[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 27th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14601 2445 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
301/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
9
000/00:00:00
000 0
0 0
0 221
2
304/19:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
3
000/00:00:00
000 0
0 0
0 221
8
305/15:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
2
000/00:00:00
000 0
0 0
0 221
9
306/13:59:43
634 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 222
1
308/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
3
308/09:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
3
311/22:40:58
115 1
0 1
3 1
3
N/A 0
6 -0
0 226
0
000/00:05:52
230 0
6 0
0 223
7
312/03:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
0
000/00:00:00
000 0
0 0
0 223
6
Coasting Arc #1 (Orbit 3546)
---------------------------------------
Vector Time (GMT): 2019/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4303316
29 A = 6789324
13 meter
Y = -160203
91 meter E =
0005233
Z = 5245972
16 I = 51
99493
XDOT = -1150
055131 Wp = 152
00519
YDOT = -7486
193503 meter/sec RA = 74
29718 deg
ZDOT = -1176
037114 TA = 309
20018
MA = 309
24664
Ha = 228
457 n
mi
Hp = 220
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14118491
77 X = -4326687
43
Y = -525603
36 feet Y = -208456
94 meter
Z = 17211194
76 Z = 5225011
18
XDOT = -3773
146755 XDOT = -1060
544242
YDOT = -24561
002307 feet/sec YDOT = -7498
553825 meter/sec
ZDOT = -3858
389480 ZDOT = -1181
405816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12262220
44 X = 3737524
79
Y = -7247652
48 feet Y = -2209084
48 meter
Z = 17115571
19 Z = 5216826
10
XDOT = 15892
336245 XDOT = 4843
984087
YDOT = 17751
207628 feet/sec YDOT = 5410
568085 meter/sec
ZDOT = -3882
298261 ZDOT = -1183
324510
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 19298
54632874
00016717 00000-0 10270-3 0 9005
2 25544 51
6402 74
8919 0006900 187
3660 172
7390 15
50181118 35473
Satellite: ISS
Catalog Number: 25544
Epoch time: 19298
54632874 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 74
8919 deg
Eccentricity:
0006900
Arg of perigee: 187
3660 deg
Mean anomaly: 172
7390 deg
Mean motion: 15
50181118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3547
Checksum: 322
Coasting Arc #2 (Orbit 3561)
---------------------------------------
Vector Time (GMT): 2019/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4421620
09 A = 6789636
60 meter
Y = 306038
25 meter E =
0015160
Z = -5155857
47 I = 51
98725
XDOT = 1402
083825 Wp = 129
39759
YDOT = 7342
670483 meter/sec RA = 69
36339 deg
ZDOT = 1632
111279 TA = 156
34554
MA = 156
27577
Ha = 228
123 n
mi
Hp = 221
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14506627
60 X = 4442914
08
Y = 1004062
50 feet Y = 355602
63 meter
Z = -16915542
87 Z = -5134326
75
XDOT = 4600
012548 XDOT = 1311
943688
YDOT = 24090
126257 feet/sec YDOT = 7357
845683 meter/sec
ZDOT = 5354
695796 ZDOT = 1638
702768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12722403
03 X = -3877788
44
Y = 7273491
79 feet Y = 2216960
30 meter
Z = -16817334
95 Z = -5125923
69
XDOT = -16627
304092 XDOT = -5068
002287
YDOT = -16587
723221 feet/sec YDOT = -5055
938038 meter/sec
ZDOT = 5384
177725 ZDOT = 1641
097370
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 19299
51329462
00016717 00000-0 10270-3 0 9010
2 25544 51
6412 70
1004 0006921 192
0124 168
0862 15
50227754 35625
Satellite: ISS
Catalog Number: 25544
Epoch time: 19299
