[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 4th 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
249/00:35:06
532 0
6 0
7 0
7
N/A -0
2 -0
1 223
0
000/00:00:13
064 0
2 -0
0 213
7
249/22:52:00
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
8
253/11:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 214
0
253/22:49:12
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 214
1
257/11:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 214
4
257/13:50:00
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
3
Coasting Arc #1 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2018/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5247528
21 A = 6784935
57 meter
Y = -2515717
64 meter E =
0010405
Z = -3499839
83 I = 51
66595
XDOT = 4848
498831 Wp = 104
38744
YDOT = 3822
398159 meter/sec RA = 2
78131 deg
ZDOT = 4530
854374 TA = 214
53843
MA = 214
60607
Ha = 223
362 n
mi
Hp = 213
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17216299
90 X = 5292270
03
Y = -8253666
79 feet Y = -2456786
22 meter
Z = -11482414
15 Z = -3474240
32
XDOT = 15907
148395 XDOT = 4783
386862
YDOT = 12540
676375 feet/sec YDOT = 3876
253685 meter/sec
ZDOT = 14865
007789 ZDOT = 4554
248287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19108493
22 X = -5824268
73
Y = 1422199
49 feet Y = 433486
40 meter
Z = -11367175
03 Z = -3464714
95
XDOT = -10080
510831 XDOT = -3072
539701
YDOT = -16027
033117 feet/sec YDOT = -4885
039694 meter/sec
ZDOT = 14969
439348 ZDOT = 4562
685113
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 18243
50726606
00016717 00000-0 10270-3 0 9007
2 25544 51
6412 3
3493 0005655 116
0578 244
1157 15
53891350 10221
Satellite: ISS
Catalog Number: 25544
Epoch time: 18243
50726606 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 3
3493 deg
Eccentricity:
0005655
Arg of perigee: 116
0578 deg
Mean anomaly: 244
1157 deg
Mean motion: 15
53891350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 282
Coasting Arc #2 (Orbit 1037)
---------------------------------------
Vector Time (GMT): 2018/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6169775
66 A = 6788231
60 meter
Y = 1884508
11 meter E =
0019652
Z = 2081091
27 I = 51
64355
XDOT = -3179
411487 Wp = 113
54232
YDOT = -4260
723683 meter/sec RA = 357
80554 deg
ZDOT = -5533
990777 TA = 43
40890
MA = 43
25431
Ha = 223
380 n
mi
Hp = 213
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20242046
12 X = -6200499
06
Y = 6182769
40 feet Y = 1815341
73 meter
Z = 6827727
26 Z = 2051045
87
XDOT = -10431
140050 XDOT = -3104
649338
YDOT = -13978
752240 feet/sec YDOT = -4295
860339 meter/sec
ZDOT = -18156
137720 ZDOT = -5549
253469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21172638
25 X = 6453420
14
Y = 1230006
95 feet Y = 374906
12 meter
Z = 6692637
81 Z = 2039916
00
XDOT = 4916
535706 XDOT = 1498
560083
YDOT = 15142
785004 feet/sec YDOT = 4615
520869 meter/sec
ZDOT = -18224
010680 ZDOT = -5554
678455
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 18244
53624211
00016717 00000-0 10270-3 0 9011
2 25544 51
6408 358
2215 0005780 121
1162 239
0558 15
53900969 10387
Satellite: ISS
Catalog Number: 25544
Epoch time: 18244
53624211 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 358
2215 deg
Eccentricity:
0005780
Arg of perigee: 121
1162 deg
Mean anomaly: 239
0558 deg
Mean motion: 15
53900969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1038
Checksum: 292
Coasting Arc #3 (Orbit 1052)
---------------------------------------
Vector Time (GMT): 2018/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6652428
12 A = 6789843
23 meter
Y = -1244157
94 meter E =
0013262
Z = -510822
09 I = 51
61754
XDOT = 1311
691498 Wp = 66
