[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 10th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 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
132/13:18:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
2
135/07:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
1
Coasting Arc #1 (Orbit 3896)
---------------------------------------
Vector Time (GMT): 2016/130/12:43:45
138
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4545357
60 A = 6781178
29 meter
Y = 2970189
51 meter E =
0012324
Z = 4053131
79 I = 51
29101
XDOT = -868
111093 Wp = 80
81291
YDOT = 6585
704575 meter/sec RA = 249
90566 deg
ZDOT = -3840
609422 TA = 49
13946
MA = 49
03272
Ha = 220
980 n
mi
Hp = 213
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14912590
56 X = 4492117
74
Y = 9744716
23 feet Y = 3020720
80 meter
Z = 13297676
48 Z = 4075083
16
XDOT = -2848
133508 XDOT = -923
033283
YDOT = 21606
642307 feet/sec YDOT = 6575
689913 meter/sec
ZDOT = -12600
424612 ZDOT = -3844
959569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16141310
98 X = 4919871
59
Y = -7366976
14 feet Y = -2245454
33 meter
Z = 13392490
19 Z = 4082031
01
XDOT = 16282
860603 XDOT = 4963
015912
YDOT = 12662
677908 feet/sec YDOT = 3859
584226 meter/sec
ZDOT = -12620
497677 ZDOT = -3846
727692
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 16130
57153142
00016717 00000-0 10270-3 0 9006
2 25544 51
6430 250
6723 0001862 101
2349 258
9013 15
54497794 38973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16130
57153142 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 250
6723 deg
Eccentricity:
0001862
Arg of perigee: 101
2349 deg
Mean anomaly: 258
9013 deg
Mean motion: 15
54497794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3897
Checksum: 303
Coasting Arc #2 (Orbit 3911)
---------------------------------------
Vector Time (GMT): 2016/131/12:43:45
138
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4419028
49 A = 6785144
37 meter
Y = -4407720
23 meter E =
0006158
Z = -2662462
10 I = 51
31653
XDOT = 2118
758788 Wp = 66
27099
YDOT = -5242
189869 meter/sec RA = 244
89796 deg
ZDOT = 5173
810005 TA = 263
55397
MA = 263
62409
Ha = 220
949 n
mi
Hp = 213
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14498124
98 X = -4356478
61
Y = -14461024
38 feet Y = -4456786
86 meter
Z = -8735111
89 Z = -2683777
18
XDOT = 6951
308358 XDOT = 2152
088410
YDOT = -17198
785659 feet/sec YDOT = -5218
310442 meter/sec
ZDOT = 16974
442272 ZDOT = 5184
183156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19848242
14 X = -6049744
20
Y = 4873580
68 feet Y = 1485467
39 meter
Z = -8826920
71 Z = -2690445
43
XDOT = -10819
410942 XDOT = -3297
756455
YDOT = -13306
604515 feet/sec YDOT = -4055
853056 meter/sec
ZDOT = 17020
432550 ZDOT = 5187
827841
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 16131
53581438
00016717 00000-0 10270-3 0 9017
2 25544 51
6432 245
8637 0001604 99
7640 260
3694 15
54510772 39126
Satellite: ISS
Catalog Number: 25544
Epoch time: 16131
53581438 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 245
8637 deg
Eccentricity:
0001604
Arg of perigee: 99
7640 deg
Mean anomaly: 260
3694 deg
Mean motion: 15
54510772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3912
Checksum: 307
Coasting Arc #3 (Orbit 3927)
---------------------------------------
Vector Time (GMT): 2016/132/12:43:45
138
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3977704
90 A = 6787767
95 meter
Y = 5416168
05 meter E =
0015134
Z = 906429
52 I = 51
33960
XDOT = -3421
196797 Wp = 123
14011
YDOT = 3510
670277 meter/sec RA = 239
