[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 5th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
249/00:50:06
532 0
3 0
7 0
7
N/A 0
2 -0
1 223
1
000/00:00:13
064 0
5 -0
0 213
7
249/22:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
7
253/11:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
9
253/22:49:12
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 214
0
257/11:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
2
257/13:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 1099)
---------------------------------------
Vector Time (GMT): 2018/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5371262
39 A = 6783142
69 meter
Y = -1223321
15 meter E =
0010748
Z = -3965676
48 I = 51
49887
XDOT = 4099
565445 Wp = 99
03822
YDOT = -5092
853297 meter/sec RA = 337
89584 deg
ZDOT = -3992
497164 TA = 129
25343
MA = 129
15801
Ha = 223
035 n
mi
Hp = 213
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17622251
93 X = -5337920
67
Y = -4013520
82 feet Y = -1283199
96 meter
Z = -13010749
60 Z = -3991686
99
XDOT = 13450
017865 XDOT = 4175
603737
YDOT = -16708
836277 feet/sec YDOT = -5046
584022 meter/sec
ZDOT = -13098
743975 ZDOT = -3972
398304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15698776
54 X = 4784987
09
Y = 8783790
34 feet Y = 2677299
30 meter
Z = -13127267
81 Z = -4001191
23
XDOT = -17049
074256 XDOT = -5196
557833
YDOT = 11083
852487 feet/sec YDOT = 3378
358238 meter/sec
ZDOT = -13007
848241 ZDOT = -3964
792144
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 18248
52349744
00016717 00000-0 10270-3 0 9008
2 25544 51
6418 338
3524 0005561 134
0975 226
0636 15
53924252 11006
Satellite: ISS
Catalog Number: 25544
Epoch time: 18248
52349744 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 338
3524 deg
Eccentricity:
0005561
Arg of perigee: 134
0975 deg
Mean anomaly: 226
0636 deg
Mean motion: 15
53924252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1100
Checksum: 298
Coasting Arc #2 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2018/249/00:50:13
064
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5326088
94 A = 6789116
87 meter
Y = -3884123
15 meter E =
0009367
Z = -1622532
51 I = 51
50249
XDOT = 4024
552091 Wp = 68
38073
YDOT = 3144
890096 meter/sec RA = 335
18781 deg
ZDOT = 5712
426714 TA = 273
83792
MA = 273
94501
Ha = 223
066 n
mi
Hp = 213
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17474045
07 X = 5377007
76
Y = -12743186
19 feet Y = -3824278
46 meter
Z = -5323269
40 Z = -1596536
74
XDOT = 13203
911061 XDOT = 3961
338284
YDOT = 10317
880894 feet/sec YDOT = 3189
542102 meter/sec
ZDOT = 18741
557460 ZDOT = 5731
822781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18203638
42 X = 5548468
99
Y = -11729977
20 feet Y = -3575297
05 meter
Z = -5206095
01 Z = -1586817
76
XDOT = 11617
370858 XDOT = 3540
974638
YDOT = 9717
042999 feet/sec YDOT = 2961
754706 meter/sec
ZDOT = 18828
128389 ZDOT = 5738
813533
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 18249
03797799
00016717 00000-0 10270-3 0 9013
2 25544 51
6429 335
7915 0004833 127
7511 232
4080 15
53832130 11084
Satellite: ISS
Catalog Number: 25544
Epoch time: 18249
03797799 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 335
7915 deg
Eccentricity:
0004833
Arg of perigee: 127
7511 deg
Mean anomaly: 232
4080 deg
Mean motion: 15
53832130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 311
Coasting Arc #3 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2018/249/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3043605
47 A = 6778452
58 meter
Y = 3062480
86 meter E =
0008321
Z = 5220372
19 I = 51
43832
XDOT = -6193
094733 Wp = 126
56078
YDOT = 4414
400171 meter/sec RA = 330
62680 deg
ZDOT = 1015
071561 TA = 313
66410
MA = 313
73305
Ha = 222
857 n
mi
Hp = 213
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9985582
25 X = 2983776
28
Y = 10047509
