[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 2nd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
069/22:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
4
072/21:25:56
618 -0
5 0
7 0
7
N/A 0
4 -0
1 220
9
000/00:01:53
236 0
2 0
0 215
0
073/06:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
0
Coasting Arc #1 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2018/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4579237
31 A = 6784102
14 meter
Y = 3578103
16 meter E =
0006912
Z = -3503401
39 I = 51
57525
XDOT = -5565
714167 Wp = 110
94530
YDOT = 2708
630352 meter/sec RA = 189
43281 deg
ZDOT = -4518
092233 TA = 110
27960
MA = 110
20529
Ha = 221
709 n
mi
Hp = 214
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15023744
47 X = 4555902
99
Y = 11739183
58 feet Y = 3629180
40 meter
Z = -11494099
04 Z = -3481214
65
XDOT = -18260
217082 XDOT = -5573
643091
YDOT = 8886
582520 feet/sec YDOT = 2646
345777 meter/sec
ZDOT = -14823
137249 ZDOT = -4545
147601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9991689
96 X = 3045467
10
Y = 16307717
72 feet Y = 4970592
36 meter
Z = -11395618
30 Z = -3473384
46
XDOT = -18939
212187 XDOT = -5772
671875
YDOT = 1183
572635 feet/sec YDOT = 360
752939 meter/sec
ZDOT = -14944
021404 ZDOT = -4554
937724
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 18061
52491256
00016717 00000-0 10270-3 0 9007
2 25544 51
6397 190
4515 0003032 150
9888 209
1434 15
54166934 21926
Satellite: ISS
Catalog Number: 25544
Epoch time: 18061
52491256 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 190
4515 deg
Eccentricity:
0003032
Arg of perigee: 150
9888 deg
Mean anomaly: 209
1434 deg
Mean motion: 15
54166934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 307
Coasting Arc #2 (Orbit 2207)
---------------------------------------
Vector Time (GMT): 2018/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3119720
53 A = 6780265
06 meter
Y = -3890867
68 meter E =
0011015
Z = 4588824
54 I = 51
59597
XDOT = 6797
445334 Wp = 124
59066
YDOT = -1873
987257 meter/sec RA = 184
44158 deg
ZDOT = 3021
012599 TA = 295
18328
MA = 295
29747
Ha = 221
624 n
mi
Hp = 214
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10235303
58 X = -3098269
67
Y = -12765313
92 feet Y = -3925633
94 meter
Z = 15055198
64 Z = 4573722
93
XDOT = 22301
329837 XDOT = 6803
221317
YDOT = -6148
252155 feet/sec YDOT = -1797
940818 meter/sec
ZDOT = 9911
458659 ZDOT = 3054
045999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5438485
55 X = -1657650
40
Y = -15496670
93 feet Y = -4723385
30 meter
Z = 14988320
45 Z = 4568440
07
XDOT = 21877
527509 XDOT = 6668
270385
YDOT = 2087
093423 feet/sec YDOT = 636
146075 meter/sec
ZDOT = 10058
904496 ZDOT = 3065
954090
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 18062
55371499
00016717 00000-0 10270-3 0 9018
2 25544 51
6403 185
3230 0002993 156
0697 204
0595 15
54198844 22086
Satellite: ISS
Catalog Number: 25544
Epoch time: 18062
55371499 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 185
3230 deg
Eccentricity:
0002993
Arg of perigee: 156
0697 deg
Mean anomaly: 204
0595 deg
Mean motion: 15
54198844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2208
Checksum: 318
Coasting Arc #3 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2018/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1373144
65 A = 6777699
32 meter
Y = 4118920
47 meter E =
0014987
Z = -5217306
02 I = 51
62110
XDOT = -7498
533486 Wp = 91
94120
YDOT = 1008
211174 meter/sec RA = 179
44367 deg
ZDOT = -1181
018251 TA = 166
