[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 4th 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
170/05:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 214
4
Coasting Arc #1 (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 = 1769974
72 A = 6777168
47 meter
Y = 4255656
55 meter E =
0013486
Z = -4981010
88 I = 51
92179
XDOT = -5517
466542 Wp = 109
03947
YDOT = 4844
310688 meter/sec RA = 125
27304 deg
ZDOT = 2178
789014 TA = 182
14379
MA = 182
14958
Ha = 220
376 n
mi
Hp = 213
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5807003
68 X = 1746451
35
Y = 13962127
79 feet Y = 4275318
58 meter
Z = -16341899
21 Z = -4972469
34
XDOT = -18101
924350 XDOT = -5581
810555
YDOT = 15893
407768 feet/sec YDOT = 4782
250710 meter/sec
ZDOT = 7148
257921 ZDOT = 2151
830320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15114663
41 X = 4606949
41
Y = -1182812
86 feet Y = -360521
36 meter
Z = -16305455
46 Z = -4969902
82
XDOT = 9236
854352 XDOT = 2815
393206
YDOT = 21147
243331 feet/sec YDOT = 6445
679767 meter/sec
ZDOT = 7029
976856 ZDOT = 2142
736946
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
51235522
00016717 00000-0 10270-3 0 9000
2 25544 51
6386 126
2512 0001207 141
7461 218
3778 15
54715795 2854
Satellite: ISS
Catalog Number: 25544
Epoch time: 16155
51235522 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 126
2512 deg
Eccentricity:
0001207
Arg of perigee: 141
7461 deg
Mean anomaly: 218
3778 deg
Mean motion: 15
54715795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 285
Checksum: 298
Coasting Arc #2 (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 = -390479
17 A = 6780863
00 meter
Y = -5481182
35 meter E =
0011510
Z = 3963892
65 I = 51
95226
XDOT = 5608
539006 Wp = 84
72572
YDOT = -3330
012427 meter/sec RA = 120
29631 deg
ZDOT = -4041
090339 TA = 47
29570
MA = 47
19884
Ha = 220
315 n
mi
Hp = 213
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1281099
63 X = -348413
33
Y = -17982881
73 feet Y = -5485314
24 meter
Z = 13004897
15 Z = 3962097
27
XDOT = 18400
718524 XDOT = 5664
989339
YDOT = -10925
237622 feet/sec YDOT = -3266
977876 meter/sec
ZDOT = -13258
170402 ZDOT = -4013
708388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17560411
87 X = -5352413
54
Y = -4103024
09 feet Y = -1250601
74 meter
Z = 12998066
39 Z = 3961810
64
XDOT = -5164
114884 XDOT = -1574
022217
YDOT = -19634
639744 feet/sec YDOT = -5984
638194 meter/sec
ZDOT = -13138
294516 ZDOT = -4004
552168
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
54078338
00016717 00000-0 10270-3 0 9015
2 25544 51
6386 121
1198 0001090 143
8529 216
2698 15
54747371 3018
Satellite: ISS
Catalog Number: 25544
Epoch time: 16156
54078338 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 121
1198 deg
Eccentricity:
0001090
Arg of perigee: 143
8529 deg
Mean anomaly: 216
2698 deg
Mean motion: 15
54747371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 307
Coasting Arc #3 (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 = -841694
41 A = 6784994
41 meter
Y = 6267905
04 meter E =
0005335
Z = -2457432
54 I = 51
98166
XDOT = -5296
539897 Wp = 60
21961
YDOT = 1387
347568 meter/sec RA = 115
33372 deg
ZDOT = 5363
951900 TA = 272
40964
MA = 272
47071
Ha = 220
286 n
mi
Hp = 213
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2761464
60 X = -899783
88
Y = 20563992
92 feet Y = 6258168
20 meter
Z = -8062442
73 Z = -2461661
54
XDOT = -17377
099399 XDOT = -5337
715914
YDOT = 4551
665248 feet/sec YDOT = 1327
887159 meter/sec
ZDOT = 17598
267390 ZDOT = 5338
122578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18945968
80 X = 5774731
29