38 feet Y = 3096182
25 meter
Z = 17127205
34 Z = 5235011
33
XDOT = -20318
552274 XDOT = -6246
928114
YDOT = 14482
940195 feet/sec YDOT = 4344
843735 meter/sec
ZDOT = 3330
287275 ZDOT = 984
857136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3070219
96 X = 935803
04
Y = 13747685
60 feet Y = 4190294
57 meter
Z = 17192450
39 Z = 5240258
88
XDOT = -23919
283359 XDOT = -7290
597568
YDOT = 1322
846166 feet/sec YDOT = 403
203511 meter/sec
ZDOT = 3194
123192 ZDOT = 973
568749
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 18250
00269998
00016717 00000-0 10270-3 0 9028
2 25544 51
6412 330
9847 0004786 130
9899 229
1668 15
53856009 11232
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
00269998 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 330
9847 deg
Eccentricity:
0004786
Arg of perigee: 130
9899 deg
Mean anomaly: 229
1668 deg
Mean motion: 15
53856009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 334
Coasting Arc #4 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2018/250/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1609533
93 A = 6778479
92 meter
Y = -3983769
92 meter E =
0018587
Z = -5258929
15 I = 51
41004
XDOT = 6623
786839 Wp = 105
10046
YDOT = -3749
135594 meter/sec RA = 325
61515 deg
ZDOT = 810
465964 TA = 172
69869
MA = 172
67159
Ha = 222
993 n
mi
Hp = 213
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5280623
12 X = -1539321
96
Y = -13070111
29 feet Y = -4001376
61 meter
Z = -17253704
57 Z = -5266576
80
XDOT = 21731
584116 XDOT = 6661
281663
YDOT = -12300
313627 feet/sec YDOT = -3674
854118 meter/sec
ZDOT = 2659
009069 ZDOT = 842
732860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2283831
84 X = 696111
94
Y = -13868339
61 feet Y = -4227069
91 meter
Z = -17287463
08 Z = -5269218
75
XDOT = 23936
689697 XDOT = 7295
903020
YDOT = 436
692269 feet/sec YDOT = 133
103804 meter/sec
ZDOT = 2804
273337 ZDOT = 854
742513
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 18250
96742245
00016717 00000-0 10270-3 0 9035
2 25544 51
6416 326
1779 0004822 133
2525 226
9031 15
53827481 11387
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
96742245 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 326
1779 deg
Eccentricity:
0004822
Arg of perigee: 133
2525 deg
Mean anomaly: 226
9031 deg
Mean motion: 15
53827481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 306
Coasting Arc #5 (Orbit 1153)
---------------------------------------
Vector Time (GMT): 2018/251/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 186272
91 A = 6780417
91 meter
Y = 4791856
70 meter E =
0009712
Z = 4785135
18 I = 51
38977
XDOT = -6660
331912 Wp = 88
90063
YDOT = 2822
170942 meter/sec RA = 320
60515 deg
ZDOT = -2562
174840 TA = 26
41912
MA = 26
36963
Ha = 222
855 n
mi
Hp = 213
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 611131
61 X = 109431
85
Y = 15721314
62 feet Y = 4793510
52 meter
Z = 15699262
40 Z = 4785852
94
XDOT = -21851
482652 XDOT = -6678
949675
YDOT = 9259
091018 feet/sec YDOT = 2747
586159 meter/sec
ZDOT = -8406
085433 ZDOT = -2594
573463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7405383
17 X = -2257160
79
Y = 13878500
65 feet Y = 4230167
00 meter
Z = 15701833
48 Z = 4785918
85
XDOT = -22495
839759 XDOT = -6856
731958
YDOT = -2310
753351 feet/sec YDOT = -704
317621 meter/sec
ZDOT = -8551
798182 ZDOT = -2606
588086
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 18251
99645502
00016717 00000-0 10270-3 0 9048
2 25544 51
6413 321
0516 0004710 137
3003 222
8516 15
53845481 11540
Satellite: ISS
Catalog Number: 25544
Epoch time: 18251
99645502 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 321
0516 deg
Eccentricity:
0004710
Arg of perigee: 137
3003 deg
Mean anomaly: 222
8516 deg
Mean motion: 15
53845481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1154
Checksum: 282
Coasting Arc #6 (Orbit 1168)
---------------------------------------