30428
YDOT = 4610
311355 meter/sec RA = 352
83427 deg
ZDOT = 5981
532032 TA = 288
18598
MA = 288
33031
Ha = 223
278 n
mi
Hp = 213
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21825551
59 X = 6668327
53
Y = -4081883
02 feet Y = -1169677
00 meter
Z = -1675925
48 Z = -478468
19
XDOT = 4303
449795 XDOT = 1230
985060
YDOT = 15125
693422 feet/sec YDOT = 4624
528550 meter/sec
ZDOT = 19624
448925 ZDOT = 5987
707600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21958782
14 X = -6693036
80
Y = -3360716
15 feet Y = -1024346
28 meter
Z = -1530578
69 Z = -466520
38
XDOT = 813
456722 XDOT = 247
941609
YDOT = -14055
164002 feet/sec YDOT = -4284
013988 meter/sec
ZDOT = 19651
493625 ZDOT = 5989
775257
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 18245
50090201
00016717 00000-0 10270-3 0 9026
2 25544 51
6422 353
4146 0005677 122
5924 237
5777 15
53918132 10533
Satellite: ISS
Catalog Number: 25544
Epoch time: 18245
50090201 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 353
4146 deg
Eccentricity:
0005677
Arg of perigee: 122
5924 deg
Mean anomaly: 237
5777 deg
Mean motion: 15
53918132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1053
Checksum: 293
Coasting Arc #4 (Orbit 1068)
---------------------------------------
Vector Time (GMT): 2018/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6665360
12 A = 6789298
94 meter
Y = 489600
40 meter E =
0014737
Z = -1163533
39 I = 51
58256
XDOT = 654
259292 Wp = 135
61044
YDOT = -4897
804290 meter/sec RA = 347
86259 deg
ZDOT = -5864
128490 TA = 57
03446
MA = 56
89286
Ha = 223
169 n
mi
Hp = 213
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21867979
40 X = -6664687
76
Y = 1606300
52 feet Y = 415067
46 meter
Z = -3817366
76 Z = -1195909
75
XDOT = 2146
519988 XDOT = 737
464094
YDOT = -16068
911712 feet/sec YDOT = -4890
022798 meter/sec
ZDOT = -19239
266699 ZDOT = -5860
748141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21241353
18 X = 6474364
45
Y = 5335067
87 feet Y = 1626128
69 meter
Z = -3962698
50 Z = -1207830
50
XDOT = -6817
292507 XDOT = -2077
910756
YDOT = 12993
982772 feet/sec YDOT = 3960
565949 meter/sec
ZDOT = -19223
395113 ZDOT = -5859
290830
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 18246
52986841
00016717 00000-0 10270-3 0 9034
2 25544 51
6416 348
2868 0005711 126
5945 233
5734 15
53925368 10690
Satellite: ISS
Catalog Number: 25544
Epoch time: 18246
52986841 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 348
2868 deg
Eccentricity:
0005711
Arg of perigee: 126
5945 deg
Mean anomaly: 233
5734 deg
Mean motion: 15
53925368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1069
Checksum: 338
Coasting Arc #5 (Orbit 1084)
---------------------------------------
Vector Time (GMT): 2018/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6225163
68 A = 6786744
07 meter
Y = 303577
33 meter E =
0017652
Z = 2671997
20 I = 51
54245
XDOT = -2486
351123 Wp = 92
62167
YDOT = 5075
036025 meter/sec RA = 342
88469 deg
ZDOT = 5185
624078 TA = 297
58950
MA = 297
76867
Ha = 223
098 n
mi
Hp = 213
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20423765
35 X = 6208327
23
Y = 995988
61 feet Y = 373097
31 meter
Z = 8766395
01 Z = 2702195
86
XDOT = -8157
319957 XDOT = -2568
105711
YDOT = 16650
380660 feet/sec YDOT = 5046
774869 meter/sec
ZDOT = 17013
202357 ZDOT = 5173
347671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19145103
60 X = -5835427
58
Y = -7013855
38 feet Y = -2137823
12 meter
Z = 8901837
27 Z = 2713280
00
XDOT = 12340
747422 XDOT = 3761
459814
YDOT = -12038
708011 feet/sec YDOT = -3669
398202 meter/sec
ZDOT = 16957
396474 ZDOT = 5168
614445
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 18247