Y = 8440250
31 feet Y = 2572588
29 meter
Z = -8082011
84 Z = -2463397
21
XDOT = 11
806688 XDOT = 3
598678
YDOT = 16681
480924 feet/sec YDOT = 5084
515386 meter/sec
ZDOT = 17485
489064 ZDOT = 5329
577067
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
50493169
00016717 00000-0 10270-3 0 9026
2 25544 51
6389 116
3095 0001099 148
1720 211
9500 15
54732850 3169
Satellite: ISS
Catalog Number: 25544
Epoch time: 16157
50493169 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 116
3095 deg
Eccentricity:
0001099
Arg of perigee: 148
1720 deg
Mean anomaly: 211
9500 deg
Mean motion: 15
54732850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 316
Checksum: 299
Coasting Arc #4 (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 = -4288842
69 A = 6776128
38 meter
Y = -405406
38 meter E =
0005000
Z = 5227776
05 I = 51
95699
XDOT = 2157
140767 Wp = 131
33112
YDOT = -7263
651713 meter/sec RA = 113
67353 deg
ZDOT = 1202
463027 TA = 307
16671
MA = 307
21236
Ha = 220
405 n
mi
Hp = 213
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14071006
19 X = -4309385
04
Y = -1330073
41 feet Y = -453482
67 meter
Z = 17151496
23 Z = 5206891
82
XDOT = 7077
233486 XDOT = 2232
363327
YDOT = -23830
878323 feet/sec YDOT = -7239
108706 meter/sec
ZDOT = 3945
088670 ZDOT = 1213
123632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13982718
38 X = 4261932
56
Y = -2712221
46 feet Y = -826685
10 meter
Z = 17060585
42 Z = 5200066
44
XDOT = -264
984315 XDOT = -80
767219
YDOT = 23832
209620 feet/sec YDOT = 7264
057492 meter/sec
ZDOT = 3992
865694 ZDOT = 1217
025464
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
89058954
00016717 00000-0 10270-3 0 9038
2 25544 51
6394 114
3842 0001081 158
3655 201
7544 15
54715755 3221
Satellite: ISS
Catalog Number: 25544
Epoch time: 16157
89058954 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 114
3842 deg
Eccentricity:
0001081
Arg of perigee: 158
3655 deg
Mean anomaly: 201
7544 deg
Mean motion: 15
54715755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 322
Checksum: 313
Coasting Arc #5 (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 = 3555515
91 A = 6775811
17 meter
Y = 2363977
17 meter E =
0014981
Z = -5274381
99 I = 51
96823
XDOT = -3145
755263 Wp = 101
46719
YDOT = 6913
729637 meter/sec RA = 108
68792 deg
ZDOT = 977
594711 TA = 177
86252
MA = 177
85611
Ha = 220
184 n
mi
Hp = 213
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11665078
45 X = 3554437
81
Y = 7755830
62 feet Y = 2403732
04 meter
Z = -17304402
84 Z = -5257112
41
XDOT = -10320
719367 XDOT = -3227
581266
YDOT = 22682
840017 feet/sec YDOT = 6878
094052 meter/sec
ZDOT = 3207
331729 ZDOT = 962
115624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13550510
55 X = -4130195
61
Y = -3897954
04 feet Y = -1188096
39 meter
Z = -17229594
88 Z = -5251580
52
XDOT = 2837
393921 XDOT = 864
837667
YDOT = -23744
854880 feet/sec YDOT = -7237
431767 meter/sec
ZDOT = 3138
606183 ZDOT = 956
647165
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
85473038
00016717 00000-0 10270-3 0 9040
2 25544 51
6392 109
5722 0001163 159
6494 200
4705 15
54764190 3376
Satellite: ISS
Catalog Number: 25544
Epoch time: 16158
85473038 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 109
5722 deg
Eccentricity:
0001163
Arg of perigee: 159
6494 deg
Mean anomaly: 200
4705 deg
Mean motion: 15
54764190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 337
Checksum: 310
Coasting Arc #6 (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 = -2695348
91 A = 6778541
56 meter
Y = -4165565
55 meter E =
0008307
Z = 4612945
48 I = 51
98670
XDOT = 3879
040616 Wp = 73
65295
