[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 31st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 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
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
161/01:18:30
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
164/08:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 214
4
Coasting Arc #1 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2016/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6036196
94 A = 6784990
21 meter
Y = -1756698
66 meter E =
0006791
Z = -2549740
78 I = 51
85560
XDOT = -630
066332 Wp = 130
74567
YDOT = 5504
687061 meter/sec RA = 145
19984 deg
ZDOT = -5297
713196 TA = 77
80249
MA = 77
72643
Ha = 220
594 n
mi
Hp = 213
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19803795
75 X = 6067777
81
Y = -5763447
05 feet Y = -1689021
18 meter
Z = -8365291
27 Z = -2520341
59
XDOT = -2067
146758 XDOT = -665
840081
YDOT = 18059
996920 feet/sec YDOT = 5497
441482 meter/sec
ZDOT = -17380
948806 ZDOT = -5300
860540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2244924
06 X = 684252
85
Y = -20554757
05 feet Y = -6265089
95 meter
Z = -8236991
22 Z = -2510634
93
XDOT = 14448
840167 XDOT = 4404
006483
YDOT = 8530
987951 feet/sec YDOT = 2600
245128 meter/sec
ZDOT = -17395
593010 ZDOT = -5302
176749
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 16151
52715143
00016717 00000-0 10270-3 0 9009
2 25544 51
6388 146
1357 0001498 130
4163 229
7120 15
54700191 2233
Satellite: ISS
Catalog Number: 25544
Epoch time: 16151
52715143 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 146
1357 deg
Eccentricity:
0001498
Arg of perigee: 130
4163 deg
Mean anomaly: 229
7120 deg
Mean motion: 15
54700191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 223
Checksum: 276
Coasting Arc #2 (Orbit 238)
---------------------------------------
Vector Time (GMT): 2016/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5436430
85 A = 6780807
50 meter
Y = 415056
25 meter E =
0011993
Z = 4023780
38 I = 51
86782
XDOT = 2470
316040 Wp = 105
17397
YDOT = -6093
560189 meter/sec RA = 140
23009 deg
ZDOT = 3953
278260 TA = 303
84366
MA = 303
95774
Ha = 220
511 n
mi
Hp = 213
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17836059
20 X = -5460214
07
Y = 1361733
11 feet Y = 354129
28 meter
Z = 13201379
20 Z = 3997313
51
XDOT = 8104
711416 XDOT = 2519
068615
YDOT = -19991
995370 feet/sec YDOT = -6065
663083 meter/sec
ZDOT = 12970
073030 ZDOT = 3965
396675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5280196
03 X = -1609403
75
Y = 17179353
26 feet Y = 5236266
87 meter
Z = 13086064
69 Z = 3988632
52
XDOT = -14424
251433 XDOT = -4396
511837
YDOT = -14386
533938 feet/sec YDOT = -4385
015544 meter/sec
ZDOT = 13023
888784 ZDOT = 3969
681301
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 16152
55559634
00016717 00000-0 10270-3 0 9015
2 25544 51
6389 141
0049 0001330 138
6366 221
4888 15
54736231 2397
Satellite: ISS
Catalog Number: 25544
Epoch time: 16152
55559634 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 141
0049 deg
Eccentricity:
0001330
Arg of perigee: 138
6366 deg
Mean anomaly: 221
4888 deg
Mean motion: 15
54736231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 239
Checksum: 306
Coasting Arc #3 (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 = 4430114
78 A = 6777124
79 meter
Y = 1145291
38 meter E =
0013309
Z = -5011214
54 I = 51
87863
XDOT = -3956
739160 Wp = 79
86063
YDOT = 6219
667161 meter/sec RA = 135
24810 deg
ZDOT = -2078
845429 TA = 169
97018
MA = 169
94360
Ha = 220
472 n
mi
Hp = 213
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14534497
32 X = 4441321
27
Y = 3757517
65 feet Y = 1194894
85 meter
Z = -16440992
60 Z = -4989666