55883065
00016717 00000-0 10270-3 0 9043
2 25544 51
6419 343
1595 0005693 129
7955 230
3700 15
53945776 10850
Satellite: ISS
Catalog Number: 25544
Epoch time: 18247
55883065 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 343
1595 deg
Eccentricity:
0005693
Arg of perigee: 129
7955 deg
Mean anomaly: 230
3700 deg
Mean motion: 15
53945776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1085
Checksum: 337
Coasting Arc #6 (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 = -5364979
28 A = 6783101
34 meter
Y = -1231099
75 meter E =
0010785
Z = -3971743
27 I = 51
49875
XDOT = 4109
994288 Wp = 99
03674
YDOT = -5090
478887 meter/sec RA = 337
89588 deg
ZDOT = -3984
784396 TA = 129
35362
MA = 129
25801
Ha = 223
032 n
mi
Hp = 213
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17601638
05 X = -5331521
57
Y = -4039041
17 feet Y = -1290907
65 meter
Z = -13030653
76 Z = -3997722
97
XDOT = 13484
233227 XDOT = 4185
967789
YDOT = -16701
046216 feet/sec YDOT = -5044
093351 meter/sec
ZDOT = -13073
439621 ZDOT = -3964
635035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15671690
83 X = 4776731
36
Y = 8802448
06 feet Y = 2682986
17 meter
Z = -13147032
66 Z = -4007215
56
XDOT = -17078
194912 XDOT = -5205
433809
YDOT = 11068
775565 feet/sec YDOT = 3373
762792 meter/sec
ZDOT = -12982
317656 ZDOT = -3957
010422
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
52347976
00016717 00000-0 10270-3 0 9058
2 25544 51
6417 338
3523 0005588 134
1852 225
9760 15
53931447 11008
Satellite: ISS
Catalog Number: 25544
Epoch time: 18248
52347976 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 338
3523 deg
Eccentricity:
0005588
Arg of perigee: 134
1852 deg
Mean anomaly: 225
9760 deg
Mean motion: 15
53931447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1100
Checksum: 320
Coasting Arc #7 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2018/249/00:35:13
064
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -210718
87 A = 6778975
16 meter
Y = -4420207
36 meter E =
0017956
Z = -5151349
55 I = 51
46863
XDOT = 7228
048229 Wp = 109
20664
YDOT = -2050
851488 meter/sec RA = 335
24222 deg
ZDOT = 1462
501282 TA = 174
93984
MA = 174
92167
Ha = 222
981 n
mi
Hp = 213
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -691334
88 X = -136252
95
Y = -14501992
66 feet Y = -4422147
52 meter
Z = -16900753
12 Z = -5152192
18
XDOT = 23714
068992 XDOT = 7243
340232
YDOT = -6728
515381 feet/sec YDOT = -1969
936911 meter/sec
ZDOT = 4798
232551 ZDOT = 1497
649448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1195763
71 X = 364468
78
Y = -14465450
22 feet Y = -4409069
23 meter
Z = -16903907
54 Z = -5152311
02
XDOT = 23271
033203 XDOT = 7093
010920
YDOT = -3874
154792 feet/sec YDOT = -1180
842381 meter/sec
ZDOT = 4956
207681 ZDOT = 1510
652101
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
03795793
00016717 00000-0 10270-3 0 9060
2 25544 51
6426 335
7914 0004822 133
4971 226
6583 15
53833800 11080
Satellite: ISS
Catalog Number: 25544
Epoch time: 18249
03795793 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 335
7914 deg
Eccentricity:
0004822
Arg of perigee: 133
4971 deg
Mean anomaly: 226
6583 deg
Mean motion: 15
53833800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 324
Coasting Arc #8 (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 = 3031037
11 A = 6778418
48 meter
Y = 3071636
61 meter E =
0008248
Z = 5222619
70 I = 51
43813
XDOT = -6200
905356 Wp = 130
03805
YDOT = 4406
098849 meter/sec RA = 330
62653 deg
ZDOT = 1001
139520 TA = 310
31986
MA = 310
39189
Ha = 222
774 n
mi
Hp = 213
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9944347
46 X = 2971095
55
Y = 10077547
94 feet Y = 3105196