90093 deg
ZDOT = -5900
463049 TA = 47
00280
MA = 46
87606
Ha = 220
945 n
mi
Hp = 213
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13050212
94 X = 3912441
25
Y = 17769580
22 feet Y = 5460284
44 meter
Z = 2973850
13 Z = 925594
09
XDOT = -11224
398939 XDOT = -3431
537623
YDOT = 11517
947102 feet/sec YDOT = 3472
354650 meter/sec
ZDOT = -19358
474571 ZDOT = -5917
107421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21911928
76 X = 6678755
89
Y = -2331761
30 feet Y = -710720
84 meter
Z = 3056156
20 Z = 931516
41
XDOT = 4205
524403 XDOT = 1281
843838
YDOT = 13786
432085 feet/sec YDOT = 4202
104499 meter/sec
ZDOT = -19431
400743 ZDOT = -5922
690947
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 16132
56437256
00016717 00000-0 10270-3 0 9020
2 25544 51
6428 240
7335 0001722 106
8539 253
2802 15
54540115 39281
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
56437256 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 240
7335 deg
Eccentricity:
0001722
Arg of perigee: 106
8539 deg
Mean anomaly: 253
2802 deg
Mean motion: 15
54540115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3928
Checksum: 295
Coasting Arc #4 (Orbit 3927)
---------------------------------------
Vector Time (GMT): 2016/132/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4937547
20 A = 6779575
03 meter
Y = -1419771
88 meter E =
0011019
Z = -4434639
21 I = 51
31320
XDOT = -964
031266 Wp = 109
60374
YDOT = -6858
059952 meter/sec RA = 239
76782 deg
ZDOT = 3272
030808 TA = 193
56126
MA = 193
59090
Ha = 220
874 n
mi
Hp = 213
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16199301
82 X = -4899762
28
Y = -4658044
23 feet Y = -1474775
33 meter
Z = -14549341
24 Z = -4458533
03
XDOT = -3162
832237 XDOT = -903
165296
YDOT = -22500
196694 feet/sec YDOT = -6868
500230 meter/sec
ZDOT = 10735
009214 ZDOT = 3267
495256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10259403
62 X = -3127066
22
Y = 13260293
13 feet Y = 4041737
35 meter
Z = -14652895
60 Z = -4466202
58
XDOT = -21142
626736 XDOT = -6444
272629
YDOT = -4526
865655 feet/sec YDOT = -1379
788652 meter/sec
ZDOT = 10716
510017 ZDOT = 3266
392253
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 16132
56437168
00016717 00000-0 10270-3 0 9033
2 25544 51
6430 240
7343 0001664 102
9235 257
2104 15
54578752 39285
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
56437168 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 240
7343 deg
Eccentricity:
0001664
Arg of perigee: 102
9235 deg
Mean anomaly: 257
2104 deg
Mean motion: 15
54578752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3928
Checksum: 302
Coasting Arc #5 (Orbit 3943)
---------------------------------------
Vector Time (GMT): 2016/133/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5200313
87 A = 6783738
84 meter
Y = 2995485
82 meter E =
0014534
Z = 3148698
50 I = 51
34373
XDOT = -505
617006 Wp = 94
93584
YDOT = 5954
841474 meter/sec RA = 234
75712 deg
ZDOT = -4812
044357 TA = 48
55505
MA = 48
43030
Ha = 220
825 n
mi
Hp = 213
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17061397
21 X = 5151136
01
Y = 9827709
39 feet Y = 3053364
11 meter
Z = 10330375
66 Z = 3173841
11
XDOT = -1658
848444 XDOT = -548
793003
YDOT = 19536
881478 feet/sec YDOT = 5948
946087 meter/sec
ZDOT = -15787
547104 ZDOT = -4814
605189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15181277
20 X = 4627253
29
Y = -12447728
17 feet Y = -3794067
55 meter
Z = 10439094
49 Z = 3181836
00
XDOT = 16829
619068 XDOT = 5129
667892
YDOT = 7226
316907 feet/sec YDOT = 2202
581393 meter/sec
ZDOT = -15799