55
XDOT = -12981
427689 XDOT = -4015
896679
YDOT = 20405
732156 feet/sec YDOT = 6175
089630 meter/sec
ZDOT = -6820
359018 ZDOT = -2098
209858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8634128
37 X = 2631682
33
Y = -12405341
00 feet Y = -3781147
94 meter
Z = -16347358
52 Z = -4982674
88
XDOT = 13694
762354 XDOT = 4174
163566
YDOT = 18621
294606 feet/sec YDOT = 5675
770596 meter/sec
ZDOT = -6905
765126 ZDOT = -2104
877210
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
51976119
00016717 00000-0 10270-3 0 9024
2 25544 51
6381 136
1937 0001352 134
2925 225
8339 15
54711904 2543
Satellite: ISS
Catalog Number: 25544
Epoch time: 16153
51976119 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 136
1937 deg
Eccentricity:
0001352
Arg of perigee: 134
2925 deg
Mean anomaly: 225
8339 deg
Mean motion: 15
54711904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 254
Checksum: 301
Coasting Arc #4 (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 = -3153243
67 A = 6775633
23 meter
Y = -2744130
94 meter E =
0003341
Z = 5329784
29 I = 51
89579
XDOT = 4988
575830 Wp = 106
98960
YDOT = -5829
046178 meter/sec RA = 130
26023 deg
ZDOT = -50
734513 TA = 343
48645
MA = 343
49733
Ha = 220
514 n
mi
Hp = 213
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10345287
65 X = -3148213
98
Y = -9003054
25 feet Y = -2779364
92 meter
Z = 17486168
91 Z = 5314478
36
XDOT = 16366
718601 XDOT = 5053
633371
YDOT = -19124
167252 feet/sec YDOT = -5772
896840 meter/sec
ZDOT = -166
451814 ZDOT = -26
343313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11971572
83 X = -3648935
40
Y = 6860853
59 feet Y = 2091188
17 meter
Z = 17419994
20 Z = 5309614
23
XDOT = -12077
378630 XDOT = -3681
185007
YDOT = -20931
363156 feet/sec YDOT = -6379
879490 meter/sec
ZDOT = -59
202139 ZDOT = -18
044812
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
54819885
00016717 00000-0 10270-3 0 9035
2 25544 51
6379 131
0624 0001272 141
5451 218
5793 15
54716693 2704
Satellite: ISS
Catalog Number: 25544
Epoch time: 16154
54819885 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 131
0624 deg
Eccentricity:
0001272
Arg of perigee: 141
5451 deg
Mean anomaly: 218
5793 deg
Mean motion: 15
54716693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 270
Checksum: 313
Coasting Arc #5 (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 = 1768878
42 A = 6777163
16 meter
Y = 4256556
65 meter E =
0013474
Z = -4980613
26 I = 51
92209
XDOT = -5517
930216 Wp = 109
09139
YDOT = 4843
263891 meter/sec RA = 125
27356 deg
ZDOT = 2179
983359 TA = 182
10398
MA = 182
10965
Ha = 220
368 n
mi
Hp = 213
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5803406
88 X = 1745343
13
Y = 13965080
89 feet Y = 4276206
35 meter
Z = -16340594
69 Z = -4972077
08
XDOT = -18103
445590 XDOT = -5582
268290
YDOT = 15889
973396 feet/sec YDOT = 4781
198761 meter/sec
ZDOT = 7152
176376 ZDOT = 2153
022427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15116321
79 X = 4607454
88
Y = -1178457
61 feet Y = -359193
88 meter
Z = -16304174
42 Z = -4969512
36
XDOT = 9233
424843 XDOT = 2814
347892
YDOT = 21147
500781 feet/sec YDOT = 6445
758238 meter/sec
ZDOT = 7033
885750 ZDOT = 2143
928377
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
51235302
00016717 00000-0 10270-3 0 9040
2 25544 51
6390 126
2516 0001205 142
4122 217
7115 15
54718162 2852
Satellite: ISS
Catalog Number: 25544
Epoch time: 16155
51235302 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 126
2516 deg
Eccentricity:
0001205
Arg of perigee: 142
4122 deg
Mean anomaly: 217
7115 deg
Mean motion: 15
54718162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 285
Checksum: 266
Coasting Arc #6 (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 = -388543
