[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 18th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16550 5887 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
281/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 218
7
284/20:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 219
1
289/19:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 219
5
292/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 220
1
Coasting Arc #1 (Orbit 3268)
---------------------------------------
Vector Time (GMT): 2019/280/13:28:14
231
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6573236
01 A = 6800717
94 meter
Y = 1675407
57 meter E =
0016074
Z = 429561
57 I = 51
77145
XDOT = -793
829522 Wp = 74
70864
YDOT = -4699
028648 meter/sec RA = 162
84144 deg
ZDOT = 5997
080370 TA = 289
90590
MA = 290
07902
Ha = 229
584 n
mi
Hp = 218
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21565734
93 X = -6593568
94
Y = 5496744
01 feet Y = 1601787
34 meter
Z = 1409322
74 Z = 397581
67
XDOT = -2604
427564 XDOT = -770
355221
YDOT = -15416
760657 feet/sec YDOT = -4707
774271 meter/sec
ZDOT = 19675
460532 ZDOT = 5993
281469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13899626
28 X = 4236606
09
Y = -17392101
91 feet Y = -5301112
66 meter
Z = 1263522
28 Z = 385121
59
XDOT = 10208
890042 XDOT = 3111
669685
YDOT = 9635
699089 feet/sec YDOT = 2936
961082 meter/sec
ZDOT = 19658
367979 ZDOT = 5991
870560
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 19280
62500140
00016717 00000-0 10270-3 0 9005
2 25544 51
6419 163
7081 0007023 124
4880 235
6935 15
50197240 32690
Satellite: ISS
Catalog Number: 25544
Epoch time: 19280
62500140 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 163
7081 deg
Eccentricity:
0007023
Arg of perigee: 124
4880 deg
Mean anomaly: 235
6935 deg
Mean motion: 15
50197240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3269
Checksum: 289
Coasting Arc #2 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2019/281/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 866641
76 A = 6788960
41 meter
Y = 4159312
68 meter E =
0020972
Z = -5313194
49 I = 51
76155
XDOT = -7255
930348 Wp = 105
33111
YDOT = 2327
718784 meter/sec RA = 158
44632 deg
ZDOT = 635
373978 TA = 170
76094
MA = 170
72230
Ha = 229
577 n
mi
Hp = 218
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2843312
87 X = 845875
35
Y = 13646038
98 feet Y = 4168887
65 meter
Z = -17431740
45 Z = -5309035
34
XDOT = -23805
545761 XDOT = -7284
506604
YDOT = 7636
872652 feet/sec YDOT = 2246
418109 meter/sec
ZDOT = 2084
560295 ZDOT = 600
057721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2276128
51 X = -693763
97
Y = -13775766
79 feet Y = -4198853
72 meter
Z = -17412979
97 Z = -5307476
29
XDOT = 23165
981926 XDOT = 7060
991291
YDOT = -6272
731664 feet/sec YDOT = -1911
928611 meter/sec
ZDOT = 1923
507837 ZDOT = 586
285189
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 19281
46306287
00016717 00000-0 10270-3 0 9015
2 25544 51
6432 159
5552 0007056 126
7711 233
4089 15
50193012 32829
Satellite: ISS
Catalog Number: 25544
Epoch time: 19281
46306287 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 159
5552 deg
Eccentricity:
0007056
Arg of perigee: 126
7711 deg
Mean anomaly: 233
4089 deg
Mean motion: 15
50193012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3282
Checksum: 298
Coasting Arc #3 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2019/282/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -749434
92 A = 6789081
83 meter
Y = -4237861
59 meter E =
0008772
Z = 5243115
26 I = 51
79297
XDOT = 7132
