -19271631
80 feet Y = -5882354
21 meter
Z = -10862847
08 Z = -3314627
67
XDOT = 18733
861258 XDOT = 5711
475327
YDOT = 6222
800789 feet/sec YDOT = 1960
571451 meter/sec
ZDOT = -15553
793312 ZDOT = -4713
055211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16526146
43 X = -5037169
43
Y = 10230007
91 feet Y = 3118106
41 meter
Z = -10877691
49 Z = -3315520
37
XDOT = -1341
079495 XDOT = -408
761030
YDOT = -18520
303857 feet/sec YDOT = -5644
988616 meter/sec
ZDOT = -15432
228631 ZDOT = -4703
743287
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 17020
01317768
00016717 00000-0 10270-3 0 9156
2 25544 51
6423 56
9831 0007192 98
6229 261
5739 15
54142099 38701
Satellite: ISS
Catalog Number: 25544
Epoch time: 17020
01317768 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 56
9831 deg
Eccentricity:
0007192
Arg of perigee: 98
6229 deg
Mean anomaly: 261
5739 deg
Mean motion: 15
54142099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3870
Checksum: 321
Coasting Arc #17 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2017/020/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -410069
96 A = 6780883
21 meter
Y = 5086408
05 meter E =
0016471
Z = 4454504
38 I = 51
92774
XDOT = -6028
650671 Wp = 106
35115
YDOT = -3402
090167 meter/sec RA = 51
46910 deg
ZDOT = 3315
074668 TA = 310
30207
MA = 310
44590
Ha = 223
694 n
mi
Hp = 211
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1345373
87 X = -488554
66
Y = 16687690
45 feet Y = 5081383
49 meter
Z = 14614515
67 Z = 4452321
82
XDOT = -19779
037634 XDOT = -6006
262461
YDOT = -11161
713146 feet/sec YDOT = -3469
381454 meter/sec
ZDOT = 10876
229226 ZDOT = 3285
843885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15703322
18 X = 4786372
60
Y = -5831255
19 feet Y = -1777366
58 meter
Z = 14603946
28 Z = 4451282
83
XDOT = -2030
825141 XDOT = -618
995503
YDOT = 21570
093482 feet/sec YDOT = 6574
564493 meter/sec
ZDOT = 10748
411902 ZDOT = 3276
115948
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 17021
04199117
00016717 00000-0 10270-3 0 9167
2 25544 51
6416 51
8545 0007376 101
5324 258
6657 15
54137381 38864
Satellite: ISS
Catalog Number: 25544
Epoch time: 17021
04199117 = yrday
fracday
Element set: 916
Inclination: 51
6416 deg
RA of node: 51
8545 deg
Eccentricity:
0007376
Arg of perigee: 101
5324 deg
Mean anomaly: 258
6657 deg
Mean motion: 15
54137381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 315
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