73224
MA = 166
69278
Ha = 221
517 n
mi
Hp = 214
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4505067
76 X = 1352326
35
Y = 13513518
60 feet Y = 4134158
76 meter
Z = -17117145
74 Z = -5210687
00
XDOT = -24601
487815 XDOT = -7503
513575
YDOT = 3307
779442 feet/sec YDOT = 924
329401 meter/sec
ZDOT = -3874
731794 ZDOT = -1217
455343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 49120
63 X = 14971
97
Y = 14279425
74 feet Y = 4352368
97 meter
Z = -17088097
80 Z = -5208452
21
XDOT = -23299
568112 XDOT = -7101
708361
YDOT = -4737
726193 feet/sec YDOT = -1444
058944 meter/sec
ZDOT = -4037
267225 ZDOT = -1230
559050
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 18063
51821561
00016717 00000-0 10270-3 0 9026
2 25544 51
6413 180
5155 0002897 158
1595 201
9682 15
54182620 22238
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
51821561 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 180
5155 deg
Eccentricity:
0002897
Arg of perigee: 158
1595 deg
Mean anomaly: 201
9682 deg
Mean motion: 15
54182620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2223
Checksum: 298
Coasting Arc #4 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2018/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 463053
56 A = 6777273
35 meter
Y = -4233048
49 meter E =
0003899
Z = 5269077
53 I = 51
65284
XDOT = 7631
792125 Wp = 108
49567
YDOT = -127
470110 meter/sec RA = 174
44288 deg
ZDOT = -773
839280 TA = 348
88939
MA = 348
89799
Ha = 221
422 n
mi
Hp = 214
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1519204
61 X = 484760
05
Y = -13887954
37 feet Y = -4227748
24 meter
Z = 17286999
78 Z = 5271380
15
XDOT = 25038
688073 XDOT = 7636
409196
YDOT = -418
209023 feet/sec YDOT = -42
100451 meter/sec
ZDOT = -2538
842783 ZDOT = -736
755754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5557363
21 X = 1693884
31
Y = -12803424
13 feet Y = -3902483
67 meter
Z = 17297735
84 Z = 5272349
88
XDOT = 23064
200406 XDOT = 7029
968284
YDOT = 6807
698809 feet/sec YDOT = 2074
986597 meter/sec
ZDOT = -2373
507177 ZDOT = -723
444988
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 18064
54701088
00016717 00000-0 10270-3 0 9032
2 25544 51
6411 175
3862 0002797 160
0515 200
0748 15
54212080 22390
Satellite: ISS
Catalog Number: 25544
Epoch time: 18064
54701088 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 175
3862 deg
Eccentricity:
0002797
Arg of perigee: 160
0515 deg
Mean anomaly: 200
0748 deg
Mean motion: 15
54212080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 286
Coasting Arc #5 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2018/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2252578
01 A = 6779355
50 meter
Y = 4260895
33 meter E =
0013224
Z = -4780356
34 I = 51
69214
XDOT = -7139
725577 Wp = 119
06663
YDOT = -799
997194 meter/sec RA = 169
44863 deg
ZDOT = 2650
558795 TA = 177
11130
MA = 177
10365
Ha = 221
395 n
mi
Hp = 214
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7390347
82 X = -2276836
78
Y = 13979315
38 feet Y = 4235569
26 meter
Z = -15683583
79 Z = -4791357
93
XDOT = -23424
296512 XDOT = -7143
124094
YDOT = -2624
662711 feet/sec YDOT = -879
857208 meter/sec
ZDOT = 8696
059039 ZDOT = 2615
868539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10996115
32 X = -3351615
95
Y = 11294598
54 feet Y = 3442593
64 meter
Z = -15733111
31 Z = -4795452
33
XDOT = -20913
136109 XDOT = -6374
323886
YDOT = -8459
075631 feet/sec YDOT = -2578
326252 meter/sec
ZDOT = 8541
479819 ZDOT = 2603
443049
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 18065