82 meter
Z = 17134579
07 Z = 5237197
52
XDOT = -20344
177677 XDOT = -6254
577655
YDOT = 14455
704884 feet/sec YDOT = 4336
455968 meter/sec
ZDOT = 3284
578478 ZDOT = 970
887545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3019298
09 X = 920282
06
Y = 13751371
42 feet Y = 4191418
01 meter
Z = 17199547
73 Z = 5242422
15
XDOT = -23926
116747 XDOT = -7292
680384
YDOT = 1290
053810 feet/sec YDOT = 393
208401 meter/sec
ZDOT = 3148
247105 ZDOT = 959
585718
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
00267463
00016717 00000-0 10270-3 0 9078
2 25544 51
6410 330
9845 0004788 137
1320 223
0206 15
53864810 11238
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
00267463 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 330
9845 deg
Eccentricity:
0004788
Arg of perigee: 137
1320 deg
Mean anomaly: 223
0206 deg
Mean motion: 15
53864810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 280
Coasting Arc #9 (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 = -1591675
00 A = 6778462
07 meter
Y = -3993695
11 meter E =
0018310
Z = -5256522
85 I = 51
40991
XDOT = 6629
399896 Wp = 106
57605
YDOT = -3735
843472 meter/sec RA = 325
61474 deg
ZDOT = 828
248378 TA = 171
39692
MA = 171
36549
Ha = 222
900 n
mi
Hp = 213
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5222030
83 X = -1521365
06
Y = -13102674
26 feet Y = -4011101
55 meter
Z = -17245809
87 Z = -5264083
51
XDOT = 21749
999659 XDOT = 6666
659291
YDOT = -12256
704304 feet/sec YDOT = -3661
500543 meter/sec
ZDOT = 2717
350323 ZDOT = 860
541967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2350783
23 X = 716518
73
Y = -13866200
09 feet Y = -4226417
79 meter
Z = -17279176
78 Z = -5266693
08
XDOT = 23929
904335 XDOT = 7293
834841
YDOT = 478
489324 feet/sec YDOT = 145
843546 meter/sec
ZDOT = 2862
732504 ZDOT = 872
560867
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
96739128
00016717 00000-0 10270-3 0 9086
2 25544 51
6414 326
1777 0004811 139
3528 220
7985 15
53837106 11386
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
96739128 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 326
1777 deg
Eccentricity:
0004811
Arg of perigee: 139
3528 deg
Mean anomaly: 220
7985 deg
Mean motion: 15
53837106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 326
Coasting Arc #10 (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 = 165663
84 A = 6780421
99 meter
Y = 4800663
02 meter E =
0009372
Z = 4777241
58 I = 51
38972
XDOT = -6660
904929 Wp = 90
83160
YDOT = 2802
870623 meter/sec RA = 320
60470 deg
ZDOT = -2581
370967 TA = 24
68938
MA = 24
64455
Ha = 222
756 n
mi
Hp = 213
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 543516
55 X = 88764
17
Y = 15750206
77 feet Y = 4802086
06 meter
Z = 15673364
77 Z = 4777859
09
XDOT = -21853
362629 XDOT = -6679
213584
YDOT = 9195
769762 feet/sec YDOT = 2728
281159 meter/sec
ZDOT = -8469
064854 ZDOT = -2613
771622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7478244
88 X = -2279369
04
Y = 13869888
66 feet Y = 4227542
06 meter
Z = 15675484
96 Z = 4777887
82
XDOT = -22466
138380 XDOT = -6847
678978
YDOT = -2361
049781 feet/sec YDOT = -719
647973 meter/sec
ZDOT = -8614
784100 ZDOT = -2625
786194
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
99641713
00016717 00000-0 10270-3 0 9093
2 25544 51
6412 321
0512 0004703 143
5200 216
6274 15
53855415 11545
Satellite: ISS
Catalog Number: 25544
Epoch time: 18251
99641713 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 321
0512 deg
Eccentricity:
0004703
Arg of perigee: 143
5200 deg
Mean anomaly: 216
6274 deg
Mean motion: 15
53855415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1154
Checksum: 282