094539 Wp = 107
23859
YDOT = -2602
081296 meter/sec RA = 153
49827 deg
ZDOT = -1084
789574 TA = 353
12588
MA = 353
13790
Ha = 229
500 n
mi
Hp = 218
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2458776
00 X = -727458
49
Y = -13903745
39 feet Y = -4246119
04 meter
Z = 17201821
73 Z = 5239528
46
XDOT = 23399
260299 XDOT = 7165
931024
YDOT = -8537
012127 feet/sec YDOT = -2522
136070 meter/sec
ZDOT = -3559
020912 ZDOT = -1050
062001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2118451
07 X = 645703
89
Y = 13979528
02 feet Y = 4260960
14 meter
Z = 17185672
74 Z = 5238193
05
XDOT = -22670
129610 XDOT = -6909
855505
YDOT = 7611
755344 feet/sec YDOT = 2320
063029 meter/sec
ZDOT = -3400
619087 ZDOT = -1036
508698
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 19282
49451613
00016717 00000-0 10270-3 0 9024
2 25544 51
6432 154
4443 0006957 130
5924 229
5833 15
50225910 32983
Satellite: ISS
Catalog Number: 25544
Epoch time: 19282
49451613 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 154
4443 deg
Eccentricity:
0006957
Arg of perigee: 130
5924 deg
Mean anomaly: 229
5833 deg
Mean motion: 15
50225910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3298
Checksum: 311
Coasting Arc #4 (Orbit 3312)
---------------------------------------
Vector Time (GMT): 2019/283/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 645095
95 A = 6789557
04 meter
Y = 4372150
53 meter E =
0019936
Z = -5171897
22 I = 51
82304
XDOT = -6936
275878 Wp = 112
52111
YDOT = 2833
823344 meter/sec RA = 148
55231 deg
ZDOT = 1527
730696 TA = 172
21711
MA = 172
18613
Ha = 229
453 n
mi
Hp = 218
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2116456
54 X = 621279
74
Y = 14344325
88 feet Y = 4379230
83 meter
Z = -16968166
73 Z = -5168821
79
XDOT = -22756
810625 XDOT = -6974
869914
YDOT = 9297
320684 feet/sec YDOT = 2756
041351 meter/sec
ZDOT = 5012
239815 ZDOT = 1493
942651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2007919
94 X = -612014
00
Y = -14376224
47 feet Y = -4381873
22 meter
Z = -16954355
87 Z = -5167687
67
XDOT = 21883
354378 XDOT = 6670
046414
YDOT = -8796
281479 feet/sec YDOT = -2681
106595 meter/sec
ZDOT = 4858
091793 ZDOT = 1480
746378
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 19283
46150411
00016717 00000-0 10270-3 0 9035
2 25544 51
6426 149
6529 0006977 133
8045 226
3684 15
50198738 33133
Satellite: ISS
Catalog Number: 25544
Epoch time: 19283
46150411 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 149
6529 deg
Eccentricity:
0006977
Arg of perigee: 133
8045 deg
Mean anomaly: 226
3684 deg
Mean motion: 15
50198738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3313
Checksum: 322
Coasting Arc #5 (Orbit 3328)
---------------------------------------
Vector Time (GMT): 2019/284/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -566525
92 A = 6789922
91 meter
Y = -4502291
71 meter E =
0009464
Z = 5042309
89 I = 51
85277
XDOT = 6752
767216 Wp = 102
12070
YDOT = -3055
984803 meter/sec RA = 143
60874 deg
ZDOT = -1968
814987 TA = 6
93864
MA = 6
92554
Ha = 229
335 n
mi
Hp = 218
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1858680
83 X = -540630
88
Y = -14771298
25 feet Y = -4508481
73 meter
Z = 16543011
46 Z = 5039621
22
XDOT = 22154
748084 XDOT = 6796
001754
YDOT = -10026
196861 feet/sec YDOT = -2980
229042 meter/sec
ZDOT = -6459
366755 ZDOT = -1935
906934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1994993
35 X = 608073
97
Y = 14766994
15 feet Y = 4500979
82 meter
Z = 16530972
75 Z = 5038640
49
XDOT = -21104
129155 XDOT = -6432
538567
YDOT = 9918
323280 feet/sec YDOT = 3023