51329462 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 70
1004 deg
Eccentricity:
0006921
Arg of perigee: 192
0124 deg
Mean anomaly: 168
0862 deg
Mean motion: 15
50227754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3562
Checksum: 289
Coasting Arc #3 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2019/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4548036
09 A = 6790267
10 meter
Y = -407718
23 meter E =
0004678
Z = 5021695
05 I = 51
97755
XDOT = -1643
745475 Wp = 133
97403
YDOT = -7193
447138 meter/sec RA = 64
42827 deg
ZDOT = -2074
710859 TA = 336
11118
MA = 336
13289
Ha = 228
186 n
mi
Hp = 221
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14921378
26 X = -4567532
09
Y = -1337658
23 feet Y = -458686
30 meter
Z = 16475377
46 Z = 4999554
50
XDOT = -5392
865733 XDOT = -1553
106039
YDOT = -23600
548353 feet/sec YDOT = -7211
321983 meter/sec
ZDOT = -6806
794156 ZDOT = -2082
475198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13123843
29 X = 4000147
43
Y = -7451085
83 feet Y = -2271090
96 meter
Z = 16374400
10 Z = 4990917
15
XDOT = 17278
701100 XDOT = 5266
548095
YDOT = 15412
733529 feet/sec YDOT = 4697
801180 meter/sec
ZDOT = -6841
619244 ZDOT = -2085
325546
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 19300
54472559
00016717 00000-0 10270-3 0 9023
2 25544 51
6425 64
9884 0006824 195
0804 165
0144 15
50192044 35786
Satellite: ISS
Catalog Number: 25544
Epoch time: 19300
54472559 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 64
9884 deg
Eccentricity:
0006824
Arg of perigee: 195
0804 deg
Mean anomaly: 165
0144 deg
Mean motion: 15
50192044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3578
Checksum: 313
Coasting Arc #4 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2019/301/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3186924
32 A = 6800624
61 meter
Y = 5996218
59 meter E =
0007713
Z = 339282
93 I = 51
99757
XDOT = -4312
349656 Wp = 75
49226
YDOT = 1944
874885 meter/sec RA = 59
77247 deg
ZDOT = 6021
767040 TA = 288
13863
MA = 288
22261
Ha = 227
855 n
mi
Hp = 221
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10455788
44 X = 3117987
90
Y = 19672633
17 feet Y = 6031471
59 meter
Z = 1113132
97 Z = 354596
60
XDOT = -14148
128794 XDOT = -4363
028551
YDOT = 6380
823113 feet/sec YDOT = 1896
367999 meter/sec
ZDOT = 19756
453543 ZDOT = 6000
695496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15702367
89 X = -4786081
73
Y = -15799128
23 feet Y = -4815574
29 meter
Z = 1182481
40 Z = 360420
33
XDOT = 10665
684968 XDOT = 3250
900778
YDOT = -9102
910618 feet/sec YDOT = -2774
567156 meter/sec
ZDOT = 19660
155250 ZDOT = 5992
415320
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 19301
51168836
00016717 00000-0 10270-3 0 9032
2 25544 51
6422 60
1963 0006775 198
4695 161
6211 15
50230858 35939
Satellite: ISS
Catalog Number: 25544
Epoch time: 19301
51168836 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 60
1963 deg
Eccentricity:
0006775
Arg of perigee: 198
4695 deg
Mean anomaly: 161
6211 deg
Mean motion: 15
50230858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 315
Coasting Arc #5 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2019/302/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3380231
77 A = 6800408
25 meter
Y = -5840253
16 meter E =
0014665
Z = -766434
14 I = 51
97850
XDOT = 4450
947735 Wp = 163
97120
YDOT = -1797
042857 meter/sec RA = 54
84351 deg
ZDOT = -5977
533351 TA = 24
26517
MA = 24
19617
Ha = 227
688 n
mi