51150455
00016717 00000-0 10270-3 0 9047
2 25544 51
6408 170
5794 0002877 163
0822 197
0427 15
54213647 22546
Satellite: ISS
Catalog Number: 25544
Epoch time: 18065
51150455 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 170
5794 deg
Eccentricity:
0002877
Arg of perigee: 163
0822 deg
Mean anomaly: 197
0427 deg
Mean motion: 15
54213647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 307
Coasting Arc #6 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2018/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3827233
00 A = 6783081
71 meter
Y = -4140911
79 meter E =
0012214
Z = 3758565
43 I = 51
73654
XDOT = 6126
391500 Wp = 97
01005
YDOT = 1785
117328 meter/sec RA = 164
46321 deg
ZDOT = -4261
202825 TA = 38
04745
MA = 37
96125
Ha = 221
334 n
mi
Hp = 214
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12556538
71 X = 3854996
32
Y = -13585668
60 feet Y = -4097957
43 meter
Z = 12331251
40 Z = 3777224
53
XDOT = 20099
709647 XDOT = 6126
673071
YDOT = 5856
684148 feet/sec YDOT = 1853
628001 meter/sec
ZDOT = -13980
324228 ZDOT = -4231
442605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15687942
56 X = 4781684
89
Y = -9698197
64 feet Y = -2956010
64 meter
Z = 12414919
97 Z = 3784067
61
XDOT = 17143
689551 XDOT = 5225
396575
YDOT = 9961
510349 feet/sec YDOT = 3036
268354 meter/sec
ZDOT = -13847
821941 ZDOT = -4220
816128
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 18066
54029380
00016717 00000-0 10270-3 0 9054
2 25544 51
6408 165
4501 0002864 165
8905 194
2328 15
54186198 22700
Satellite: ISS
Catalog Number: 25544
Epoch time: 18066
54029380 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 165
4501 deg
Eccentricity:
0002864
Arg of perigee: 165
8905 deg
Mean anomaly: 194
2328 deg
Mean motion: 15
54186198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 318
Coasting Arc #7 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2018/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5051124
44 A = 6786749
95 meter
Y = 3872065
58 meter E =
0004644
Z = -2358096
42 I = 51
78041
XDOT = -4661
153266 Wp = 73
73297
YDOT = -2797
409742 meter/sec RA = 159
49087 deg
ZDOT = 5401
009626 TA = 260
02143
MA = 260
07384
Ha = 221
246 n
mi
Hp = 214
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16571930
59 X = -5082593
21
Y = 12703627
23 feet Y = 3815404
28 meter
Z = -7736536
83 Z = -2382709
64
XDOT = -15292
497593 XDOT = -4655
760534
YDOT = -9177
853485 feet/sec YDOT = -2849
503343 meter/sec
ZDOT = 17719
847854 ZDOT = 5378
380849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19207322
48 X = -5854391
89
Y = 8085322
01 feet Y = 2464406
15 meter
Z = -7846742
10 Z = -2391686
99
XDOT = -11980
102278 XDOT = -3651
535174
YDOT = -11392
008783 feet/sec YDOT = -3472
284277 meter/sec
ZDOT = 17619
249227 ZDOT = 5370
347164
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 18067
50477763
00016717 00000-0 10270-3 0 9064
2 25544 51
6411 160
6419 0002549 171
3085 188
8112 15
54180171 22851
Satellite: ISS
Catalog Number: 25544
Epoch time: 18067
50477763 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 160
6419 deg
Eccentricity:
0002549
Arg of perigee: 171
3085 deg
Mean anomaly: 188
8112 deg
Mean motion: 15
54180171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 309
Coasting Arc #8 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2018/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5846044
75 A = 6788914
89 meter
Y = -3369184
92 meter E =
0015280
Z = 670955
43 I = 51
81712
XDOT = 2901
309970 Wp = 135
12328
