[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 31st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16903 7526 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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
154/16:09:12
500 -0
0 -0
0 0
0
N/A 0
0 -0
0 227
4
000/00:00:25
000 0
0 0
0 218
6
155/08:40:30
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
3
157/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 218
1
161/12:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 217
6
Coasting Arc #1 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2019/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4196636
32 A = 6786018
02 meter
Y = -22481
40 meter E =
0008778
Z = 5331724
80 I = 52
00405
XDOT = -545
565885 Wp = 11
75749
YDOT = -7632
099925 meter/sec RA = 83
25987 deg
ZDOT = -453
109550 TA = 82
59434
MA = 82
49460
Ha = 227
155 n
mi
Hp = 218
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13768491
88 X = -4221971
96
Y = -73757
86 feet Y = -69553
33 meter
Z = 17492535
43 Z = 5311277
27
XDOT = -1789
914321 XDOT = -457
980031
YDOT = -25039
697917 feet/sec YDOT = -7637
711055 meter/sec
ZDOT = -1486
579888 ZDOT = -455
547798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5311248
60 X = -1618868
57
Y = 12829828
32 feet Y = 3910531
67 meter
Z = 17399762
88 Z = 5303447
73
XDOT = -22922
071270 XDOT = -6986
647323
YDOT = -7421
204734 feet/sec YDOT = -2261
983203 meter/sec
ZDOT = -1496
847536 ZDOT = -456
239129
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 19151
54756649
00016717 00000-0 10270-3 0 9000
2 25544 51
6414 83
8844 0007714 354
5725 5
5342 15
51179348 12666
Satellite: ISS
Catalog Number: 25544
Epoch time: 19151
54756649 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 83
8844 deg
Eccentricity:
0007714
Arg of perigee: 354
5725 deg
Mean anomaly: 5
5342 deg
Mean motion: 15
51179348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1266
Checksum: 320
Coasting Arc #2 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2019/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4292971
67 A = 6786543
43 meter
Y = 552700
44 meter E =
0014766
Z = -5237872
94 I = 52
00127
XDOT = 554
357405 Wp = 68
32621
YDOT = 7530
094632 meter/sec RA = 78
31597 deg
ZDOT = 1257
064003 TA = 213
65570
MA = 213
74956
Ha = 227
283 n
mi
Hp = 218
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14084552
72 X = 4311915
23
Y = 1813321
64 feet Y = 600814
02 meter
Z = -17184622
49 Z = -5216972
87
XDOT = 1818
757890 XDOT = 464
006322
YDOT = 24705
034882 feet/sec YDOT = 7535
788503 meter/sec
ZDOT = 4124
225732 ZDOT = 1259
538397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6825153
56 X = 2080306
81
Y = -12582855
77 feet Y = -3835254
44 meter
Z = -17089851
68 Z = -5208986
79
XDOT = 22763
059507 XDOT = 6938
180538
YDOT = 6767
905965 feet/sec YDOT = 2062
857738 meter/sec
ZDOT = 4134
646099 ZDOT = 1260
240131
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 19152
51394715
00016717 00000-0 10270-3 0 9011
2 25544 51
6421 79
0881 0007775 359
2821
8317 15
51156663 12810
Satellite: ISS
Catalog Number: 25544
Epoch time: 19152
51394715 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 79
0881 deg
Eccentricity:
0007775
Arg of perigee: 359
2821 deg
Mean anomaly:
8317 deg
Mean motion: 15
51156663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1281
Checksum: 305
Coasting Arc #3 (Orbit 1296)
---------------------------------------
Vector Time (GMT): 2019/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4426832
13 A = 6787412
00 meter
Y = -1105263
84 meter E =
0012401
Z = 5023780
58 I = 51
99638
XDOT = -516
766133 Wp = 26
06938
YDOT = -7363
460694 meter/sec RA = 73
37403 deg
ZDOT = -2062
603074 TA = 83
97149
MA = 83
83018
Ha = 227
435 n
mi
Hp = 218
