[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 1st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
157/20:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 213
6
160/13:46:59
311 -0
2 1
5 1
5
N/A 1
5 -0
1 220
1
000/00:03:58
622 0
1 -0
0 214
5
161/01:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
4
166/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 214
5
Coasting Arc #1 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2016/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4430329
97 A = 6777127
40 meter
Y = 1145011
28 meter E =
0013308
Z = -5011092
62 I = 51
87830
XDOT = -3956
462652 Wp = 79
81715
YDOT = 6219
741162 meter/sec RA = 135
24814 deg
ZDOT = -2079
142484 TA = 170
01050
MA = 169
98402
Ha = 220
472 n
mi
Hp = 213
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14535203
32 X = 4441538
98
Y = 3756598
69 feet Y = 1194617
17 meter
Z = -16440592
57 Z = -4989543
57
XDOT = -12980
520513 XDOT = -4015
619577
YDOT = 20405
974940 feet/sec YDOT = 6175
166726 meter/sec
ZDOT = -6821
333608 ZDOT = -2098
505569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8633513
10 X = 2631494
79
Y = -12406321
13 feet Y = -3781446
68 meter
Z = -16346953
87 Z = -4982551
54
XDOT = 13695
237410 XDOT = 4174
308363
YDOT = 18620
568386 feet/sec YDOT = 5675
549244 meter/sec
ZDOT = -6906
733874 ZDOT = -2105
172485
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 16153
51976175
00016717 00000-0 10270-3 0 9004
2 25544 51
6377 136
1938 0001344 134
0465 226
0799 15
54711194 2541
Satellite: ISS
Catalog Number: 25544
Epoch time: 16153
51976175 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 136
1938 deg
Eccentricity:
0001344
Arg of perigee: 134
0465 deg
Mean anomaly: 226
0799 deg
Mean motion: 15
54711194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 254
Checksum: 309
Coasting Arc #2 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2016/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3153684
90 A = 6775635
42 meter
Y = -2743665
35 meter E =
0003337
Z = 5329766
58 I = 51
89546
XDOT = 4988
234907 Wp = 106
85330
YDOT = -5829
340264 meter/sec RA = 130
26024 deg
ZDOT = -50
157585 TA = 343
61733
MA = 343
62811
Ha = 220
514 n
mi
Hp = 213
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10346735
22 X = -3148660
29
Y = -9001526
75 feet Y = -2778904
30 meter
Z = 17486110
82 Z = 5314458
49
XDOT = 16365
600088 XDOT = 5053
292960
YDOT = -19125
132099 feet/sec YDOT = -5773
194735 meter/sec
ZDOT = -164
559005 ZDOT = -25
768039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11970614
82 X = -3648643
40
Y = 6862727
02 feet Y = 2091759
20 meter
Z = 17419926
63 Z = 5309593
64
XDOT = -12078
528308 XDOT = -3681
535428
YDOT = -20930
688371 feet/sec YDOT = -6379
673815 meter/sec
ZDOT = -57
316485 ZDOT = -17
470065
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 16154
54819986
00016717 00000-0 10270-3 0 9015
2 25544 51
6376 131
0624 0001264 141
3075 218
8169 15
54715981 2701
Satellite: ISS
Catalog Number: 25544
Epoch time: 16154
54819986 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 131
0624 deg
Eccentricity:
0001264
Arg of perigee: 141
3075 deg
Mean anomaly: 218
8169 deg
Mean motion: 15
54715981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 270
Checksum: 310
Coasting Arc #3 (Orbit 284)
---------------------------------------
Vector Time (GMT): 2016/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1769592
90 A = 6777164
21 meter
Y = 4255967
19 meter E =
0013472
Z = -4980862
45 I = 51
92175
XDOT = -5517
660084 Wp = 109
04786
YDOT = 4843
932552 meter/sec RA = 125
27354 deg
ZDOT = 2179
