[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 23rd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10 7639 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 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
058/16:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 214
0
064/09:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 214
5
065/04:02:19
343 -2
5 3
4 3
4
N/A -2
1 -0
4 220
5
000/00:08:38
687 0
9 0
1 216
5
067/19:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
7
Coasting Arc #1 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2016/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3838687
94 A = 6778242
50 meter
Y = 2491429
81 meter E =
0006135
Z = 4994854
95 I = 51
25908
XDOT = -2081
577563 Wp = 89
90737
YDOT = 7122
827607 meter/sec RA = 274
11293 deg
ZDOT = -1951
018448 TA = 19
13013
MA = 19
10711
Ha = 221
427 n
mi
Hp = 213
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12594120
52 X = 3786280
56
Y = 8173982
32 feet Y = 2534064
10 meter
Z = 16387319
40 Z = 5013374
34
XDOT = -6829
322713 XDOT = -2151
595091
YDOT = 23368
856978 feet/sec YDOT = 7099
158316 meter/sec
ZDOT = -6400
979160 ZDOT = -1961
300851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6956910
44 X = 2120466
30
Y = 13206238
08 feet Y = 4025261
37 meter
Z = 16467142
09 Z = 5019184
91
XDOT = -16306
128378 XDOT = -4970
107930
YDOT = 16637
103392 feet/sec YDOT = 5070
989114 meter/sec
ZDOT = -6446
829241 ZDOT = -1964
993553
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 16053
54484014
00016717 00000-0 10270-3 0 9002
2 25544 51
6416 274
7274 0003491 158
1285 202
0018 15
54258795 26995
Satellite: ISS
Catalog Number: 25544
Epoch time: 16053
54484014 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 274
7274 deg
Eccentricity:
0003491
Arg of perigee: 158
1285 deg
Mean anomaly: 202
0018 deg
Mean motion: 15
54258795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 311
Coasting Arc #2 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2016/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3412566
17 A = 6781521
20 meter
Y = -4126771
61 meter E =
0010454
Z = -4172436
64 I = 51
26730
XDOT = 2854
966581 Wp = 124
80495
YDOT = -6080
075528 meter/sec RA = 269
09094 deg
ZDOT = 3679
231991 TA = 183
20485
MA = 183
21155
Ha = 221
540 n
mi
Hp = 213
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11196083
24 X = -3345898
48
Y = -13539276
93 feet Y = -4164560
96 meter
Z = -13689096
57 Z = -4188851
23
XDOT = 9366
688257 XDOT = 2904
871550
YDOT = -19947
754357 feet/sec YDOT = -6047
869894 meter/sec
ZDOT = 12070
971099 ZDOT = 3693
222397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3443500
58 X = -1049578
98
Y = -17171889
16 feet Y = -5233991
82 meter
Z = -13759512
75 Z = -4193899
49
XDOT = 16319
502706 XDOT = 4974
184425
YDOT = -12992
361615 feet/sec YDOT = -3960
071820 meter/sec
ZDOT = 12132
691012 ZDOT = 3698
044220
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 16054
50930370
00016717 00000-0 10270-3 0 9011
2 25544 51
6403 269
9173 0003513 160
4398 199
6890 15
54253869 27145
Satellite: ISS
Catalog Number: 25544
Epoch time: 16054
50930370 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 269
9173 deg
Eccentricity:
0003513
Arg of perigee: 160
4398 deg
Mean anomaly: 199
6890 deg
Mean motion: 15
54253869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 320
Coasting Arc #3 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2016/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2872617
24 A = 6785314
43 meter
Y = 5428064
28 meter E =
0015000
Z = 2865967
78 I = 51
28145
XDOT = -3580
429581 Wp = 110
59080
YDOT = 4558
458525 meter/sec RA = 264
