[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 4th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24322 131 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
006/12:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 212
6
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 3628)
---------------------------------------
Vector Time (GMT): 2017/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2894867
64 A = 6777739
50 meter
Y = 3036750
58 meter E =
0020605
Z = -5340405
81 I = 51
88795
XDOT = -5357
678880 Wp = 78
50193
YDOT = 5461
488677 meter/sec RA = 133
23976 deg
ZDOT = 206
039485 TA = 193
43140
MA = 193
48633
Ha = 223
518 n
mi
Hp = 212
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9497597
23 X = 2886635
75
Y = 9963092
44 feet Y = 3069077
05 meter
Z = -17521016
42 Z = -5326363
39
XDOT = -17577
686615 XDOT = -5419
353296
YDOT = 17918
269939 feet/sec YDOT = 5401
230659 meter/sec
ZDOT = 675
982562 ZDOT = 179
863970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7457001
57 X = -2272894
08
Y = 11661911
43 feet Y = 3554550
61 meter
Z = -17459854
80 Z = -5321763
74
XDOT = -20661
199881 XDOT = -6297
533724
YDOT = -12395
846261 feet/sec YDOT = -3778
253940 meter/sec
ZDOT = 560
121968 ZDOT = 170
725176
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 17004
51581192
00016717 00000-0 10270-3 0 9001
2 25544 51
6407 134
2254 0007004 49
3951 310
7810 15
54001916 36290
Satellite: ISS
Catalog Number: 25544
Epoch time: 17004
51581192 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 134
2254 deg
Eccentricity:
0007004
Arg of perigee: 49
3951 deg
Mean anomaly: 310
7810 deg
Mean motion: 15
54001916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3629
Checksum: 275
Coasting Arc #2 (Orbit 3644)
---------------------------------------
Vector Time (GMT): 2017/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1635431
37 A = 6779166
59 meter
Y = -4261242
81 meter E =
0013024
Z = 5005585
50 I = 51
91457
XDOT = 5739
174824 Wp = 54
94194
YDOT = -4652
362676 meter/sec RA = 128
25943 deg
ZDOT = -2074
335917 TA = 55
20583
MA = 55
08334
Ha = 223
657 n
mi
Hp = 212
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5365588
50 X = -1611974
19
Y = -13980455
42 feet Y = -4279400
27 meter
Z = 16422524
59 Z = 4997697
95
XDOT = 18829
313728 XDOT = 5800
848302
YDOT = -15263
657073 feet/sec YDOT = -4587
838473 meter/sec
ZDOT = -6805
564032 ZDOT = -2046
307102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12176655
92 X = 3711444
72
Y = -8779798
94 feet Y = -2676082
72 meter
Z = 16388598
74 Z = 4995244
90
XDOT = 18841
746998 XDOT = 5742
964485
YDOT = 13591
205910 feet/sec YDOT = 4142
599561 meter/sec
ZDOT = -6681
683483 ZDOT = -2036
577126
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 17005
54473716
00016717 00000-0 10270-3 0 9018
2 25544 51
6412 129
0965 0007032 53
1625 307
0172 15
53976617 36455
Satellite: ISS
Catalog Number: 25544
Epoch time: 17005
54473716 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 129
0965 deg
Eccentricity:
0007032
Arg of perigee: 53
1625 deg
Mean anomaly: 307
0172 deg
Mean motion: 15
53976617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3645
Checksum: 297
Coasting Arc #3 (Orbit 3659)
---------------------------------------
Vector Time (GMT): 2017/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 462677
50 A = 6782179
42 meter
Y = 5303615
07 meter E =
0013333
Z = -4212486
79 I = 51
94508
XDOT = -5742
558618 Wp = 84
87503
YDOT = 3444
390990 meter/sec RA = 123
28832 deg
ZDOT = 3717
092716 TA = 223
12353
MA = 223
22804
Ha = 223
588 n
mi
Hp = 212
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1517970