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14523727
47 X = -4438546
85
Y = -3626193
71 feet Y = -1154834
02 meter
Z = 16482219
75 Z = 5002247
74
XDOT = -1695
426947 XDOT = -424
368275
YDOT = -24158
335609 feet/sec YDOT = -7368
722603 meter/sec
ZDOT = -6767
070452 ZDOT = -2064
890030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8459061
38 X = -2578321
91
Y = 12479560
62 feet Y = 3803770
08 meter
Z = 16384637
79 Z = 4994037
60
XDOT = -22330
472196 XDOT = -6806
327925
YDOT = -6183
848805 feet/sec YDOT = -1884
837116 meter/sec
ZDOT = -6776
636692 ZDOT = -2065
518864
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 19153
54475221
00016717 00000-0 10270-3 0 9028
2 25544 51
6420 73
9738 0007814 3
0344 357
0853 15
51165592 12971
Satellite: ISS
Catalog Number: 25544
Epoch time: 19153
54475221 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 73
9738 deg
Eccentricity:
0007814
Arg of perigee: 3
0344 deg
Mean anomaly: 357
0853 deg
Mean motion: 15
51165592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1297
Checksum: 303
Coasting Arc #4 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2019/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4605197
11 A = 6788585
22 meter
Y = 1567012
90 meter E =
0011808
Z = -4742741
88 I = 51
99061
XDOT = 456
073621 Wp = 69
13154
YDOT = 7110
925251 meter/sec RA = 68
43163 deg
ZDOT = 2802
019559 TA = 228
49348
MA = 228
59487
Ha = 227
485 n
mi
Hp = 218
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15108914
41 X = 4610369
96
Y = 5141118
45 feet Y = 1618541
15 meter
Z = -15560176
78 Z = -4720358
44
XDOT = 1496
304530 XDOT = 362
912501
YDOT = 23329
807255 feet/sec YDOT = 7115
504023 meter/sec
ZDOT = 9192
977557 ZDOT = 2804
009932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9864299
71 X = 3006638
55
Y = -12670871
45 feet Y = -3862081
62 meter
Z = -15458787
24 Z = -4711838
35
XDOT = 21576
980981 XDOT = 6576
663803
YDOT = 5611
124345 feet/sec YDOT = 1710
270700 meter/sec
ZDOT = 9201
206162 ZDOT = 2804
527638
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 19154
51113205
00016717 00000-0 10270-3 0 9038
2 25544 51
6429 69
1781 0007778 6
3955 353
7294 15
51166211 13127
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
51113205 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 69
1781 deg
Eccentricity:
0007778
Arg of perigee: 6
3955 deg
Mean anomaly: 353
7294 deg
Mean motion: 15
51166211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 299
Coasting Arc #5 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2019/154/16:09:25
000
Vector Time (MET): N/A
Weight (LBS) : 945426
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2193644
16 A = 6797897
83 meter
Y = -6412406
31 meter E =
0007925
Z = -531747
58 I = 52
01893
XDOT = 4622
846993 Wp = 93
79563
YDOT = -1089
814066 meter/sec RA = 67
60245 deg
ZDOT = -6006
201118 TA = 91
89963
MA = 91
80886
Ha = 227
391 n
mi
Hp = 218
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7196995
29 X = -2119192
80
Y = -21038078
46 feet Y = -6436520
80 meter
Z = -1744578
67 Z = -542223
87
XDOT = 15166
820842 XDOT = 4663
865166
YDOT = -3575
505465 feet/sec YDOT = -1037
887791 meter/sec
ZDOT = -19705
384244 ZDOT = -5983
645338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10385826
09 X = -3165599
79
Y = 19656209
78 feet Y = 5991212
74 meter
Z = -1791389
02 Z = -546015
37
XDOT = -11660
828882 XDOT = -3554
220643
YDOT = -7925
228889 feet/sec YDOT = -2415
609765 meter/sec
ZDOT = -19602
911453 ZDOT = -5974
967411
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 19154
70440637
00016717 00000-0 10270-3 0 9042
2 25544 51
6424 68
2191 0007679 5
4567 354
6667 15
51139717 13154
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
70440637 = yrday
fracday
Element set: 904
Inclination: 51
6424 deg
RA of node: 68