87 A = 6780858
52 meter
Y = -5482278
10 meter E =
0011501
Z = 3962561
90 I = 51
95257
XDOT = 5608
721137 Wp = 84
77628
YDOT = -3327
627350 meter/sec RA = 120
29686 deg
ZDOT = -4042
803835 TA = 47
26672
MA = 47
16997
Ha = 220
305 n
mi
Hp = 213
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1274750
22 X = -346459
46
Y = -17986476
72 feet Y = -5486388
25 meter
Z = 13000531
17 Z = 3960775
96
XDOT = 18401
316067 XDOT = 5665
153109
YDOT = -10917
412564 feet/sec YDOT = -3264
590864 meter/sec
ZDOT = -13263
792110 ZDOT = -4015
421044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17561924
14 X = -5352874
48
Y = -4110187
28 feet Y = -1252785
08 meter
Z = 12993741
75 Z = 3960492
49
XDOT = -5156
984028 XDOT = -1571
848732
YDOT = -19632
782083 feet/sec YDOT = -5984
071979 meter/sec
ZDOT = -13143
912994 ZDOT = -4006
264680
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
54077939
00016717 00000-0 10270-3 0 9055
2 25544 51
6390 121
1202 0001088 144
6237 215
4988 15
54750428 3011
Satellite: ISS
Catalog Number: 25544
Epoch time: 16156
54077939 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 121
1202 deg
Eccentricity:
0001088
Arg of perigee: 144
6237 deg
Mean anomaly: 215
4988 deg
Mean motion: 15
54750428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 300
Coasting Arc #7 (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 = -844550
68 A = 6784989
22 meter
Y = 6268608
79 meter E =
0005325
Z = -2454619
08 I = 51
98197
XDOT = -5295
969690 Wp = 60
11973
YDOT = 1383
111890 meter/sec RA = 115
33429 deg
ZDOT = 5365
625850 TA = 272
54353
MA = 272
60449
Ha = 220
275 n
mi
Hp = 213
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2770835
58 X = -902661
48
Y = 20566301
79 feet Y = 6258839
88 meter
Z = -8053212
20 Z = -2458862
01
XDOT = -17375
228641 XDOT = -5337
106516
YDOT = 4537
768668 feet/sec YDOT = 1323
658077 meter/sec
ZDOT = 17603
759351 ZDOT = 5339
799392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18945504
00 X = 5774589
62
Y = 8449948
18 feet Y = 2575544
21 meter
Z = -8072842
12 Z = -2460602
28
XDOT = -
288055 XDOT = -
087799
YDOT = 16675
806954 feet/sec YDOT = 5082
785960 meter/sec
ZDOT = 17490
994279 ZDOT = 5331
255056
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
50492560
00016717 00000-0 10270-3 0 9064
2 25544 51
6393 116
3099 0001097 148
9708 211
1510 15
54736640 3164
Satellite: ISS
Catalog Number: 25544
Epoch time: 16157
50492560 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 116
3099 deg
Eccentricity:
0001097
Arg of perigee: 148
9708 deg
Mean anomaly: 211
1510 deg
Mean motion: 15
54736640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 316
Checksum: 302
Coasting Arc #8 (Orbit 331)
---------------------------------------
Vector Time (GMT): 2016/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1914157
98 A = 6787352
61 meter
Y = -6477644
56 meter E =
0014056
Z = 591175
70 I = 52
00485
XDOT = 4697
191657 Wp = 130
67326
YDOT = 832
061064 meter/sec RA = 110
38279 deg
ZDOT = -6007
666154 TA = 42
97468
MA = 42
86497
Ha = 220
216 n
mi
Hp = 213
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6280045
87 X = 1983578
67
Y = -21252114
71 feet Y = -6455851
10 meter
Z = 1939552
81 Z = 600641
92
XDOT = 15410
733782 XDOT = 4716
721003
YDOT = 2729
859134 feet/sec YDOT = 884
698246 meter/sec
ZDOT = -19710
190794 ZDOT = -5984
800722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18799866
10 X = -5730199
19
Y = -11725611
19 feet Y = -3573966
29 meter
Z = 1981993
28 Z = 604111
55
XDOT = 5931
103372 XDOT = 1807
800308
YDOT = -12869
959785 feet/sec YDOT = -3922
763742 meter/sec
ZDOT = -19610
720158 ZDOT = -5977
347504
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
53334279