08149 deg
ZDOT = -5028
653604 TA = 36
58895
MA = 36
48659
Ha = 221
302 n
mi
Hp = 213
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9424597
23 X = 2797784
38
Y = 17808609
85 feet Y = 5459769
77 meter
Z = 9402781
45 Z = 2879739
50
XDOT = -11746
816211 XDOT = -3606
710680
YDOT = 14955
572589 feet/sec YDOT = 4518
272153 meter/sec
ZDOT = -16498
207361 ZDOT = -5046
110581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 244430
65 X = 74502
46
Y = 20119685
17 feet Y = 6132480
04 meter
Z = 9461524
15 Z = 2883872
56
XDOT = -15699
145868 XDOT = -4785
099660
YDOT = 8010
012555 feet/sec YDOT = 2441
451827 meter/sec
ZDOT = -16574
673196 ZDOT = -5051
960390
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 16055
53805378
00016717 00000-0 10270-3 0 9025
2 25544 51
6399 264
7884 0003362 164
6423 195
4833 15
54296030 27304
Satellite: ISS
Catalog Number: 25544
Epoch time: 16055
53805378 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 264
7884 deg
Eccentricity:
0003362
Arg of perigee: 164
6423 deg
Mean anomaly: 195
4833 deg
Mean motion: 15
54296030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 323
Coasting Arc #4 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2016/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2247634
19 A = 6788205
48 meter
Y = -6276554
95 meter E =
0007058
Z = -1270382
81 I = 51
29433
XDOT = 4222
024534 Wp = 59
30301
YDOT = -2681
743060 meter/sec RA = 259
08051 deg
ZDOT = 5807
442894 TA = 286
81836
MA = 286
89576
Ha = 221
344 n
mi
Hp = 214
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7374127
92 X = -2171110
26
Y = -20592371
87 feet Y = -6301261
79 meter
Z = -4167922
60 Z = -1281114
37
XDOT = 13851
786529 XDOT = 4223
488995
YDOT = -8798
369620 feet/sec YDOT = -2634
520586 meter/sec
ZDOT = 19053
290335 ZDOT = 5827
956071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2443821
74 X = 744876
87
Y = -21727183
79 feet Y = -6622445
62 meter
Z = -4213352
64 Z = -1284229
88
XDOT = 14613
209698 XDOT = 4454
106316
YDOT = -2051
096667 feet/sec YDOT = -625
174264 meter/sec
ZDOT = 19142
670226 ZDOT = 5834
685885
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 16056
50249957
00016717 00000-0 10270-3 0 9039
2 25544 51
6391 259
9788 0003502 170
2692 189
8529 15
54272446 27452
Satellite: ISS
Catalog Number: 25544
Epoch time: 16056
50249957 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 259
9788 deg
Eccentricity:
0003502
Arg of perigee: 170
2692 deg
Mean anomaly: 189
8529 deg
Mean motion: 15
54272446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 345
Coasting Arc #5 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2016/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1461070
11 A = 6788753
54 meter
Y = 6602736
05 meter E =
0014019
Z = -506087
61 I = 51
30334
XDOT = -4790
542834 Wp = 146
31878
YDOT = 610
212180 meter/sec RA = 254
08561 deg
ZDOT = -5959
954151 TA = 39
16829
MA = 39
06691
Ha = 221
252 n
mi
Hp = 214
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4793537
10 X = 1389586
42
Y = 21662519
83 feet Y = 6618674
94 meter
Z = -1660392
42 Z = -499164
69
XDOT = -15717
004047 XDOT = -4768
059752
YDOT = 2002
008463 feet/sec YDOT = 556
766054 meter/sec
ZDOT = -19553
655350 ZDOT = -5983
170629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4826468
39 X = -1471107
56
Y = 21657401
24 feet Y = 6601175
90 meter
Z = -1631514
96 Z = -497285
76
XDOT = -13390
718977 XDOT = -4081
491144
YDOT = -4441
949140 feet/sec YDOT = -1353
906098 meter/sec
ZDOT = -19654
395405 ZDOT = -5990
659720
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 16057
53122995
00016717 00000-0 10270-3 0 9046
2 25544 51
6391 254
8487 0003419 172