2191 deg
Eccentricity:
0007679
Arg of perigee: 5
4567 deg
Mean anomaly: 354
6667 deg
Mean motion: 15
51139717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 320
Coasting Arc #6 (Orbit 1325)
---------------------------------------
Vector Time (GMT): 2019/155/08:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2630047
99 A = 6787088
59 meter
Y = 3663309
59 meter E =
0007304
Z = 5065982
70 I = 51
97334
XDOT = -4515
229205 Wp = 51
95306
YDOT = -5893
691722 meter/sec RA = 64
21306 deg
ZDOT = 1920
226948 TA = 19
52664
MA = 19
49868
Ha = 227
525 n
mi
Hp = 218
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8628766
37 X = -2695424
65
Y = 12018732
24 feet Y = 3633532
10 meter
Z = 16620678
16 Z = 5053048
66
XDOT = -14813
744111 XDOT = -4458
316163
YDOT = -19336
258931 feet/sec YDOT = -5943
866299 meter/sec
ZDOT = 6299
957178 ZDOT = 1898
430625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3665878
18 X = -1117359
67
Y = 14402373
30 feet Y = 4389843
38 meter
Z = 16561565
65 Z = 5047965
21
XDOT = -19911
152752 XDOT = -6068
919359
YDOT = -12190
049025 feet/sec YDOT = -3715
526943 meter/sec
ZDOT = 6201
729809 ZDOT = 1890
287246
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 19155
41308353
00016717 00000-0 10270-3 0 9050
2 25544 51
6415 64
7017 0007725 8
5277 351
6004 15
51191040 13267
Satellite: ISS
Catalog Number: 25544
Epoch time: 19155
41308353 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 64
7017 deg
Eccentricity:
0007725
Arg of perigee: 8
5277 deg
Mean anomaly: 351
6004 deg
Mean motion: 15
51191040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1326
Checksum: 281
Coasting Arc #7 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2019/156/08:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2887918
63 A = 6786427
50 meter
Y = -3196079
08 meter E =
0018570
Z = -5259307
13 I = 51
95517
XDOT = 4596
527384 Wp = 58
14869
YDOT = 6011
904818 meter/sec RA = 59
26701 deg
ZDOT = -1122
836029 TA = 201
07253
MA = 201
14914
Ha = 227
624 n
mi
Hp = 218
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9474798
65 X = 2948990
36
Y = -10485823
77 feet Y = -3163441
90 meter
Z = -17254944
64 Z = -5245130
90
XDOT = 15080
470421 XDOT = 4534
413062
YDOT = 19724
097172 feet/sec YDOT = 6062
959311 meter/sec
ZDOT = -3683
845240 ZDOT = -1100
657469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4794074
26 X = 1461233
84
Y = -13377963
95 feet Y = -4077603
41 meter
Z = -17190240
16 Z = -5239585
20
XDOT = 20576
764504 XDOT = 6271
797821
YDOT = 12006
997887 feet/sec YDOT = 3659
732956 meter/sec
ZDOT = -3583
906147 ZDOT = -1092
374594
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 19156
37946145
00016717 00000-0 10270-3 0 9064
2 25544 51
6415 59
9054 0007846 12
9212 347
2139 15
51156213 13416
Satellite: ISS
Catalog Number: 25544
Epoch time: 19156
37946145 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 59
9054 deg
Eccentricity:
0007846
Arg of perigee: 12
9212 deg
Mean anomaly: 347
2139 deg
Mean motion: 15
51156213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 304
Coasting Arc #8 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2019/157/08:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3201135
15 A = 6785967
53 meter
Y = 2703158
59 meter E =
0008453
Z = 5333807
95 I = 51
93570
XDOT = -4655
641724 Wp = 32
97115
YDOT = -6085
558606 meter/sec RA = 54
32058 deg
ZDOT = 296
702411 TA = 54
25111
MA = 54
17253
Ha = 227
802 n
mi
Hp = 217
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10502411
91 X = -3257033
37
Y = 8868630
54 feet Y = 2667047
73 meter
Z = 17499369
93 Z = 5318122
78
XDOT = -15274
415105 XDOT = -4588
686469
YDOT = -19965
743457 feet/sec YDOT = -6137
246935 meter/sec
ZDOT = 973
433106 ZDOT = 274
248576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6155948