00016717 00000-0 10270-3 0 9071
2 25544 51
6412 111
1783 0001059 155
8871 204
2331 15
54756280 3329
Satellite: ISS
Catalog Number: 25544
Epoch time: 16158
53334279 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 111
1783 deg
Eccentricity:
0001059
Arg of perigee: 155
8871 deg
Mean anomaly: 204
2331 deg
Mean motion: 15
54756280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 332
Checksum: 294
Coasting Arc #9 (Orbit 347)
---------------------------------------
Vector Time (GMT): 2016/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2740468
66 A = 6786743
37 meter
Y = 6060780
72 meter E =
0013694
Z = 1317083
03 I = 52
01306
XDOT = -3904
053084 Wp = 63
79445
YDOT = -3047
113492 meter/sec RA = 105
43541 deg
ZDOT = 5857
502939 TA = 310
47310
MA = 310
59239
Ha = 220
182 n
mi
Hp = 213
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8991038
92 X = -2814435
97
Y = 19884451
17 feet Y = 6029721
21 meter
Z = 4321138
56 Z = 1303591
70
XDOT = -12808
573110 XDOT = -3898
142552
YDOT = -9997
091509 feet/sec YDOT = -3090
738974 meter/sec
ZDOT = 19217
529327 ZDOT = 5838
551964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16984960
70 X = 5177016
02
Y = 13720623
80 feet Y = 4182046
14 meter
Z = 4261221
65 Z = 1298820
36
XDOT = -11920
484840 XDOT = -3633
363779
YDOT = 8771
145368 feet/sec YDOT = 2673
445108 meter/sec
ZDOT = 19135
519235 ZDOT = 5832
506263
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
56175360
00016717 00000-0 10270-3 0 9080
2 25544 51
6410 106
0475 0001042 156
9742 203
1458 15
54773270 3482
Satellite: ISS
Catalog Number: 25544
Epoch time: 16159
56175360 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 106
0475 deg
Eccentricity:
0001042
Arg of perigee: 156
9742 deg
Mean anomaly: 203
1458 deg
Mean motion: 15
54773270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 348
Checksum: 296
Coasting Arc #10 (Orbit 362)
---------------------------------------
Vector Time (GMT): 2016/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3380417
43 A = 6783425
18 meter
Y = -5004596
70 meter E =
0005141
Z = -3090258
92 I = 52
01022
XDOT = 2981
713749 Wp = 115
47956
YDOT = 5053
838625 meter/sec RA = 100
48250 deg
ZDOT = -4931
408049 TA = 99
82925
MA = 99
77121
Ha = 220
144 n
mi
Hp = 213
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11090608
36 X = 3451139
94
Y = -16419280
51 feet Y = -4966398
80 meter
Z = -10138644
73 Z = -3073666
59
XDOT = 9782
525423 XDOT = 2948
933426
YDOT = 16580
835385 feet/sec YDOT = 5086
999460 meter/sec
ZDOT = -16179
160265 ZDOT = -4917
002666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13349590
69 X = -4068955
24
Y = -14692265
34 feet Y = -4478202
47 meter
Z = -10065398
69 Z = -3067933
52
XDOT = 17362
790341 XDOT = 5292
178496
YDOT = -4753
677550 feet/sec YDOT = -1448
920917 meter/sec
ZDOT = -16117
332899 ZDOT = -4912
563068
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
52588522
00016717 00000-0 10270-3 0 9097
2 25544 51
6414 101
2372 0000938 159
5698 200
5493 15
54785389 3632
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
52588522 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 101
2372 deg
Eccentricity:
0000938
Arg of perigee: 159
5698 deg
Mean anomaly: 200
5493 deg
Mean motion: 15
54785389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 363
Checksum: 323
Coasting Arc #11 (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 = 3875313
01 A = 6776544
60 meter
Y = 1777692
41 meter E =
0013732
Z = -5279148
27 I = 51
98638
XDOT = -2056
648196 Wp = 101
50088
YDOT = 7315
808780 meter/sec RA = 100
07529 deg
ZDOT = 953
202770 TA = 177
59131
MA = 177
58469
Ha = 220
123 n
mi
Hp = 214
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12714281
51 X = 3880790
12