185533 TA = 182
13943
MA = 182
14519
Ha = 220
368 n
mi
Hp = 213
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5805750
98 X = 1746065
36
Y = 13963146
94 feet Y = 4275624
92 meter
Z = -16341412
25 Z = -4972322
78
XDOT = -18102
559330 XDOT = -5582
001780
YDOT = 15892
167164 feet/sec YDOT = 4781
870422 meter/sec
ZDOT = 7149
558835 ZDOT = 2152
225904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15115232
05 X = 4607122
73
Y = -1181298
78 feet Y = -360059
87 meter
Z = -16304976
68 Z = -4969756
89
XDOT = 9235
584329 XDOT = 2815
006104
YDOT = 21147
418897 feet/sec YDOT = 6445
733280 meter/sec
ZDOT = 7031
273768 ZDOT = 2143
132244
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 16155
51235446
00016717 00000-0 10270-3 0 9027
2 25544 51
6386 126
2517 0001197 142
1441 217
9796 15
54717449 2853
Satellite: ISS
Catalog Number: 25544
Epoch time: 16155
51235446 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 126
2517 deg
Eccentricity:
0001197
Arg of perigee: 142
1441 deg
Mean anomaly: 217
9796 deg
Mean motion: 15
54717449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 285
Checksum: 314
Coasting Arc #4 (Orbit 300)
---------------------------------------
Vector Time (GMT): 2016/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -389467
54 A = 6780858
50 meter
Y = -5481761
73 meter E =
0011500
Z = 3963194
65 I = 51
95223
XDOT = 5608
653262 Wp = 84
71735
YDOT = -3328
746736 meter/sec RA = 120
29680 deg
ZDOT = -4041
964951 TA = 47
31526
MA = 47
21845
Ha = 220
306 n
mi
Hp = 213
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1277780
64 X = -347391
91
Y = -17984782
56 feet Y = -5485882
25 meter
Z = 13002607
11 Z = 3961404
20
XDOT = 18401
093379 XDOT = 5665
093681
YDOT = -10921
085092 feet/sec YDOT = -3265
710962 meter/sec
ZDOT = -13261
039867 ZDOT = -4014
582470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17561223
00 X = -5352660
77
Y = -4106775
02 feet Y = -1251745
03 meter
Z = 12995797
97 Z = 3961119
22
XDOT = -5160
309924 XDOT = -1572
862465
YDOT = -19633
707691 feet/sec YDOT = -5984
354104 meter/sec
ZDOT = -13141
161897 ZDOT = -4005
426146
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 16156
54078128
00016717 00000-0 10270-3 0 9034
2 25544 51
6386 121
1202 0001080 144
3159 215
8067 15
54749716 3018
Satellite: ISS
Catalog Number: 25544
Epoch time: 16156
54078128 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 121
1202 deg
Eccentricity:
0001080
Arg of perigee: 144
3159 deg
Mean anomaly: 215
8067 deg
Mean motion: 15
54749716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 286
Coasting Arc #5 (Orbit 315)
---------------------------------------
Vector Time (GMT): 2016/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -843466
12 A = 6784989
15 meter
Y = 6268335
77 meter E =
0005329
Z = -2455681
50 I = 51
98163
XDOT = -5296
214341 Wp = 60
06658
YDOT = 1384
708031 meter/sec RA = 115
33420 deg
ZDOT = 5364
976965 TA = 272
58371
MA = 272
64471
Ha = 220
276 n
mi
Hp = 213
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2767277
29 X = -901568
78
Y = 20565406
07 feet Y = 6258579
04 meter
Z = -8056697
82 Z = -2459919
14
XDOT = -17376
031302 XDOT = -5337
365846
YDOT = 4543
005351 feet/sec YDOT = 1325
251400 meter/sec
ZDOT = 17601
630464 ZDOT = 5339
149283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18945662
23 X = 5774637
85
Y = 8446260
48 feet Y = 2574420
19 meter
Z = -8076304
65 Z = -2461657
66
XDOT = 4
239560 XDOT = 1
292218
YDOT = 16678
039626 feet/sec YDOT = 5083
466478 meter/sec
ZDOT = 17488
859769 ZDOT = 5330
604458
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 16157
50492791