79 X = 423798
97
Y = 17400311
91 feet Y = 5308571
79 meter
Z = -13820494
70 Z = -4210333
50
XDOT = -18840
415413 XDOT = -5798
703748
YDOT = 11300
495374 feet/sec YDOT = 3379
859792 meter/sec
ZDOT = 12195
186076 ZDOT = 3689
060811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16347365
05 X = -4982676
87
Y = 6170513
84 feet Y = 1880772
62 meter
Z = -13811936
08 Z = -4209878
12
XDOT = -15470
061019 XDOT = -4715
274599
YDOT = -14046
609108 feet/sec YDOT = -4281
406456 meter/sec
ZDOT = 12071
479236 ZDOT = 3679
386871
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
50934658
00016717 00000-0 10270-3 0 9023
2 25544 51
6420 124
2897 0007016 55
7324 304
4492 15
54007151 36603
Satellite: ISS
Catalog Number: 25544
Epoch time: 17006
50934658 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 124
2897 deg
Eccentricity:
0007016
Arg of perigee: 55
7324 deg
Mean anomaly: 304
4492 deg
Mean motion: 15
54007151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3660
Checksum: 290
Coasting Arc #4 (Orbit 3659)
---------------------------------------
Vector Time (GMT): 2017/006/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2827284
11 A = 6789069
04 meter
Y = 6044893
25 meter E =
0016003
Z = -1216988
88 I = 51
96834
XDOT = -4800
319298 Wp = 45
83130
YDOT = -1072
470378 meter/sec RA = 123
26686 deg
ZDOT = 5883
532460 TA = 301
00306
MA = 301
16014
Ha = 223
623 n
mi
Hp = 212
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9275866
50 X = -2888757
98
Y = 19832326
95 feet Y = 6012932
98 meter
Z = -3992745
68 Z = -1230872
11
XDOT = -15749
079061 XDOT = -4816
549279
YDOT = -3518
603604 feet/sec YDOT = -1126
241712 meter/sec
ZDOT = 19302
928019 ZDOT = 5860
174480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21715279
26 X = -6618817
12
Y = -2703805
95 feet Y = -824120
05 meter
Z = -4054749
03 Z = -1235887
51
XDOT = -1731
600006 XDOT = -527
791682
YDOT = -14602
997168 feet/sec YDOT = -4450
993537 meter/sec
ZDOT = 19200
515819 ZDOT = 5852
317222
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
50934649
00016717 00000-0 10270-3 0 9034
2 25544 51
6423 124
2894 0007113 55
3979 304
7844 15
53994018 36603
Satellite: ISS
Catalog Number: 25544
Epoch time: 17006
50934649 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 124
2894 deg
Eccentricity:
0007113
Arg of perigee: 55
3979 deg
Mean anomaly: 304
7844 deg
Mean motion: 15
53994018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3660
Checksum: 321
Coasting Arc #5 (Orbit 3675)
---------------------------------------
Vector Time (GMT): 2017/007/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3544796
00 A = 6789562
14 meter
Y = -5766964
56 meter E =
0014309
Z = -492082
17 I = 51
98631
XDOT = 3808
679206 Wp = 109
48729
YDOT = 2841
740867 meter/sec RA = 118
32049 deg
ZDOT = -6013
967424 TA = 75
79273
MA = 75
63382
Ha = 223
642 n
mi
Hp = 212
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11629908
13 X = 3611410
53
Y = -18920487
40 feet Y = -5726951
78 meter
Z = -1614442
80 Z = -474701
05
XDOT = 12495
666686 XDOT = 3805
832077
YDOT = 9323
296808 feet/sec YDOT = 2884
316440 meter/sec
ZDOT = -19730
864251 ZDOT = -5995
472750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21670358
82 X = 6605125
37
Y = 4886602
95 feet Y = 1489436
58 meter
Z = -1537105
19 Z = -468509
66
XDOT = -4375
481284 XDOT = -1333
646695
YDOT = 13381
575909 feet/sec YDOT = 4078
704337 meter/sec
ZDOT = -19650
111706 ZDOT = -5989
354048
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
53825815
00016717 00000-0 10270-3 0 9043
2 25544 51
6415 119
1613 0007073 59
8494 300
3359 15
54014772 36763
Satellite: ISS
Catalog Number: 25544