Vector Time (GMT): 2018/252/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1117905
58 A = 6783763
97 meter
Y = -5449702
10 meter E =
0010648
Z = -3894354
87 I = 51
37673
XDOT = 6286
677252 Wp = 119
70603
YDOT = -1612
138541 meter/sec RA = 315
59885 deg
ZDOT = 4063
861724 TA = 193
06847
MA = 193
09608
Ha = 222
855 n
mi
Hp = 213
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3667669
22 X = 1197679
12
Y = -17879600
07 feet Y = -5436755
30 meter
Z = -12776754
84 Z = -3888730
17
XDOT = 20625
581536 XDOT = 6284
497486
YDOT = -5289
168440 feet/sec YDOT = -1541
848290 meter/sec
ZDOT = 13332
879673 ZDOT = 4094
394809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11937234
89 X = 3638469
19
Y = -13831011
23 feet Y = -4215692
22 meter
Z = -12750800
44 Z = -3886443
97
XDOT = 19522
002189 XDOT = 5950
306267
YDOT = 4440
727003 feet/sec YDOT = 1353
533590 meter/sec
ZDOT = 13470
047563 ZDOT = 4105
670497
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 18252
96116989
00016717 00000-0 10270-3 0 9059
2 25544 51
6420 316
2441 0004733 139
9959 220
1543 15
53844836 11694
Satellite: ISS
Catalog Number: 25544
Epoch time: 18252
96116989 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 316
2441 deg
Eccentricity:
0004733
Arg of perigee: 139
9959 deg
Mean anomaly: 220
1543 deg
Mean motion: 15
53844836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 327
Coasting Arc #7 (Orbit 1176)
---------------------------------------
Vector Time (GMT): 2018/253/11:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2896038
10 A = 6778286
46 meter
Y = -3107156
51 meter E =
0018131
Z = -5297812
20 I = 51
34494
XDOT = 5372
444905 Wp = 104
44071
YDOT = -5446
978754 meter/sec RA = 313
08298 deg
ZDOT = 254
106632 TA = 168
01715
MA = 167
97396
Ha = 222
847 n
mi
Hp = 213
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9501437
34 X = -2835343
98
Y = -10194083
04 feet Y = -3139203
28 meter
Z = -17381273
63 Z = -5311732
27
XDOT = 17626
131578 XDOT = 5431
720935
YDOT = -17870
665202 feet/sec YDOT = -5386
568886 meter/sec
ZDOT = 833
683177 ZDOT = 280
348528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4008318
64 X = 1221735
52
Y = 13265369
74 feet Y = 4043284
70 meter
Z = -17443298
46 Z = -5316717
37
XDOT = -22677
154426 XDOT = -6911
996669
YDOT = 8120
096020 feet/sec YDOT = 2475
005267 meter/sec
ZDOT = 952
103774 ZDOT = 290
201230
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 18253
47568256
00016717 00000-0 10270-3 0 9065
2 25544 51
6406 313
6785 0004866 146
1469 213
9995 15
53820106 11777
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
47568256 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 313
6785 deg
Eccentricity:
0004866
Arg of perigee: 146
1469 deg
Mean anomaly: 213
9995 deg
Mean motion: 15
53820106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1177
Checksum: 336
Coasting Arc #8 (Orbit 1184)
---------------------------------------
Vector Time (GMT): 2018/253/22:49:12
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1273965
86 A = 6785233
25 meter
Y = 5702342
89 meter E =
0015717
Z = 3432577
46 I = 51
35731
XDOT = -6010
145349 Wp = 103
57727
YDOT = 1410
043195 meter/sec RA = 310
60809 deg
ZDOT = -4559
050742 TA = 35
99225
MA = 35
88650
Ha = 222
858 n
mi
Hp = 213
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4179678
02 X = -1354309
93
Y = 18708474
05 feet Y = 5687647
70 meter
Z = 11261737
08 Z = 3426193
18
XDOT = -19718
324636 XDOT = -6003
320793
YDOT = 4626
125968 feet/sec YDOT = 1342
871189 meter/sec
ZDOT = -14957
515559 ZDOT = -4588
229400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12706527
74 X = -3872949
65
Y = 14376431
10 feet Y = 4381936
20 meter
Z = 11232355
65 Z = 3423622
00
XDOT = -18384
658379 XDOT = -5603
643874
YDOT = -4424
505294 feet/sec YDOT = -1348
589214 meter/sec
ZDOT = -15088
569434 ZDOT = -4598
995963