00016717 00000-0 10270-3 0 9048
2 25544 51
6389 116
3099 0001089 148
6708 211
4510 15
54735906 3164
Satellite: ISS
Catalog Number: 25544
Epoch time: 16157
50492791 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 116
3099 deg
Eccentricity:
0001089
Arg of perigee: 148
6708 deg
Mean anomaly: 211
4510 deg
Mean motion: 15
54735906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 316
Checksum: 316
Coasting Arc #6 (Orbit 321)
---------------------------------------
Vector Time (GMT): 2016/157/20:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4288012
97 A = 6776116
78 meter
Y = -408233
79 meter E =
0004982
Z = 5228233
54 I = 51
95694
XDOT = 2159
303229 Wp = 131
39988
YDOT = -7263
430655 meter/sec RA = 113
67396 deg
ZDOT = 1199
889687 TA = 307
12291
MA = 307
16842
Ha = 220
394 n
mi
Hp = 213
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14068284
04 X = -4308526
00
Y = -1339349
71 feet Y = -456300
64 meter
Z = 17152997
17 Z = 5207353
40
XDOT = 7084
328178 XDOT = 2234
535656
YDOT = -23830
153068 feet/sec YDOT = -7238
863410 meter/sec
ZDOT = 3936
645954 ZDOT = 1210
560821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13982723
38 X = 4261934
09
Y = -2702556
87 feet Y = -823739
34 meter
Z = 17062104
75 Z = 5200529
53
XDOT = -271
343833 XDOT = -82
705600
YDOT = 23833
523964 feet/sec YDOT = 7264
458104 meter/sec
ZDOT = 3984
468807 ZDOT = 1214
466092
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 16157
89058497
00016717 00000-0 10270-3 0 9052
2 25544 51
6394 114
3846 0001074 158
9584 201
1613 15
54719035 3220
Satellite: ISS
Catalog Number: 25544
Epoch time: 16157
89058497 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 114
3846 deg
Eccentricity:
0001074
Arg of perigee: 158
9584 deg
Mean anomaly: 201
1613 deg
Mean motion: 15
54719035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 322
Checksum: 316
Coasting Arc #7 (Orbit 336)
---------------------------------------
Vector Time (GMT): 2016/158/20:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3553647
67 A = 6775802
05 meter
Y = 2368045
80 meter E =
0014964
Z = -5273789
38 I = 51
96819
XDOT = -3148
464813 Wp = 101
49525
YDOT = 6911
957891 meter/sec RA = 108
68831 deg
ZDOT = 981
534577 TA = 177
87235
MA = 177
86597
Ha = 220
173 n
mi
Hp = 213
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11658949
05 X = 3552521
33
Y = 7769179
13 feet Y = 2407779
51 meter
Z = -17302458
61 Z = -5256529
01
XDOT = -10329
608967 XDOT = -3230
289940
YDOT = 22677
027201 feet/sec YDOT = 6876
292010 meter/sec
ZDOT = 3220
257799 ZDOT = 966
042329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13548619
88 X = -4129619
34
Y = -3912525
75 feet Y = -1192537
85 meter
Z = -17227691
45 Z = -5251000
35
XDOT = 2846
627099 XDOT = 867
651940
YDOT = -23742
114953 feet/sec YDOT = -7236
596638 meter/sec
ZDOT = 3151
475241 ZDOT = 960
569653
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 16158
85472354
00016717 00000-0 10270-3 0 9062
2 25544 51
6392 109
5726 0001155 160
2176 199
9022 15
54768173 3375
Satellite: ISS
Catalog Number: 25544
Epoch time: 16158
85472354 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 109
5726 deg
Eccentricity:
0001155
Arg of perigee: 160
2176 deg
Mean anomaly: 199
9022 deg
Mean motion: 15
54768173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 337
Checksum: 321
Coasting Arc #8 (Orbit 352)
---------------------------------------
Vector Time (GMT): 2016/159/20:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2692108
35 A = 6778537
48 meter
Y = -4170447
95 meter E =
0008308
Z = 4610424
35 I = 51
98669
XDOT = 3881
938868 Wp = 73
65355