Epoch time: 17007
53825815 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 119
1613 deg
Eccentricity:
0007073
Arg of perigee: 59
8494 deg
Mean anomaly: 300
3359 deg
Mean motion: 15
54014772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3676
Checksum: 310
Coasting Arc #6 (Orbit 3691)
---------------------------------------
Vector Time (GMT): 2017/008/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3976500
19 A = 6787812
82 meter
Y = 5072437
66 meter E =
0021031
Z = 2096018
44 I = 51
99603
XDOT = -2788
017239 Wp = 67
34933
YDOT = -4497
610977 meter/sec RA = 113
37354 deg
ZDOT = 5558
679311 TA = 315
75928
MA = 315
92723
Ha = 223
707 n
mi
Hp = 212
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13046260
45 X = -4043107
41
Y = 16641855
84 feet Y = 5027597
20 meter
Z = 6876700
91 Z = 2076540
32
XDOT = -9147
038185 XDOT = -2764
518006
YDOT = -14755
941524 feet/sec YDOT = -4528
657428 meter/sec
ZDOT = 18237
136847 ZDOT = 5545
192728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20102010
69 X = -6127092
86
Y = -6651836
79 feet Y = -2027479
85 meter
Z = 6790252
30 Z = 2069668
90
XDOT = 10239
659128 XDOT = 3121
048102
YDOT = -12264
236469 feet/sec YDOT = -3738
139276 meter/sec
ZDOT = 18178
671263 ZDOT = 5540
859001
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
56716407
00016717 00000-0 10270-3 0 9054
2 25544 51
6425 114
0337 0007132 63
2536 296
9346 15
54027557 36922
Satellite: ISS
Catalog Number: 25544
Epoch time: 17008
56716407 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 114
0337 deg
Eccentricity:
0007132
Arg of perigee: 63
2536 deg
Mean anomaly: 296
9346 deg
Mean motion: 15
54027557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3692
Checksum: 310
Coasting Arc #7 (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 = -3467428
55 A = 6777915
31 meter
Y = -2457386
02 meter E =
0010773
Z = 5272608
69 I = 51
96592
XDOT = 3428
387005 Wp = 60
63318
YDOT = -6806
236473 meter/sec RA = 111
36946 deg
ZDOT = -911
003374 TA = 38
07209
MA = 37
99601
Ha = 223
863 n
mi
Hp = 212
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11376077
93 X = -3465303
53
Y = -8062290
09 feet Y = -2496149
63 meter
Z = 17298584
95 Z = 5255769
94
XDOT = 11247
988861 XDOT = 3508
666507
YDOT = -22330
172156 feet/sec YDOT = -6767
449008 meter/sec
ZDOT = -2988
856213 ZDOT = -894
154794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10911663
18 X = -3325874
94
Y = 8825552
32 feet Y = 2690028
35 meter
Z = 17225038
31 Z = 5250191
68
XDOT = -17722
668230 XDOT = -5401
869276
YDOT = -16183
091772 feet/sec YDOT = -4932
606372 meter/sec
ZDOT = -2913
649166 ZDOT = -888
080266
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
95300325
00016717 00000-0 10270-3 0 9066
2 25544 51
6403 112
1133 0007382 61
1068 299
0829 15
54021704 36989
Satellite: ISS
Catalog Number: 25544
Epoch time: 17008
95300325 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 112
1133 deg
Eccentricity:
0007382
Arg of perigee: 61
1068 deg
Mean anomaly: 299
0829 deg
Mean motion: 15
54021704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3698
Checksum: 289
Coasting Arc #8 (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 = 2721474
92 A = 6780052
81 meter
Y = 3983936
12 meter E =
0017165
Z = -4778435
93 I = 51
98467
XDOT = -3966
498757 Wp = 91
23330
YDOT = 5957
926678 meter/sec RA = 106
39631 deg
ZDOT = 2716
314477 TA = 205
49103
MA = 205
57578
Ha = 223
778 n
mi
Hp = 212
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8928723
48 X = 2699934
52
Y = 13070656
55 feet Y = 4014249
45 meter
Z = -15677283
24 Z = -4765267
84
XDOT = -13013
447365 XDOT = -4046
021534
YDOT = 19547