0879 188
0328 15
54290932 27612
Satellite: ISS
Catalog Number: 25544
Epoch time: 16057
53122995 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 254
8487 deg
Eccentricity:
0003419
Arg of perigee: 172
0879 deg
Mean anomaly: 188
0328 deg
Mean motion: 15
54290932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 332
Coasting Arc #6 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2016/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -561238
82 A = 6786734
61 meter
Y = -6393090
45 meter E =
0013376
Z = 2194199
60 I = 51
30519
XDOT = 5210
840972 Wp = 86
11762
YDOT = 1420
551902 meter/sec RA = 249
08874 deg
ZDOT = 5443
928328 TA = 298
37032
MA = 298
50513
Ha = 221
184 n
mi
Hp = 214
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1841334
69 X = -500366
37
Y = -20974706
19 feet Y = -6399025
95 meter
Z = 7198817
59 Z = 2191621
93
XDOT = 17095
934949 XDOT = 5168
124685
YDOT = 4660
603352 feet/sec YDOT = 1478
584839 meter/sec
ZDOT = 17860
657245 ZDOT = 5469
137144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6835069
27 X = 2083329
11
Y = -19918729
74 feet Y = -6071228
82 meter
Z = 7188728
80 Z = 2191124
54
XDOT = 12147
993476 XDOT = 3702
708411
YDOT = 10686
932840 feet/sec YDOT = 3257
377130 meter/sec
ZDOT = 17969
691598 ZDOT = 5477
161999
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 16058
55994938
00016717 00000-0 10270-3 0 9054
2 25544 51
6378 249
7184 0003602 176
7712 183
3464 15
54321915 27777
Satellite: ISS
Catalog Number: 25544
Epoch time: 16058
55994938 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 249
7184 deg
Eccentricity:
0003602
Arg of perigee: 176
7712 deg
Mean anomaly: 183
3464 deg
Mean motion: 15
54321915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 345
Coasting Arc #7 (Orbit 2778)
---------------------------------------
Vector Time (GMT): 2016/058/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3293140
71 A = 6777409
28 meter
Y = 2920566
59 meter E =
0014143
Z = -5165459
83 I = 51
27813
XDOT = -3750
444818 Wp = 95
93494
YDOT = -6546
785518 meter/sec RA = 248
22644 deg
ZDOT = -1315
098064 TA = 161
37662
MA = 161
32481
Ha = 221
270 n
mi
Hp = 213
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10804267
43 X = -3300463
07
Y = 9581911
38 feet Y = 2883698
91 meter
Z = -16947046
67 Z = -5181475
10
XDOT = -12304
608982 XDOT = -3670
570169
YDOT = -21478
955112 feet/sec YDOT = -6588
279042 meter/sec
ZDOT = -4314
626194 ZDOT = -1333
121810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2693340
76 X = -820930
26
Y = 14103773
19 feet Y = 4298830
07 meter
Z = -17016965
32 Z = -5186771
03
XDOT = -21759
523059 XDOT = -6632
302628
YDOT = -9436
148765 feet/sec YDOT = -2876
138144 meter/sec
ZDOT = -4391
646993 ZDOT = -1338
574003
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 16058
68854085
00016717 00000-0 10270-3 0 9067
2 25544 51
6400 249
0757 0003909 175
0393 185
0799 15
54313288 27795
Satellite: ISS
Catalog Number: 25544
Epoch time: 16058
68854085 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 249
0757 deg
Eccentricity:
0003909
Arg of perigee: 175
0393 deg
Mean anomaly: 185
0799 deg
Mean motion: 15
54313288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2779
Checksum: 346
Coasting Arc #8 (Orbit 2794)
---------------------------------------
Vector Time (GMT): 2016/059/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4103461
09 A = 6776905
88 meter
Y = -1212931
18 meter E =
0003726
Z = 5252561
84 I = 51
29023
XDOT = 2950
542705 Wp = 133
17228
YDOT = 7048
772570 meter/sec RA = 243
19937 deg
ZDOT = -679
539270 TA = 323
33300
MA = 323
35849
Ha = 221
037 n
mi
Hp = 214