YDOT = -5881
703771 meter/sec RA = 103
70881 deg
ZDOT = -3037
955941 TA = 46
55041
MA = 46
48133
Ha = 220
245 n
mi
Hp = 213
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8843008
24 X = -2670975
86
Y = -13666553
63 feet Y = -4195571
07 meter
Z = 15134335
57 Z = 4599910
81
XDOT = 12726
511207 XDOT = 3959
280060
YDOT = -19296
928383 feet/sec YDOT = -5837
876704 meter/sec
ZDOT = -9967
047052 ZDOT = -3018
918457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12779008
50 X = 3895041
79
Y = 10166758
50 feet Y = 3098827
99 meter
Z = 15078314
21 Z = 4595870
17
XDOT = -5342
764716 XDOT = -1628
474685
YDOT = 21406
164442 feet/sec YDOT = 6524
598922 meter/sec
ZDOT = -9882
990765 ZDOT = -3012
335585
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
88314345
00016717 00000-0 10270-3 0 9050
2 25544 51
6392 104
4411 0001153 168
0197 192
0983 15
54751536 3530
Satellite: ISS
Catalog Number: 25544
Epoch time: 16159
88314345 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 104
4411 deg
Eccentricity:
0001153
Arg of perigee: 168
0197 deg
Mean anomaly: 192
0983 deg
Mean motion: 15
54751536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 304
Coasting Arc #7 (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 = 3878145
21 A = 6776556
25 meter
Y = 1767787
28 meter E =
0013755
Z = -5280429
48 I = 51
98607
XDOT = -2049
916910 Wp = 101
39536
YDOT = 7318
850999 meter/sec RA = 100
07483 deg
ZDOT = 944
110784 TA = 177
60946
MA = 177
60288
Ha = 220
138 n
mi
Hp = 214
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12723573
53 X = 3883739
10
Y = 5799827
03 feet Y = 1811187
21 meter
Z = -17324243
71 Z = -5261576
68
XDOT = -6725
449179 XDOT = -2136
191849
YDOT = 24011
978342 feet/sec YDOT = 7295
444955 meter/sec
ZDOT = 3097
476324 ZDOT = 933
944182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2576673
44 X = 785370
07
Y = -13846173
05 feet Y = -4220313
54 meter
Z = -17242418
13 Z = -5255489
05
XDOT = 23917
985698 XDOT = 7290
202041
YDOT = 648
290401 feet/sec YDOT = 197
598914 meter/sec
ZDOT = 3051
796908 ZDOT = 930
187697
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
59017690
00016717 00000-0 10270-3 0 9064
2 25544 51
6425 100
9165 0001221 222
8987 137
2070 15
54501777 3646
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
59017690 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 100
9165 deg
Eccentricity:
0001221
Arg of perigee: 222
8987 deg
Mean anomaly: 137
2070 deg
Mean motion: 15
54501777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 364
Checksum: 294
Coasting Arc #8 (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 = -3735299
99 A = 6777049
47 meter
Y = -2354893
04 meter E =
0003433
Z = 5138791
30 I = 51
99143
XDOT = 2252
484507 Wp = 63
17216
YDOT = -7148
124526 meter/sec RA = 97
66750 deg
ZDOT = -1636
046330 TA = 42
54585
MA = 42
51926
Ha = 220
206 n
mi
Hp = 214
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12254921
24 X = -3733651
30
Y = -7726027
05 feet Y = -2396655
02 meter
Z = 16859551
52 Z = 5120649
96
XDOT = 7390
041033 XDOT = 2340
196392
YDOT = -23451
852119 feet/sec YDOT = -7122
445131 meter/sec
ZDOT = -5367
606071 ZDOT = -1624
892145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5870119
20 X = 1789212
33
Y = -13343948
90 feet Y = -4067235
62 meter
Z = 16780935
45 Z = 5114829
12
XDOT = 23302
058669 XDOT = 7102
467482
YDOT = 3553
738232 feet/sec YDOT = 1083
179413 meter/sec
ZDOT = -5317
648646 ZDOT = -1620
819307
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
10446878
00016717 00000-0 10270-3 0 9077
2 25544 51
6432 98
3481 0001659 217
9223 142
1813 15
54529050 3721
Satellite: ISS