003538 feet/sec YDOT = 5913
125748 meter/sec
ZDOT = 8911
792903 ZDOT = 2696
853847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14960437
97 X = 4559941
49
Y = -5342112
43 feet Y = -1628275
87 meter
Z = -15620131
44 Z = -4761016
06
XDOT = 15111
463514 XDOT = 4605
974079
YDOT = 16592
078877 feet/sec YDOT = 5057
265642 meter/sec
ZDOT = 8825
237291 ZDOT = 2689
932326
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
91759383
00016717 00000-0 10270-3 0 9076
2 25544 51
6410 107
3056 0007386 63
9056 296
2856 15
54023484 37132
Satellite: ISS
Catalog Number: 25544
Epoch time: 17009
91759383 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 107
3056 deg
Eccentricity:
0007386
Arg of perigee: 63
9056 deg
Mean anomaly: 296
2856 deg
Mean motion: 15
54023484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3713
Checksum: 322
Coasting Arc #9 (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 = -1927649
44 A = 6783580
09 meter
Y = -5296316
74 meter E =
0018894
Z = 3762664
54 I = 52
00518
XDOT = 4353
620021 Wp = 77
27582
YDOT = -4644
061363 meter/sec RA = 101
43207 deg
ZDOT = -4284
462792 TA = 57
93113
MA = 57
74780
Ha = 223
820 n
mi
Hp = 212
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6324309
18 X = -1886558
45
Y = -17376367
24 feet Y = -5317643
60 meter
Z = 12344699
92 Z = 3753399
99
XDOT = 14283
530251 XDOT = 4426
039222
YDOT = -15236
421793 feet/sec YDOT = -4594
970937 meter/sec
ZDOT = -14056
636457 ZDOT = -4263
138929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18408722
53 X = -5610978
63
Y = 2008511
32 feet Y = 612194
25 meter
Z = 12304936
35 Z = 3750544
60
XDOT = -11158
979989 XDOT = -3401
257101
YDOT = -16292
900769 feet/sec YDOT = -4966
076154 meter/sec
ZDOT = -13962
108043 ZDOT = -4255
650531
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
94648529
00016717 00000-0 10270-3 0 9081
2 25544 51
6412 102
1778 0007484 67
1012 293
0930 15
54053057 37299
Satellite: ISS
Catalog Number: 25544
Epoch time: 17010
94648529 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 102
1778 deg
Eccentricity:
0007484
Arg of perigee: 67
1012 deg
Mean anomaly: 293
0930 deg
Mean motion: 15
54053057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 304
Coasting Arc #10 (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 = 1192530
72 A = 6787115
26 meter
Y = 6228218
05 meter E =
0012686
Z = -2418047
71 I = 52
02244
XDOT = -4572
467148 Wp = 60
67542
YDOT = 2958
395247 meter/sec RA = 96
47863 deg
ZDOT = 5392
219285 TA = 272
45248
MA = 272
59771
Ha = 223
810 n
mi
Hp = 212
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3912502
37 X = 1134542
10
Y = 20433786
27 feet Y = 6241229
71 meter
Z = -7933227
40 Z = -2412395
13
XDOT = -15001
532637 XDOT = -4631
401291
YDOT = 9706
021152 feet/sec YDOT = 2906
932846 meter/sec
ZDOT = 17691
008153 ZDOT = 5369
865044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20800789
55 X = 6340080
65
Y = 741767
71 feet Y = 226090
80 meter
Z = -7909508
69 Z = -2410818
25
XDOT = 6106
244539 XDOT = 1861
183336
YDOT = 15397
944125 feet/sec YDOT = 4693
293369 meter/sec
ZDOT = 17592
238856 ZDOT = 5362
114403
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
91106662
00016717 00000-0 10270-3 0 9097
2 25544 51
6412 97
3710 0007409 70
8034 289
3920 15
54040343 37440
Satellite: ISS
Catalog Number: 25544
Epoch time: 17011
91106662 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 97
3710 deg
Eccentricity:
0007409
Arg of perigee: 70
8034 deg
Mean anomaly: 289
3920 deg
Mean motion: 15
54040343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3744
Checksum: 291
Coasting Arc #11 (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 = -418484