104936 meter/sec
ZDOT = -6309
203076 ZDOT = -1923
045098
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 19284
49295295
00016717 00000-0 10270-3 0 9040
2 25544 51
6428 144
5420 0006840 138
5667 221
6004 15
50235607 33298
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
49295295 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 144
5420 deg
Eccentricity:
0006840
Arg of perigee: 138
5667 deg
Mean anomaly: 221
6004 deg
Mean motion: 15
50235607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3329
Checksum: 312
Coasting Arc #6 (Orbit 3334)
---------------------------------------
Vector Time (GMT): 2019/284/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3774885
37 A = 6789569
87 meter
Y = 2220646
83 meter E =
0018169
Z = -5202950
87 I = 51
86131
XDOT = -5146
119725 Wp = 100
27591
YDOT = 5483
488084 meter/sec RA = 141
59117 deg
ZDOT = -1400
584242 TA = 156
30427
MA = 156
22050
Ha = 229
461 n
mi
Hp = 219
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12384794
51 X = 3775046
25
Y = 7285586
72 feet Y = 2262860
66 meter
Z = -17070048
79 Z = -5184613
50
XDOT = -16883
594899 XDOT = -5200
251865
YDOT = 17990
446471 feet/sec YDOT = 5425
637731 meter/sec
ZDOT = -4595
092658 ZDOT = -1425
714476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7018463
56 X = 2139227
69
Y = 12650983
42 feet Y = 3856019
75 meter
Z = -16986561
22 Z = -5177503
86
XDOT = -22758
225115 XDOT = -6936
707015
YDOT = 6334
046640 feet/sec YDOT = 1930
617416 meter/sec
ZDOT = -4709
924150 ZDOT = -1435
584881
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 19284
87974684
00016717 00000-0 10270-3 0 9059
2 25544 51
6422 142
6217 0007206 142
7062 217
4590 15
50176077 33353
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
87974684 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 142
6217 deg
Eccentricity:
0007206
Arg of perigee: 142
7062 deg
Mean anomaly: 217
4590 deg
Mean motion: 15
50176077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3335
Checksum: 316
Coasting Arc #7 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2019/285/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3629924
13 A = 6789064
37 meter
Y = -2257865
17 meter E =
0010577
Z = 5269172
90 I = 51
88596
XDOT = 4984
656138 Wp = 137
93600
YDOT = -5744
968924 meter/sec RA = 136
64946 deg
ZDOT = 963
404952 TA = 302
82287
MA = 302
92467
Ha = 229
436 n
mi
Hp = 219
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11909199
91 X = -3630001
38
Y = -7407694
12 feet Y = -2298457
46 meter
Z = 17287312
67 Z = 5251539
84
XDOT = 16353
858721 XDOT = 5043
847813
YDOT = -18848
323241 feet/sec YDOT = -5688
895924 meter/sec
ZDOT = 3160
777400 ZDOT = 987
763265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6762849
68 X = -2061316
58
Y = -12399030
96 feet Y = -3779224
64 meter
Z = 17207034
89 Z = 5244704
23
XDOT = 22629
756858 XDOT = 6897
549890
YDOT = -7761
957730 feet/sec YDOT = -2365
844716 meter/sec
ZDOT = 3272
119679 ZDOT = 997
342078
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 19285
91119073
00016717 00000-0 10270-3 0 9069
2 25544 51
6426 137
5104 0007163 145
5085 214
6532 15
50225594 33515
Satellite: ISS
Catalog Number: 25544
Epoch time: 19285
91119073 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 137
5104 deg
Eccentricity:
0007163
Arg of perigee: 145
5085 deg
Mean anomaly: 214
6532 deg
Mean motion: 15
50225594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 298
Coasting Arc #8 (Orbit 3365)
---------------------------------------
Vector Time (GMT): 2019/286/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3491781