70 X = -1876333
16
Y = 12391726
02 feet Y = 3776998
09 meter
Z = 17427869
44 Z = 5312014
61
XDOT = -21116
209036 XDOT = -6436
220514
YDOT = -11685
868473 feet/sec YDOT = -3561
852710 meter/sec
ZDOT = 872
260602 ZDOT = 265
865032
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 19157
41026282
00016717 00000-0 10270-3 0 9072
2 25544 51
6412 54
7908 0007904 16
1990 343
9412 15
51178987 13574
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41026282 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 54
7908 deg
Eccentricity:
0007904
Arg of perigee: 16
1990 deg
Mean anomaly: 343
9412 deg
Mean motion: 15
51178987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 320
Coasting Arc #9 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2019/157/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3984409
15 A = 6786336
33 meter
Y = -1550469
52 meter E =
0017435
Z = -5283571
40 I = 51
93632
XDOT = 3816
108069 Wp = 70
66688
YDOT = 6562
897067 meter/sec RA = 54
14005 deg
ZDOT = 960
077278 TA = 208
45491
MA = 208
55021
Ha = 227
752 n
mi
Hp = 218
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13072208
48 X = 4027115
43
Y = -5086842
25 feet Y = -1505673
32 meter
Z = -17334551
83 Z = -5264113
21
XDOT = 12520
039598 XDOT = 3737
772745
YDOT = 21531
814524 feet/sec YDOT = 6605
133284 meter/sec
ZDOT = 3149
859837 ZDOT = 978
425418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7653567
77 X = 2332807
46
Y = -11884501
95 feet Y = -3622396
19 meter
Z = -17246066
21 Z = -5256600
98
XDOT = 21922
578460 XDOT = 6682
001915
YDOT = 9466
657652 feet/sec YDOT = 2885
437252 meter/sec
ZDOT = 3232
343695 ZDOT = 985
218358
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 19157
41026342
00016717 00000-0 10270-3 0 9080
2 25544 51
6415 54
7906 0007908 16
6199 343
5210 15
51158781 13577
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41026342 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 54
7906 deg
Eccentricity:
0007908
Arg of perigee: 16
6199 deg
Mean anomaly: 343
5210 deg
Mean motion: 15
51158781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 311
Coasting Arc #10 (Orbit 1372)
---------------------------------------
Vector Time (GMT): 2019/158/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4337249
27 A = 6787065
43 meter
Y = 1093115
54 meter E =
0012700
Z = 5101371
28 I = 51
91883
XDOT = -3733
022776 Wp = 33
84806
YDOT = -6455
621931 meter/sec RA = 49
19254 deg
ZDOT = -1778
158118 TA = 73
35927
MA = 73
21987
Ha = 227
901 n
mi
Hp = 217
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14229820
44 X = -4373929
95
Y = 3586337
06 feet Y = 1044407
43 meter
Z = 16736782
41 Z = 5080213
74
XDOT = -12247
450052 XDOT = -3651
919464
YDOT = -21179
861977 feet/sec YDOT = -6496
913432 meter/sec
ZDOT = -5833
852093 ZDOT = -1796
095748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9273294
41 X = -2826500
14
Y = 11513674
09 feet Y = 3509367
86 meter
Z = 16640637
26 Z = 5072066
24
XDOT = -21674
704007 XDOT = -6606
449781
YDOT = -8849
844997 feet/sec YDOT = -2697
432755 meter/sec
ZDOT = -5914
479172 ZDOT = -1802
733252
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 19158
44106472
00016717 00000-0 10270-3 0 9098
2 25544 51
6419 49
6758 0007894 19
8453 340
3004 15
51167772 13735
Satellite: ISS
Catalog Number: 25544
Epoch time: 19158
44106472 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 49
6758 deg
Eccentricity:
0007894
Arg of perigee: 19
8453 deg
Mean anomaly: 340
3004 deg
Mean motion: 15
51167772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1373
Checksum: 327
Coasting Arc #11 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2019/159/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4699383
35 A = 6788131
01 meter
Y = -735327
25 meter E =