44 A = 6789293
52 meter
Y = -6727076
66 meter E =
0018782
Z = 766663
25 I = 52
03379
XDOT = 4695
992462 Wp = 108
46560
YDOT = -986
837857 meter/sec RA = 91
53260 deg
ZDOT = -5981
932470 TA = 63
29231
MA = 63
10017
Ha = 223
808 n
mi
Hp = 212
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1372980
44 X = -346953
44
Y = -22070461
47 feet Y = -6731356
53 meter
Z = 2515299
37 Z = 764803
65
XDOT = 15406
799415 XDOT = 4735
735338
YDOT = -3237
657010 feet/sec YDOT = -934
101453 meter/sec
ZDOT = -19625
762696 ZDOT = -5959
024711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21874782
70 X = -6667433
77
Y = -3243324
76 feet Y = -988565
39 meter
Z = 2508346
46 Z = 764544
00
XDOT = -165
586344 XDOT = -50
470718
YDOT = -14272
929591 feet/sec YDOT = -4350
388939 meter/sec
ZDOT = -19524
906396 ZDOT = -5951
191470
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
93994672
00016717 00000-0 10270-3 0 9108
2 25544 51
6425 92
2424 0007444 74
3367 285
8606 15
54056264 37606
Satellite: ISS
Catalog Number: 25544
Epoch time: 17012
93994672 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 92
2424 deg
Eccentricity:
0007444
Arg of perigee: 74
3367 deg
Mean anomaly: 285
8606 deg
Mean motion: 15
54056264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 318
Coasting Arc #12 (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 = -304494
18 A = 6789185
97 meter
Y = 6713698
89 meter E =
0020594
Z = 901231
36 I = 52
03260
XDOT = -4720
377270 Wp = 62
73308
YDOT = -1026
867024 meter/sec RA = 86
58997 deg
ZDOT = 5959
918467 TA = 306
97279
MA = 307
16115
Ha = 223
844 n
mi
Hp = 212
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -998996
67 X = -383923
52
Y = 22026571
17 feet Y = 6709849
67 meter
Z = 2956795
79 Z = 899559
67
XDOT = -15486
802067 XDOT = -4737
493570
YDOT = -3368
986298 feet/sec YDOT = -1079
749466 meter/sec
ZDOT = 19553
538277 ZDOT = 5936
947141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21423314
40 X = 6529826
23
Y = 5221115
48 feet Y = 1591396
00 meter
Z = 2948224
24 Z = 898618
75
XDOT = -5916
642288 XDOT = -1803
392569
YDOT = 13116
516764 feet/sec YDOT = 3997
914310 meter/sec
ZDOT = 19452
762559 ZDOT = 5929
202028
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
96882057
00016717 00000-0 10270-3 0 9116
2 25544 51
6417 87
1147 0007513 77
5306 282
6687 15
54062161 37761
Satellite: ISS
Catalog Number: 25544
Epoch time: 17013
96882057 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 87
1147 deg
Eccentricity:
0007513
Arg of perigee: 77
5306 deg
Mean anomaly: 282
6687 deg
Mean motion: 15
54062161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3776
Checksum: 321
Coasting Arc #13 (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 = 1096004
15 A = 6786739
81 meter
Y = -6198699
00 meter E =
0011603
Z = -2543022
76 I = 52
02252
XDOT = 4634
345700 Wp = 100
76676
YDOT = 2991
269794 meter/sec RA = 81
64368 deg
ZDOT = -5316
610773 TA = 107
60528
MA = 107
47851
Ha = 223
801 n
mi
Hp = 212
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3595814
14 X = 1177590
67
Y = -20336938
98 feet Y = -6185986
50 meter
Z = -8343250
53 Z = -2537500
81
XDOT = 15204
546261 XDOT = 4626
377119
YDOT = 9813
877278 feet/sec YDOT = 3043
049751 meter/sec
ZDOT = -17442
948730 ZDOT = -5294
118258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19386887
26 X = -5909123
24
Y = -7147928
19 feet Y = -2178688
51 meter
Z = -8317843
49 Z = -2535278
70
XDOT = 11816
900951 XDOT = 3601
791410
YDOT = -11953
443959 feet/sec YDOT = -3643
409719 meter/sec
ZDOT = -17344
634801 ZDOT = -5286
644687
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
93338465
00016717 00000-0 10270-3 0 9124