Catalog Number: 25544
Epoch time: 16161
10446878 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 98
3481 deg
Eccentricity:
0001659
Arg of perigee: 217
9223 deg
Mean anomaly: 142
1813 deg
Mean motion: 15
54529050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 372
Checksum: 302
Coasting Arc #9 (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 = 3208222
25 A = 6780211
03 meter
Y = 4103042
52 meter E =
0008195
Z = -4349571
81 I = 52
00538
XDOT = -3033
802771 Wp = 121
22338
YDOT = 6095
090855 meter/sec RA = 92
69506 deg
ZDOT = 3512
653360 TA = 184
35077
MA = 184
35790
Ha = 220
042 n
mi
Hp = 214
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10525663
54 X = 3183230
81
Y = 13461425
58 feet Y = 4138779
68 meter
Z = -14270248
70 Z = -4334047
44
XDOT = -9953
421165 XDOT = -3118
797006
YDOT = 19997
017241 feet/sec YDOT = 6060
689283 meter/sec
ZDOT = 11524
453281 ZDOT = 3497
710117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11581236
93 X = -3529961
02
Y = 12640365
48 feet Y = 3852783
40 meter
Z = -14203368
67 Z = -4329186
77
XDOT = -20426
636495 XDOT = -6226
038804
YDOT = -5842
863080 feet/sec YDOT = -1780
904667 meter/sec
ZDOT = 11458
169775 ZDOT = 3492
450147
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
06876522
00016717 00000-0 10270-3 0 9087
2 25544 51
6432 93
5396 0001625 220
2247 139
8786 15
54534330 3874
Satellite: ISS
Catalog Number: 25544
Epoch time: 16162
06876522 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 93
5396 deg
Eccentricity:
0001625
Arg of perigee: 220
2247 deg
Mean anomaly: 139
8786 deg
Mean motion: 15
54534330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 387
Checksum: 315
Coasting Arc #10 (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 = -2575762
13 A = 6784370
07 meter
Y = -5495593
84 meter E =
0012278
Z = 3018132
50 I = 52
01927
XDOT = 3718
888732 Wp = 102
42824
YDOT = -4489
775634 meter/sec RA = 87
73329 deg
ZDOT = -4986
978516 TA = 43
17638
MA = 43
08017
Ha = 220
103 n
mi
Hp = 214
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8450663
15 X = -2528778
32
Y = -18030163
53 feet Y = -5524135
28 meter
Z = 9902009
51 Z = 3005733
80
XDOT = 12201
078518 XDOT = 3793
042645
YDOT = -14730
235019 feet/sec YDOT = -4447
773514 meter/sec
ZDOT = -16361
478072 ZDOT = -4968
733403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16231956
76 X = 4947500
42
Y = -11578887
67 feet Y = -3529244
96 meter
Z = 9849022
14 Z = 3001981
95
XDOT = 15837
612538 XDOT = 4827
304302
YDOT = 8312
776135 feet/sec YDOT = 2533
734166 meter/sec
ZDOT = -16281
099619 ZDOT = -4962
479164
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
09734261
00016717 00000-0 10270-3 0 9095
2 25544 51
6428 88
4097 0001506 224
7475 135
3557 15
54519313 4030
Satellite: ISS
Catalog Number: 25544
Epoch time: 16163
09734261 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 88
4097 deg
Eccentricity:
0001506
Arg of perigee: 224
7475 deg
Mean anomaly: 135
3557 deg
Mean motion: 15
54519313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 403
Checksum: 309
Coasting Arc #11 (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 = 1868073
41 A = 6787523
58 meter
Y = 6381297
85 meter E =
0007350
Z = -1347178
81 I = 52
02694
XDOT = -4287
631189 Wp = 33
87212
YDOT = 2485
665391 meter/sec RA = 82
78217 deg
ZDOT = 5849
827566 TA = 311
53770
MA = 311
60072
Ha = 220
013 n
mi
Hp = 214
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6128849
76 X = 1803121
30
Y = 20936016
57 feet Y = 6401824
82 meter
Z = -4419878
00 Z = -1338261
48
XDOT = -14067
031460 XDOT = -4343
523765
YDOT = 8155
070182 feet/sec YDOT = 2437
405295 meter/sec