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 18253
99019790
00016717 00000-0 10270-3 0 9077
2 25544 51
6407 311
1177 0004790 143
2819 216
8662 15
53826470 11851
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
99019790 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 311
1177 deg
Eccentricity:
0004790
Arg of perigee: 143
2819 deg
Mean anomaly: 216
8662 deg
Mean motion: 15
53826470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1185
Checksum: 322
Coasting Arc #9 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2018/254/22:49:12
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2288454
67 A = 6788314
57 meter
Y = -6045832
19 meter E =
0006751
Z = -2075410
31 I = 51
34778
XDOT = 5324
518597 Wp = 81
15769
YDOT = 130
470314 meter/sec RA = 305
61104 deg
ZDOT = 5507
424965 TA = 255
79924
MA = 255
87425
Ha = 222
682 n
mi
Hp = 214
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7508053
39 X = 2365972
02
Y = -19835407
45 feet Y = -6019807
92 meter
Z = -6809088
94 Z = -2064104
80
XDOT = 17468
893036 XDOT = 5295
911737
YDOT = 428
052210 feet/sec YDOT = 189
853472 meter/sec
ZDOT = 18068
979545 ZDOT = 5533
220137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15901938
71 X = 4846910
92
Y = -14058487
73 feet Y = -4285027
06 meter
Z = -6757604
20 Z = -2059717
76
XDOT = 14139
107919 XDOT = 4309
600094
YDOT = 7278
241108 feet/sec YDOT = 2218
407890 meter/sec
ZDOT = 18184
649143 ZDOT = 5542
681059
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 18254
95490793
00016717 00000-0 10270-3 0 9081
2 25544 51
6413 306
3102 0004632 148
9208 211
2220 15
53857108 12000
Satellite: ISS
Catalog Number: 25544
Epoch time: 18254
95490793 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 306
3102 deg
Eccentricity:
0004632
Arg of perigee: 148
9208 deg
Mean anomaly: 211
2220 deg
Mean motion: 15
53857108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 285
Coasting Arc #10 (Orbit 1215)
---------------------------------------
Vector Time (GMT): 2018/255/22:49:12
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3105715
63 A = 6790172
22 meter
Y = 6008469
28 meter E =
0017385
Z = 484549
18 I = 51
33527
XDOT = -4469
047427 Wp = 135
67367
YDOT = -1819
504182 meter/sec RA = 300
62009 deg
ZDOT = -5964
763888 TA = 39
07552
MA = 38
95007
Ha = 222
706 n
mi
Hp = 214
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10189355
74 X = -3175026
87
Y = 19712825
74 feet Y = 5973351
53 meter
Z = 1589728
29 Z = 469293
66
XDOT = -14662
229092 XDOT = -4419
395285
YDOT = -5969
501909 feet/sec YDOT = -1869
203178 meter/sec
ZDOT = -19569
435328 ZDOT = -5986
352262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17967108
85 X = -5476374
78
Y = 13031371
55 feet Y = 3971962
05 meter
Z = 1520545
98 Z = 463462
41
XDOT = -9351
409997 XDOT = -2850
309767
YDOT = -10551
604962 feet/sec YDOT = -3216
129192 meter/sec
ZDOT = -19666
017877 ZDOT = -5994
202249
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 18255
98393092
00016717 00000-0 10270-3 0 9090
2 25544 51
6414 301
1827 0004746 152
4069 207
7336 15
53808883 12160
Satellite: ISS
Catalog Number: 25544
Epoch time: 18255
98393092 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 301
1827 deg
Eccentricity:
0004746
Arg of perigee: 152
4069 deg
Mean anomaly: 207
7336 deg
Mean motion: 15
53808883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 324
Coasting Arc #11 (Orbit 1231)
---------------------------------------
Vector Time (GMT): 2018/256/22:49:12
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3670770
01 A = 6789583
72 meter
Y = -5597947
77 meter E =
0013770
Z = 1109473
69 I = 51
31707
XDOT = 3524
796835 Wp = 76
00758
YDOT = 3482
342241 meter/sec RA = 295
62861 deg
ZDOT = 5850
476931 TA = 296
08309
MA = 296
22475
Ha = 222
530 n
mi
Hp = 214
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12043208
69 X = 3727705
72
Y = -18365970
38 feet Y = -5556580
23 meter