0014562
Z = -4853510
78 I = 51
90052
XDOT = 3587
992045 Wp = 74
81175
YDOT = 6268
378718 meter/sec RA = 44
24330 deg
ZDOT = 2534
412977 TA = 220
01657
MA = 220
12396
Ha = 227
922 n
mi
Hp = 217
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15417924
39 X = 4730832
22
Y = -2412490
99 feet Y = -682598
92 meter
Z = -15923591
81 Z = -4830606
81
XDOT = 11771
627445 XDOT = 3505
319893
YDOT = 20565
546975 feet/sec YDOT = 6308
039546 meter/sec
ZDOT = 8315
003205 ZDOT = 2551
642086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10728839
64 X = 3270150
32
Y = -11477223
14 feet Y = -3498257
61 meter
Z = -15819564
80 Z = -4821803
35
XDOT = 21071
420411 XDOT = 6422
568941
YDOT = 8175
508212 feet/sec YDOT = 2491
894903 meter/sec
ZDOT = 8392
431270 ZDOT = 2558
013051
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 19159
40743889
00016717 00000-0 10270-3 0 9106
2 25544 51
6426 44
8793 0007957 23
5753 336
5761 15
51172858 13888
Satellite: ISS
Catalog Number: 25544
Epoch time: 19159
40743889 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 44
8793 deg
Eccentricity:
0007957
Arg of perigee: 23
5753 deg
Mean anomaly: 336
5761 deg
Mean motion: 15
51172858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 348
Coasting Arc #12 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2019/160/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5084982
78 A = 6789615
99 meter
Y = 379265
05 meter E =
0016089
Z = 4478314
76 I = 51
88050
XDOT = -3353
095809 Wp = 49
63054
YDOT = -6065
301600 meter/sec RA = 39
29516 deg
ZDOT = -3275
768665 TA = 73
35803
MA = 73
18145
Ha = 228
097 n
mi
Hp = 217
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16683014
37 X = -5110598
94
Y = 1244307
91 feet Y = 322257
45 meter
Z = 14692633
72 Z = 4453551
79
XDOT = -11000
970501 XDOT = -3269
110897
YDOT = -19899
283463 feet/sec YDOT = -6102
328289 meter/sec
ZDOT = -10747
272522 ZDOT = -3291
853390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12241923
53 X = -3731338
29
Y = 11545446
26 feet Y = 3519052
02 meter
Z = 14580217
25 Z = 4444050
22
XDOT = -20186
480313 XDOT = -6152
839200
YDOT = -7666
013585 feet/sec YDOT = -2336
600941 meter/sec
ZDOT = -10819
525067 ZDOT = -3297
791240
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 19160
43823744
00016717 00000-0 10270-3 0 9111
2 25544 51
6424 39
7643 0008017 27
6594 332
4982 15
51162662 14040
Satellite: ISS
Catalog Number: 25544
Epoch time: 19160
43823744 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 39
7643 deg
Eccentricity:
0008017
Arg of perigee: 27
6594 deg
Mean anomaly: 332
4982 deg
Mean motion: 15
51162662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 305
Coasting Arc #13 (Orbit 1418)
---------------------------------------
Vector Time (GMT): 2019/161/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5446859
23 A = 6791081
84 meter
Y = -138543
47 meter E =
0011738
Z = -4059264
98 I = 51
85977
XDOT = 3060
645280 Wp = 65
94685
YDOT = 5821
322936 meter/sec RA = 34
34637 deg
ZDOT = 3921
794952 TA = 244
62329
MA = 244
74487
Ha = 228
082 n
mi
Hp = 217
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17870273
08 X = 5467721
24
Y = -454538
96 feet Y = -77515
82 meter
Z = -13317798
49 Z = -4032755
60
XDOT = 10041
487138 XDOT = 2976
272266
YDOT = 19098
828529 feet/sec YDOT = 5855
077062 meter/sec
ZDOT = 12866
781340 ZDOT = 3936
458039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13451462
84 X = 4100005
87
Y = -11908037
34 feet Y = -3629569
78 meter
Z = -13197492
81 Z = -4022595
81
XDOT = 19043
841400 XDOT = 5804
562859
YDOT = 7229
051748 feet/sec YDOT = 2203
414973 meter/sec
ZDOT = 12932
604301 ZDOT = 3941
857791
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 19161
40461048
00016717 00000-0 10270-3 0 9125
2 25544 51
6430 34
9683 0007977 30