50 A = 6788967
51 meter
Y = 2367281
05 meter E =
0019022
Z = -5334609
28 I = 51
90712
XDOT = -4781
481764 Wp = 105
63417
YDOT = 5949
394287 meter/sec RA = 131
70903 deg
ZDOT = -496
086987 TA = 159
67660
MA = 159
60079
Ha = 229
306 n
mi
Hp = 219
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11455976
05 X = 3490963
46
Y = 7766670
12 feet Y = 2406323
56 meter
Z = -17501998
94 Z = -5317649
37
XDOT = -15687
276127 XDOT = -4845
244480
YDOT = 19519
010129 feet/sec YDOT = 5895
567817 meter/sec
ZDOT = -1627
581978 ZDOT = -519
469516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6406354
56 X = 1952656
87
Y = 12378031
88 feet Y = 3772824
12 meter
Z = -17424794
60 Z = -5311077
39
XDOT = -22233
512815 XDOT = -6776
774706
YDOT = 9095
385254 feet/sec YDOT = 2772
273425 meter/sec
ZDOT = -1734
504736 ZDOT = -528
677043
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 19286
87816906
00016717 00000-0 10270-3 0 9075
2 25544 51
6410 132
7189 0007100 148
7680 211
3893 15
50181801 33667
Satellite: ISS
Catalog Number: 25544
Epoch time: 19286
87816906 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 132
7189 deg
Eccentricity:
0007100
Arg of perigee: 148
7680 deg
Mean anomaly: 211
3893 deg
Mean motion: 15
50181801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3366
Checksum: 316
Coasting Arc #9 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2019/287/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3383773
84 A = 6788720
82 meter
Y = -2461082
05 meter E =
0008619
Z = 5341184
97 I = 51
92828
XDOT = 4561
595628 Wp = 139
04267
YDOT = -6162
049081 meter/sec RA = 126
77021 deg
ZDOT = 44
189425 TA = 310
50031
MA = 310
57539
Ha = 229
283 n
mi
Hp = 219
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11101620
21 X = -3381946
95
Y = -8074416
16 feet Y = -2498911
16 meter
Z = 17523572
72 Z = 5324752
10
XDOT = 14965
864920 XDOT = 4629
947766
YDOT = -20216
696459 feet/sec YDOT = -6110
655914 meter/sec
ZDOT = 144
978428 ZDOT = 66
514969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6161497
87 X = -1878024
55
Y = -12373112
34 feet Y = -3771324
64 meter
Z = 17448776
57 Z = 5318387
10
XDOT = 21761
936640 XDOT = 6633
038288
YDOT = -10458
766889 feet/sec YDOT = -3187
832148 meter/sec
ZDOT = 247
114215 ZDOT = 75
320413
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 19287
90960833
00016717 00000-0 10270-3 0 9080
2 25544 51
6411 127
6077 0007118 152
8392 207
3132 15
50229831 33827
Satellite: ISS
Catalog Number: 25544
Epoch time: 19287
90960833 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 127
6077 deg
Eccentricity:
0007118
Arg of perigee: 152
8392 deg
Mean anomaly: 207
3132 deg
Mean motion: 15
50229831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 311
Coasting Arc #10 (Orbit 3396)
---------------------------------------
Vector Time (GMT): 2019/288/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3296944
58 A = 6788904
69 meter
Y = 2617272
86 meter E =
0019029
Z = -5341895
78 I = 51
94704
XDOT = -4307
091724 Wp = 112
45390
YDOT = 6306
319858 meter/sec RA = 121
83163 deg
ZDOT = 425
667310 TA = 161
63328
MA = 161
56448
Ha = 229
124 n
mi
Hp = 219
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10816747
30 X = 3293381
08
Y = 8586853
23 feet Y = 2654121
38 meter
Z = -17525904
78 Z = -5325888
85
XDOT = -14130
878359 XDOT = -4379
358417
YDOT = 20690
025781 feet/sec YDOT = 6257
750875 meter/sec
ZDOT = 1396
546294 ZDOT = 404
568627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5888099
63 X = 1794692
77
Y = 12594219
46 feet Y = 3838718
09 meter
Z = -17453060
70 Z = -5319692
