[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 1st 2019
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) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
123/07:11:34
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 217
5
125/02:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 217
4
128/05:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
2
131/09:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
3
134/18:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
1
Coasting Arc #1 (Orbit 799)
---------------------------------------
Vector Time (GMT): 2019/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940331
60 A = 6781967
66 meter
Y = -1755839
08 meter E =
0002322
Z = 5231822
96 I = 51
31589
XDOT = 4074
021524 Wp = 49
42809
YDOT = 6431
896795 meter/sec RA = 232
16990 deg
ZDOT = -907
994527 TA = 49
30766
MA = 49
28749
Ha = 222
785 n
mi
Hp = 217
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12927597
10 X = 3934259
48
Y = -5760626
90 feet Y = -1711809
37 meter
Z = 17164773
50 Z = 5250949
11
XDOT = 13366
212348 XDOT = 4006
206012
YDOT = 21102
023607 feet/sec YDOT = 6477
076157 meter/sec
ZDOT = -2978
984670 ZDOT = -888
369110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6497631
82 X = 1980478
18
Y = -12454182
25 feet Y = -3796034
75 meter
Z = 17251410
48 Z = 5258229
91
XDOT = 22666
937310 XDOT = 6908
882492
YDOT = 7813
713035 feet/sec YDOT = 2381
619733 meter/sec
ZDOT = -2890
748039 ZDOT = -881
100002
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 19121
54678499
00016717 00000-0 10270-3 0 9003
2 25544 51
6411 233
0175 0001173 260
8293 99
2726 15
52630930 8000
Satellite: ISS
Catalog Number: 25544
Epoch time: 19121
54678499 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 233
0175 deg
Eccentricity:
0001173
Arg of perigee: 260
8293 deg
Mean anomaly: 99
2726 deg
Mean motion: 15
52630930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 800
Checksum: 297
Coasting Arc #2 (Orbit 814)
---------------------------------------
Vector Time (GMT): 2019/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4605578
62 A = 6783301
95 meter
Y = 823671
28 meter E =
0011307
Z = -4922130
74 I = 51
34201
XDOT = -3526
213582 Wp = 108
93349
YDOT = -6422
072802 meter/sec RA = 227
16737 deg
ZDOT = 2225
371329 TA = 182
91346
MA = 182
92005
Ha = 222
916 n
mi
Hp = 217
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15110166
09 X = -4590537
54
Y = 2702333
59 feet Y = 772252
49 meter
Z = -16148722
91 Z = -4944466
71
XDOT = -11568
942197 XDOT = -3464
947830
YDOT = -21069
792657 feet/sec YDOT = -6461
162797 meter/sec
ZDOT = 7301
087036 ZDOT = 2208
390972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9912425
50 X = -3021307
29
Y = 11579661
97 feet Y = 3529480
97 meter
Z = -16249806
99 Z = -4952941
17
XDOT = -21479
456159 XDOT = -6546
938237
YDOT = -8251
031868 feet/sec YDOT = -2514
914513 meter/sec
ZDOT = 7224
796646 ZDOT = 2202
118018
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 19122
51225826
00016717 00000-0 10270-3 0 9014
2 25544 51
6414 228
2172 0001157 260
9931 99
1090 15
52638838 8152
Satellite: ISS
Catalog Number: 25544
Epoch time: 19122
51225826 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 228
2172 deg
Eccentricity:
0001157
Arg of perigee: 260
9931 deg
Mean anomaly: 99
1090 deg
Mean motion: 15
52638838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 815
Checksum: 300
Coasting Arc #3 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2019/123/07:11:34
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2430267
36 A = 6781984
64 meter
Y = -3502534
03 meter E =
0001837
Z = 5273327
33 I = 51
35179
XDOT = 5868
046144 Wp = 122
28537
YDOT = 4904
277892 meter/sec RA = 223
19620 deg
ZDOT = 551
958127 TA = 322
41958
MA = 322
43242
Ha = 222
947 n
mi
Hp = 217