ZDOT = 19192
347657 ZDOT = 5828
863777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19339482
70 X = -5894674
33
Y = 10109167
61 feet Y = 3081274
29 meter
Z = -4382242
56 Z = -1335707
53
XDOT = -10022
408805 XDOT = -3054
830204
YDOT = -10924
050858 feet/sec YDOT = -3329
650702 meter/sec
ZDOT = 19100
497671 ZDOT = 5821
831690
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
06162869
00016717 00000-0 10270-3 0 9104
2 25544 51
6424 83
6003 0001526 236
0794 124
0214 15
54487975 4181
Satellite: ISS
Catalog Number: 25544
Epoch time: 16164
06162869 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 83
6003 deg
Eccentricity:
0001526
Arg of perigee: 236
0794 deg
Mean anomaly: 124
0214 deg
Mean motion: 15
54487975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 418
Checksum: 299
Coasting Arc #12 (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 = -1027506
81 A = 6788032
42 meter
Y = -6683997
03 meter E =
0010917
Z = -517374
94 I = 52
02411
XDOT = 4747
239063 Wp = 146
48416
YDOT = -269
330842 meter/sec RA = 77
83672 deg
ZDOT = -6017
636808 TA = 39
06923
MA = 38
99043
Ha = 219
947 n
mi
Hp = 214
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3371085
32 X = -950175
12
Y = -21929124
12 feet Y = -6695054
87 meter
Z = -1697424
34 Z = -522178
98
XDOT = 15574
931308 XDOT = 4779
129093
YDOT = -883
631371 feet/sec YDOT = -216
065304 meter/sec
ZDOT = -19742
902913 ZDOT = -5994
498434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20724806
91 X = 6316921
14
Y = -7916187
67 feet Y = -2412854
00 meter
Z = -1717062
00 Z = -523360
50
XDOT = 3604
807996 XDOT = 1098
745477
YDOT = 13649
317611 feet/sec YDOT = 4160
312008 meter/sec
ZDOT = -19642
001189 ZDOT = -5986
881962
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
09019512
00016717 00000-0 10270-3 0 9115
2 25544 51
6423 78
4701 0001516 235
0560 125
0450 15
54534598 4341
Satellite: ISS
Catalog Number: 25544
Epoch time: 16165
09019512 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 78
4701 deg
Eccentricity:
0001516
Arg of perigee: 235
0560 deg
Mean anomaly: 125
0450 deg
Mean motion: 15
54534598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 434
Checksum: 280
Coasting Arc #13 (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 = 90447
27 A = 6785899
17 meter
Y = 6380101
39 meter E =
0012468
Z = 2292975
36 I = 52
00967
XDOT = -5044
465393 Wp = 73
45500
YDOT = -1897
625501 meter/sec RA = 72
88796 deg
ZDOT = 5458
025636 TA = 311
95588
MA = 312
06206
Ha = 219
929 n
mi
Hp = 214
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 296743
00 X = 7958
32
Y = 20932091
17 feet Y = 6380651
43 meter
Z = 7522885
04 Z = 2293214
87
XDOT = -16550
083309 XDOT = -5049
383598
YDOT = -6225
805449 feet/sec YDOT = -1954
063997 meter/sec
ZDOT = 17906
908255 ZDOT = 5433
508688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20324838
81 X = -6195010
87
Y = 5014437
84 feet Y = 1528400
65 meter
Z = 7522674
88 Z = 2292911
30
XDOT = 2626
139821 XDOT = 800
447418
YDOT = -16163
240720 feet/sec YDOT = -4926
555772 meter/sec
ZDOT = 17800
423419 ZDOT = 5425
569058
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
11875375
00016717 00000-0 10270-3 0 9127
2 25544 51
6426 73
3395 0001402 241
7112 118
3899 15
54542370 4505
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
11875375 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 73
3395 deg
Eccentricity:
0001402
Arg of perigee: 241
7112 deg
Mean anomaly: 118
3899 deg
Mean motion: 15
54542370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 450
Checksum: 296
Coasting Arc #14 (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 = 3706451