Hp = 221
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11089999
24 X = -3310950
11
Y = -19160935
58 feet Y = -5877665
93 meter
Z = -2514547
70 Z = -782686
19
XDOT = 14602
846901 XDOT = 4499
748375
YDOT = -5895
809899 feet/sec YDOT = -1746
996407 meter/sec
ZDOT = -19611
329891 ZDOT = -5955
793133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16409806
16 X = 5001708
92
Y = 14848303
42 feet Y = 4525762
88 meter
Z = -2588171
74 Z = -788874
74
XDOT = -11137
482701 XDOT = -3394
704727
YDOT = 8930
370191 feet/sec YDOT = 2721
976834 meter/sec
ZDOT = -19511
990755 ZDOT = -5947
254782
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 19302
47865224
00016717 00000-0 10270-3 0 9044
2 25544 51
6416 55
4049 0006725 202
8422 157
2431 15
50235865 36082
Satellite: ISS
Catalog Number: 25544
Epoch time: 19302
47865224 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 55
4049 deg
Eccentricity:
0006725
Arg of perigee: 202
8422 deg
Mean anomaly: 157
2431 deg
Mean motion: 15
50235865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 300
Coasting Arc #6 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2019/303/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3577541
81 A = 6800070
96 meter
Y = 5662451
07 meter E =
0008680
Z = 1162119
22 I = 51
95881
XDOT = -4598
321423 Wp = 81
94644
YDOT = 1689
605289 meter/sec RA = 49
91284 deg
ZDOT = 5886
737402 TA = 290
59004
MA = 290
68312
Ha = 227
572 n
mi
Hp = 221
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11737341
89 X = 3508311
66
Y = 18577595
36 feet Y = 5702070
55 meter
Z = 3812727
12 Z = 1179330
00
XDOT = -15086
356374 XDOT = -4645
468604
YDOT = 5543
324439 feet/sec YDOT = 1637
919900 meter/sec
ZDOT = 19313
442920 ZDOT = 5864
285381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17079021
38 X = -5205685
72
Y = -13805738
96 feet Y = -4207989
24 meter
Z = 3890723
92 Z = 1185892
65
XDOT = 11606
977530 XDOT = 3537
806751
YDOT = -8911
979104 feet/sec YDOT = -2716
371231 meter/sec
ZDOT = 19210
862796 ZDOT = 5855
470980
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 19303
51007870
00016717 00000-0 10270-3 0 9056
2 25544 51
6431 50
2939 0006773 206
4447 153
6358 15
50236882 36246
Satellite: ISS
Catalog Number: 25544
Epoch time: 19303
51007870 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 50
2939 deg
Eccentricity:
0006773
Arg of perigee: 206
4447 deg
Mean anomaly: 153
6358 deg
Mean motion: 15
50236882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 306
Coasting Arc #7 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2019/304/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3716822
38 A = 6799577
39 meter
Y = -5461434
86 meter E =
0012132
Z = -1578098
02 I = 51
93517
XDOT = 4789
623869 Wp = 172
38248
YDOT = -1598
118150 meter/sec RA = 44
98061 deg
ZDOT = -5766
820555 TA = 24
78162
MA = 24
72339
Ha = 227
385 n
mi
Hp = 221
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12194299
14 X = -3647809
08
Y = -17918093
38 feet Y = -5502613
06 meter
Z = -5177486
95 Z = -1595985
94
XDOT = 15713
989073 XDOT = 4835
151188
YDOT = -5243
169784 feet/sec YDOT = -1544
302444 meter/sec
ZDOT = -18920
014944 ZDOT = -5743
443279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17511754
03 X = 5337582
63
Y = 12737786
61 feet Y = 3882477
36 meter
Z = -5258577
39 Z = -1602814
39
XDOT = -12197
980815 XDOT = -3717
944552
YDOT = 9025
266795 feet/sec YDOT = 2750
901319 meter/sec
ZDOT = -18813
219307 ZDOT = -5734
269245
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 19304