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13462798
87 X = 4091204
89
Y = -3979432
99 feet Y = -1167111
47 meter
Z = 17232814
43 Z = 5272465
66
XDOT = 9680
258217 XDOT = 2874
803181
YDOT = 23125
894257 feet/sec YDOT = 7081
343933 meter/sec
ZDOT = -2229
459546 ZDOT = -665
391145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8008545
52 X = 2441004
67
Y = -11399898
49 feet Y = -3474689
06 meter
Z = 17319302
71 Z = 5278923
47
XDOT = 21113
967890 XDOT = 6435
537413
YDOT = 11547
967791 feet/sec YDOT = 3519
820583 meter/sec
ZDOT = -2169
310895 ZDOT = -661
205961
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 16059
71724943
00016717 00000-0 10270-3 0 9072
2 25544 51
6408 243
9456 0003843 179
6148 180
5008 15
54328583 27952
Satellite: ISS
Catalog Number: 25544
Epoch time: 16059
71724943 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 243
9456 deg
Eccentricity:
0003843
Arg of perigee: 179
6148 deg
Mean anomaly: 180
5008 deg
Mean motion: 15
54328583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2795
Checksum: 338
Coasting Arc #9 (Orbit 2809)
---------------------------------------
Vector Time (GMT): 2016/060/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4805878
75 A = 6778932
51 meter
Y = -505603
70 meter E =
0012954
Z = -4766490
92 I = 51
31333
XDOT = -1858
076851 Wp = 125
02856
YDOT = -6956
292757 meter/sec RA = 238
17696 deg
ZDOT = 2609
070496 TA = 170
86105
MA = 170
83745
Ha = 221
065 n
mi
Hp = 214
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15767318
73 X = -4776714
36
Y = -1658804
79 feet Y = -559183
66 meter
Z = -15638093
57 Z = -4789765
64
XDOT = -6096
052661 XDOT = -1792
825429
YDOT = -22822
482798 feet/sec YDOT = -6976
705889 meter/sec
ZDOT = 8559
942572 ZDOT = 2600
203698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13173899
48 X = -4015404
56
Y = 8639728
93 feet Y = 2633389
38 meter
Z = -15738913
57 Z = -4797220
86
XDOT = -18586
312901 XDOT = -5665
108172
YDOT = -12801
503248 feet/sec YDOT = -3901
898190 meter/sec
ZDOT = 8522
661552 ZDOT = 2597
707241
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 16060
68165303
00016717 00000-0 10270-3 0 9080
2 25544 51
6416 239
1376 0003817 182
2956 177
8180 15
54355888 28103
Satellite: ISS
Catalog Number: 25544
Epoch time: 16060
68165303 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 239
1376 deg
Eccentricity:
0003817
Arg of perigee: 182
2956 deg
Mean anomaly: 177
8180 deg
Mean motion: 15
54355888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2810
Checksum: 327
Coasting Arc #10 (Orbit 2825)
---------------------------------------
Vector Time (GMT): 2016/061/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 890597
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5270791
00 A = 6782740
72 meter
Y = 2073335
99 meter E =
0011506
Z = 3719700
76 I = 51
34302
XDOT = 509
114393 Wp = 102
99728
YDOT = 6362
480447 meter/sec RA = 233
16371 deg
ZDOT = -4259
220348 TA = 32
33782
MA = 32
26734
Ha = 220
919 n
mi
Hp = 214
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17292621
41 X = 5229146
14
Y = 6802283
44 feet Y = 2132044
98 meter
Z = 12203742
66 Z = 3745203
42
XDOT = 1670
322813 XDOT = 458
619033
YDOT = 20874
279681 feet/sec YDOT = 6367
890965 meter/sec
ZDOT = -13973
820039 ZDOT = -4256
870460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17529606
52 X = 5343024
07
Y = -5942738
37 feet Y = -1811346
65 meter
Z = 12313971
99 Z = 3753298
66
XDOT = 14407
526647 XDOT = 4391
414122
YDOT = 13504
451185 feet/sec YDOT = 4116
156721 meter/sec
ZDOT = -13964
684156 ZDOT = -4256
435731
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 16061
71034037
00016717 00000-0 10270-3 0 9095
2 25544 51