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7973318
11 X = 2443637
74
Y = -11491253
39 feet Y = -3475282
29 meter
Z = 17300942
68 Z = 5285165
35
XDOT = 19252
119894 XDOT = 5810
087834
YDOT = 16090
150564 feet/sec YDOT = 4969
574431 meter/sec
ZDOT = 1810
886244 ZDOT = 580
322575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12761026
68 X = 3889560
93
Y = -5560022
56 feet Y = -1694694
88 meter
Z = 17354759
32 Z = 5289730
64
XDOT = 7345
837904 XDOT = 2239
011393
YDOT = 22922
649889 feet/sec YDOT = 6986
823686 meter/sec
ZDOT = 1938
795844 ZDOT = 590
944973
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 19123
34900073
00016717 00000-0 10270-3 0 9021
2 25544 51
6377 224
0545 0001098 280
6787 79
4241 15
52576915 8280
Satellite: ISS
Catalog Number: 25544
Epoch time: 19123
34900073 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 224
0545 deg
Eccentricity:
0001098
Arg of perigee: 280
6787 deg
Mean anomaly: 79
4241 deg
Mean motion: 15
52576915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 315
Coasting Arc #4 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2019/124/07:11:34
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3327461
08 A = 6781928
96 meter
Y = 2724771
17 meter E =
0013595
Z = -5255784
02 I = 51
37826
XDOT = -5555
374375 Wp = 95
99749
YDOT = -5203
874394 meter/sec RA = 218
19344 deg
ZDOT = 819
714631 TA = 181
87663
MA = 181
88174
Ha = 223
013 n
mi
Hp = 217
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10916867
05 X = -3332152
76
Y = 8939537
95 feet Y = 2687535
00 meter
Z = -17243385
88 Z = -5271959
25
XDOT = -18226
293882 XDOT = -5500
752078
YDOT = -17073
078719 feet/sec YDOT = -5265
693077 meter/sec
ZDOT = 2689
352465 ZDOT = 792
860784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13865784
08 X = -4226290
99
Y = 2073019
80 feet Y = 631856
44 meter
Z = -17316763
62 Z = -5278149
55
XDOT = -6649
143451 XDOT = -2026
658924
YDOT = -23032
187853 feet/sec YDOT = -7020
210857 meter/sec
ZDOT = 2568
283376 ZDOT = 782
812773
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 19124
31446737
00016717 00000-0 10270-3 0 9032
2 25544 51
6387 219
2526 0000954 282
2813 77
8232 15
52629349 8433
Satellite: ISS
Catalog Number: 25544
Epoch time: 19124
31446737 = yrday
fracday
Element set: 903
Inclination: 51
6387 deg
RA of node: 219
2526 deg
Eccentricity:
0000954
Arg of perigee: 282
2813 deg
Mean anomaly: 77
8232 deg
Mean motion: 15
52629349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 319
Coasting Arc #5 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2019/125/02:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4912917
98 A = 6784646
00 meter
Y = -1058794
05 meter E =
0007802
Z = 4554281
53 I = 51
41231
XDOT = 4081
122444 Wp = 57
32605
YDOT = 5722
487203 meter/sec RA = 214
14807 deg
ZDOT = -3064
149039 TA = 63
46143
MA = 63
38146
Ha = 222
719 n
mi
Hp = 217
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16118497
31 X = 4902269
95
Y = -3473733
77 feet Y = -1003914
03 meter
Z = 14941868
53 Z = 4578121
25
XDOT = 13389
509331 XDOT = 4031
712889
YDOT = 18774
564313 feet/sec YDOT = 5767
848993 meter/sec
ZDOT = -10052
982413 ZDOT = -3044
443907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 866811
94 X = 264204
28
Y = 16367177
24 feet Y = 4988715
62 meter
Z = 15049796
11 Z = 4587177
86
XDOT = -19490
497976 XDOT = -5940
703783
YDOT = 10218
351308 feet/sec YDOT = 3114
553479 meter/sec
ZDOT = -9964
279844 ZDOT = -3037
112496
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 19125
15120166
00016717 00000-0 10270-3 0 9041
2 25544 51
6416 215
0958 0001495 302
4359 57
6648 15
52674109 8565
Satellite: ISS
Catalog Number: 25544
Epoch time: 19125
15120166 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 215
0958 deg
Eccentricity:
0001495
Arg of perigee: 302