Z = 3640005
53 Z = 1127443
90
XDOT = 11564
294079 XDOT = 3457
175651
YDOT = 11425
007354 feet/sec YDOT = 3521
381390 meter/sec
ZDOT = 19194
478120 ZDOT = 5867
434717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18795027
31 X = 5728724
32
Y = -11335619
35 feet Y = -3455096
78 meter
Z = 3721298
99 Z = 1134251
93
XDOT = 4522
351931 XDOT = 1378
412869
YDOT = 13885
399912 feet/sec YDOT = 4232
269893 meter/sec
ZDOT = 19270
084697 ZDOT = 5873
521816
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 18257
01294917
00016717 00000-0 10270-3 0 9104
2 25544 51
6406 296
0545 0004491 155
7173 204
4191 15
53854047 12323
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
01294917 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 296
0545 deg
Eccentricity:
0004491
Arg of perigee: 155
7173 deg
Mean anomaly: 204
4191 deg
Mean motion: 15
53854047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1232
Checksum: 301
Coasting Arc #12 (Orbit 1239)
---------------------------------------
Vector Time (GMT): 2018/257/11:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 943674
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1409499
29 A = 6782773
03 meter
Y = 5179209
39 meter E =
0011993
Z = 4135143
48 I = 51
28532
XDOT = -5090
387107 Wp = 98
70364
YDOT = 4367
870356 meter/sec RA = 292
91153 deg
ZDOT = -3728
099040 TA = 29
83844
MA = 29
77012
Ha = 222
473 n
mi
Hp = 214
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4624341
49 X = 1331392
70
Y = 16992156
78 feet Y = 5194534
99 meter
Z = 13566743
70 Z = 4141800
26
XDOT = -16700
745101 XDOT = -5120
742267
YDOT = 14330
283320 feet/sec YDOT = 4310
776094 meter/sec
ZDOT = -12231
296064 ZDOT = -3752
900598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -755892
78 X = -230396
12
Y = -17571378
69 feet Y = -5355756
23 meter
Z = 13595945
63 Z = 4144044
23
XDOT = 18040
954552 XDOT = 5498
882948
YDOT = -10345
589734 feet/sec YDOT = -3153
335751 meter/sec
ZDOT = -12343
064528 ZDOT = -3762
166068
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 18257
52745811
00016717 00000-0 10270-3 0 9115
2 25544 51
6390 293
4894 0004741 158
0468 202
0889 15
53874621 12401
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
52745811 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 293
4894 deg
Eccentricity:
0004741
Arg of perigee: 158
0468 deg
Mean anomaly: 202
0889 deg
Mean motion: 15
53874621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1240
Checksum: 320
Coasting Arc #13 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2018/257/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943674
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3740567
12 A = 6778289
87 meter
Y = -2045387
88 meter E =
0017398
Z = -5284442
42 I = 51
26843
XDOT = 3218
498730 Wp = 107
37399
YDOT = -6934
454857 meter/sec RA = 292
48129 deg
ZDOT = 401
840773 TA = 166
50754
MA = 166
46097
Ha = 222
615 n
mi
Hp = 214
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12272201
84 X = -3691747
83
Y = -6710590
17 feet Y = -2086944
95 meter
Z = -17337409
53 Z = -5302494
17
XDOT = 10559
379035 XDOT = 3293
850580
YDOT = -22750
836145 feet/sec YDOT = -6898
042023 meter/sec
ZDOT = 1318
375238 ZDOT = 417
658777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13723353
66 X = 4182878
19
Y = 2122244
38 feet Y = 646860
09 meter
Z = -17418104
68 Z = -5309038
31
XDOT = -1928
979790 XDOT = -587
953040
YDOT = 23990
567534 feet/sec YDOT = 7312
324984 meter/sec
ZDOT = 1390
178809 ZDOT = 423
726501
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 18257
59177210
00016717 00000-0 10270-3 0 9125
2 25544 51
6387 293
1693 0004767 157
4274 202
7088 15
53829894 12418
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
59177210 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 293
1693 deg
Eccentricity:
0004767
Arg of perigee: 157
4274 deg
Mean anomaly: 202
7088 deg
Mean motion: 15