6410 234
0081 0003822 184
6955 175
4163 15
54336851 28266
Satellite: ISS
Catalog Number: 25544
Epoch time: 16061
71034037 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 234
0081 deg
Eccentricity:
0003822
Arg of perigee: 184
6955 deg
Mean anomaly: 175
4163 deg
Mean motion: 15
54336851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2826
Checksum: 295
Coasting Arc #11 (Orbit 2840)
---------------------------------------
Vector Time (GMT): 2016/062/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 875488
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5441886
94 A = 6786446
50 meter
Y = -3363193
19 meter E =
0003422
Z = -2266902
91 I = 51
37604
XDOT = 1038
565381 Wp = 79
77656
YDOT = -5323
949108 meter/sec RA = 228
16338 deg
ZDOT = 5413
068243 TA = 254
91315
MA = 254
95102
Ha = 220
838 n
mi
Hp = 214
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17853959
79 X = -5392862
89
Y = -11034098
41 feet Y = -3423774
07 meter
Z = -7437345
50 Z = -2293218
63
XDOT = 3407
366736 XDOT = 1071
727797
YDOT = -17467
024632 feet/sec YDOT = -5312
149296 meter/sec
ZDOT = 17759
410245 ZDOT = 5418
194288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20661156
42 X = -6297520
48
Y = 3453955
45 feet Y = 1052765
62 meter
Z = -7550902
13 Z = -2301514
97
XDOT = -8795
448953 XDOT = -2680
852841
YDOT = -13791
473367 feet/sec YDOT = -4203
641082 meter/sec
ZDOT = 17782
511220 ZDOT = 5420
109420
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 16062
67472336
00016717 00000-0 10270-3 0 9101
2 25544 51
6416 229
1996 0003619 191
7608 168
3461 15
54346177 28411
Satellite: ISS
Catalog Number: 25544
Epoch time: 16062
67472336 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 229
1996 deg
Eccentricity:
0003619
Arg of perigee: 191
7608 deg
Mean anomaly: 168
3461 deg
Mean motion: 15
54346177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2841
Checksum: 326
Coasting Arc #12 (Orbit 2856)
---------------------------------------
Vector Time (GMT): 2016/063/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 875488
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5205275
26 A = 6788471
53 meter
Y = 4312679
90 meter E =
0015002
Z = 521530
61 I = 51
40484
XDOT = -2703
436703 Wp = 142
36262
YDOT = 3994
129806 meter/sec RA = 223
17293 deg
ZDOT = -5967
020154 TA = 31
98908
MA = 31
89810
Ha = 220
738 n
mi
Hp = 214
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17077674
74 X = 5154129
60
Y = 14149212
29 feet Y = 4370602
82 meter
Z = 1711058
43 Z = 546691
65
XDOT = -8869
542990 XDOT = -2718
914257
YDOT = 13104
100413 feet/sec YDOT = 3963
811154 meter/sec
ZDOT = -19576
837777 ZDOT = -5980
190536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22146135
62 X = 6750142
14
Y = -1006533
16 feet Y = -306791
31 meter
Z = 1819470
24 Z = 554574
53
XDOT = 2267
763372 XDOT = 691
214276
YDOT = 13961
989830 feet/sec YDOT = 4255
614500 meter/sec
ZDOT = -19634
602370 ZDOT = -5984
626802
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 16063
70338794
00016717 00000-0 10270-3 0 9116
2 25544 51
6414 224
0699 0003723 193
9964 166
1086 15
54380142 28574
Satellite: ISS
Catalog Number: 25544
Epoch time: 16063
70338794 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 224
0699 deg
Eccentricity:
0003723
Arg of perigee: 193
9964 deg
Mean anomaly: 166
1086 deg
Mean motion: 15
54380142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2857
Checksum: 324
Coasting Arc #13 (Orbit 2867)
---------------------------------------
Vector Time (GMT): 2016/064/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 875488
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 375883
90 A = 6779781
80 meter