2 25544 51
6424 82
3070 0007455 81
1284 279
0712 15
54080368 37917
Satellite: ISS
Catalog Number: 25544
Epoch time: 17014
93338465 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 82
3070 deg
Eccentricity:
0007455
Arg of perigee: 81
1284 deg
Mean anomaly: 279
0712 deg
Mean motion: 15
54080368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 305
Coasting Arc #14 (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 = -1867886
58 A = 6783137
37 meter
Y = 5236695
47 meter E =
0018627
Z = 3870475
36 I = 52
00473
XDOT = -4445
405781 Wp = 92
82550
YDOT = -4673
901474 meter/sec RA = 76
68841 deg
ZDOT = 4160
285467 TA = 313
64265
MA = 313
79697
Ha = 223
853 n
mi
Hp = 212
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6128236
81 X = -1945106
38
Y = 17180759
40 feet Y = 5215375
72 meter
Z = 12698409
98 Z = 3861214
37
XDOT = -14584
664637 XDOT = -4413
018899
YDOT = -15334
322422 feet/sec YDOT = -4723
431927 meter/sec
ZDOT = 13649
230534 ZDOT = 4138
770076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15986663
68 X = 4872735
09
Y = 8844034
26 feet Y = 2695661
64 meter
Z = 12656738
86 Z = 3857774
00
XDOT = -16811
389712 XDOT = -5124
111584
YDOT = 10904
052717 feet/sec YDOT = 3323
555268 meter/sec
ZDOT = 13555
523199 ZDOT = 4131
723471
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
96224749
00016717 00000-0 10270-3 0 9138
2 25544 51
6423 77
1787 0007454 84
8958 275
3046 15
54084378 38072
Satellite: ISS
Catalog Number: 25544
Epoch time: 17015
96224749 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 77
1787 deg
Eccentricity:
0007454
Arg of perigee: 84
8958 deg
Mean anomaly: 275
3046 deg
Mean motion: 15
54084378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 344
Coasting Arc #15 (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 = -3702861
61 A = 6785228
97 meter
Y = -4707353
38 meter E =
0020279
Z = 3171121
64 I = 52
01235
XDOT = 2600
688158 Wp = 90
73808
YDOT = -5338
214296 meter/sec RA = 76
23505 deg
ZDOT = -4861
032608 TA = 52
84098
MA = 52
65595
Ha = 223
836 n
mi
Hp = 212
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12148496
08 X = -3665351
06
Y = -15444072
77 feet Y = -4748551
55 meter
Z = 10403942
39 Z = 3153225
68
XDOT = 8532
441464 XDOT = 2683
800271
YDOT = -17513
826431 feet/sec YDOT = -5308
666928 meter/sec
ZDOT = -15948
269712 ZDOT = -4848
197638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10223325
71 X = -3116069
68
Y = 16828594
22 feet Y = 5129355
52 meter
Z = 10326150
59 Z = 3147410
70
XDOT = -18199
022943 XDOT = -5547
062193
YDOT = -1251
407087 feet/sec YDOT = -381
428880 meter/sec
ZDOT = -15890
870140 ZDOT = -4843
537219
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
02655056
00016717 00000-0 10270-3 0 9146
2 25544 51
6435 76
8592 0007440 84
6769 275
5233 15
54094059 38086
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
02655056 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 76
8592 deg
Eccentricity:
0007440
Arg of perigee: 84
6769 deg
Mean anomaly: 275
5233 deg
Mean motion: 15
54094059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3808
Checksum: 326
Coasting Arc #16 (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 = 3311780
75 A = 6788199
45 meter
Y = 5679638
69 meter E =
0013747
Z = -1682833
96 I = 52
01382
XDOT = -3472
315948 Wp = 61
95309
YDOT = 3712
057067 meter/sec RA = 71
28340 deg
ZDOT = 5736
788912 TA = 279
70957
MA = 279
86482
Ha = 223
745 n
mi
Hp = 212
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10865422
39 X = 3256197
69
Y = 18633985
20 feet Y = 5716362
45 meter
Z = -5521108
78 Z = -1666881
64
XDOT = -11392
112690 XDOT = -3541
433169
YDOT = 12178