47703949
00016717 00000-0 10270-3 0 9063
2 25544 51
6435 45
5024 0006654 210
3216 149
7551 15
50238101 36391
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
47703949 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 45
5024 deg
Eccentricity:
0006654
Arg of perigee: 210
3216 deg
Mean anomaly: 149
7551 deg
Mean motion: 15
50238101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 298
Coasting Arc #8 (Orbit 3644)
---------------------------------------
Vector Time (GMT): 2019/304/19:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5284386
80 A = 6793179
46 meter
Y = -387605
80 meter E =
0006824
Z = 4244042
67 I = 51
90208
XDOT = -2484
679591 Wp = 111
00614
YDOT = -6258
017454 meter/sec RA = 43
09776 deg
ZDOT = -3662
930935 TA = 16
39513
MA = 16
37307
Ha = 227
327 n
mi
Hp = 221
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17337227
05 X = -5300275
39
Y = -1271672
58 feet Y = -446788
54 meter
Z = 13924024
51 Z = 4218333
93
XDOT = -8151
835928 XDOT = -2396
723078
YDOT = -20531
553326 feet/sec YDOT = -6285
310963 meter/sec
ZDOT = -12017
489943 ZDOT = -3674
787441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15249772
31 X = -4648130
60
Y = -8537699
66 feet Y = -2602290
86 meter
Z = 13806780
24 Z = 4208306
62
XDOT = 768
278208 XDOT = 234
171198
YDOT = -20905
552913 feet/sec YDOT = -6372
012528 meter/sec
ZDOT = -12070
985568 ZDOT = -3679
236401
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 19304
86382237
00016717 00000-0 10270-3 0 9070
2 25544 51
6408 43
5896 0006211 213
7948 146
2807 15
50237831 36456
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
86382237 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 43
5896 deg
Eccentricity:
0006211
Arg of perigee: 213
7948 deg
Mean anomaly: 146
2807 deg
Mean motion: 15
50237831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3645
Checksum: 320
Coasting Arc #9 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2019/305/15:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5816943
77 A = 6796523
02 meter
Y = -1521223
32 meter E =
0011110
Z = 3153652
67 I = 51
89428
XDOT = -1121
748684 Wp = 123
55380
YDOT = -5815
184517 meter/sec RA = 38
94541 deg
ZDOT = -4867
794632 TA = 20
26768
MA = 20
22361
Ha = 227
203 n
mi
Hp = 221
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19084461
20 X = -5814819
66
Y = -4990890
14 feet Y = -1586260
73 meter
Z = 10346629
48 Z = 3125400
71
XDOT = -3680
277834 XDOT = -1032
992751
YDOT = -19078
689361 feet/sec YDOT = -5827
232244 meter/sec
ZDOT = -15970
454828 ZDOT = -4873
028423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2102215
39 X = 640755
25
Y = -19681303
66 feet Y = -5998861
35 meter
Z = 10217894
20 Z = 3114414
15
XDOT = 16906
183589 XDOT = 5153
004758
YDOT = -6508
593492 feet/sec YDOT = -1983
819296 meter/sec
ZDOT = -15993
771075 ZDOT = -4874
901424
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 19305
70185324
00016717 00000-0 10270-3 0 9083
2 25544 51
6428 39
4368 0006244 216
1894 143
8835 15
50252696 36583
Satellite: ISS
Catalog Number: 25544
Epoch time: 19305
70185324 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 39
4368 deg
Eccentricity:
0006244
Arg of perigee: 216
1894 deg
Mean anomaly: 143
8835 deg
Mean motion: 15
50252696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 330
Coasting Arc #10 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2019/306/13:59:43
634
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -607078
59 A = 6791441