Y = 5832324
17 feet Y = 1821060
01 meter
Z = -17320040
24 Z = -5260309
50
XDOT = -6747
533451 XDOT = -2142
932781
YDOT = 24001
997310 feet/sec YDOT = 7292
327408 meter/sec
ZDOT = 3127
305677 ZDOT = 943
003446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2610455
09 X = 795666
71
Y = -13844856
79 feet Y = -4219912
35 meter
Z = -17238277
71 Z = -5254227
05
XDOT = 23913
692215 XDOT = 7288
893387
YDOT = 669
837870 feet/sec YDOT = 204
166583 meter/sec
ZDOT = 3081
484233 ZDOT = 939
236394
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
59016121
00016717 00000-0 10270-3 0 9107
2 25544 51
6428 100
9169 0001235 223
3363 136
7693 15
54507656 3649
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
59016121 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 100
9169 deg
Eccentricity:
0001235
Arg of perigee: 223
3363 deg
Mean anomaly: 136
7693 deg
Mean motion: 15
54507656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 364
Checksum: 290
Coasting Arc #12 (Orbit 371)
---------------------------------------
Vector Time (GMT): 2016/161/01:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4228030
54 A = 6776482
54 meter
Y = 557093
73 meter E =
0003884
Z = 5265081
91 I = 51
98989
XDOT = 243
578237 Wp = 149
07992
YDOT = -7601
697320 meter/sec RA = 97
71201 deg
ZDOT = 996
361345 TA = 291
41025
MA = 291
45168
Ha = 220
196 n
mi
Hp = 214
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13871491
28 X = -4259521
26
Y = 1827735
34 feet Y = 509636
40 meter
Z = 17273890
77 Z = 5244466
85
XDOT = 799
141199 XDOT = 323
724346
YDOT = -24939
951837 feet/sec YDOT = -7598
525456 meter/sec
ZDOT = 3268
902050 ZDOT = 997
738377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3429601
34 X = -1045342
49
Y = -13678305
64 feet Y = -4169147
56 meter
Z = 17183945
38 Z = 5237666
55
XDOT = 23865
545531 XDOT = 7274
218278
YDOT = -1853
056489 feet/sec YDOT = -564
811618 meter/sec
ZDOT = 3276
336028 ZDOT = 998
627221
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
10445073
00016717 00000-0 10270-3 0 9118
2 25544 51
6436 98
3486 0001758 217
0021 143
1011 15
54538773 3720
Satellite: ISS
Catalog Number: 25544
Epoch time: 16161
10445073 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 98
3486 deg
Eccentricity:
0001758
Arg of perigee: 217
0021 deg
Mean anomaly: 143
1011 deg
Mean motion: 15
54538773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 372
Checksum: 282
Coasting Arc #13 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2016/162/01:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4045635
70 A = 6776574
29 meter
Y = 1425181
30 meter E =
0013434
Z = -5258029
23 I = 51
99349
XDOT = -1213
098130 Wp = 104
01563
YDOT = 7482
937328 meter/sec RA = 92
73276 deg
ZDOT = 1094
029748 TA = 176
43359
MA = 176
42400
Ha = 220
026 n
mi
Hp = 214
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13273083
01 X = 4054939
41
Y = 4675791
68 feet Y = 1470474
82 meter
Z = -17250752
08 Z = -5238353
90
XDOT = -3979
980743 XDOT = -1301
998353
YDOT = 24550
319319 feet/sec YDOT = 7468
874481 meter/sec
ZDOT = 3589
336444 ZDOT = 1087
921642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2861147
16 X = -872077
65
Y = 13885008
33 feet Y = 4232150
54 meter
Z = -17165272
74 Z = -5231975
13
XDOT = -23852
002378 XDOT = -7270
090325
YDOT = -508
942694 feet/sec YDOT = -155
125733 meter/sec
ZDOT = 3561
295252 ZDOT = 1085
482793
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
06874324
00016717 00000-0 10270-3 0 9120
2 25544 51
6436 93
5399 0001599 222
6652 137
4377 15
54531050 3873
Satellite: ISS
Catalog Number: 25544
Epoch time: 16162
06874324 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 93
5399 deg
Eccentricity:
0001599
Arg of perigee: 222
6652 deg