664918 feet/sec YDOT = 3672
840889 meter/sec
ZDOT = 18821
485932 ZDOT = 5719
753810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13382434
77 X = 4078966
12
Y = -16939630
41 feet Y = -5163199
35 meter
Z = -5452046
54 Z = -1661783
79
XDOT = 14302
480373 XDOT = 4359
396018
YDOT = 5310
440822 feet/sec YDOT = 1618
622362 meter/sec
ZDOT = 18745
920612 ZDOT = 5713
756603
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
99110211
00016717 00000-0 10270-3 0 9152
2 25544 51
6434 72
0507 0007362 87
7607 272
4389 15
54111979 38233
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
99110211 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 72
0507 deg
Eccentricity:
0007362
Arg of perigee: 87
7607 deg
Mean anomaly: 272
4389 deg
Mean motion: 15
54111979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 309
Coasting Arc #17 (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 = -2692170
82 A = 6789507
78 meter
Y = -6226378
26 meter E =
0018164
Z = -42270
16 I = 52
00576
XDOT = 4343
244983 Wp = 118
93408
YDOT = -1850
238762 meter/sec RA = 66
33835 deg
ZDOT = -6043
447700 TA = 61
51896
MA = 61
33612
Ha = 223
801 n
mi
Hp = 212
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8832581
42 X = -2622140
44
Y = -20427750
20 feet Y = -6256092
37 meter
Z = -138681
64 Z = -55177
58
XDOT = 14249
491415 XDOT = 4392
967805
YDOT = -6070
337145 feet/sec YDOT = -1801
391729 meter/sec
ZDOT = -19827
584316 ZDOT = -6022
229011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15535503
18 X = -4735221
37
Y = 15935404
41 feet Y = 4857111
26 meter
Z = -194249
14 Z = -59207
14
XDOT = -9921
000155 XDOT = -3023
920847
YDOT = -9856
529118 feet/sec YDOT = -3004
270075 meter/sec
ZDOT = -19733
974822 ZDOT = -6014
915526
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
01995414
00016717 00000-0 10270-3 0 9164
2 25544 51
6427 66
9223 0007387 92
9504 267
2494 15
54066614 38394
Satellite: ISS
Catalog Number: 25544
Epoch time: 17018
01995414 = yrday
fracday
Element set: 916
Inclination: 51
6427 deg
RA of node: 66
9223 deg
Eccentricity:
0007387
Arg of perigee: 92
9504 deg
Mean anomaly: 267
2494 deg
Mean motion: 15
54066614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3839
Checksum: 332
Coasting Arc #18 (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 = 1911009
07 A = 6788087
10 meter
Y = 6279296
94 meter E =
0020481
Z = 1700283
20 I = 51
98793
XDOT = -5104
804321 Wp = 74
59929
YDOT = -11
167893 meter/sec RA = 61
39136 deg
ZDOT = 5726
806733 TA = 303
95975
MA = 304
15425
Ha = 223
634 n
mi
Hp = 212
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6269714
78 X = 1832391
25
Y = 20601367
92 feet Y = 6300227
57 meter
Z = 5578356
97 Z = 1709375
21
XDOT = -16748
045671 XDOT = -5132
117812
YDOT = -36
640068 feet/sec YDOT = -68
405927 meter/sec
ZDOT = 18788
736002 ZDOT = 5701
943057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16448055
21 X = 5013367
23
Y = -13883552
78 feet Y = -4231706
89 meter
Z = 5617133
79 Z = 1712102
38
XDOT = 5637
344592 XDOT = 1718
262632
YDOT = 14304
579734 feet/sec YDOT = 4360
035903 meter/sec
ZDOT = 18679
456075 ZDOT = 5693
498212
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
04879769
00016717 00000-0 10270-3 0 9173
2 25544 51
6428 61
7935 0007206 95
3275 264
8700 15
54130433 38552
Satellite: ISS
Catalog Number: 25544
Epoch time: 17019
04879769 = yrday
fracday
Element set: 917
Inclination: 51
6428 deg
RA of node: 61
7935 deg
Eccentricity:
0007206
Arg of perigee: 95
3275 deg
Mean anomaly: 264
8700 deg
Mean motion: 15
54130433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 329
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