53829894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 337
Coasting Arc #14 (Orbit 1256)
---------------------------------------
Vector Time (GMT): 2018/258/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943674
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3020615
18 A = 6779747
71 meter
Y = 3547747
48 meter E =
0007068
Z = 4918452
35 I = 51
26136
XDOT = -3817
272820 Wp = 98
01588
YDOT = 6286
035522 meter/sec RA = 287
45911 deg
ZDOT = -2188
131677 TA = 13
43840
MA = 13
41959
Ha = 222
381 n
mi
Hp = 214
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9910154
81 X = 2956827
41
Y = 11639591
48 feet Y = 3581169
75 meter
Z = 16136654
70 Z = 4932970
37
XDOT = -12523
860959 XDOT = -3876
652460
YDOT = 20623
476123 feet/sec YDOT = 6243
015978 meter/sec
ZDOT = -7178
909700 ZDOT = -2206
819389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13335876
57 X = -4064775
18
Y = -7331745
55 feet Y = -2234716
04 meter
Z = 16201320
51 Z = 4938162
49
XDOT = 3681
253492 XDOT = 1122
046064
YDOT = -22758
936905 feet/sec YDOT = -6936
923969 meter/sec
ZDOT = -7263
490831 ZDOT = -2213
912005
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 18258
62078851
00016717 00000-0 10270-3 0 9132
2 25544 51
6381 288
0412 0004702 160
8068 199
3263 15
53860167 12573
Satellite: ISS
Catalog Number: 25544
Epoch time: 18258
62078851 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 288
0412 deg
Eccentricity:
0004702
Arg of perigee: 160
8068 deg
Mean anomaly: 199
3263 deg
Mean motion: 15
53860167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1257
Checksum: 319
Coasting Arc #15 (Orbit 1271)
---------------------------------------
Vector Time (GMT): 2018/259/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943674
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2299988
58 A = 6782977
85 meter
Y = -4889066
85 meter E =
0010915
Z = -4112950
38 I = 51
26316
XDOT = 4229
537183 Wp = 128
77548
YDOT = -5155
844558 meter/sec RA = 282
44348 deg
ZDOT = 3763
639181 TA = 180
28207
MA = 180
28269
Ha = 222
478 n
mi
Hp = 214
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7545894
29 X = -2225168
12
Y = -16040245
57 feet Y = -4914368
80 meter
Z = -13493931
70 Z = -4123940
97
XDOT = 13876
434327 XDOT = 4268
595081
YDOT = -16915
500520 feet/sec YDOT = -5108
328345 meter/sec
ZDOT = 12347
897574 ZDOT = 3784
280028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12939956
22 X = 3944098
65
Y = 12061139
85 feet Y = 3676235
43 meter
Z = -13542622
71 Z = -4127791
40
XDOT = -5543
230026 XDOT = -1689
576512
YDOT = 19916
121437 feet/sec YDOT = 6070
433814 meter/sec
ZDOT = 12441
089643 ZDOT = 3792
044123
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 18259
58548962
00016717 00000-0 10270-3 0 9144
2 25544 51
6382 283
2346 0004600 162
4674 197
6639 15
53834565 12723
Satellite: ISS
Catalog Number: 25544
Epoch time: 18259
58548962 = yrday
fracday
Element set: 914
Inclination: 51
6382 deg
RA of node: 283
2346 deg
Eccentricity:
0004600
Arg of perigee: 162
4674 deg
Mean anomaly: 197
6639 deg
Mean motion: 15
53834565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1272
Checksum: 341
Coasting Arc #16 (Orbit 1287)
---------------------------------------
Vector Time (GMT): 2018/260/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943674
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1569145
14 A = 6786476
69 meter
Y = 5923657
03 meter E =
0015413
Z = 2895690
55 I = 51
26782
XDOT = -4525
844661 Wp = 113
98435
YDOT = 3653
197273 meter/sec RA = 277
43576 deg
ZDOT = -5005
784774 TA = 32
80717
MA = 32
71157
Ha = 222
205 n
mi
Hp = 214
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5148113
98 X = 1488722
79
Y = 19434570
30 feet Y = 5940754
78 meter
Z = 9500297
08 Z = 2903117
28
XDOT = -14848
571723 XDOT = -4542
043867
YDOT = 11985
555356 feet/sec YDOT = 3602
495300 meter/sec
ZDOT = -16423
178393 ZDOT = -5027