708949 ZDOT = -4815
751288
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 16133
59291774
00016717 00000-0 10270-3 0 9049
2 25544 51
6427 235
6039 0001690 100
6646 259
4697 15
54573906 39441
Satellite: ISS
Catalog Number: 25544
Epoch time: 16133
59291774 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 235
6039 deg
Eccentricity:
0001690
Arg of perigee: 100
6646 deg
Mean anomaly: 259
4697 deg
Mean motion: 15
54573906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3944
Checksum: 334
Coasting Arc #6 (Orbit 3958)
---------------------------------------
Vector Time (GMT): 2016/134/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5119979
40 A = 6787102
64 meter
Y = -4189291
00 meter E =
0008995
Z = -1504277
86 I = 51
37321
XDOT = 2101
978846 Wp = 46
59822
YDOT = -4621
696150 meter/sec RA = 229
75941 deg
ZDOT = 5744
445922 TA = 296
91347
MA = 297
00535
Ha = 220
859 n
mi
Hp = 213
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16797832
67 X = -5065446
00
Y = -13744393
05 feet Y = -4246241
07 meter
Z = -4935294
80 Z = -1529017
18
XDOT = 6896
256058 XDOT = 2125
599413
YDOT = -15163
045113 feet/sec YDOT = -4598
058476 meter/sec
ZDOT = 18846
607357 ZDOT = 5754
714130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18576834
42 X = -5662219
13
Y = 11176376
84 feet Y = 3406559
66 meter
Z = -5042071
14 Z = -1536823
28
XDOT = -11190
795451 XDOT = -3410
954454
YDOT = -10118
083113 feet/sec YDOT = -3083
991733 meter/sec
ZDOT = 18892
020426 ZDOT = 5758
287826
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 16134
55716937
00016717 00000-0 10270-3 0 9050
2 25544 51
6419 230
7946 0001529 99
7017 260
4309 15
54548202 39595
Satellite: ISS
Catalog Number: 25544
Epoch time: 16134
55716937 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 230
7946 deg
Eccentricity:
0001529
Arg of perigee: 99
7017 deg
Mean anomaly: 260
4309 deg
Mean motion: 15
54548202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3959
Checksum: 329
Coasting Arc #7 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3693427
71 A = 6776200
92 meter
Y = 2215233
30 meter E =
0016353
Z = -5245810
27 I = 51
35132
XDOT = -4773
789700 Wp = 97
82687
YDOT = -5924
881796 meter/sec RA = 225
95986 deg
ZDOT = 859
218138 TA = 180
43319
MA = 180
43461
Ha = 220
908 n
mi
Hp = 213
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12117544
99 X = -3692442
48
Y = 7267825
79 feet Y = 2173936
51 meter
Z = -17210663
61 Z = -5263749
69
XDOT = -15662
039698 XDOT = -4711
355126
YDOT = -19438
588571 feet/sec YDOT = -5977
916408 meter/sec
ZDOT = 2818
957146 ZDOT = 836
179707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13503203
09 X = -4115776
30
Y = 3823242
51 feet Y = 1165324
32 meter
Z = -17288998
04 Z = -5269686
60
XDOT = -9686
808421 XDOT = -2952
539207
YDOT = -21914
978417 feet/sec YDOT = -6679
685421 meter/sec
ZDOT = 2719
856409 ZDOT = 829
012234
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 16135
32856499
00016717 00000-0 10270-3 0 9065
2 25544 51
6399 226
9444 0001855 106
2184 253
9173 15
54604509 39716
Satellite: ISS
Catalog Number: 25544
Epoch time: 16135
32856499 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 226
9444 deg
Eccentricity:
0001855
Arg of perigee: 106
2184 deg
Mean anomaly: 253
9173 deg
Mean motion: 15
54604509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 335
Coasting Arc #8 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2016/136/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4884972
18 A = 6778719
17 meter
Y = -674201
15 meter E =
0009502
Z = 4644688
51 I = 51
38239