34 meter
Y = -4880997
35 meter E =
0006138
Z = -4687520
87 I = 51
85239
XDOT = 6823
763387 Wp = 103
64276
YDOT = 1925
081208 meter/sec RA = 34
44601 deg
ZDOT = -2892
871012 TA = 137
67089
MA = 137
62351
Ha = 227
076 n
mi
Hp = 222
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1991727
67 X = -529683
03
Y = -16013770
83 feet Y = -4887353
22 meter
Z = -15379005
49 Z = -4690282
07
XDOT = 22387
675155 XDOT = 6815
781585
YDOT = 6315
883229 feet/sec YDOT = 2001
344821 meter/sec
ZDOT = -9491
046627 ZDOT = -2859
742543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15732186
58 X = 4795170
47
Y = 3540226
23 feet Y = 1079060
95 meter
Z = -15391125
65 Z = -4691215
10
XDOT = -13157
782637 XDOT = -4010
492148
YDOT = 17930
349842 feet/sec YDOT = 5465
170632 meter/sec
ZDOT = -9340
109317 ZDOT = -2846
865320
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 19306
60434842
00016717 00000-0 10270-3 0 9096
2 25544 51
6425 34
9638 0006487 219
1963 140
8718 15
50217295 36728
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
60434842 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 34
9638 deg
Eccentricity:
0006487
Arg of perigee: 219
1963 deg
Mean anomaly: 140
8718 deg
Mean motion: 15
50217295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 328
Coasting Arc #11 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2019/307/13:59:43
634
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 550424
21 A = 6790644
63 meter
Y = 4706964
68 meter E =
0008313
Z = 4865331
46 I = 51
82218
XDOT = -7035
990376 Wp = 168
59714
YDOT = -1744
799015 meter/sec RA = 29
50208 deg
ZDOT = 2475
334198 TA = 257
08380
MA = 257
17667
Ha = 226
807 n
mi
Hp = 222
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1805853
70 X = 474115
28
Y = 15442797
51 feet Y = 4712693
12 meter
Z = 15962373
55 Z = 4867820
03
XDOT = -23083
957925 XDOT = -7027
980544
YDOT = -5724
406217 feet/sec YDOT = -1823
435705 meter/sec
ZDOT = 8121
175189 ZDOT = 2441
174976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15189091
23 X = -4629635
01
Y = -3268773
78 feet Y = -996322
25 meter
Z = 15973261
96 Z = 4868650
25
XDOT = 12503
420853 XDOT = 3811
042676
YDOT = -19036
593883 feet/sec YDOT = -5802
353816 meter/sec
ZDOT = 7965
524924 ZDOT = 2427
891997
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 19307
63576741
00016717 00000-0 10270-3 0 9107
2 25544 51
6429 29
8523 0006418 223
9735 136
0905 15
50243944 36884
Satellite: ISS
Catalog Number: 25544
Epoch time: 19307
63576741 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 29
8523 deg
Eccentricity:
0006418
Arg of perigee: 223
9735 deg
Mean anomaly: 136
0905 deg
Mean motion: 15
50243944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 325
Coasting Arc #12 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1192776
89 A = 6791134
45 meter
Y = 4724420
69 meter E =
0008430
Z = 4731970
02 I = 51
80136
XDOT = -7065
323012 Wp = 163
53072
YDOT = -1010
888664 meter/sec RA = 25
99801 deg
ZDOT = 2781
118526 TA = 258
90575
MA = 259
00056
Ha = 226
731 n
mi
Hp = 222
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3913310
00 X = 1116872
85
Y = 15500067
89 feet Y = 4737334
68 meter
Z = 15524836
01 Z = 4737579
87
XDOT = -23180
193609 XDOT = -7067
003134
YDOT = -3316
563857 feet/sec YDOT = -1089
907537 meter/sec
ZDOT = 9124
404612 ZDOT = 2746
793343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5157094
00 X = 1571882
25
Y = -15105953
46 feet Y = -4604294
62 meter
Z = 15549957
70 Z = 4739627
11
XDOT = 16677