YDOT = 3828
608092 meter/sec RA = 154
52960 deg
ZDOT = -5981
635345 TA = 37
64485
MA = 37
53801
Ha = 221
255 n
mi
Hp = 214
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19179936
83 X = 5880026
28
Y = -11053756
30 feet Y = -3303620
38 meter
Z = 2201297
36 Z = 699436
06
XDOT = 9518
733496 XDOT = 2887
337199
YDOT = 12561
050172 feet/sec YDOT = 3860
973936 meter/sec
ZDOT = -19624
787878 ZDOT = -5967
576143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21242313
02 X = 6474657
01
Y = -6184048
18 feet Y = -1884897
88 meter
Z = 2328712
29 Z = 709791
51
XDOT = 5937
098867 XDOT = 1809
627735
YDOT = 12943
027908 feet/sec YDOT = 3945
034906 meter/sec
ZDOT = -19562
519007 ZDOT = -5962
655793
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 18068
53355879
00016717 00000-0 10270-3 0 9072
2 25544 51
6401 155
5134 0002728 172
8094 187
3098 15
54198897 23012
Satellite: ISS
Catalog Number: 25544
Epoch time: 18068
53355879 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 155
5134 deg
Eccentricity:
0002728
Arg of perigee: 172
8094 deg
Mean anomaly: 187
3098 deg
Mean motion: 15
54198897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 338
Coasting Arc #9 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2018/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6153939
06 A = 6788673
13 meter
Y = 2652174
30 meter E =
0012443
Z = 1056220
30 I = 51
84605
XDOT = -1035
388978 Wp = 66
64343
YDOT = -4775
806064 meter/sec RA = 149
57221 deg
ZDOT = 5909
205784 TA = 304
77647
MA = 304
89353
Ha = 221
156 n
mi
Hp = 214
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20190088
77 X = -6188269
53
Y = 8701359
26 feet Y = 2583164
85 meter
Z = 3465289
70 Z = 1026243
32
XDOT = -3396
945467 XDOT = -1010
611182
YDOT = -15668
655065 feet/sec YDOT = -4787
245501 meter/sec
ZDOT = 19387
158084 ZDOT = 5904
236821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21635091
64 X = -6594375
93
Y = 4023315
32 feet Y = 1226306
51 meter
Z = 3331263
04 Z = 1015368
97
XDOT = 315
302487 XDOT = 96
104198
YDOT = -14481
084269 feet/sec YDOT = -4413
834485 meter/sec
ZDOT = 19365
543520 ZDOT = 5902
617665
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 18069
56233547
00016717 00000-0 10270-3 0 9084
2 25544 51
6406 150
3843 0002573 177
1415 182
9753 15
54204526 23173
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
56233547 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 150
3843 deg
Eccentricity:
0002573
Arg of perigee: 177
1415 deg
Mean anomaly: 182
9753 deg
Mean motion: 15
54204526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 311
Coasting Arc #10 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2018/069/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 29884
85 A = 6778607
98 meter
Y = 4621419
63 meter E =
0013380
Z = -4971309
68 I = 51
82460
XDOT = -6936
364057 Wp = 114
87576
YDOT = 2398
099157 meter/sec RA = 147
38030 deg
ZDOT = 2186
745969 TA = 176
42812
MA = 176
41855
Ha = 221
062 n
mi
Hp = 214
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 98047
42 X = 2352
40
Y = 15162137
91 feet Y = 4621599
50 meter
Z = -16310071
14 Z = -4971231
74
XDOT = -22757
099923 XDOT = -6973
286672
YDOT = 7867
779386 feet/sec YDOT = 2320
325688 meter/sec
ZDOT = 7174
363414 ZDOT = 2152
962033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8626297
75 X = 2629295
55
Y = -12469198
67 feet Y = -3800611
75 meter
Z = -16310258
47 Z = -4971366
78
XDOT = 22230
533497 XDOT = 6775
866610
YDOT = 6188
644703 feet/sec YDOT = 1886
298906 meter/sec
ZDOT = 7023
374734 ZDOT = 2140