Mean anomaly: 137
4377 deg
Mean motion: 15
54531050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 387
Checksum: 317
Coasting Arc #14 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2016/163/01:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3727971
04 A = 6779199
30 meter
Y = -3290118
98 meter E =
0007115
Z = 4603620
42 I = 52
00300
XDOT = 2130
022586 Wp = 69
89340
YDOT = -6704
321570 meter/sec RA = 87
75712 deg
ZDOT = -3060
375256 TA = 50
55115
MA = 50
48821
Ha = 220
085 n
mi
Hp = 214
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12230876
10 X = -3713265
36
Y = -10794353
60 feet Y = -3331725
79 meter
Z = 15103741
53 Z = 4585546
37
XDOT = 6988
263079 XDOT = 2219
699618
YDOT = -21995
805677 feet/sec YDOT = -6680
000573 meter/sec
ZDOT = -10040
601234 ZDOT = -3049
810910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8829748
44 X = 2691307
32
Y = -13802260
30 feet Y = -4206928
94 meter
Z = 15025596
87 Z = 4579801
92
XDOT = 21797
160054 XDOT = 6643
774385
YDOT = 3043
069500 feet/sec YDOT = 927
527584 meter/sec
ZDOT = -9993
275172 ZDOT = -3045
950272
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
09731496
00016717 00000-0 10270-3 0 9137
2 25544 51
6436 88
4096 0001531 228
4964 131
6057 15
54548378 4037
Satellite: ISS
Catalog Number: 25544
Epoch time: 16163
09731496 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 88
4096 deg
Eccentricity:
0001531
Arg of perigee: 228
4964 deg
Mean anomaly: 131
6057 deg
Mean motion: 15
54548378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 403
Checksum: 318
Coasting Arc #15 (Orbit 417)
---------------------------------------
Vector Time (GMT): 2016/164/01:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3299761
89 A = 6783254
21 meter
Y = 4847818
95 meter E =
0003686
Z = -3413279
50 I = 52
01334
XDOT = -2989
435206 Wp = 105
13656
YDOT = 5306
893379 meter/sec RA = 82
79251 deg
ZDOT = 4650
508566 TA = 215
20187
MA = 215
22623
Ha = 219
943 n
mi
Hp = 214
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10825990
45 X = 3261887
34
Y = 15904917
80 feet Y = 4884507
57 meter
Z = -11198423
56 Z = -3397341
73
XDOT = -9807
858288 XDOT = -3071
146178
YDOT = 17411
067517 feet/sec YDOT = 5273
006304 meter/sec
ZDOT = 15257
574036 ZDOT = 4635
788583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13868660
83 X = -4227167
82
Y = 13392493
39 feet Y = 4082031
98 meter
Z = -11129893
86 Z = -3392391
65
XDOT = -17841
533707 XDOT = -5438
099474
YDOT = -5859
059122 feet/sec YDOT = -1785
841220 meter/sec
ZDOT = 15192
393589 ZDOT = 4630
641566
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
06159666
00016717 00000-0 10270-3 0 9149
2 25544 51
6426 83
6008 0001644 230
7018 129
3989 15
54539471 4185
Satellite: ISS
Catalog Number: 25544
Epoch time: 16164
06159666 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 83
6008 deg
Eccentricity:
0001644
Arg of perigee: 230
7018 deg
Mean anomaly: 129
3989 deg
Mean motion: 15
54539471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 418
Checksum: 318
Coasting Arc #16 (Orbit 422)
---------------------------------------
Vector Time (GMT): 2016/164/08:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4243870
46 A = 6776628
25 meter
Y = -693471
04 meter E =
0002679
Z = 5235886
37 I = 51
98701
XDOT = -215
190758 Wp = 54
43080
YDOT = -7577
079078 meter/sec RA = 81
40778 deg
ZDOT = -1176
033549 TA = 46
80122
MA = 46
77885
Ha = 220
123 n
mi
Hp = 214
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13923459
53 X = -4261234
15
Y = -2275167
44 feet Y = -741026
29 meter
Z = 17178104
87 Z = 5215228
49
XDOT = -706
006424 XDOT = -124
733304
YDOT = -24859
183328 feet/sec YDOT = -7578
979621 meter/sec
ZDOT = -3858
377784 ZDOT = -1176