312206 XDOT = 5083
244760
YDOT = 14955
743740 feet/sec YDOT = 4558
510692 meter/sec
ZDOT = 8967
930442 ZDOT = 2733
425199
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 19308
34486785
00016717 00000-0 10270-3 0 9115
2 25544 51
6412 26
3346 0006439 225
3487 134
7140 15
50255605 36999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
34486785 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 26
3346 deg
Eccentricity:
0006439
Arg of perigee: 225
3487 deg
Mean anomaly: 134
7140 deg
Mean motion: 15
50255605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 318
Coasting Arc #13 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4659195
92 A = 6798142
26 meter
Y = -4320605
77 meter E =
0008314
Z = -2401801
07 I = 51
82423
XDOT = 4932
410040 Wp = 183
03145
YDOT = -2331
531751 meter/sec RA = 25
55188 deg
ZDOT = -5381
301529 TA = 23
69743
MA = 23
65916
Ha = 226
744 n
mi
Hp = 222
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15286075
85 X = -4598868
62
Y = -14175215
78 feet Y = -4372370
84 meter
Z = -7879924
76 Z = -2424287
50
XDOT = 16182
447637 XDOT = 4984
254989
YDOT = -7649
382385 feet/sec YDOT = -2276
084088 meter/sec
ZDOT = -17655
188744 ZDOT = -5357
215572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15216645
53 X = 4638033
56
Y = 14192757
26 feet Y = 4325952
41 meter
Z = -7982068
14 Z = -2432934
37
XDOT = -15274
861864 XDOT = -4655
777896
YDOT = 6522
561767 feet/sec YDOT = 1988
076826 meter/sec
ZDOT = -17545
090200 ZDOT = -5347
743493
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 19308
40933190
00016717 00000-0 10270-3 0 9120
2 25544 51
6435 26
0156 0006469 224
8506 135
2122 15
50244754 37001
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
40933190 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 26
0156 deg
Eccentricity:
0006469
Arg of perigee: 224
8506 deg
Mean anomaly: 135
2122 deg
Mean motion: 15
50244754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 285
Coasting Arc #14 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4679500
34 A = 6797296
65 meter
Y = 4081497
98 meter E =
0008592
Z = 2760692
10 I = 51
79117
XDOT = -5138
663522 Wp = 102
46377
YDOT = 2398
165867 meter/sec RA = 20
60928 deg
ZDOT = 5149
401296 TA = 288
66907
MA = 288
76232
Ha = 226
614 n
mi
Hp = 222
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15352691
41 X = 4620101
99
Y = 13390741
39 feet Y = 4133495
32 meter
Z = 9057388
78 Z = 2783279
36
XDOT = -16859
132289 XDOT = -5190
111810
YDOT = 7867
998252 feet/sec YDOT = 2340
414018 meter/sec
ZDOT = 16894
361208 ZDOT = 5124
314359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15504570
62 X = -4725793
12
Y = -13143664
90 feet Y = -4006189
06 meter
Z = 9160007
79 Z = 2791970
38
XDOT = 15885
602330 XDOT = 4841
931590
YDOT = -7010
325708 feet/sec YDOT = -2136
747276 meter/sec
ZDOT = 16779
695684 ZDOT = 5114
451244
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 19309
44074739
00016717 00000-0 10270-3 0 9131
2 25544 51
6437 20
9046 0006458 228
2929 131
7669 15
50265174 37162
Satellite: ISS
Catalog Number: 25544
Epoch time: 19309
44074739 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 20
9046 deg
Eccentricity:
0006458
Arg of perigee: 228
2929 deg
Mean anomaly: 131
7669 deg
Mean motion: 15
50265174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 327
Coasting Arc #15 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4641612
51 A = 6796459
98 meter
Y = -3855946
76 meter E =
0005041
Z = -3120570
80 I = 51
75654