724619
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 18069
94812655
00016717 00000-0 10270-3 0 9090
2 25544 51
6402 148
4626 0002159 175
8754 184
2417 15
54220582 23236
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
94812655 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 148
4626 deg
Eccentricity:
0002159
Arg of perigee: 175
8754 deg
Mean anomaly: 184
2417 deg
Mean motion: 15
54220582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 320
Coasting Arc #11 (Orbit 2338)
---------------------------------------
Vector Time (GMT): 2018/070/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1520885
15 A = 6782018
28 meter
Y = -5202166
47 meter E =
0010456
Z = 4067867
21 I = 51
86321
XDOT = 6508
496355 Wp = 89
24777
YDOT = -1150
792960 meter/sec RA = 142
40226 deg
ZDOT = -3896
304500 TA = 41
00629
MA = 40
92772
Ha = 221
043 n
mi
Hp = 214
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4989780
68 X = 1559184
86
Y = -17067475
28 feet Y = -5184944
41 meter
Z = 13346021
02 Z = 4075348
49
XDOT = 21353
334499 XDOT = 6539
807060
YDOT = -3775
567453 feet/sec YDOT = -1077
835727 meter/sec
ZDOT = -12783
151247 ZDOT = -3864
612758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13699650
66 X = -4175653
52
Y = 11296367
17 feet Y = 3443132
71 meter
Z = 13380006
03 Z = 4078225
84
XDOT = -18987
433356 XDOT = -5787
369687
YDOT = -8019
619959 feet/sec YDOT = -2444
380164 meter/sec
ZDOT = -12641
621898 ZDOT = -3853
166355
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 18070
97689797
00016717 00000-0 10270-3 0 9106
2 25544 51
6403 143
3343 0002140 177
3659 182
7505 15
54213975 23394
Satellite: ISS
Catalog Number: 25544
Epoch time: 18070
97689797 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 143
3343 deg
Eccentricity:
0002140
Arg of perigee: 177
3659 deg
Mean anomaly: 182
7505 deg
Mean motion: 15
54213975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2339
Checksum: 324
Coasting Arc #12 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2018/071/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2828799
18 A = 6785765
20 meter
Y = 5523459
17 meter E =
0004000
Z = -2748113
13 I = 51
90183
XDOT = -5645
123889 Wp = 85
18155
YDOT = -321
249486 meter/sec RA = 137
43542 deg
ZDOT = 5171
981445 TA = 243
85250
MA = 243
89365
Ha = 220
942 n
mi
Hp = 214
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9280837
21 X = -2877005
07
Y = 18121585
20 feet Y = 5491555
81 meter
Z = -9016119
19 Z = -2761971
84
XDOT = -18520
747667 XDOT = -5666
234429
YDOT = -1053
968130 feet/sec YDOT = -384
494711 meter/sec
ZDOT = 16968
443061 ZDOT = 5144
508551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17687779
83 X = 5391235
29
Y = -10026841
12 feet Y = -3056181
17 meter
Z = -9078606
55 Z = -2767159
27
XDOT = 14228
611678 XDOT = 4336
880840
YDOT = 9867
149249 feet/sec YDOT = 3007
507091 meter/sec
ZDOT = 16845
894402 ZDOT = 5134
628614
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 18071
94136821
00016717 00000-0 10270-3 0 9110
2 25544 51
6407 138
5257 0002123 182
4643 177
6500 15
54236916 23544
Satellite: ISS
Catalog Number: 25544
Epoch time: 18071
94136821 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 138
5257 deg
Eccentricity:
0002123
Arg of perigee: 182
4643 deg
Mean anomaly: 177
6500 deg
Mean motion: 15
54236916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2354
Checksum: 298
Coasting Arc #13 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2018/072/21:26:53
236
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1099878