Coasting Arc #11 (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 = 1142210
13 A = 6783782
79 meter
Y = -5455827
39 meter E =
0010369
Z = -3878502
76 I = 51
37675
XDOT = 6281
253831 Wp = 122
16633
YDOT = -1585
612765 meter/sec RA = 315
59838 deg
ZDOT = 4082
892372 TA = 190
85868
MA = 190
88108
Ha = 222
747 n
mi
Hp = 214
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3747408
57 X = 1221973
36
Y = -17899696
16 feet Y = -5442608
85 meter
Z = -12724746
60 Z = -3872760
02
XDOT = 20607
788159 XDOT = 6278
685410
YDOT = -5202
141619 feet/sec YDOT = -1515
385334 meter/sec
ZDOT = 13395
316182 ZDOT = 4113
398166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12016433
85 X = 3662609
04
Y = -13810171
28 feet Y = -4209340
21 meter
Z = -12698261
93 Z = -3870430
24
XDOT = 19465
468598 XDOT = 5933
074829
YDOT = 4502
300084 feet/sec YDOT = 1372
301066 meter/sec
ZDOT = 13532
358126 ZDOT = 4124
662757
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
96112514
00016717 00000-0 10270-3 0 9105
2 25544 51
6419 316
2437 0004717 146
1933 213
9521 15
53856371 11694
Satellite: ISS
Catalog Number: 25544
Epoch time: 18252
96112514 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 316
2437 deg
Eccentricity:
0004717
Arg of perigee: 146
1933 deg
Mean anomaly: 213
9521 deg
Mean motion: 15
53856371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 303
Coasting Arc #12 (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 = -2873522
09 A = 6778256
81 meter
Y = -3129661
12 meter E =
0017798
Z = -5296438
83 I = 51
34480
XDOT = 5387
811050 Wp = 105
84038
YDOT = -5430
858962 meter/sec RA = 313
08224 deg
ZDOT = 282
025051 TA = 166
88681
MA = 166
84048
Ha = 222
741 n
mi
Hp = 214
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9427565
93 X = -2812584
66
Y = -10267917
07 feet Y = -3161454
74 meter
Z = -17376767
80 Z = -5310248
92
XDOT = 17676
545439 XDOT = 5446
770070
YDOT = -17817
778747 feet/sec YDOT = -5370
279029 meter/sec
ZDOT = 925
279039 ZDOT = 308
340818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3909692
95 X = 1191674
41
Y = 13299672
87 feet Y = 4053740
29 meter
Z = -17438296
42 Z = -5315192
75
XDOT = -22696
448336 XDOT = -6917
877453
YDOT = 8057
983641 feet/sec YDOT = 2456
073414 meter/sec
ZDOT = 1044
028836 ZDOT = 318
219989
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
47563398
00016717 00000-0 10270-3 0 9113
2 25544 51
6404 313
6781 0004886 152
1258 208
0157 15
53832172 11777
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
47563398 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 313
6781 deg
Eccentricity:
0004886
Arg of perigee: 152
1258 deg
Mean anomaly: 208
0157 deg
Mean motion: 15
53832172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1177
Checksum: 314
Coasting Arc #13 (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 = -1300043
62 A = 6785257
33 meter
Y = 5708430
02 meter E =
0015424
Z = 3412718
89 I = 51
35734
XDOT = -6002
881223 Wp = 105
16805
YDOT = 1377
977569 meter/sec RA = 310
60760 deg
ZDOT = -4578
317290 TA = 34
68365
MA = 34
58317
Ha = 222
743 n
mi
Hp = 214
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4265234
98 X = -1380357
36
Y = 18728444
95 feet Y = 5693443
38 meter
Z = 11196584
27 Z = 3406208
00
XDOT = -19694
492202 XDOT = -5995
605054
YDOT = 4520
923784 feet/sec YDOT = 1310
889319 meter/sec
ZDOT = -15020
726017 ZDOT = -4607
459560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12790796
47 X = -3898634
76
Y = 14353124
57 feet Y = 4374832
37 meter
Z = 11166634
22 Z = 3403590
11
XDOT = -18314
618004 XDOT = -5582
295568
YDOT = -4499
044920 feet/sec YDOT = -1371
308891 meter/sec
ZDOT = -15151
612488 ZDOT = -4618
211486
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