XDOT = 5352
036194 Wp = 187
52108
YDOT = -2495
089091 meter/sec RA = 15
66448 deg
ZDOT = -4881
661687 TA = 28
27281
MA = 28
24545
Ha = 226
429 n
mi
Hp = 222
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15228387
50 X = -4582991
02
Y = -12650743
95 feet Y = -3907524
80 meter
Z = -10238093
17 Z = -3142975
89
XDOT = 17559
173865 XDOT = 5403
251937
YDOT = -8185
987830 feet/sec YDOT = -2434
952515 meter/sec
ZDOT = -16015
950417 ZDOT = -4855
538753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15571542
17 X = 4746206
05
Y = 12139905
49 feet Y = 3700243
19 meter
Z = -10339895
03 Z = -3151600
01
XDOT = -16499
404954 XDOT = -5029
018630
YDOT = 7634
834302 feet/sec YDOT = 2327
097495 meter/sec
ZDOT = -15896
557693 ZDOT = -4845
270785
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 19310
40770070
00016717 00000-0 10270-3 0 9141
2 25544 51
6437 16
1135 0006480 232
2351 127
8213 15
50240808 37312
Satellite: ISS
Catalog Number: 25544
Epoch time: 19310
40770070 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 16
1135 deg
Eccentricity:
0006480
Arg of perigee: 232
2351 deg
Mean anomaly: 127
8213 deg
Mean motion: 15
50240808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 267
Coasting Arc #16 (Orbit 3746)
---------------------------------------
Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4590905
96 A = 6795465
98 meter
Y = 3635694
13 meter E =
0007899
Z = 3445104
49 I = 51
72193
XDOT = -5539
028783 Wp = 118
47336
YDOT = 2636
191914 meter/sec RA = 10
71616 deg
ZDOT = 4587
533651 TA = 281
76105
MA = 281
84965
Ha = 226
250 n
mi
Hp = 222
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15062027
42 X = 4533174
70
Y = 11928130
35 feet Y = 3686710
15 meter
Z = 11302836
24 Z = 3467265
45
XDOT = -18172
666612 XDOT = -5590
379809
YDOT = 8648
923603 feet/sec YDOT = 2573
963539 meter/sec
ZDOT = 15050
963422 ZDOT = 4560
501942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15568273
33 X = -4745209
71
Y = -11157386
54 feet Y = -3400771
42 meter
Z = 11403537
24 Z = 3475798
15
XDOT = 17000
452225 XDOT = 5181
737838
YDOT = -8425
731241 feet/sec YDOT = -2568
162882 meter/sec
ZDOT = 14927
421478 ZDOT = 4549
878066
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 19311
43911320
00016717 00000-0 10270-3 0 9151
2 25544 51
6446 11
0021 0006455 236
2921 123
7615 15
50272921 37478
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
43911320 = yrday
fracday
Element set: 915
Inclination: 51
6446 deg
RA of node: 11
0021 deg
Eccentricity:
0006455
Arg of perigee: 236
2921 deg
Mean anomaly: 123
7615 deg
Mean motion: 15
50272921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3747
Checksum: 273
Coasting Arc #17 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/311/22:43:54
230
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5300298
66 A = 6795793
03 meter
Y = -2180112
62 meter E =
0003053
Z = -3653851
02 I = 51
70200
XDOT = 4723
988628 Wp = 197
26482
YDOT = 4142
575986 meter/sec RA = 7
87120 deg
ZDOT = 4377
145036 TA = 119
49995
MA = 119
46950
Ha = 225
966 n
mi
Hp = 223
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17389431
29 X = 5342032
06
Y = -7152600
46 feet Y = -2120607
66 meter
Z = -11987700
20 Z = -3628002
30
XDOT = 15498
650355 XDOT = 4656
051934
YDOT = 13591
128564 feet/sec YDOT = 4195
023195 meter/sec
ZDOT = 14360
712062 ZDOT = 4399
927705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12336855
84 X = 3760273
66
Y = -14288857
21 feet Y = -4355243
68 meter
Z = -11869604
77 Z = -3617855