20 A = 6779127
88 meter
Y = 4521803
04 meter E =
0012128
Z = -4940791
46 I = 51
90068
XDOT = -6122
410658 Wp = 116
25006
YDOT = 3991
466618 meter/sec RA = 132
68131 deg
ZDOT = 2289
188260 TA = 176
07745
MA = 176
06794
Ha = 220
874 n
mi
Hp = 215
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3608524
29 X = 1073231
82
Y = 14835311
81 feet Y = 4533953
14 meter
Z = -16209945
74 Z = -4935513
90
XDOT = -20086
649141 XDOT = -6177
708795
YDOT = 13095
362920 feet/sec YDOT = 3922
692658 meter/sec
ZDOT = 7510
460172 ZDOT = 2259
313453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8469174
24 X = 2581404
31
Y = -12732897
48 feet Y = -3880987
15 meter
Z = -16186929
12 Z = -4933776
00
XDOT = 22310
260957 XDOT = 6800
167540
YDOT = 5458
093784 feet/sec YDOT = 1663
626985 meter/sec
ZDOT = 7376
671573 ZDOT = 2248
409495
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 18072
90583641
00016717 00000-0 10270-3 0 9124
2 25544 51
6406 133
7167 0002026 204
4848 155
6208 15
54095409 23691
Satellite: ISS
Catalog Number: 25544
Epoch time: 18072
90583641 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 133
7167 deg
Eccentricity:
0002026
Arg of perigee: 204
4848 deg
Mean anomaly: 155
6208 deg
Mean motion: 15
54095409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 309
Coasting Arc #14 (Orbit 2374)
---------------------------------------
Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -592805
34 A = 6782732
24 meter
Y = 5466430
80 meter E =
0007100
Z = -3979620
23 I = 51
92069
XDOT = -6112
215761 Wp = 128
06319
YDOT = 2265
987825 meter/sec RA = 130
73638 deg
ZDOT = 4023
665883 TA = 183
79077
MA = 183
79615
Ha = 220
934 n
mi
Hp = 215
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1944899
42 X = -634557
80
Y = 17934484
27 feet Y = 5459567
76 meter
Z = -13056496
81 Z = -3982601
83
XDOT = -20053
201314 XDOT = -6156
644932
YDOT = 7434
343257 feet/sec YDOT = 2197
388845 meter/sec
ZDOT = 13201
003552 ZDOT = 3993
867162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18003629
52 X = -5487506
28
Y = -965976
66 feet Y = -294429
69 meter
Z = -13070450
72 Z = -3983873
38
XDOT = -8496
576962 XDOT = -2589
756658
YDOT = -18433
062732 feet/sec YDOT = -5618
397521 meter/sec
ZDOT = 13067
752972 ZDOT = 3983
051106
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 18073
29165686
00016717 00000-0 10270-3 0 9133
2 25544 51
6399 131
7893 0002488 201
7587 158
3461 15
54086141 23759
Satellite: ISS
Catalog Number: 25544
Epoch time: 18073
29165686 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 131
7893 deg
Eccentricity:
0002488
Arg of perigee: 201
7587 deg
Mean anomaly: 158
3461 deg
Mean motion: 15
54086141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2375
Checksum: 336
Coasting Arc #15 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1770451
73 A = 6786480
26 meter
Y = -5988647
59 meter E =
0013344
Z = 2638158
88 I = 51
95373
XDOT = 5552
947622 Wp = 113
27773
YDOT = -678
192387 meter/sec RA = 125
77504 deg
ZDOT = -5250
196522 TA = 37
10838
MA = 37
01620
Ha = 220
926 n
mi
Hp = 215
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5808568
67 X = 1824472
23
Y = -19647793
93 feet Y = -5968546
81 meter
Z = 8655376
90 Z = 2646890
94
XDOT = 18218
332093 XDOT = 5585
620971
YDOT = -2225
040639 feet/sec YDOT = -615
913471 meter/sec
ZDOT = -17225
054207 ZDOT = -5223
143181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19987520
78 X = 6092196
33
Y = 4425574
24 feet Y = 1348915
03 meter
Z = 8695063
62 Z = 2650255
39
XDOT = 3769
082825 XDOT = 1148
816445
YDOT = 16684