XDOT = 3585
671834 Wp = 72
39647
YDOT = 6146
351311 meter/sec RA = 220
93801 deg
ZDOT = -2871
316171 TA = 46
25799
MA = 46
17936
Ha = 220
823 n
mi
Hp = 213
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16026811
60 X = 4869586
13
Y = -2211946
02 feet Y = -619660
19 meter
Z = 15238479
38 Z = 4668381
29
XDOT = 11764
015204 XDOT = 3530
623024
YDOT = 20165
194590 feet/sec YDOT = 6186
140900 meter/sec
ZDOT = -9420
328646 ZDOT = -2854
031415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15978072
76 X = 4870116
58
Y = 1816699
51 feet Y = 553730
01 meter
Z = 15341559
33 Z = 4676107
28
XDOT = 6575
593738 XDOT = 2004
240971
YDOT = 21304
918348 feet/sec YDOT = 6493
739113 meter/sec
ZDOT = -9346
253355 ZDOT = -2848
738023
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 16136
35708244
00016717 00000-0 10270-3 0 9074
2 25544 51
6397 221
8124 0001917 109
0890 251
0471 15
54581332 39872
Satellite: ISS
Catalog Number: 25544
Epoch time: 16136
35708244 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 221
8124 deg
Eccentricity:
0001917
Arg of perigee: 109
0890 deg
Mean anomaly: 251
0471 deg
Mean motion: 15
54581332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 310
Coasting Arc #9 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2016/137/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5772968
13 A = 6782627
58 meter
Y = -747265
63 meter E =
0006951
Z = -3488250
20 I = 51
42150
XDOT = -1964
027468 Wp = 99
49206
YDOT = -5870
722311 meter/sec RA = 215
93024 deg
ZDOT = 4514
644503 TA = 219
39725
MA = 219
44783
Ha = 220
848 n
mi
Hp = 213
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18940184
15 X = -5747238
36
Y = -2451658
90 feet Y = -811678
93 meter
Z = -11444390
41 Z = -3516231
63
XDOT = -6443
659671 XDOT = -1920
164038
YDOT = -19260
899972 feet/sec YDOT = -5892
440140 meter/sec
ZDOT = 14811
825796 ZDOT = 4505
210162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17783835
23 X = -5420512
98
Y = -6758767
81 feet Y = -2060072
43 meter
Z = -11565878
30 Z = -3525279
71
XDOT = -2389
660806 XDOT = -728
368614
YDOT = -18953
835222 feet/sec YDOT = -5777
128976 meter/sec
ZDOT = 14771
810703 ZDOT = 4502
447902
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 16137
32130813
00016717 00000-0 10270-3 0 9084
2 25544 51
6404 217
0032 0001869 111
2247 248
9105 15
54621344 40029
Satellite: ISS
Catalog Number: 25544
Epoch time: 16137
32130813 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 217
0032 deg
Eccentricity:
0001869
Arg of perigee: 111
2247 deg
Mean anomaly: 248
9105 deg
Mean motion: 15
54621344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 267
Coasting Arc #10 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2016/138/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6206713
71 A = 6786345
04 meter
Y = 1994066
47 meter E =
0015728
Z = 1858339
45 I = 51
46031
XDOT = 12
818981 Wp = 113
90541
YDOT = 5225
100523 meter/sec RA = 210
93544 deg
ZDOT = -5618
136303 TA = 45
57792
MA = 45
44931
Ha = 220
760 n
mi
Hp = 213
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20363233
95 X = 6174927
13
Y = 6542212
82 feet Y = 2063296
33 meter
Z = 6096914
20 Z = 1888413
33
XDOT = 42
057024 XDOT = -18
319500
YDOT = 17142
718250 feet/sec YDOT = 5225
069820 meter/sec
ZDOT = -18432
205718 ZDOT = -5618
149614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18441400
26 X = 5620938
80
Y = 10759633
35 feet Y = 3279536
25 meter
Z = 6227299
16 Z = 1898080
78
XDOT = -2743
995514 XDOT = -836
369833
YDOT = 15429
888710 feet/sec YDOT = 4703
030079 meter/sec
ZDOT = -18433