53
XDOT = 18844
728836 XDOT = 5743
873349
YDOT = 4244
676280 feet/sec YDOT = 1293
777330 meter/sec
ZDOT = 14464
191605 ZDOT = 4408
685601
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 19311
95482037
00016717 00000-0 10270-3 0 9167
2 25544 51
6450 8
4505 0006631 250
9973 109
0459 15
50015593 37558
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
95482037 = yrday
fracday
Element set: 916
Inclination: 51
6450 deg
RA of node: 8
4505 deg
Eccentricity:
0006631
Arg of perigee: 250
9973 deg
Mean anomaly: 109
0459 deg
Mean motion: 15
50015593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 309
Coasting Arc #18 (Orbit 3757)
---------------------------------------
Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1913317
76 A = 6790816
73 meter
Y = -4204148
60 meter E =
0005946
Z = -4983344
05 I = 51
67539
XDOT = 7310
171501 Wp = 78
25540
YDOT = -799
559945 meter/sec RA = 7
01313 deg
ZDOT = -2133
122138 TA = 170
94971
MA = 170
93898
Ha = 225
964 n
mi
Hp = 223
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6277289
24 X = -1841956
79
Y = -13793138
47 feet Y = -4225145
78 meter
Z = -16349553
95 Z = -4992464
98
XDOT = 23983
502300 XDOT = 7328
930812
YDOT = -2623
228166 feet/sec YDOT = -717
707598 meter/sec
ZDOT = -6998
432210 ZDOT = -2097
565850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13526325
85 X = -4122824
12
Y = 6733911
96 feet Y = 2052496
37 meter
Z = -16390725
49 Z = -4995893
13
XDOT = -3127
577137 XDOT = -953
285511
YDOT = -22914
263747 feet/sec YDOT = -6984
267590 meter/sec
ZDOT = -6836
208735 ZDOT = -2083
676422
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 19312
14823929
00016717 00000-0 10270-3 0 9179
2 25544 51
6409 7
4896 0006672 251
0571 108
9856 15
50006660 37582
Satellite: ISS
Catalog Number: 25544
Epoch time: 19312
14823929 = yrday
fracday
Element set: 917
Inclination: 51
6409 deg
RA of node: 7
4896 deg
Eccentricity:
0006672
Arg of perigee: 251
0571 deg
Mean anomaly: 108
9856 deg
Mean motion: 15
50006660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3758
Checksum: 325
Coasting Arc #19 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1857040
55 A = 6790487
54 meter
Y = 4097503
91 meter E =
0005139
Z = 5089549
03 I = 51
64006
XDOT = -7364
896213 Wp = 203
59836
YDOT = 1135
975158 meter/sec RA = 2
05904 deg
ZDOT = 1768
719961 TA = 229
25119
MA = 229
29582
Ha = 225
768 n
mi
Hp = 223
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6092652
72 X = 1786360
31
Y = 13443254
29 feet Y = 4117875
55 meter
Z = 16697995
51 Z = 5098398
28
XDOT = -24163
045317 XDOT = -7385
643284
YDOT = 3726
952617 feet/sec YDOT = 1053
499717 meter/sec
ZDOT = 5802
887012 ZDOT = 1732
892873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13070204
90 X = 3983798
45
Y = -6758392
78 feet Y = -2059958
12 meter
Z = 16737933
80 Z = 5101722
22
XDOT = 4648
191509 XDOT = 1416
768772
YDOT = 22988
154287 feet/sec YDOT = 7006
789427 meter/sec
ZDOT = 5639
409921 ZDOT = 1718
892144
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 19313
17981351
00016717 00000-0 10270-3 0 9188
2 25544 51
6404 2
3792 0006614 255
1704 104
8714 15
49963270 37748
Satellite: ISS
Catalog Number: 25544
Epoch time: 19313
17981351 = yrday
fracday
Element set: 918
Inclination: 51
6404 deg
RA of node: 2
3792 deg
Eccentricity:
0006614
Arg of perigee: 255
1704 deg
Mean anomaly: 104
8714 deg
Mean motion: 15
49963270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 310
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