YDOT = -5877
257722 meter/sec RA = 103
70917 deg
ZDOT = -3042
851260 TA = 46
60354
MA = 46
53439
Ha = 220
232 n
mi
Hp = 213
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8832376
49 X = -2667668
69
Y = -13682572
02 feet Y = -4200416
87 meter
Z = 15126064
15 Z = 4597405
58
XDOT = 12736
019909 XDOT = 3962
152159
YDOT = -19282
341606 feet/sec YDOT = -5833
398390 meter/sec
ZDOT = -9983
107810 ZDOT = -3023
799760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12773894
02 X = 3893482
90
Y = 10185322
48 feet Y = 3104486
29 meter
Z = 15070113
00 Z = 4593370
44
XDOT = -5355
116618 XDOT = -1632
239545
YDOT = 21395
707935 feet/sec YDOT = 6521
411778 meter/sec
ZDOT = -9898
991278 ZDOT = -3017
212542
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 16159
88313371
00016717 00000-0 10270-3 0 9070
2 25544 51
6392 104
4415 0001147 168
6609 191
4570 15
54756293 3531
Satellite: ISS
Catalog Number: 25544
Epoch time: 16159
88313371 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 104
4415 deg
Eccentricity:
0001147
Arg of perigee: 168
6609 deg
Mean anomaly: 191
4570 deg
Mean motion: 15
54756293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 315
Coasting Arc #9 (Orbit 363)
---------------------------------------
Vector Time (GMT): 2016/160/13:48:58
622
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3876004
18 A = 6776545
42 meter
Y = 1775359
86 meter E =
0013734
Z = -5279429
35 I = 51
98604
XDOT = -2055
065179 Wp = 101
44497
YDOT = 7316
529250 meter/sec RA = 100
07513 deg
ZDOT = 951
063237 TA = 177
62664
MA = 177
62012
Ha = 220
124 n
mi
Hp = 214
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12716549
14 X = 3881508
69
Y = 5824671
47 feet Y = 1818735
35 meter
Z = -17320962
42 Z = -5260587
16
XDOT = -6742
339825 XDOT = -2141
347545
YDOT = 24004
361057 feet/sec YDOT = 7293
065593 meter/sec
ZDOT = 3120
286211 ZDOT = 940
871608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2602481
09 X = 793236
24
Y = -13845243
51 feet Y = -4220030
22 meter
Z = -17239184
53 Z = -5254503
45
XDOT = 23914
712295 XDOT = 7289
204308
YDOT = 664
768685 feet/sec YDOT = 202
621495 meter/sec
ZDOT = 3074
498167 ZDOT = 937
107041
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 16160
59016488
00016717 00000-0 10270-3 0 9080
2 25544 51
6425 100
9168 0001227 223
5230 136
5826 15
54506964 3648
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
59016488 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 100
9168 deg
Eccentricity:
0001227
Arg of perigee: 223
5230 deg
Mean anomaly: 136
5826 deg
Mean motion: 15
54506964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 364
Checksum: 302
Coasting Arc #10 (Orbit 371)
---------------------------------------
Vector Time (GMT): 2016/161/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3732626
46 A = 6777041
84 meter
Y = -2363336
97 meter E =
0003442
Z = 5136851
45 I = 51
99141
XDOT = 2258
157885 Wp = 62
97536
YDOT = -7144
554574 meter/sec RA = 97
66778 deg
ZDOT = -1643
803578 TA = 42
81915
MA = 42
79235
Ha = 220
192 n
mi
Hp = 214
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12246149
79 X = -3730874
12
Y = -7753730
20 feet Y = -2405068
47 meter
Z = 16853187
17 Z = 5118723
34
XDOT = 7408
654477 XDOT = 2345
867110
YDOT = -23440
139678 feet/sec YDOT = -7118
811750 meter/sec
ZDOT = -5393
056358 ZDOT = -1632
621839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5898800
87 X = 1797954
50
Y = -13339203
82 feet Y = -4065789
32 meter
Z = 16774630
38 Z = 5112907
34
XDOT = 23293
510709 XDOT = 7099
862064
YDOT = 3571
910055 feet/sec YDOT = 1088
718185 meter/sec
ZDOT = -5342