139515 ZDOT = -5618
420924
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 16138
34980855
00016717 00000-0 10270-3 0 9097
2 25544 51
6403 211
8720 0001774 117
1082 243
0252 15
54630680 40180
Satellite: ISS
Catalog Number: 25544
Epoch time: 16138
34980855 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 211
8720 deg
Eccentricity:
0001774
Arg of perigee: 117
1082 deg
Mean anomaly: 243
0252 deg
Mean motion: 15
54630680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 291
Coasting Arc #11 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2016/139/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6108266
97 A = 6787811
99 meter
Y = -2948383
52 meter E =
0012685
Z = -27552
28 I = 51
49503
XDOT = 2060
560545 Wp = 53
11394
YDOT = -4307
060129 meter/sec RA = 205
95119 deg
ZDOT = 6001
275321 TA = 306
58864
MA = 306
70528
Ha = 220
770 n
mi
Hp = 213
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20040245
97 X = -6074709
59
Y = -9673174
29 feet Y = -3016502
60 meter
Z = -90394
61 Z = -57143
74
XDOT = 6760
369241 XDOT = 2079
417942
YDOT = -14130
774702 feet/sec YDOT = -4283
912246 meter/sec
ZDOT = 19689
223495 ZDOT = 6011
330892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17724687
37 X = -5402484
71
Y = -13452792
66 feet Y = -4100411
20 meter
Z = -218535
87 Z = -66609
73
XDOT = 8321
018253 XDOT = 2536
246364
YDOT = -11241
542696 feet/sec YDOT = -3426
422214 meter/sec
ZDOT = 19733
655264 ZDOT = 6014
818124
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 16139
31401994
00016717 00000-0 10270-3 0 9109
2 25544 51
6420 207
0623 0001800 116
0231 244
1108 15
54649296 40334
Satellite: ISS
Catalog Number: 25544
Epoch time: 16139
31401994 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 207
0623 deg
Eccentricity:
0001800
Arg of perigee: 116
0231 deg
Mean anomaly: 244
1108 deg
Mean motion: 15
54649296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4033
Checksum: 267
Coasting Arc #12 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2016/140/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5409805
43 A = 6786349
11 meter
Y = 3649847
31 meter E =
0008991
Z = -1851948
40 I = 51
51871
XDOT = -4092
034901 Wp = 137
24803
YDOT = 3221
631173 meter/sec RA = 200
96941 deg
ZDOT = -5626
701955 TA = 63
16275
MA = 63
07084
Ha = 220
781 n
mi
Hp = 213
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17748705
46 X = 5377585
98
Y = 11974564
65 feet Y = 3710163
26 meter
Z = -6075946
20 Z = -1825746
58
XDOT = -13425
311355 XDOT = -4100
423266
YDOT = 10569
656081 feet/sec YDOT = 3175
824598 meter/sec
ZDOT = -18460
308252 ZDOT = -5646
600668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15321872
38 X = 4670106
70
Y = 15000365
26 feet Y = 4572111
33 meter
Z = -5962644
97 Z = -1817414
19
XDOT = -13907
733957 XDOT = -4239
077310
YDOT = 6863
179808 feet/sec YDOT = 2091
897205 meter/sec
ZDOT = -18547
355104 ZDOT = -5653
233836
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 16140
34250506
00016717 00000-0 10270-3 0 9116
2 25544 51
6411 201
9317 0001803 118
1181 242
0154 15
54670453 40491
Satellite: ISS
Catalog Number: 25544
Epoch time: 16140
34250506 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 201
9317 deg
Eccentricity:
0001803
Arg of perigee: 118
1181 deg
Mean anomaly: 242
0154 deg
Mean motion: 15
54670453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4049
Checksum: 261
Coasting Arc #13 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2016/141/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4181463
62 A = 6782655
15 meter
Y = -4057700
61 meter E =
0013841