90
XDOT = -21032
339688 XDOT = -6410
657137
YDOT = 11661
331345 feet/sec YDOT = 3554
373794 meter/sec
ZDOT = 1299
973572 ZDOT = 396
231945
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 19288
87658115
00016717 00000-0 10270-3 0 9095
2 25544 51
6406 122
8153 0007011 155
7641 204
3840 15
50190548 33975
Satellite: ISS
Catalog Number: 25544
Epoch time: 19288
87658115 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 122
8153 deg
Eccentricity:
0007011
Arg of perigee: 155
7641 deg
Mean anomaly: 204
3840 deg
Mean motion: 15
50190548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3397
Checksum: 314
Coasting Arc #11 (Orbit 3411)
---------------------------------------
Vector Time (GMT): 2019/289/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2234403
76 A = 6800189
32 meter
Y = -6308517
57 meter E =
0019862
Z = 1139579
92 I = 52
00154
XDOT = 4852
824590 Wp = 134
66648
YDOT = 643
530908 meter/sec RA = 117
14811 deg
ZDOT = -5903
197370 TA = 33
03452
MA = 32
91059
Ha = 229
086 n
mi
Hp = 219
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7330720
98 X = 2299245
77
Y = -20697236
11 feet Y = -6283168
29 meter
Z = 3738779
28 Z = 1150591
85
XDOT = 15921
340520 XDOT = 4873
942992
YDOT = 2111
321878 feet/sec YDOT = 697
916464 meter/sec
ZDOT = -19367
445438 ZDOT = -5879
572267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19737392
23 X = 6015957
15
Y = -9600495
01 feet Y = -2926230
88 meter
Z = 3789375
50 Z = 1155001
65
XDOT = 9242
987672 XDOT = 2817
262643
YDOT = 11337
363670 feet/sec YDOT = 3455
628447 meter/sec
ZDOT = -19259
742339 ZDOT = -5870
369465
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 19289
84355005
00016717 00000-0 10270-3 0 9107
2 25544 51
6414 118
0229 0007113 158
2342 201
9112 15
50209461 34122
Satellite: ISS
Catalog Number: 25544
Epoch time: 19289
84355005 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 118
0229 deg
Eccentricity:
0007113
Arg of perigee: 158
2342 deg
Mean anomaly: 201
9112 deg
Mean motion: 15
50209461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 273
Coasting Arc #12 (Orbit 3426)
---------------------------------------
Vector Time (GMT): 2019/290/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2000919
17 A = 6800577
34 meter
Y = 6455539
10 meter E =
0008902
Z = -754212
07 I = 52
01658
XDOT = -4723
847187 Wp = 81
02009
YDOT = -773
271870 meter/sec RA = 112
21983 deg
ZDOT = 5975
098223 TA = 270
89100
MA = 270
99299
Ha = 228
957 n
mi
Hp = 219
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6564695
43 X = -2069294
53
Y = 21179590
23 feet Y = 6432781
09 meter
Z = -2474449
06 Z = -764098
24
XDOT = -15498
186309 XDOT = -4743
873611
YDOT = -2536
981201 feet/sec YDOT = -826
209124 meter/sec
ZDOT = 19603
340628 ZDOT = 5952
102323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19353998
64 X = -5899098
79
Y = 10810448
45 feet Y = 3295024
69 meter
Z = -2519942
02 Z = -768078
33
XDOT = -8774
246207 XDOT = -2674
390244
YDOT = -11209
567936 feet/sec YDOT = -3416
676307 meter/sec
ZDOT = 19498
508159 ZDOT = 5943
145287
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 19290
81051600
00016717 00000-0 10270-3 0 9111
2 25544 51
6411 113
2311 0006866 161
7189 198
4209 15
50178955 34276
Satellite: ISS
Catalog Number: 25544
Epoch time: 19290
81051600 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 113
2311 deg
Eccentricity:
0006866
Arg of perigee: 161
7189 deg
Mean anomaly: 198
4209 deg
Mean motion: 15
50178955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3427
Checksum: 301