809318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12293896
02 X = -3747179
51
Y = -15888527
83 feet Y = -4842823
28 meter
Z = 9532893
00 Z = 2905625
79
XDOT = 7705
725893 XDOT = 2348
705252
YDOT = -15904
963279 feet/sec YDOT = -4847
832807 meter/sec
ZDOT = -16522
387707 ZDOT = -5036
023773
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 18260
61450148
00016717 00000-0 10270-3 0 9159
2 25544 51
6369 278
1066 0004441 167
8293 192
2968 15
53878244 12884
Satellite: ISS
Catalog Number: 25544
Epoch time: 18260
61450148 = yrday
fracday
Element set: 915
Inclination: 51
6369 deg
RA of node: 278
1066 deg
Eccentricity:
0004441
Arg of perigee: 167
8293 deg
Mean anomaly: 192
2968 deg
Mean motion: 15
53878244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1288
Checksum: 337
Coasting Arc #17 (Orbit 1302)
---------------------------------------
Vector Time (GMT): 2018/261/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943674
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -871806
61 A = 6789173
55 meter
Y = -6577974
14 meter E =
0006357
Z = -1435006
27 I = 51
27353
XDOT = 4699
199078 Wp = 70
55463
YDOT = -1873
339937 meter/sec RA = 272
43723 deg
ZDOT = 5755
366099 TA = 273
72485
MA = 273
79754
Ha = 222
286 n
mi
Hp = 214
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2860257
90 X = -791214
59
Y = -21581279
97 feet Y = -6587272
74 meter
Z = -4708025
81 Z = -1439045
09
XDOT = 15417
319811 XDOT = 4691
841532
YDOT = -6146
128401 feet/sec YDOT = -1820
831058 meter/sec
ZDOT = 18882
434709 ZDOT = 5778
175381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11380242
32 X = 3468697
86
Y = 18554224
09 feet Y = 5655327
50 meter
Z = -4725365
68 Z = -1440291
46
XDOT = -10105
750914 XDOT = -3080
232878
YDOT = 11014
286485 feet/sec YDOT = 3357
154521 meter/sec
ZDOT = 18984
949393 ZDOT = 5786
612575
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 18261
57919989
00016717 00000-0 10270-3 0 9169
2 25544 51
6367 273
3003 0004668 169
8102 190
3146 15
53877375 13031
Satellite: ISS
Catalog Number: 25544
Epoch time: 18261
57919989 = yrday
fracday
Element set: 916
Inclination: 51
6367 deg
RA of node: 273
3003 deg
Eccentricity:
0004668
Arg of perigee: 169
8102 deg
Mean anomaly: 190
3146 deg
Mean motion: 15
53877375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1303
Checksum: 334
Coasting Arc #18 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2018/262/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943674
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 144745
05 A = 6790062
18 meter
Y = 6777168
89 meter E =
0015424
Z = -196886
93 I = 51
27682
XDOT = -4803
401421 Wp = 146
23102
YDOT = -64
236068 meter/sec RA = 267
44202 deg
ZDOT = -5981
112785 TA = 35
90161
MA = 35
79807
Ha = 222
104 n
mi
Hp = 214
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 474885
34 X = 69906
48
Y = 22234806
07 feet Y = 6778369
07 meter
Z = -645954
51 Z = -196366
00
XDOT = -15759
191015 XDOT = -4773
273115
YDOT = -210
748254 feet/sec YDOT = -117
782944 meter/sec
ZDOT = -19623
073441 ZDOT = -6004
372788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9845293
89 X = -3000845
58
Y = -19942023
82 feet Y = -6078328
86 meter
Z = -644397
83 Z = -196412
46
XDOT = 12795
042144 XDOT = 3899
928846
YDOT = -5704
763159 feet/sec YDOT = -1738
811811 meter/sec
ZDOT = -19727
386272 ZDOT = -6012
907336
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 18262
60820749
00016717 00000-0 10270-3 0 9170
2 25544 51
6375 268
1716 0004400 174
1202 186
0003 15
53871811 13197
Satellite: ISS
Catalog Number: 25544
Epoch time: 18262
60820749 = yrday
fracday
Element set: 917
Inclination: 51
6375 deg
RA of node: 268
1716 deg
Eccentricity:
0004400
Arg of perigee: 174
1202 deg
Mean anomaly: 186
0003 deg
Mean motion: 15
53871811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 291
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