71 A = 6785931
37 meter
Y = 5209791
11 meter E =
0004976
Z = -2268726
13 I = 52
00613
XDOT = -2956
627873 Wp = 36
16916
YDOT = 4481
855887 meter/sec RA = 70
66167 deg
ZDOT = 5471
627677 TA = 298
72231
MA = 298
77231
Ha = 219
914 n
mi
Hp = 214
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12160274
63 X = 3658939
60
Y = 17092490
52 feet Y = 5250973
65 meter
Z = -7443327
21 Z = -2250836
00
XDOT = -9700
222682 XDOT = -3033
104313
YDOT = 14704
251599 feet/sec YDOT = 4448
364856 meter/sec
ZDOT = 17951
534373 ZDOT = 5457
079654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18562396
36 X = 5657818
41
Y = -9828656
88 feet Y = -2995774
62 meter
Z = -7366381
49 Z = -2245273
08
XDOT = 12554
529001 XDOT = 3826
620440
YDOT = 10329
197126 feet/sec YDOT = 3148
339284 meter/sec
ZDOT = 17887
241428 ZDOT = 5452
031187
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
50446308
00016717 00000-0 10270-3 0 9131
2 25544 51
6430 71
4176 0001237 253
6191 106
4826 15
54560475 4561
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
50446308 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 71
4176 deg
Eccentricity:
0001237
Arg of perigee: 253
6191 deg
Mean anomaly: 106
4826 deg
Mean motion: 15
54560475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 456
Checksum: 296
Coasting Arc #15 (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 = -3103123
46 A = 6788071
18 meter
Y = -6012909
97 meter E =
0012191
Z = 454889
46 I = 52
00184
XDOT = 4017
241631 Wp = 135
47274
YDOT = -2535
502826 meter/sec RA = 65
71337 deg
ZDOT = -6021
973678 TA = 39
64441
MA = 39
55534
Ha = 219
902 n
mi
Hp = 214
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10180851
23 X = -3037864
63
Y = -19727394
90 feet Y = -6047246
32 meter
Z = 1492419
49 Z = 439973
11
XDOT = 13179
926611 XDOT = 4074
548045
YDOT = -8318
578825 feet/sec YDOT = -2490
258383 meter/sec
ZDOT = -19757
131489 ZDOT = -6002
319826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20774642
48 X = -6332111
03
Y = 7837121
31 feet Y = 2388754
57 meter
Z = 1428606
66 Z = 435439
31
XDOT = -6151
893164 XDOT = -1875
097036
YDOT = -12666
158626 feet/sec YDOT = -3860
645149 meter/sec
ZDOT = -19670
964019 ZDOT = -5995
709833
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
53301433
00016717 00000-0 10270-3 0 9145
2 25544 51
6434 66
2880 0001355 252
7568 107
3437 15
54534189 4727
Satellite: ISS
Catalog Number: 25544
Epoch time: 16167
53301433 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 66
2880 deg
Eccentricity:
0001355
Arg of perigee: 252
7568 deg
Mean anomaly: 107
3437 deg
Mean motion: 15
54534189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 306
Coasting Arc #16 (Orbit 487)
---------------------------------------
Vector Time (GMT): 2016/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908273
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2251033
23 A = 6787238
44 meter
Y = 6243879
20 meter E =
0012661
Z = 1388294
03 I = 51
98625
XDOT = -4956
282700 Wp = 57
53616
YDOT = 482
465246 meter/sec RA = 60
76473 deg
ZDOT = 5834
408436 TA = 317
52575
MA = 317
62365
Ha = 219
828 n
mi
Hp = 214
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7385279
61 X = 2174301
51
Y = 20485167
97 feet Y = 6268622
57 meter
Z = 4554770
45 Z = 1399043
36
XDOT = -16260
770012 XDOT = -4989
650648
YDOT = 1582
891227 feet/sec YDOT = 426
853607 meter/sec
ZDOT = 19141
759959 ZDOT = 5810
250865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21111617
17 X = 6434820
91
Y = -5297800
46 feet Y = -1614769
58 meter
Z = 4600361
57 Z = 1402190
21
XDOT = -426
548500 XDOT = -130
011983
YDOT = 14920