99014536
00016717 00000-0 10270-3 0 9126
2 25544 51
6406 311
1172 0004769 149
4089 210
7343 15
53838132 11855
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
99014536 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 311
1172 deg
Eccentricity:
0004769
Arg of perigee: 149
4089 deg
Mean anomaly: 210
7343 deg
Mean motion: 15
53838132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1185
Checksum: 305
Coasting Arc #14 (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 = 2316146
99 A = 6788327
40 meter
Y = -6045059
76 meter E =
0006310
Z = -2046636
96 I = 51
34780
XDOT = 5309
345804 Wp = 81
88551
YDOT = 170
297047 meter/sec RA = 305
61058 deg
ZDOT = 5521
028738 TA = 255
40879
MA = 255
47877
Ha = 222
561 n
mi
Hp = 214
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7598907
44 X = 2393513
87
Y = -19832873
22 feet Y = -6018726
65 meter
Z = -6714688
19 Z = -2035197
30
XDOT = 17419
113529 XDOT = 5280
228637
YDOT = 558
717345 feet/sec YDOT = 229
507681 meter/sec
ZDOT = 18113
611344 ZDOT = 5546
748961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15980661
07 X = 4870905
49
Y = -14014331
94 feet Y = -4271568
37 meter
Z = -6662601
90 Z = -2030761
06
XDOT = 14037
291827 XDOT = 4278
566549
YDOT = 7364
962285 feet/sec YDOT = 2244
840505 meter/sec
ZDOT = 18228
939663 ZDOT = 5556
180809
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
95484763
00016717 00000-0 10270-3 0 9137
2 25544 51
6411 306
3096 0004630 155
2402 204
8973 15
53869964 12001
Satellite: ISS
Catalog Number: 25544
Epoch time: 18254
95484763 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 306
3096 deg
Eccentricity:
0004630
Arg of perigee: 155
2402 deg
Mean anomaly: 204
8973 deg
Mean motion: 15
53869964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 312
Coasting Arc #15 (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 = -3131322
14 A = 6790147
04 meter
Y = 5997731
19 meter E =
0017174
Z = 450107
37 I = 51
33516
XDOT = -4445
953571 Wp = 137
55692
YDOT = -1864
190537 meter/sec RA = 300
61965 deg
ZDOT = -5968
354817 TA = 37
56635
MA = 37
44649
Ha = 222
578 n
mi
Hp = 214
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10273366
60 X = -3200344
10
Y = 19677595
75 feet Y = 5962328
69 meter
Z = 1476730
22 Z = 434728
16
XDOT = -14586
461847 XDOT = -4395
786007
YDOT = -6116
110686 feet/sec YDOT = -1913
628400 meter/sec
ZDOT = -19581
216592 ZDOT = -5989
829753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18025668
69 X = -5494223
82
Y = 12962492
14 feet Y = 3950967
61 meter
Z = 1406994
61 Z = 428851
96
XDOT = -9222
819427 XDOT = -2811
115361
YDOT = -10644
258093 feet/sec YDOT = -3244
369867 meter/sec
ZDOT = -19677
284706 ZDOT = -5997
636378
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
98386189
00016717 00000-0 10270-3 0 9145
2 25544 51
6412 301
1821 0004740 158
5912 201
5439 15
53822048 12165
Satellite: ISS
Catalog Number: 25544
Epoch time: 18255
98386189 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 301
1821 deg
Eccentricity:
0004740
Arg of perigee: 158
5912 deg
Mean anomaly: 201
5439 deg
Mean motion: 15
53822048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 304
Coasting Arc #16 (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 = 3694307
04 A = 6789505
00 meter
Y = -5574615
15 meter E =
0013330
Z = 1148650
39 I = 51
31678
XDOT = 3493
426655 Wp = 76
65232
YDOT = 3529
760069 meter/sec RA = 295
62806 deg
ZDOT = 5840
686497 TA = 295
87198
MA = 296
00936
Ha = 222
393 n
mi
Hp = 214
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12120429
91 X = 3750789
79
Y = -18289419
78 feet Y = -5532986
93 meter
Z = 3768538
02 Z = 1166733
83
XDOT = 11461
373539 XDOT = 3425
325119