4359 deg
Mean anomaly: 57
6648 deg
Mean motion: 15
52674109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 310
Coasting Arc #6 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2019/126/02:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5595410
17 A = 6787349
01 meter
Y = 372190
96 meter E =
0004957
Z = -3828709
86 I = 51
44820
XDOT = -3209
806456 Wp = 100
28775
YDOT = -5579
843526 meter/sec RA = 209
15713 deg
ZDOT = 4152
229235 TA = 213
57433
MA = 213
60575
Ha = 222
887 n
mi
Hp = 217
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18357644
93 X = -5580558
12
Y = 1221098
96 feet Y = 309702
41 meter
Z = -12561384
05 Z = -3855854
74
XDOT = -10530
861076 XDOT = -3167
342141
YDOT = -18306
573247 feet/sec YDOT = -5615
500607 meter/sec
ZDOT = 13622
799326 ZDOT = 4136
739726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1403374
51 X = 427748
55
Y = -18259888
55 feet Y = -5565614
03 meter
Z = -12684226
01 Z = -3866152
09
XDOT = 18304
078551 XDOT = 5579
083142
YDOT = -7999
509177 feet/sec YDOT = -2438
250397 meter/sec
ZDOT = 13553
145973 ZDOT = 4130
998892
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 19126
11666686
00016717 00000-0 10270-3 0 9051
2 25544 51
6406 210
2939 0001453 303
0159 57
0853 15
52636093 8718
Satellite: ISS
Catalog Number: 25544
Epoch time: 19126
11666686 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 210
2939 deg
Eccentricity:
0001453
Arg of perigee: 303
0159 deg
Mean anomaly: 57
0853 deg
Mean motion: 15
52636093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 303
Coasting Arc #7 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2019/127/02:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6140470
24 A = 6789973
50 meter
Y = 247697
31 meter E =
0011922
Z = 2875803
71 I = 51
48743
XDOT = 2152
158375 Wp = 94
56130
YDOT = 5362
397773 meter/sec RA = 204
17345 deg
ZDOT = -5040
070283 TA = 52
64109
MA = 52
53256
Ha = 222
825 n
mi
Hp = 217
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20145899
73 X = 6123274
72
Y = 812655
21 feet Y = 316267
99 meter
Z = 9435051
53 Z = 2905590
64
XDOT = 7060
887057 XDOT = 2116
516892
YDOT = 17593
168548 feet/sec YDOT = 5386
265796 meter/sec
ZDOT = -16535
663658 ZDOT = -5029
701883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3334129
80 X = -1016242
76
Y = 19820192
32 feet Y = 6041194
62 meter
Z = 9569819
06 Z = 2916880
85
XDOT = -16909
399711 XDOT = -5153
985032
YDOT = 5143
762661 feet/sec YDOT = 1567
818859 meter/sec
ZDOT = -16489
155514 ZDOT = -5025
894601
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 19127
14649174
00016717 00000-0 10270-3 0 9069
2 25544 51
6411 205
1717 0001613 310
8799 49
2213 15
52669658 8878
Satellite: ISS
Catalog Number: 25544
Epoch time: 19127
14649174 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 205
1717 deg
Eccentricity:
0001613
Arg of perigee: 310
8799 deg
Mean anomaly: 49
2213 deg
Mean motion: 15
52669658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 321
Coasting Arc #8 (Orbit 901)
---------------------------------------
Vector Time (GMT): 2019/128/02:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6503473
53 A = 6792255
43 meter
Y = -752803
44 meter E =
0007510
Z = -1795956
77 I = 51
52370
XDOT = -966
280026 Wp = 27
11532
YDOT = -5089
842469 meter/sec RA = 199
19561 deg
ZDOT = 5648
425841 TA = 313
13429
MA = 313
19706
Ha = 222
923 n
mi
Hp = 217
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21336855
42 X = -6485848
22
Y = -2469827
57 feet Y = -825431
12 meter
Z = -5892246
63 Z = -1827505
96
XDOT = -3170
210058 XDOT = -936
729482
YDOT = -16698
958233 feet/sec YDOT = -5100
483368 meter/sec
ZDOT = 18531
580842 ZDOT = 5643
803258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4771920
09 X = 1454481
24
Y = -20901863
52 feet Y = -6370888
00 meter