Coasting Arc #13 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2019/291/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1776471
12 A = 6800669
85 meter
Y = -6545580
66 meter E =
0018909
Z = 319773
80 I = 52
02868
XDOT = 4634
789555 Wp = 143
40084
YDOT = 954
901581 meter/sec RA = 107
29316 deg
ZDOT = -6033
639510 TA = 33
17417
MA = 33
05575
Ha = 228
894 n
mi
Hp = 219
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5828317
31 X = 1847980
35
Y = -21475002
16 feet Y = -6525315
07 meter
Z = 1049126
63 Z = 328577
13
XDOT = 15206
002476 XDOT = 4653
075853
YDOT = 3132
879203 feet/sec YDOT = 1006
833301 meter/sec
ZDOT = -19795
405216 ZDOT = -6011
080501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18830842
03 X = 5739640
65
Y = -11851480
59 feet Y = -3612331
28 meter
Z = 1089708
04 Z = 332143
01
XDOT = 8296
357618 XDOT = 2528
729802
YDOT = 11322
578096 feet/sec YDOT = 3451
121804 meter/sec
ZDOT = -19692
570353 ZDOT = -6002
295444
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 19291
84194518
00016717 00000-0 10270-3 0 9122
2 25544 51
6410 108
1200 0007028 165
3527 194
7828 15
50221479 34436
Satellite: ISS
Catalog Number: 25544
Epoch time: 19291
84194518 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 108
1200 deg
Eccentricity:
0007028
Arg of perigee: 165
3527 deg
Mean anomaly: 194
7828 deg
Mean motion: 15
50221479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 302
Coasting Arc #14 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2019/292/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1513598
47 A = 6800802
08 meter
Y = 6628427
29 meter E =
0010322
Z = 75530
92 I = 52
03819
XDOT = -4575
689762 Wp = 79
89094
YDOT = -1121
602029 meter/sec RA = 102
36631 deg
ZDOT = 6036
467445 TA = 280
91635
MA = 281
03248
Ha = 228
755 n
mi
Hp = 220
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4965874
25 X = -1587973
87
Y = 21746808
69 feet Y = 6611085
30 meter
Z = 247804
87 Z = 67997
69
XDOT = -15012
105519 XDOT = -4592
129984
YDOT = -3679
796684 feet/sec YDOT = -1172
862591 meter/sec
ZDOT = 19804
683217 ZDOT = 6014
200086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18167177
45 X = -5537355
69
Y = 12944238
13 feet Y = 3945403
78 meter
Z = 212991
46 Z = 64919
80
XDOT = -7925
341323 XDOT = -2415
644035
YDOT = -11491
259662 feet/sec YDOT = -3502
535945 meter/sec
ZDOT = 19703
183537 ZDOT = 6005
530342
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 19292
87337120
00016717 00000-0 10270-3 0 9135
2 25544 51
6415 103
0083 0006749 168
7069 191
4234 15
50187981 34592
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
87337120 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 103
0083 deg
Eccentricity:
0006749
Arg of perigee: 168
7069 deg
Mean anomaly: 191
4234 deg
Mean motion: 15
50187981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 321
Coasting Arc #15 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2019/292/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4028100
67 A = 6788825
72 meter
Y = 1164009
32 meter E =
0017712
Z = -5353457
93 I = 51
99901
XDOT = -1800
002743 Wp = 114
07305
YDOT = 7430
761350 meter/sec RA = 102
12389 deg
ZDOT = 254
955270 TA = 158
38839
MA = 158
31355
Ha = 228
781 n
mi
Hp = 220
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13215553
39 X = 4040789
63
Y = 3818928
20 feet Y = 1209125
37 meter
Z = -17563838
36 Z = -5333859
72
XDOT = -5905
520810 XDOT = -1884
200346
YDOT = 24379
138289 feet/sec YDOT = 7410
161669 meter/sec
ZDOT = 836
467422 ZDOT = 246
006919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10610175
57 X = 3233981
51
Y = 8932463
57 feet Y = 2722614
90 meter