Y = 5022671
13 meter E =
0008181
Z = -4545675
70 I = 51
38948
XDOT = -6630
051020 Wp = 87
30914
YDOT = -2290
131097 meter/sec RA = 219
60500 deg
ZDOT = -3083
121179 TA = 151
71892
MA = 151
67448
Ha = 220
520 n
mi
Hp = 214
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1233214
89 X = 341771
84
Y = 16478579
82 feet Y = 5026683
40 meter
Z = -14913634
17 Z = -4543933
05
XDOT = -21752
135894 XDOT = -6588
973182
YDOT = -7513
553467 feet/sec YDOT = -2364
043307 meter/sec
ZDOT = -10115
226964 ZDOT = -3115
227893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13316865
66 X = -4058980
65
Y = 9794216
13 feet Y = 2985277
08 meter
Z = -14906888
20 Z = -4543619
52
XDOT = -4296
809648 XDOT = -1309
667581
YDOT = -21426
906004 feet/sec YDOT = -6530
920950 meter/sec
ZDOT = -10254
102369 ZDOT = -3125
450402
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 16064
41058641
00016717 00000-0 10270-3 0 9126
2 25544 51
6379 220
5440 0003154 199
4629 160
6403 15
54404021 28683
Satellite: ISS
Catalog Number: 25544
Epoch time: 16064
41058641 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 220
5440 deg
Eccentricity:
0003154
Arg of perigee: 199
4629 deg
Mean anomaly: 160
6403 deg
Mean motion: 15
54404021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2868
Checksum: 293
Coasting Arc #14 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/065/04:06:38
687
Vector Time (MET): N/A
Weight (LBS) : 875138
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4897074
28 A = 6781328
78 meter
Y = 996852
32 meter E =
0008180
Z = -4591771
95 I = 51
41159
XDOT = -3995
127444 Wp = 134
11212
YDOT = -5808
612555 meter/sec RA = 215
64721 deg
ZDOT = 2997
484702 TA = 165
93811
MA = 165
91532
Ha = 220
525 n
mi
Hp = 216
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16066516
66 X = -4885552
87
Y = 3270512
86 feet Y = 942153
99 meter
Z = -15064868
61 Z = -4615532
44
XDOT = -13107
373505 XDOT = -3944
437432
YDOT = -19057
127804 feet/sec YDOT = -5853
005026 meter/sec
ZDOT = 9834
267394 ZDOT = 2978
201329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9180183
16 X = 2798119
83
Y = -13469702
23 feet Y = -4105565
24 meter
Z = -15168086
15 Z = -4623232
66
XDOT = 21741
485028 XDOT = 6626
804637
YDOT = 3828
370154 feet/sec YDOT = 1166
887223 meter/sec
ZDOT = 9751
559964 ZDOT = 2972
275477
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 16065
18207264
00016717 00000-0 10270-3 0 9139
2 25544 51
6411 216
6978 0004339 240
2790 119
7931 15
53769031 28801
Satellite: ISS
Catalog Number: 25544
Epoch time: 16065
18207264 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 216
6978 deg
Eccentricity:
0004339
Arg of perigee: 240
2790 deg
Mean anomaly: 119
7931 deg
Mean motion: 15
53769031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 314
Coasting Arc #15 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2016/066/04:06:38
687
Vector Time (MET): N/A
Weight (LBS) : 875138
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5751596
41 A = 6784799
70 meter
Y = 82756
34 meter E =
0008045
Z = 3589999
73 I = 51
44957
XDOT = 2677
057397 Wp = 98
55354
YDOT = 5673
320044 meter/sec RA = 210
64830 deg
ZDOT = -4412
434115 TA = 38
83669
MA = 38
77890
Ha = 220
295 n
mi
Hp = 216
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18870066
95 X = 5732805
17
Y = 271510
31 feet Y = 146969
83 meter
Z = 11778214
34 Z = 3617893
40
XDOT = 8782
996708 XDOT = 2634
851287
YDOT = 18613
254737 feet/sec YDOT = 5703
020220 meter/sec
ZDOT = -14476
489878 ZDOT = -4399
532987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13450032
81 X = -4099570
00
Y = 13129552
25 feet Y = 4001887
52 meter
Z = 11899199
67 Z = 3626876