979528 ZDOT = -1628
540160
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 16161
10445497
00016717 00000-0 10270-3 0 9095
2 25544 51
6432 98
3484 0001664 218
3806 141
7228 15
54534532 3728
Satellite: ISS
Catalog Number: 25544
Epoch time: 16161
10445497 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 98
3484 deg
Eccentricity:
0001664
Arg of perigee: 218
3806 deg
Mean anomaly: 141
7228 deg
Mean motion: 15
54534532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 372
Checksum: 307
Coasting Arc #11 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2016/162/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3203589
81 A = 6780212
02 meter
Y = 4112263
71 meter E =
0008151
Z = -4344229
48 I = 52
00541
XDOT = -3040
031140 Wp = 121
27198
YDOT = 6087
172585 meter/sec RA = 92
69532 deg
ZDOT = 3521
061679 TA = 184
40013
MA = 184
40730
Ha = 220
027 n
mi
Hp = 214
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10510465
24 X = 3178469
64
Y = 13491678
82 feet Y = 4147948
34 meter
Z = -14252721
38 Z = -4328727
92
XDOT = -9973
855445 XDOT = -3124
977212
YDOT = 19971
038666 feet/sec YDOT = 6052
701632 meter/sec
ZDOT = 11552
039629 ZDOT = 3506
088297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11613557
20 X = -3539812
24
Y = 12630109
57 feet Y = 3849657
40 meter
Z = -14185942
52 Z = -4323875
28
XDOT = -20405
053803 XDOT = -6219
460399
YDOT = -5865
020314 feet/sec YDOT = -1787
658192 meter/sec
ZDOT = 11485
626271 ZDOT = 3500
818887
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 16162
06874765
00016717 00000-0 10270-3 0 9107
2 25544 51
6432 93
5399 0001631 220
7193 139
3838 15
54540641 3874
Satellite: ISS
Catalog Number: 25544
Epoch time: 16162
06874765 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 93
5399 deg
Eccentricity:
0001631
Arg of perigee: 220
7193 deg
Mean anomaly: 139
3838 deg
Mean motion: 15
54540641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 387
Checksum: 315
Coasting Arc #12 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2016/163/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2568687
42 A = 6784372
96 meter
Y = -5504077
18 meter E =
0012280
Z = 3008686
27 I = 52
01930
XDOT = 3725
149968 Wp = 102
57926
YDOT = -4476
435895 meter/sec RA = 87
73357 deg
ZDOT = -4994
296098 TA = 43
14805
MA = 43
05188
Ha = 220
086 n
mi
Hp = 214
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8427452
17 X = -2521563
39
Y = -18057996
01 feet Y = -5532538
72 meter
Z = 9871017
95 Z = 2996322
28
XDOT = 12221
620630 XDOT = 3799
189793
YDOT = -14686
469472 feet/sec YDOT = -4434
364396 meter/sec
ZDOT = -16385
485886 ZDOT = -4976
020845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16263504
99 X = 4957116
32
Y = -11560789
08 feet Y = -3523728
51 meter
Z = 9818183
47 Z = 2992582
32
XDOT = 15799
536821 XDOT = 4815
698823
YDOT = 8338
610372 feet/sec YDOT = 2541
608441 meter/sec
ZDOT = -16304
978625 ZDOT = -4969
757485
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 16163
09732050
00016717 00000-0 10270-3 0 9112
2 25544 51
6427 88
4099 0001513 225
2515 134
8515 15
54526543 4031
Satellite: ISS
Catalog Number: 25544
Epoch time: 16163
09732050 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 88
4099 deg
Eccentricity:
0001513
Arg of perigee: 225
2515 deg
Mean anomaly: 134
8515 deg
Mean motion: 15
54526543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 403
Checksum: 287
Coasting Arc #13 (Orbit 417)
---------------------------------------
Vector Time (GMT): 2016/164/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1858071
02 A = 6787515
57 meter
Y = 6387029
62 meter E =
0007386
Z = -1333585