Z = 3461342
21 I = 51
53727
XDOT = 5812
139059 Wp = 95
26224
YDOT = -2094
425890 meter/sec RA = 195
98152 deg
ZDOT = 4549
136077 TA = 305
45048
MA = 305
57961
Ha = 220
707 n
mi
Hp = 213
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13718712
67 X = -4152592
65
Y = -13312666
06 feet Y = -4104299
27 meter
Z = 11356109
60 Z = 3441099
24
XDOT = 19068
697700 XDOT = 5813
029313
YDOT = -6871
476016 feet/sec YDOT = -2029
425929 meter/sec
ZDOT = 14924
987129 ZDOT = 4577
372598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11416223
81 X = -3479665
02
Y = -15397271
57 feet Y = -4693088
37 meter
Z = 11268772
90 Z = 3434721
98
XDOT = 18720
529588 XDOT = 5706
017418
YDOT = -2826
053623 feet/sec YDOT = -861
381144 meter/sec
ZDOT = 15048
107933 ZDOT = 4586
663298
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 16141
37098268
00016717 00000-0 10270-3 0 9126
2 25544 51
6415 196
8013 0001776 126
9450 233
1866 15
54702388 40657
Satellite: ISS
Catalog Number: 25544
Epoch time: 16141
37098268 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 196
8013 deg
Eccentricity:
0001776
Arg of perigee: 126
9450 deg
Mean anomaly: 233
1866 deg
Mean motion: 15
54702388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4065
Checksum: 317
Coasting Arc #14 (Orbit 4079)
---------------------------------------
Vector Time (GMT): 2016/142/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2480266
94 A = 6778591
72 meter
Y = 4255926
39 meter E =
0011505
Z = -4667557
79 I = 51
55504
XDOT = -7036
765230 Wp = 77
92875
YDOT = 956
115965 meter/sec RA = 190
98320 deg
ZDOT = -2871
073949 TA = 163
49775
MA = 163
46027
Ha = 220
686 n
mi
Hp = 213
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8137358
72 X = 2455165
18
Y = 13963013
08 feet Y = 4283522
34 meter
Z = -15313509
81 Z = -4655569
73
XDOT = -23086
500098 XDOT = -7032
987062
YDOT = 3136
863403 feet/sec YDOT = 877
447489 meter/sec
ZDOT = -9419
533954 ZDOT = -2905
248207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6088509
95 X = 1855777
83
Y = 15022799
07 feet Y = 4578949
16 meter
Z = -15262092
87 Z = -4651885
91
XDOT = -22140
630076 XDOT = -6748
464047
YDOT = -735
267902 feet/sec YDOT = -224
109656 meter/sec
ZDOT = -9568
300178 ZDOT = -2916
417894
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 16142
33517642
00016717 00000-0 10270-3 0 9136
2 25544 51
6420 191
9916 0001720 127
1217 233
0094 15
54670249 40803
Satellite: ISS
Catalog Number: 25544
Epoch time: 16142
33517642 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 191
9916 deg
Eccentricity:
0001720
Arg of perigee: 127
1217 deg
Mean anomaly: 233
0094 deg
Mean motion: 15
54670249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4080
Checksum: 283
Coasting Arc #15 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2016/143/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -512622
92 A = 6775874
48 meter
Y = -4243929
48 meter E =
0005080
Z = 5253928
84 I = 51
57799
XDOT = 7625
313599 Wp = 123
33689
YDOT = 126
181494 meter/sec RA = 185
97580 deg
ZDOT = 842
599630 TA = 318
58617
MA = 318
62467
Ha = 220
602 n
mi
Hp = 213
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1681833
72 X = -490649
91
Y = -13923653
13 feet Y = -4249539
54 meter
Z = 17237299
36 Z = 5251491
63
XDOT = 25017
433069 XDOT = 7619
242816
YDOT = 413
981280 feet/sec YDOT = 211
418811 meter/sec
ZDOT = 2764
434481 ZDOT = 879
627416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 36871
94 X = 11238
57
Y = -14036953
94 feet Y = -4278463
56 meter
Z = 17227412
31 Z = 5250915
27
XDOT = 23708
324172 XDOT = 7226
297208