Z = -6034972
88 Z = -1839459
73
XDOT = 15432
764555 XDOT = 4703
906636
YDOT = -1806
679314 feet/sec YDOT = -550
675855 meter/sec
ZDOT = 18511
047147 ZDOT = 5642
167170
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 19128
11195131
00016717 00000-0 10270-3 0 9077
2 25544 51
6393 200
3687 0001583 312
6456 47
4562 15
52629146 9029
Satellite: ISS
Catalog Number: 25544
Epoch time: 19128
11195131 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 200
3687 deg
Eccentricity:
0001583
Arg of perigee: 312
6456 deg
Mean anomaly: 47
4562 deg
Mean motion: 15
52629146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 902
Checksum: 300
Coasting Arc #9 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2019/128/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5283704
84 A = 6786875
37 meter
Y = 1556590
31 meter E =
0006004
Z = -3971218
96 I = 51
50772
XDOT = -4414
739717 Wp = 104
93449
YDOT = -4826
315859 meter/sec RA = 198
56702 deg
ZDOT = 3985
585600 TA = 206
71808
MA = 206
74903
Ha = 223
031 n
mi
Hp = 217
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17334989
62 X = -5281428
11
Y = 5106923
58 feet Y = 1497517
32 meter
Z = -13028933
61 Z = -3996879
94
XDOT = -14484
054189 XDOT = -4379
802416
YDOT = -15834
369617 feet/sec YDOT = -4875
489586 meter/sec
ZDOT = 13076
068241 ZDOT = 3964
224541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14710644
50 X = -4483804
44
Y = -10350680
27 feet Y = -3154887
35 meter
Z = -13145189
27 Z = -4006653
69
XDOT = 2611
089218 XDOT = 795
859994
YDOT = -20180
410206 feet/sec YDOT = -6150
989031 meter/sec
ZDOT = 12979
758336 ZDOT = 3956
230341
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 19128
24068065
00016717 00000-0 10270-3 0 9087
2 25544 51
6373 199
7247 0000999 306
8460 53
2600 15
52638683 9046
Satellite: ISS
Catalog Number: 25544
Epoch time: 19128
24068065 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 199
7247 deg
Eccentricity:
0000999
Arg of perigee: 306
8460 deg
Mean anomaly: 53
2600 deg
Mean motion: 15
52638683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 904
Checksum: 327
Coasting Arc #10 (Orbit 919)
---------------------------------------
Vector Time (GMT): 2019/129/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5970961
45 A = 6789662
48 meter
Y = -1046080
31 meter E =
0012060
Z = 3046926
85 I = 51
54737
XDOT = 3362
855430 Wp = 93
38386
YDOT = 4828
936323 meter/sec RA = 193
58712 deg
ZDOT = -4916
060278 TA = 51
62367
MA = 51
51539
Ha = 222
970 n
mi
Hp = 217
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19589768
53 X = 5967414
81
Y = -3432022
02 feet Y = -979328
97 meter
Z = 9996479
17 Z = 3075923
13
XDOT = 11032
990256 XDOT = 3332
486688
YDOT = 15842
966939 feet/sec YDOT = 4866
372810 meter/sec
ZDOT = -16128
806687 ZDOT = -4899
797900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15034659
15 X = 4582564
11
Y = 12917191
32 feet Y = 3937159
91 meter
Z = 10127812
92 Z = 3086957
38
XDOT = -4240
098422 XDOT = -1292
381999
YDOT = 17564
589070 feet/sec YDOT = 5353
686749 meter/sec
ZDOT = -16055
558147 ZDOT = -4893
734123
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 19129
27050218
00016717 00000-0 10270-3 0 9093
2 25544 51
6358 194
6026 0001103 305
7142 54
3907 15
52627868 9204
Satellite: ISS
Catalog Number: 25544
Epoch time: 19129
27050218 = yrday
fracday
Element set: 909
Inclination: 51
6358 deg
RA of node: 194
6026 deg
Eccentricity:
0001103
Arg of perigee: 305
7142 deg
Mean anomaly: 54
3907 deg
Mean motion: 15
52627868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 920
Checksum: 301
Coasting Arc #11 (Orbit 934)
---------------------------------------
Vector Time (GMT): 2019/130/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6462449
82 A = 6791892
61 meter
Y = 615165
93 meter E =
0006744
Z = -1987870
24 I = 51