774122 feet/sec YDOT = 4547
851953 meter/sec
ZDOT = 19036
372117 ZDOT = 5802
286221
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 16168
56155696
00016717 00000-0 10270-3 0 9158
2 25544 51
6443 61
1571 0001352 268
3966 91
7032 15
54562117 4886
Satellite: ISS
Catalog Number: 25544
Epoch time: 16168
56155696 = yrday
fracday
Element set: 915
Inclination: 51
6443 deg
RA of node: 61
1571 deg
Eccentricity:
0001352
Arg of perigee: 268
3966 deg
Mean anomaly: 91
7032 deg
Mean motion: 15
54562117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 488
Checksum: 318
Coasting Arc #17 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2016/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908273
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1107859
56 A = 6783995
64 meter
Y = -5936334
82 meter E =
0003148
Z = -3092136
64 I = 51
95886
XDOT = 5678
408591 Wp = 113
11696
YDOT = 1502
448228 meter/sec RA = 55
81042 deg
ZDOT = -4924
075596 TA = 102
24242
MA = 102
20716
Ha = 219
779 n
mi
Hp = 214
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3634709
86 X = -1026375
26
Y = -19476164
12 feet Y = -5948267
67 meter
Z = -10144805
25 Z = -3097321
18
XDOT = 18629
949447 XDOT = 5685
105023
YDOT = 4929
292085 feet/sec YDOT = 1565
986009 meter/sec
ZDOT = -16155
103661 ZDOT = -4896
474648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19703366
74 X = -6005586
18
Y = 1968512
47 feet Y = 600002
60 meter
Z = -10166191
81 Z = -3098655
26
XDOT = 6583
076323 XDOT = 2006
521663
YDOT = -16832
525179 feet/sec YDOT = -5130
553675 meter/sec
ZDOT = -16035
111654 ZDOT = -4887
502032
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 16169
52580945
00016717 00000-0 10270-3 0 9165
2 25544 51
6442 56
3483 0001462 268
4434 91
6551 15
54561981 5037
Satellite: ISS
Catalog Number: 25544
Epoch time: 16169
52580945 = yrday
fracday
Element set: 916
Inclination: 51
6442 deg
RA of node: 56
3483 deg
Eccentricity:
0001462
Arg of perigee: 268
4434 deg
Mean anomaly: 91
6551 deg
Mean motion: 15
54561981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 316
Coasting Arc #18 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2016/170/05:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 893042
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 447406
56 A = 6781498
84 meter
Y = 5534074
00 meter E =
0009862
Z = 3887001
61 I = 51
93338
XDOT = -5988
818157 Wp = 100
41650
YDOT = -2426
952355 meter/sec RA = 52
12857 deg
ZDOT = 4134
058351 TA = 306
34099
MA = 306
43199
Ha = 219
737 n
mi
Hp = 214
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1467869
31 X = 366608
41
Y = 18156410
77 feet Y = 5538624
92 meter
Z = 12752629
96 Z = 3888979
49
XDOT = -19648
353533 XDOT = -5981
315868
YDOT = -7962
442108 feet/sec YDOT = -2493
881902 meter/sec
ZDOT = 13563
183565 ZDOT = 4104
983877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -860865
34 X = -262391
75
Y = 18190048
40 feet Y = 5544326
75 meter
Z = 12760114
15 Z = 3889282
79
XDOT = -17278
422074 XDOT = -5266
463048
YDOT = -10268
025231 feet/sec YDOT = -3129
694090 meter/sec
ZDOT = 13436
961118 ZDOT = 4095
585749
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 16170
29720716
00016717 00000-0 10270-3 0 9174
2 25544 51
6403 52
4997 0001393 266
6121 93
4873 15
54613387 5155
Satellite: ISS
Catalog Number: 25544
Epoch time: 16170
29720716 = yrday
fracday
Element set: 917
Inclination: 51
6403 deg
RA of node: 52
4997 deg
Eccentricity:
0001393
Arg of perigee: 266
6121 deg
Mean anomaly: 93
4873 deg
Mean motion: 15
54613387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 313
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