Z = -17474517
19 Z = -5326232
84
XDOT = -14704
430617 XDOT = -4481
910452
YDOT = 19062
737749 feet/sec YDOT = 5810
322466 meter/sec
ZDOT = 795
143305 ZDOT = 242
359679
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 19292
87337017
00016717 00000-0 10270-3 0 9141
2 25544 51
6418 103
0085 0006844 168
3952 191
7357 15
50205698 34595
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
87337017 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 103
0085 deg
Eccentricity:
0006844
Arg of perigee: 168
3952 deg
Mean anomaly: 191
7357 deg
Mean motion: 15
50205698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 330
Coasting Arc #16 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2019/293/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4014504
37 A = 6788829
87 meter
Y = -1317500
29 meter E =
0006518
Z = 5309969
31 I = 52
00505
XDOT = 1510
156010 Wp = 144
58796
YDOT = -7481
165043 meter/sec RA = 97
19096 deg
ZDOT = -719
214334 TA = 312
22176
MA = 312
27705
Ha = 228
753 n
mi
Hp = 219
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13170946
10 X = -4025266
61
Y = -4322507
50 feet Y = -1362453
52 meter
Z = 17421159
15 Z = 5290441
91
XDOT = 4954
580084 XDOT = 1597
193925
YDOT = -24544
504734 feet/sec YDOT = -7463
790747 meter/sec
ZDOT = -2359
627081 ZDOT = -711
667109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10522541
45 X = -3207270
63
Y = -9193844
70 feet Y = -2802283
86 meter
Z = 17332167
20 Z = 5282844
56
XDOT = 13541
845760 XDOT = 4127
554588
YDOT = -19851
987199 feet/sec YDOT = -6050
885698 meter/sec
ZDOT = -2324
671461 ZDOT = -708
559861
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 19293
90479063
00016717 00000-0 10270-3 0 9155
2 25544 51
6415 97
8978 0006776 171
2769 188
8501 15
50248281 34757
Satellite: ISS
Catalog Number: 25544
Epoch time: 19293
90479063 = yrday
fracday
Element set: 915
Inclination: 51
6415 deg
RA of node: 97
8978 deg
Eccentricity:
0006776
Arg of perigee: 171
2769 deg
Mean anomaly: 188
8501 deg
Mean motion: 15
50248281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 356
Coasting Arc #17 (Orbit 3489)
---------------------------------------
Vector Time (GMT): 2019/294/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4046561
96 A = 6789242
15 meter
Y = 1506974
61 meter E =
0017033
Z = -5253147
81 I = 52
00970
XDOT = -1224
283074 Wp = 121
68160
YDOT = 7457
057118 meter/sec RA = 92
25727 deg
ZDOT = 1190
281523 TA = 159
73849
MA = 159
67082
Ha = 228
556 n
mi
Hp = 220
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13276121
93 X = 4054926
96
Y = 4944142
44 feet Y = 1552272
88 meter
Z = -17234736
90 Z = -5233470
58
XDOT = -4016
676752 XDOT = -1313
360853
YDOT = 24465
410491 feet/sec YDOT = 7442
868258 meter/sec
ZDOT = 3905
123108 ZDOT = 1184
117972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10541067
39 X = 3212917
34
Y = 9626449
52 feet Y = 2934141
81 meter
Z = -17145071
65 Z = -5225817
84
XDOT = -12264
694115 XDOT = -3738
278766
YDOT = 20368
470739 feet/sec YDOT = 6208
309881 meter/sec
ZDOT = 3876
465200 ZDOT = 1181
546593
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 19294
87174664
00016717 00000-0 10270-3 0 9162
2 25544 51
6421 93
1057 0006738 175
2507 184
8709 15
50215636 34904
Satellite: ISS
Catalog Number: 25544
Epoch time: 19294
87174664 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 93
1057 deg
Eccentricity:
0006738
Arg of perigee: 175
2507 deg
Mean anomaly: 184
8709 deg
Mean motion: 15
50215636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3490
Checksum: 330
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