859738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13891607
91 X = -4234162
09
Y = 3023739
13 feet Y = 921635
69 meter
Z = 17088201
50 Z = 5208483
82
XDOT = -9517
127427 XDOT = -2900
820440
YDOT = -21870
182371 feet/sec YDOT = -6666
031587 meter/sec
ZDOT = -3860
513834 ZDOT = -1176
684617
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
38302329
00016717 00000-0 10270-3 0 9151
2 25544 51
6396 81
9985 0001301 239
5744 120
5280 15
54532813 4235
Satellite: ISS
Catalog Number: 25544
Epoch time: 16164
38302329 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 81
9985 deg
Eccentricity:
0001301
Arg of perigee: 239
5744 deg
Mean anomaly: 120
5280 deg
Mean motion: 15
54532813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 423
Checksum: 300
Coasting Arc #17 (Orbit 437)
---------------------------------------
Vector Time (GMT): 2016/165/08:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4298621
21 A = 6779414
48 meter
Y = 2580839
42 meter E =
0008993
Z = -4572076
16 I = 51
99154
XDOT = -840
523145 Wp = 115
57606
YDOT = 6941
989682 meter/sec RA = 76
43186 deg
ZDOT = 3129
360159 TA = 185
64579
MA = 185
65594
Ha = 219
976 n
mi
Hp = 214
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14103087
96 X = 4291651
36
Y = 8467320
93 feet Y = 2628870
83 meter
Z = -15000249
86 Z = -4551211
22
XDOT = -2757
621868 XDOT = -933
288863
YDOT = 22775
556701 feet/sec YDOT = 6932
071477 meter/sec
ZDOT = 10266
929655 ZDOT = 3125
052295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16357045
16 X = 4985627
37
Y = 2396801
19 feet Y = 730545
00 meter
Z = -14909813
11 Z = -4544511
04
XDOT = 6269
690131 XDOT = 1911
001552
YDOT = 20934
029478 feet/sec YDOT = 6380
692185 meter/sec
ZDOT = 10246
798951 ZDOT = 3123
224320
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
34729606
00016717 00000-0 10270-3 0 9160
2 25544 51
6406 77
1889 0001216 246
4232 113
6793 15
54530213 4381
Satellite: ISS
Catalog Number: 25544
Epoch time: 16165
34729606 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 77
1889 deg
Eccentricity:
0001216
Arg of perigee: 246
4232 deg
Mean anomaly: 113
6793 deg
Mean motion: 15
54530213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 438
Checksum: 305
Coasting Arc #18 (Orbit 453)
---------------------------------------
Vector Time (GMT): 2016/166/08:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4152524
48 A = 6783430
17 meter
Y = -4194900
77 meter E =
0011455
Z = 3332219
81 I = 51
99665
XDOT = 1974
582938 Wp = 93
40182
YDOT = -5715
290206 meter/sec RA = 71
46597 deg
ZDOT = -4720
979319 TA = 47
99769
MA = 47
90020
Ha = 219
965 n
mi
Hp = 214
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13623767
97 X = -4121493
98
Y = -13762797
81 feet Y = -4241163
83 meter
Z = 10932479
68 Z = 3312122
82
XDOT = 6478
290478 XDOT = 2061
278584
YDOT = -18750
952120 feet/sec YDOT = -5692
723983 meter/sec
ZDOT = -15488
777292 ZDOT = -4711
177124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18039845
17 X = -5498544
81
Y = -7174625
76 feet Y = -2186825
93 meter
Z = 10845713
47 Z = 3305773
47
XDOT = -1952
099889 XDOT = -595
000046
YDOT = -18505
741817 feet/sec YDOT = -5640
550106 meter/sec
ZDOT = -15444
927490 ZDOT = -4707
613899
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
37584655
00016717 00000-0 10270-3 0 9178
2 25544 51
6404 72
0584 0001229 255
4972 104
6045 15
54562604 4547
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
37584655 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 72
0584 deg
Eccentricity:
0001229
Arg of perigee: 255
4972 deg
Mean anomaly: 104
6045 deg
Mean motion: 15
54562604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 454
Checksum: 309
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