8563 329
3056 15
51179568 14190
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
40461048 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 34
9683 deg
Eccentricity:
0007977
Arg of perigee: 30
8563 deg
Mean anomaly: 329
3056 deg
Mean motion: 15
51179568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1419
Checksum: 319
Coasting Arc #14 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2019/161/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3399479
02 A = 6786438
52 meter
Y = -2681099
62 meter E =
0018442
Z = -5240570
19 I = 51
84066
XDOT = 5717
775748 Wp = 75
21739
YDOT = 4943
303945 meter/sec RA = 33
75008 deg
ZDOT = 1188
091167 TA = 206
12594
MA = 206
21912
Ha = 227
996 n
mi
Hp = 217
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11153146
40 X = 3454662
90
Y = -8796258
59 feet Y = -2642775
19 meter
Z = -17193471
74 Z = -5223923
07
XDOT = 18759
106784 XDOT = 5656
302283
YDOT = 16218
188796 feet/sec YDOT = 5006
900282 meter/sec
ZDOT = 3897
936900 ZDOT = 1215
717098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7716078
77 X = -2351860
81
Y = -12034616
48 feet Y = -3668151
10 meter
Z = -17117606
29 Z = -5217446
40
XDOT = 17005
974399 XDOT = 5183
420997
YDOT = -16587
384083 feet/sec YDOT = -5055
834669 meter/sec
ZDOT = 4022
685926 ZDOT = 1226
114670
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 19161
53345855
00016717 00000-0 10270-3 0 9137
2 25544 51
6427 34
3290 0007939 30
1176 330
0430 15
51184136 14210
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
53345855 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 34
3290 deg
Eccentricity:
0007939
Arg of perigee: 30
1176 deg
Mean anomaly: 330
0430 deg
Mean motion: 15
51184136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 281
Coasting Arc #15 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2019/162/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3885569
22 A = 6787258
15 meter
Y = 2376057
93 meter E =
0013596
Z = 5027375
49 I = 51
81618
XDOT = -5579
952093 Wp = 42
46288
YDOT = -4863
053297 meter/sec RA = 28
79527 deg
ZDOT = -2001
309116 TA = 67
00285
MA = 66
85950
Ha = 228
094 n
mi
Hp = 217
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12747930
50 X = -3936270
43
Y = 7795465
66 feet Y = 2332322
81 meter
Z = 16494014
09 Z = 5008377
90
XDOT = -18306
929439 XDOT = -5515
436064
YDOT = -15954
899268 feet/sec YDOT = -4925
091309 meter/sec
ZDOT = -6565
974790 ZDOT = -2028
258248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6803963
49 X = 2073848
07
Y = 13410098
74 feet Y = 4087398
10 meter
Z = 16407524
20 Z = 5001013
37
XDOT = -16310
189421 XDOT = -4971
345736
YDOT = 16510
096157 feet/sec YDOT = 5032
277309 meter/sec
ZDOT = -6687
649578 ZDOT = -2038
395591
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 19162
56425450
00016717 00000-0 10270-3 0 9142
2 25544 51
6436 29
2136 0007895 32
6327 327
5310 15
51204243 14375
Satellite: ISS
Catalog Number: 25544
Epoch time: 19162
56425450 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 29
2136 deg
Eccentricity:
0007895
Arg of perigee: 32
6327 deg
Mean anomaly: 327
5310 deg
Mean motion: 15
51204243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 291
Coasting Arc #16 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2019/163/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4345805
59 A = 6788491
36 meter
Y = -2170833
23 meter E =
0015273
Z = -4753495
52 I = 51
78942
XDOT = 5354
533295 Wp = 78
93912
YDOT = 4729
209495 meter/sec RA = 23
83881 deg
ZDOT = 2745
895058 TA = 218
17509
MA = 218
28336
Ha = 228
140 n
mi
Hp = 217
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14257892
36 X = 4392847
45
Y = -7122156
25 feet Y = -2121971
86 meter
Z = -15595457
75 Z = -4732271
07
XDOT = 17567
366452 XDOT = 5287
913856