391329 feet/sec YDOT = 5085
402477 meter/sec
ZDOT = -17104
233337 ZDOT = -5213
370321
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 18074
32051061
00016717 00000-0 10270-3 0 9140
2 25544 51
6398 126
6605 0002497 202
9406 157
1636 15
54084351 23915
Satellite: ISS
Catalog Number: 25544
Epoch time: 18074
32051061 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 126
6605 deg
Eccentricity:
0002497
Arg of perigee: 202
9406 deg
Mean anomaly: 157
1636 deg
Mean motion: 15
54084351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 299
Coasting Arc #16 (Orbit 2405)
---------------------------------------
Vector Time (GMT): 2018/075/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2704805
64 A = 6788934
14 meter
Y = 6134525
66 meter E =
0007221
Z = -1049613
69 I = 51
98047
XDOT = -4745
123120 Wp = 42
23528
YDOT = -1083
830130 meter/sec RA = 120
82414 deg
ZDOT = 5922
232079 TA = 306
44200
MA = 306
50854
Ha = 220
823 n
mi
Hp = 215
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8874034
27 X = -2768104
14
Y = 20126396
52 feet Y = 6103924
59 meter
Z = -3443614
46 Z = -1062907
11
XDOT = -15567
989238 XDOT = -4761
417507
YDOT = -3555
873129 feet/sec YDOT = -1136
983659 meter/sec
ZDOT = 19429
895272 ZDOT = 5899
142773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20798312
70 X = -6339325
71
Y = -7129738
57 feet Y = -2173144
32 meter
Z = -3503686
39 Z = -1067923
61
XDOT = 1703
833986 XDOT = 519
328599
YDOT = -14422
325005 feet/sec YDOT = -4395
924661 meter/sec
ZDOT = 19326
971160 ZDOT = 5890
860810
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 18075
28505849
00016717 00000-0 10270-3 0 9155
2 25544 51
6399 121
8530 0002393 207
4119 152
6908 15
54096497 24069
Satellite: ISS
Catalog Number: 25544
Epoch time: 18075
28505849 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 121
8530 deg
Eccentricity:
0002393
Arg of perigee: 207
4119 deg
Mean anomaly: 152
6908 deg
Mean motion: 15
54096497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2406
Checksum: 328
Coasting Arc #17 (Orbit 2421)
---------------------------------------
Vector Time (GMT): 2018/076/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3413102
29 A = 6789188
98 meter
Y = -5822156
06 meter E =
0011624
Z = -677965
41 I = 51
99740
XDOT = 3792
302331 Wp = 151
27253
YDOT = 2915
157767 meter/sec RA = 115
87803 deg
ZDOT = -5995
160388 TA = 36
01493
MA = 35
93666
Ha = 220
767 n
mi
Hp = 215
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11197842
15 X = 3481246
72
Y = -19101561
89 feet Y = -5783607
48 meter
Z = -2224295
97 Z = -661219
54
XDOT = 12441
936781 XDOT = 3788
543474
YDOT = 9564
165902 feet/sec YDOT = 2957
544020 meter/sec
ZDOT = -19669
161377 ZDOT = -5976
748411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20137453
35 X = 6137895
78
Y = 9223572
12 feet Y = 2811344
78 meter
Z = -2148841
07 Z = -654966
76
XDOT = -7570
026150 XDOT = -2307
343970
YDOT = 12005
473809 feet/sec YDOT = 3659
268417 meter/sec
ZDOT = -19587
334380 ZDOT = -5970
219519
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 18076
31390718
00016717 00000-0 10270-3 0 9168
2 25544 51
6399 116
7242 0002439 212
0804 148
0200 15
54114233 24227
Satellite: ISS
Catalog Number: 25544
Epoch time: 18076
31390718 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 116
7242 deg
Eccentricity:
0002439
Arg of perigee: 212
0804 deg
Mean anomaly: 148
0200 deg
Mean motion: 15
54114233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2422
Checksum: 279
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