21 I = 52
02695
XDOT = -4293
185170 Wp = 33
80121
YDOT = 2466
713854 meter/sec RA = 82
78246 deg
ZDOT = 5853
826342 TA = 311
75897
MA = 311
82208
Ha = 219
995 n
mi
Hp = 214
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6096033
54 X = 1792989
54
Y = 20954821
57 feet Y = 6407444
01 meter
Z = -4375279
55 Z = -1324716
77
XDOT = -14085
253184 XDOT = -4348
884837
YDOT = 8092
893222 feet/sec YDOT = 2418
392727 meter/sec
ZDOT = 19205
467002 ZDOT = 5832
836041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19364367
58 X = -5902259
24
Y = 10080352
00 feet Y = 3072491
29 meter
Z = -4337858
36 Z = -1322179
23
XDOT = -9967
078452 XDOT = -3037
965512
YDOT = -10952
278496 feet/sec YDOT = -3338
254485 meter/sec
ZDOT = 19113
505116 ZDOT = 5825
796359
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 16164
06160181
00016717 00000-0 10270-3 0 9121
2 25544 51
6424 83
6005 0001535 236
5298 123
5709 15
54495986 4181
Satellite: ISS
Catalog Number: 25544
Epoch time: 16164
06160181 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 83
6005 deg
Eccentricity:
0001535
Arg of perigee: 236
5298 deg
Mean anomaly: 123
5709 deg
Mean motion: 15
54495986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 418
Checksum: 306
Coasting Arc #14 (Orbit 433)
---------------------------------------
Vector Time (GMT): 2016/165/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1014213
89 A = 6787998
61 meter
Y = -6684696
57 meter E =
0010868
Z = -534170
17 I = 52
02404
XDOT = 4750
900682 Wp = 146
68395
YDOT = -245
422659 meter/sec RA = 77
83697 deg
ZDOT = -6015
758604 TA = 39
05032
MA = 38
97191
Ha = 219
927 n
mi
Hp = 214
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3327473
40 X = -936793
79
Y = -21931419
18 feet Y = -6695605
26 meter
Z = -1752526
81 Z = -538909
42
XDOT = 15586
944495 XDOT = 4782
513969
YDOT = -805
192451 feet/sec YDOT = -192
117722 meter/sec
ZDOT = -19736
740827 ZDOT = -5992
603113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20736341
81 X = 6320436
98
Y = -7873699
23 feet Y = -2399903
53 meter
Z = -1771881
95 Z = -540069
62
XDOT = 3533
765514 XDOT = 1077
091729
YDOT = 13676
747615 feet/sec YDOT = 4168
672673 meter/sec
ZDOT = -19635
769152 ZDOT = -5984
982437
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 16165
09016257
00016717 00000-0 10270-3 0 9130
2 25544 51
6423 78
4703 0001526 235
5357 124
5652 15
54543625 4342
Satellite: ISS
Catalog Number: 25544
Epoch time: 16165
09016257 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 78
4703 deg
Eccentricity:
0001526
Arg of perigee: 235
5357 deg
Mean anomaly: 124
5652 deg
Mean motion: 15
54543625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 434
Checksum: 296
Coasting Arc #15 (Orbit 449)
---------------------------------------
Vector Time (GMT): 2016/166/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73632
23 A = 6785833
80 meter
Y = 6373715
88 meter E =
0012445
Z = 2311113
10 I = 52
00951
XDOT = -5044
820648 Wp = 73
70473
YDOT = -1924
791514 meter/sec RA = 72
88810 deg
ZDOT = 5448
204966 TA = 311
92191
MA = 312
02795
Ha = 219
906 n
mi
Hp = 214
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 241575
57 X = -8872
17
Y = 20911141
34 feet Y = 6374077
80 meter
Z = 7582392
04 Z = 2311270
89
XDOT = -16551
248845 XDOT = -5049
387345
YDOT = -6314
932790 feet/sec YDOT = -1981
232017 meter/sec
ZDOT = 17874
688208 ZDOT = 5423
687144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20317111
73 X = -6192655
66
Y = 4955575
73 feet Y = 1510459
48 meter
Z = 7581826
95 Z = 2310940
85
XDOT = 2708
411864 XDOT = 825
523936
YDOT = -16185
058735 feet/sec YDOT = -4933