YDOT = 15515
779182 feet/sec YDOT = 4788
714861 meter/sec
ZDOT = 9008
842054 ZDOT = 2771
744206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6273720
35 X = -1912229
96
Y = -14753156
71 feet Y = -4496762
16 meter
Z = -15498893
73 Z = -4724062
81
XDOT = 15434
882512 XDOT = 4704
552190
YDOT = -16114
553606 feet/sec YDOT = -4911
715939 meter/sec
ZDOT = 9125
528573 ZDOT = 2781
461109
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 19163
53062605
00016717 00000-0 10270-3 0 9150
2 25544 51
6426 24
4167 0007958 36
7949 323
3747 15
51184877 14525
Satellite: ISS
Catalog Number: 25544
Epoch time: 19163
53062605 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 24
4167 deg
Eccentricity:
0007958
Arg of perigee: 36
7949 deg
Mean anomaly: 323
3747 deg
Mean motion: 15
51184877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 329
Coasting Arc #17 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2019/164/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4820004
04 A = 6789955
52 meter
Y = 1973481
81 meter E =
0017019
Z = 4349451
78 I = 51
76319
XDOT = -5040
803872 Wp = 57
18939
YDOT = -4616
233053 meter/sec RA = 18
88309 deg
ZDOT = -3472
744431 TA = 68
11861
MA = 67
93772
Ha = 228
229 n
mi
Hp = 217
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15813661
54 X = -4862841
23
Y = 6474677
85 feet Y = 1919341
10 meter
Z = 14269854
91 Z = 4325934
00
XDOT = -16538
070447 XDOT = -4971
940393
YDOT = -15145
121565 feet/sec YDOT = -4672
217394 meter/sec
ZDOT = -11393
518475 ZDOT = -3497
064271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5815935
49 X = 1772697
14
Y = 16161956
14 feet Y = 4926164
23 meter
Z = 14162915
38 Z = 4316856
61
XDOT = -14631
481145 XDOT = -4459
675453
YDOT = 15400
324124 feet/sec YDOT = 4694
018793 meter/sec
ZDOT = -11503
267393 ZDOT = -3506
195901
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 19164
56142038
00016717 00000-0 10270-3 0 9164
2 25544 51
6422 19
3015 0007985 39
8497 320
3239 15
51207067 14685
Satellite: ISS
Catalog Number: 25544
Epoch time: 19164
56142038 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 19
3015 deg
Eccentricity:
0007985
Arg of perigee: 39
8497 deg
Mean anomaly: 320
3239 deg
Mean motion: 15
51207067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 313
Coasting Arc #18 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2019/165/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5232627
29 A = 6791580
79 meter
Y = -1878075
38 meter E =
0012248
Z = -3907740
05 I = 51
73528
XDOT = 4659
482320 Wp = 70
60488
YDOT = 4485
532168 meter/sec RA = 13
92649 deg
ZDOT = 4097
925353 TA = 242
30674
MA = 242
43107
Ha = 228
241 n
mi
Hp = 217
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17167412
38 X = 5272221
36
Y = -6161664
62 feet Y = -1819338
53 meter
Z = -12820669
46 Z = -3882225
78
XDOT = 15287
015484 XDOT = 4589
071897
YDOT = 14716
312887 feet/sec YDOT = 4537
243491 meter/sec
ZDOT = 13444
636986 ZDOT = 4120
389199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5747899
19 X = -1751959
67
Y = -17395639
22 feet Y = -5302190
83 meter
Z = -12704688
71 Z = -3872389
12
XDOT = 13808
168042 XDOT = 4208
729619
YDOT = -14420
715780 feet/sec YDOT = -4395
434170 meter/sec
ZDOT = 13545
970904 ZDOT = 4128
811931
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 19165
52779187
00016717 00000-0 10270-3 0 9173
2 25544 51
6410 14
5054 0007847 44
2677 315
9100 15
51180368 14837
Satellite: ISS
Catalog Number: 25544
Epoch time: 19165
52779187 = yrday
fracday
Element set: 917
Inclination: 51
6410 deg
RA of node: 14
5054 deg
Eccentricity:
0007847
Arg of perigee: 44
2677 deg
Mean anomaly: 315
9100 deg
Mean motion: 15
51180368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 314
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