YDOT = 3666
038382 feet/sec YDOT = 1117
408499 meter/sec
ZDOT = 2925
449840 ZDOT = 891
677111
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 16143
36364015
00016717 00000-0 10270-3 0 9145
2 25544 51
6417 186
8604 0001690 127
4833 232
6473 15
54724158 40961
Satellite: ISS
Catalog Number: 25544
Epoch time: 16143
36364015 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 186
8604 deg
Eccentricity:
0001690
Arg of perigee: 127
4833 deg
Mean anomaly: 232
6473 deg
Mean motion: 15
54724158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4096
Checksum: 310
Coasting Arc #16 (Orbit 4110)
---------------------------------------
Vector Time (GMT): 2016/144/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1545017
47 A = 6776167
05 meter
Y = 4088224
12 meter E =
0015621
Z = -5192238
21 I = 51
61063
XDOT = -7455
972168 Wp = 103
18015
YDOT = -1160
106657 meter/sec RA = 180
96825 deg
ZDOT = 1305
015127 TA = 179
37858
MA = 179
37664
Ha = 220
608 n
mi
Hp = 213
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5068954
96 X = -1565396
15
Y = 13412808
80 feet Y = 4070833
25 meter
Z = -17034902
26 Z = -5199792
75
XDOT = -24461
850944 XDOT = -7448
784716
YDOT = -3806
124202 feet/sec YDOT = -1243
444233 meter/sec
ZDOT = 4281
545692 ZDOT = 1268
812674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6446066
68 X = -1964761
12
Y = 12763301
45 feet Y = 3890254
28 meter
Z = -17068450
42 Z = -5202463
69
XDOT = -22969
648635 XDOT = -7001
148904
YDOT = -6084
591962 feet/sec YDOT = -1854
583630 meter/sec
ZDOT = 4124
270887 ZDOT = 1257
077766
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 16144
32782208
00016717 00000-0 10270-3 0 9151
2 25544 51
6414 182
0514 0001755 128
3412 231
7899 15
54717531 41118
Satellite: ISS
Catalog Number: 25544
Epoch time: 16144
32782208 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 182
0514 deg
Eccentricity:
0001755
Arg of perigee: 128
3412 deg
Mean anomaly: 231
7899 deg
Mean motion: 15
54717531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4111
Checksum: 293
Coasting Arc #17 (Orbit 4126)
---------------------------------------
Vector Time (GMT): 2016/145/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3459677
84 A = 6779186
64 meter
Y = -3766878
76 meter E =
0010053
Z = 4442244
06 I = 51
65308
XDOT = 6586
472860 Wp = 78
03361
YDOT = 2150
676483 meter/sec RA = 175
96632 deg
ZDOT = -3297
581346 TA = 45
23391
MA = 45
15217
Ha = 220
543 n
mi
Hp = 213
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11350649
08 X = 3479964
12
Y = -12358526
10 feet Y = -3728077
36 meter
Z = 14574291
52 Z = 4459099
41
XDOT = 21609
162926 XDOT = 6577
952357
YDOT = 7056
025207 feet/sec YDOT = 2224
283494 meter/sec
ZDOT = -10818
836437 ZDOT = -3265
605997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12392458
71 X = 3777221
42
Y = -11217664
62 feet Y = -3419144
18 meter
Z = 14648253
91 Z = 4464787
79
XDOT = 20081
670406 XDOT = 6120
893140
YDOT = 8202
906592 feet/sec YDOT = 2500
245929 meter/sec
ZDOT = -10680
094700 ZDOT = -3255
292865
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 16145
35627589
00016717 00000-0 10270-3 0 9166
2 25544 51
6416 176
9197 0001750 130
2897 229
8409 15
54703131 41276
Satellite: ISS
Catalog Number: 25544
Epoch time: 16145
35627589 = yrday
fracday
Element set: 916
Inclination: 51
6416 deg
RA of node: 176
9197 deg
Eccentricity:
0001750
Arg of perigee: 130
2897 deg
Mean anomaly: 229
8409 deg
Mean motion: 15
54703131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4127
Checksum: 326
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