06
XDOT = -18496
163918 XDOT = -5637
630762
YDOT = -5856
128813 feet/sec YDOT = -1784
948062 meter/sec
ZDOT = -14421
426767 ZDOT = -4395
650879
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 16066
21114267
00016717 00000-0 10270-3 0 9145
2 25544 51
6410 211
5715 0004392 243
7540 116
3161 15
53767734 28966
Satellite: ISS
Catalog Number: 25544
Epoch time: 16066
21114267 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 211
5715 deg
Eccentricity:
0004392
Arg of perigee: 243
7540 deg
Mean anomaly: 116
3161 deg
Mean motion: 15
53767734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 295
Coasting Arc #16 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2016/067/04:06:38
687
Vector Time (MET): N/A
Weight (LBS) : 875138
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6312377
08 A = 6787981
75 meter
Y = -1028850
67 meter E =
0002560
Z = -2269496
86 I = 51
49022
XDOT = -1083
673642 Wp = 359
33198
YDOT = -5307
475356 meter/sec RA = 205
65822 deg
ZDOT = 5422
657812 TA = 335
36721
MA = 335
37944
Ha = 220
186 n
mi
Hp = 216
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20709898
57 X = -6289379
03
Y = -3375494
32 feet Y = -1099311
56 meter
Z = -7445855
85 Z = -2300104
27
XDOT = -3555
359717 XDOT = -1050
584059
YDOT = -17412
976891 feet/sec YDOT = -5319
408016 meter/sec
ZDOT = 17790
872086 ZDOT = 5417
474731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16753875
54 X = 5106581
27
Y = -12554240
17 feet Y = -3826532
40 meter
Z = -7578478
61 Z = -2309920
28
XDOT = 14179
070236 XDOT = 4321
780608
YDOT = 8200
452930 feet/sec YDOT = 2499
498053 meter/sec
ZDOT = 17769
219233 ZDOT = 5416
058022
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 16067
17588306
00016717 00000-0 10270-3 0 9151
2 25544 51
6426 206
7638 0004435 249
1710 110
8967 15
53813239 29113
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
17588306 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 206
7638 deg
Eccentricity:
0004435
Arg of perigee: 249
1710 deg
Mean anomaly: 110
8967 deg
Mean motion: 15
53813239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 318
Coasting Arc #17 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2016/067/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 875138
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6187763
70 A = 6790228
62 meter
Y = -2772896
71 meter E =
0008709
Z = 252307
61 I = 51
51542
XDOT = 2159
568250 Wp = 37
23969
YDOT = -4264
388052 meter/sec RA = 202
44323 deg
ZDOT = 5994
805222 TA = 325
48306
MA = 325
53958
Ha = 220
202 n
mi
Hp = 216
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20301062
00 X = -6157522
17
Y = -9097430
15 feet Y = -2841923
27 meter
Z = 827780
89 Z = 222323
36
XDOT = 7085
197669 XDOT = 2177
973504
YDOT = -13990
774448 feet/sec YDOT = -4240
134580 meter/sec
ZDOT = 19667
996134 ZDOT = 6005
340980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5394122
57 X = -1644128
56
Y = 21586978
46 feet Y = 6579711
03 meter
Z = 698124
33 Z = 212788
30
XDOT = -13418
655803 XDOT = -4090
006289
YDOT = -4003
390703 feet/sec YDOT = -1220
233486 meter/sec
ZDOT = 19714
371193 ZDOT = 6008
940340
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 16067
88335285
00016717 00000-0 10270-3 0 9166
2 25544 51
6416 203
2380 0004260 250
1537 109
9157 15
53812725 29224
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
88335285 = yrday
fracday
Element set: 916
Inclination: 51
6416 deg
RA of node: 203
2380 deg
Eccentricity:
0004260
Arg of perigee: 250
1537 deg
Mean anomaly: 109
9157 deg
Mean motion: 15
53812725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 304
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