YDOT = 11580
577653 feet/sec YDOT = 3568
445728 meter/sec
ZDOT = 19162
357273 ZDOT = 5857
490726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18830630
58 X = 5739576
20
Y = -11233514
07 feet Y = -3423975
09 meter
Z = 3850336
31 Z = 1173582
51
XDOT = 4369
782837 XDOT = 1331
909809
YDOT = 13978
432844 feet/sec YDOT = 4260
626331 meter/sec
ZDOT = 19237
269243 ZDOT = 5863
519665
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
01287098
00016717 00000-0 10270-3 0 9151
2 25544 51
6404 296
0538 0004480 162
2122 197
9188 15
53867847 12322
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
01287098 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 296
0538 deg
Eccentricity:
0004480
Arg of perigee: 162
2122 deg
Mean anomaly: 197
9188 deg
Mean motion: 15
53867847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1232
Checksum: 327
Coasting Arc #17 (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 = 1374050
69 A = 6782823
70 meter
Y = 5209606
96 meter E =
0011668
Z = 4109097
65 I = 51
28547
XDOT = -5102
717270 Wp = 100
11686
YDOT = 4321
204910 meter/sec RA = 292
91049 deg
ZDOT = -3765
088474 TA = 28
87801
MA = 28
81348
Ha = 222
335 n
mi
Hp = 214
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4508040
32 X = 1295733
34
Y = 17091886
34 feet Y = 5224534
97 meter
Z = 13481291
50 Z = 4115581
71
XDOT = -16741
198393 XDOT = -5132
370012
YDOT = 14177
181464 feet/sec YDOT = 4263
976688 meter/sec
ZDOT = -12352
652473 ZDOT = -3789
948218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -621351
32 X = -189387
88
Y = -17643745
26 feet Y = -5377813
56 meter
Z = 13509715
11 Z = 4117761
16
XDOT = 18041
309894 XDOT = 5498
991256
YDOT = -10197
340699 feet/sec YDOT = -3108
149445 meter/sec
ZDOT = -12464
676010 ZDOT = -3799
233248
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
52737515
00016717 00000-0 10270-3 0 9162
2 25544 51
6388 293
4886 0004733 164
1945 195
9356 15
53889024 12400
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
52737515 = yrday
fracday
Element set: 916
Inclination: 51
6388 deg
RA of node: 293
4886 deg
Eccentricity:
0004733
Arg of perigee: 164
1945 deg
Mean anomaly: 195
9356 deg
Mean motion: 15
53889024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1240
Checksum: 346
Coasting Arc #18 (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 = -3717249
74 A = 6778261
68 meter
Y = -2094801
20 meter E =
0016989
Z = -5281101
69 I = 51
26832
XDOT = 3252
396745 Wp = 108
69889
YDOT = -6916
069888 meter/sec RA = 292
47990 deg
ZDOT = 449
885648 TA = 165
64544
MA = 165
59712
Ha = 222
475 n
mi
Hp = 214
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12195701
25 X = -3667895
86
Y = -6872707
35 feet Y = -2136094
52 meter
Z = -17326449
10 Z = -5299038
87
XDOT = 10670
592995 XDOT = 3327
307112
YDOT = -22690
518005 feet/sec YDOT = -6879
280447 meter/sec
ZDOT = 1476
002781 ZDOT = 465
867244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13707334
94 X = 4177995
69
Y = 2300755
03 feet Y = 701270
13 meter
Z = -17406624
28 Z = -5305539
08
XDOT = -2040
153874 XDOT = -621
838901
YDOT = 23972
966918 feet/sec YDOT = 7306
960317 meter/sec
ZDOT = 1548
537658 ZDOT = 471
994278
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
59168853
00016717 00000-0 10270-3 0 9173
2 25544 51
6385 293
1686 0004750 163
5533 196
5774 15
53844435 12416
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
59168853 = yrday
fracday
Element set: 917
Inclination: 51
6385 deg
RA of node: 293
1686 deg
Eccentricity:
0004750
Arg of perigee: 163
5533 deg
Mean anomaly: 196
5774 deg
Mean motion: 15
53844435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 343
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