205902 meter/sec
ZDOT = 17768
204902 ZDOT = 5415
748854
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 16166
11871484
00016717 00000-0 10270-3 0 9146
2 25544 51
6426 73
3397 0001415 242
1563 117
9447 15
54552733 4504
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
11871484 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 73
3397 deg
Eccentricity:
0001415
Arg of perigee: 242
1563 deg
Mean anomaly: 117
9447 deg
Mean motion: 15
54552733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 450
Checksum: 304
Coasting Arc #16 (Orbit 455)
---------------------------------------
Vector Time (GMT): 2016/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908273
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3695802
63 A = 6785938
16 meter
Y = 5225771
80 meter E =
0005031
Z = -2249110
49 I = 52
00621
XDOT = -2973
571878 Wp = 35
65196
YDOT = 4458
016173 meter/sec RA = 70
66179 deg
ZDOT = 5481
995882 TA = 299
47127
MA = 299
52145
Ha = 219
891 n
mi
Hp = 214
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12125336
70 X = 3648017
32
Y = 17144920
62 feet Y = 5266833
73 meter
Z = -7378971
43 Z = -2231272
75
XDOT = -9755
813247 XDOT = -3049
830841
YDOT = 14626
037314 feet/sec YDOT = 4424
336877 meter/sec
ZDOT = 17985
550793 ZDOT = 5467
366075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18609670
06 X = 5672227
43
Y = -9786650
72 feet Y = -2982971
14 meter
Z = -7302257
23 Z = -2225728
00
XDOT = 12472
658879 XDOT = 3801
666426
YDOT = 10370
671287 feet/sec YDOT = 3160
980608 meter/sec
ZDOT = 17920
906099 ZDOT = 5462
292179
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 16166
50442163
00016717 00000-0 10270-3 0 9158
2 25544 51
6430 71
4177 0001252 254
0555 106
0460 15
54570875 4563
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
50442163 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 71
4177 deg
Eccentricity:
0001252
Arg of perigee: 254
0555 deg
Mean anomaly: 106
0460 deg
Mean motion: 15
54570875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 456
Checksum: 285
Coasting Arc #17 (Orbit 471)
---------------------------------------
Vector Time (GMT): 2016/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908273
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3086249
03 A = 6788046
74 meter
Y = -6023435
26 meter E =
0012142
Z = 429680
97 I = 52
00184
XDOT = 4033
839429 Wp = 135
80192
YDOT = -2503
254941 meter/sec RA = 65
71351 deg
ZDOT = -6024
357606 TA = 39
58642
MA = 39
49782
Ha = 219
877 n
mi
Hp = 214
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10125488
96 X = -3020751
31
Y = -19761926
71 feet Y = -6057581
57 meter
Z = 1409714
46 Z = 414847
17
XDOT = 13234
381329 XDOT = 4090
795586
YDOT = -8212
778678 feet/sec YDOT = -2457
826849 meter/sec
ZDOT = -19764
952777 ZDOT = -6004
623974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20802476
62 X = -6340594
87
Y = 7777603
08 feet Y = 2370613
42 meter
Z = 1346263
53 Z = 410341
12
XDOT = -6044
833712 XDOT = -1842
465316
YDOT = -12706
013785 feet/sec YDOT = -3872
793002 meter/sec
ZDOT = -19678
444019 ZDOT = -5997
989737
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 16167
53296558
00016717 00000-0 10270-3 0 9168
2 25544 51
6434 66
2881 0001371 253
1912 106
9090 15
54545678 4729
Satellite: ISS
Catalog Number: 25544
Epoch time: 16167
53296558 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 66
2881 deg
Eccentricity:
0001371
Arg of perigee: 253
1912 deg
Mean anomaly: 106
9090 deg
Mean motion: 15
54545678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 321
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