58983
XDOT = -2165
938712 Wp = 32
17362
YDOT = -4796
002728 meter/sec RA = 188
61390 deg
ZDOT = 5571
465818 TA = 305
88447
MA = 305
94706
Ha = 223
018 n
mi
Hp = 217
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21202263
19 X = -6459192
45
Y = 2018260
93 feet Y = 542916
70 meter
Z = -6521883
99 Z = -2019254
61
XDOT = -7106
098135 XDOT = -2139
210704
YDOT = -15734
917085 feet/sec YDOT = -4820
074853 meter/sec
ZDOT = 18279
087331 ZDOT = 5561
008902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15236409
68 X = -4644057
67
Y = -14818467
66 feet Y = -4516668
94 meter
Z = -6664018
95 Z = -2031192
98
XDOT = 6230
274474 XDOT = 1898
987660
YDOT = -14584
518130 feet/sec YDOT = -4445
361126 meter/sec
ZDOT = 18232
104288 ZDOT = 5557
145387
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 19130
23595887
00016717 00000-0 10270-3 0 9109
2 25544 51
6380 189
8003 0001027 311
5740 48
5323 15
52645799 9350
Satellite: ISS
Catalog Number: 25544
Epoch time: 19130
23595887 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 189
8003 deg
Eccentricity:
0001027
Arg of perigee: 311
5740 deg
Mean anomaly: 48
5323 deg
Mean motion: 15
52645799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 935
Checksum: 313
Coasting Arc #12 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2019/131/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6738500
66 A = 6793306
09 meter
Y = -197500
34 meter E =
0012258
Z = 790171
87 I = 51
62719
XDOT = 843
504313 Wp = 125
18584
YDOT = 4769
086802 meter/sec RA = 183
64650 deg
ZDOT = -5943
013943 TA = 46
27469
MA = 46
17325
Ha = 223
066 n
mi
Hp = 217
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22107941
80 X = 6736370
12
Y = -647967
01 feet Y = -122157
69 meter
Z = 2592427
40 Z = 822899
88
XDOT = 2767
402601 XDOT = 818
980266
YDOT = 15646
610244 feet/sec YDOT = 4778
382808 meter/sec
ZDOT = -19498
077241 ZDOT = -5938
975690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15075891
40 X = 4595131
70
Y = 16158837
60 feet Y = 4925213
70 meter
Z = 2740638
15 Z = 835346
51
XDOT = -8655
144714 XDOT = -2638
088109
YDOT = 11409
718608 feet/sec YDOT = 3477
682232 meter/sec
ZDOT = -19480
145407 ZDOT = -5937
548320
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 19131
26577598
00016717 00000-0 10270-3 0 9113
2 25544 51
6375 184
6774 0001151 320
3774 39
7294 15
52660406 9514
Satellite: ISS
Catalog Number: 25544
Epoch time: 19131
26577598 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 184
6774 deg
Eccentricity:
0001151
Arg of perigee: 320
3774 deg
Mean anomaly: 39
7294 deg
Mean motion: 15
52660406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 951
Checksum: 321
Coasting Arc #13 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2019/131/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -324536
75 A = 6781673
38 meter
Y = 4207027
97 meter E =
0014020
Z = -5321227
95 I = 51
59631
XDOT = -7640
922260 Wp = 87
20720
YDOT = -467
752044 meter/sec RA = 182
92704 deg
ZDOT = 97
091067 TA = 183
71485
MA = 183
72527
Ha = 223
042 n
mi
Hp = 217
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1064753
11 X = -345709
19
Y = 13802585
21 feet Y = 4203280
80 meter
Z = -17458096
95 Z = -5322855
53
XDOT = -25068
642584 XDOT = -7635
595450
YDOT = -1534
619566 feet/sec YDOT = -553
168408 meter/sec
ZDOT = 318
540246 ZDOT = 59
987148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 72660
15 X = 22146
81
Y = 13833708
75 feet Y = 4216514
43 meter
Z = -17465778
81 Z = -5323569
38
XDOT = -24106
352305 XDOT = -7347
616182
YDOT = 313
026438 feet/sec YDOT = 95
410458 meter/sec
ZDOT = 150
560375 ZDOT = 45
890802
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 19131
39450258
00016717 00000-0 10270-3 0 9121
2 25544 51
6408 184
0396 0001244 316
0136 44
0916 15
52647548 9536
Satellite: ISS
Catalog Number: 25544
Epoch time: 19131
39450258 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 184
0396 deg
Eccentricity:
0001244
Arg of perigee: 316
0136 deg
Mean anomaly: 44
0916 deg
Mean motion: 15
52647548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 953
Checksum: 301
Coasting Arc #14 (Orbit 968)
---------------------------------------
Vector Time (GMT): 2019/132/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1515730
23 A = 6782234
67 meter
Y = -4137500
74 meter E =
0004582
Z = 5154073
22 I = 51
63201
XDOT = 7471
309216 Wp = 39
28816
YDOT = 897
782774 meter/sec RA = 177
94135 deg
ZDOT = -1472
300126 TA = 64
91160
MA = 64
86406
Ha = 222
953 n
mi
Hp = 217
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4972868
21 X = 1536848
62
Y = -13574477
50 feet Y = -4120432
99 meter
Z = 16909689
04 Z = 5161487
15
XDOT = 24512
169345 XDOT = 7467
866299
YDOT = 2945
481541 feet/sec YDOT = 981
313014 meter/sec
ZDOT = -4830
380990 ZDOT = -1436
015558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3605630
36 X = 1098996
14
Y = -13958807
90 feet Y = -4254644
65 meter
Z = 16943569
65 Z = 5164400
03
XDOT = 23692
208175 XDOT = 7221
385052
YDOT = 439
326058 feet/sec YDOT = 133
906582 meter/sec
ZDOT = -4666
118447 ZDOT = -1422
232903
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 19132
42431824
00016717 00000-0 10270-3 0 9135
2 25544 51
6409 178
9173 0001287 319
6153 40
4903 15
52681536 9695
Satellite: ISS
Catalog Number: 25544
Epoch time: 19132
42431824 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 178
9173 deg
Eccentricity:
0001287
Arg of perigee: 319
6153 deg
Mean anomaly: 40
4903 deg
Mean motion: 15
52681536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 969
Checksum: 314
Coasting Arc #15 (Orbit 983)
---------------------------------------
Vector Time (GMT): 2019/133/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2638366
07 A = 6784031
87 meter
Y = 4094724
34 meter E =
0010116
Z = -4731430
89 I = 51
67076
XDOT = -7016
925036 Wp = 105
26406
YDOT = -1333
269432 meter/sec RA = 172
96168 deg
ZDOT = 2761
294678 TA = 192
08962
MA = 192
11392
Ha = 223
069 n
mi
Hp = 217
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8656056
65 X = -2660975
61
Y = 13434134
98 feet Y = 4065094
03 meter
Z = -15523067
22 Z = -4744301
90
XDOT = -23021
407600 XDOT = -7014
907408
YDOT = -4374
243542 feet/sec YDOT = -1411
726418 meter/sec
ZDOT = 9059
365740 ZDOT = 2727
213821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7050935
12 X = -2149125
03
Y = 14278128
20 feet Y = 4351973
48 meter
Z = -15581665
00 Z = -4749291
49
XDOT = -22377
809951 XDOT = -6820
756473
YDOT = -1341
001831 feet/sec YDOT = -408
737358 meter/sec
ZDOT = 8905
094752 ZDOT = 2714
272880
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 19133
38977115
00016717 00000-0 10270-3 0 9140
2 25544 51
6404 174
1163 0001195 326
1869 33
9207 15
52673688 9842
Satellite: ISS
Catalog Number: 25544
Epoch time: 19133
38977115 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 174
1163 deg
Eccentricity:
0001195
Arg of perigee: 326
1869 deg
Mean anomaly: 33
9207 deg
Mean motion: 15
52673688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 984
Checksum: 326
Coasting Arc #16 (Orbit 999)
---------------------------------------
Vector Time (GMT): 2019/134/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3664849
72 A = 6786572
55 meter
Y = -4036618
44 meter E =
0010376
Z = 4035374
89 I = 51
71300
XDOT = 6333
201801 Wp = 70
75423
YDOT = 1817
608136 meter/sec RA = 167
98728 deg
ZDOT = -3921
952400 TA = 59
96272
MA = 59
85982
Ha = 223
027 n
mi
Hp = 217
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12023785
18 X = 3690114
21
Y = -13243498
81 feet Y = -3995494
36 meter
Z = 13239418
93 Z = 4053238
75
XDOT = 20778
221133 XDOT = 6331
456893
YDOT = 5963
281285 feet/sec YDOT = 1888
420773 meter/sec
ZDOT = -12867
297901 ZDOT = -3891
192056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10184508
39 X = 3104238
16
Y = -14631483
36 feet Y = -4459676
13 meter
Z = 13320636
92 Z = 4060130
13
XDOT = 20379
043288 XDOT = 6211
532394
YDOT = 2563
083449 feet/sec YDOT = 781
227835 meter/sec
ZDOT = -12728
086085 ZDOT = -3879
520639
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 19134
41958398
00016717 00000-0 10270-3 0 9158
2 25544 51
6411 168
9938 0001396 331
6446 28
4630 15
52676377 10003
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
41958398 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 168
9938 deg
Eccentricity:
0001396
Arg of perigee: 331
6446 deg
Mean anomaly: 28
4630 deg
Mean motion: 15
52676377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1000
Checksum: 325
Coasting Arc #17 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2019/134/18:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3771475
19 A = 6783896
30 meter
Y = -2966590
28 meter E =
0006419
Z = 4791134
45 I = 51
71418
XDOT = 6210
631705 Wp = 109
43872
YDOT = -3657
559034 meter/sec RA = 166
17470 deg
ZDOT = 2619
226672 TA = 314
74175
MA = 314
79398
Ha = 223
239 n
mi
Hp = 217
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12373606
25 X = -3761294
49
Y = -9732907
75 feet Y = -3008708
75 meter
Z = 15718945
06 Z = 4772838
54
XDOT = 20376
088271 XDOT = 6238
347127
YDOT = -11999
865596 feet/sec YDOT = -3587
952494 meter/sec
ZDOT = 8593
263359 ZDOT = 2649
463085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3923447
29 X = 1195866
73
Y = 15330826
04 feet Y = 4672835
78 meter
Z = 15636278
11 Z = 4765937
57
XDOT = -22296
271931 XDOT = -6795
903685
YDOT = -3215
056325 feet/sec YDOT = -979
949168 meter/sec
ZDOT = 8730
507487 ZDOT = 2661
058682
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 19134
80576369
00016717 00000-0 10270-3 0 9166
2 25544 51
6393 167
0748 0001604 338
2218 21
8866 15
52686516 10063
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
80576369 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 167
0748 deg
Eccentricity:
0001604
Arg of perigee: 338
2218 deg
Mean anomaly: 21
8866 deg
Mean motion: 15
52686516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 323
Coasting Arc #18 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2019/135/18:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2719237
09 A = 6782247
92 meter
Y = 3410908
80 meter E =
0013987
Z = -5205647
13 I = 51
73992
XDOT = -6742
667437 Wp = 73
25699
YDOT = 3382
525914 meter/sec RA = 161
19864 deg
ZDOT = -1304
753968 TA = 184
20108
MA = 184
21283
Ha = 223
291 n
mi
Hp = 217
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8921381
52 X = 2706179
70
Y = 11190645
68 feet Y = 3441244
35 meter
Z = -17078894
78 Z = -5192469
54
XDOT = -22121
612325 XDOT = -6773
652823
YDOT = 11097
525966 feet/sec YDOT = 3306
951470 meter/sec
ZDOT = -4280
688873 ZDOT = -1337
582912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -555067
36 X = -169184
53
Y = -14371523
60 feet Y = -4380440
39 meter
Z = -17019443
45 Z = -5187526
36
XDOT = 23296
427743 XDOT = 7100
751176
YDOT = 4350
058378 feet/sec YDOT = 1325
897794 meter/sec
ZDOT = -4429
676329 ZDOT = -1350
165345
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 19135
77121362
00016717 00000-0 10270-3 0 9173
2 25544 51
6387 162
2726 0001681 348
8655 11
2460 15
52657958 10214
Satellite: ISS
Catalog Number: 25544
Epoch time: 19135
77121362 = yrday
fracday
Element set: 917
Inclination: 51
6387 deg
RA of node: 162
2726 deg
Eccentricity:
0001681
Arg of perigee: 348
8655 deg
Mean anomaly: 11
2460 deg
Mean motion: 15
52657958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 311
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