[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 25th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14119 0213 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
205/22:24:29
000 0
0 0
0 0
0
N/A 0
0 0
0 227
2
000/00:00:00
000 0
0 0
0 219
2
207/04:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 219
4
210/10:44:30
000 0
0 0
0 0
0
N/A 0
0 0
0 226
6
000/00:00:00
000 0
0 0
0 219
9
212/15:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 220
2
213/11:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 220
3
216/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
8
000/00:00:00
000 0
0 0
0 220
9
Coasting Arc #1 (Orbit 2103)
---------------------------------------
Vector Time (GMT): 2019/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5716236
47 A = 6795491
68 meter
Y = -2569747
96 meter E =
0016514
Z = 2600478
79 I = 51
67773
XDOT = 4103
075166 Wp = 124
94844
YDOT = 3801
170480 meter/sec RA = 174
93815 deg
ZDOT = -5248
546184 TA = 25
80940
MA = 25
72710
Ha = 227
090 n
mi
Hp = 219
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18754056
66 X = 5731915
72
Y = -8430931
63 feet Y = -2505737
48 meter
Z = 8531754
55 Z = 2628283
80
XDOT = 13461
532696 XDOT = 4085
758736
YDOT = 12471
031759 feet/sec YDOT = 3846
957453 meter/sec
ZDOT = -17219
639711 ZDOT = -5228
656977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16862457
14 X = -5139676
94
Y = -11673810
94 feet Y = -3558177
57 meter
Z = 8658277
10 Z = 2639042
86
XDOT = 2834
075747 XDOT = 863
826288
YDOT = -16832
865357 feet/sec YDOT = -5130
657361 meter/sec
ZDOT = -17129
506703 ZDOT = -5221
073643
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 19205
53757005
00016717 00000-0 10270-3 0 9006
2 25544 51
6383 175
9689 0006402 176
6753 183
4441 15
51001776 21045
Satellite: ISS
Catalog Number: 25544
Epoch time: 19205
53757005 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 175
9689 deg
Eccentricity:
0006402
Arg of perigee: 176
6753 deg
Mean anomaly: 183
4441 deg
Mean motion: 15
51001776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2104
Checksum: 305
Coasting Arc #2 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2019/205/22:24:29
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4420723
07 A = 6790744
20 meter
Y = -2859251
69 meter E =
0013521
Z = 4286928
05 I = 51
67543
XDOT = 5774
056995 Wp = 135
21341
YDOT = -3563
479776 meter/sec RA = 172
83088 deg
ZDOT = 3561
301586 TA = 278
38263
MA = 278
53588
Ha = 227
228 n
mi
Hp = 219
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14503684
63 X = -4409244
90
Y = -9380747
02 feet Y = -2908623
43 meter
Z = 14064724
58 Z = 4265481
68
XDOT = 18943
756545 XDOT = 5796
177019
YDOT = -11691
206613 feet/sec YDOT = -3498
786771 meter/sec
ZDOT = 11684
060322 ZDOT = 3589
403067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7371597
14 X = 2246862
81
Y = -15708013
48 feet Y = -4787802
51 meter
Z = 13967448
87 Z = 4257278
41
XDOT = 12931
991756 XDOT = 3941
671087
YDOT = 16619
663720 feet/sec YDOT = 5065
673502 meter/sec
ZDOT = 11812
002400 ZDOT = 3600
298332
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 19205
98859232
00016717 00000-0 10270-3 0 9011
2 25544 51
6376 173
7281 0006703 179
9583 180
1570 15
51014125 21119
Satellite: ISS
Catalog Number: 25544
Epoch time: 19205
98859232 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 173
7281 deg
Eccentricity:
0006703
Arg of perigee: 179
9583 deg
Mean anomaly: 180
1570 deg
Mean motion: 15
51014125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 304
Coasting Arc #3 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2019/206/22:24:29
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3982269
79 A = 6789294
30 meter
Y = 2915171
94 meter E =
0010169
Z = -4669195
21 I = 51
70505
XDOT = -6070
498051 Wp = 108
40776
YDOT = 3651
575340 meter/sec RA = 167
87074 deg
ZDOT = -2905
915104 TA = 132
71698
MA = 132
63132
Ha = 227
154 n
mi
Hp = 219
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13065189
59 X = 3972055
75
Y = 9564212
39 feet Y = 2959647
75 meter
Z = -15318881
93 Z = -4649875
52
XDOT = -19916
332187 XDOT = -6096
764607
YDOT = 11980
234056 feet/sec YDOT = 3583
544139 meter/sec
ZDOT = -9533
842206 ZDOT = -2935
466636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7494691
72 X = -2284382
04
Y = 14445748
46 feet Y = 4403064
13 meter
Z = -15231264
83 Z = -4642489
52
XDOT = -13750
070192 XDOT = -4191
021394
YDOT = -17298
919145 feet/sec YDOT = -5272
710555 meter/sec
ZDOT = -9668
399123 ZDOT = -2946
928053
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 19206
95507013
00016717 00000-0 10270-3 0 9027
2 25544 51
6390 168
9328 0006639 180
7328 179
3814 15
51017206 21268
Satellite: ISS
Catalog Number: 25544
Epoch time: 19206
95507013 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 168
9328 deg
Eccentricity:
0006639
Arg of perigee: 180
7328 deg
Mean anomaly: 179
3814 deg
Mean motion: 15
51017206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 309
Coasting Arc #4 (Orbit 2129)
---------------------------------------
Vector Time (GMT): 2019/207/04:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3904511
51 A = 6789115
71 meter
Y = 2912396
64 meter E =
0010169
Z = -4736035
54 I = 51
71464
XDOT = -6105
993117 Wp = 108
53858
YDOT = 3700
276826 meter/sec RA = 166
59340 deg
ZDOT = -2766
504479 TA = 134
09672
MA = 134
01299
Ha = 227
126 n
mi
Hp = 219
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12810077
15 X = 3894658
97
Y = 9555107
08 feet Y = 2956004
95 meter
Z = -15538174
35 Z = -4717092
67
XDOT = -20032
785816 XDOT = -6133
478802
YDOT = 12140
015832 feet/sec YDOT = 3631
841878 meter/sec
ZDOT = -9076
458263 ZDOT = -2796
231378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14583615
34 X = 4445085
95
Y = 6736364
62 feet Y = 2053243
94 meter
Z = -15452267
32 Z = -4709851
08
XDOT = -16602
984334 XDOT = -5060
589625
YDOT = 14874
080368 feet/sec YDOT = 4533
619696 meter/sec
ZDOT = -9211
820873 ZDOT = -2807
763002
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 19207
21279611
00016717 00000-0 10270-3 0 9038
2 25544 51
6411 167
6561 0006728 184
3688 175
7405 15
50987495 21301
Satellite: ISS
Catalog Number: 25544
Epoch time: 19207
21279611 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 167
6561 deg
Eccentricity:
0006728
Arg of perigee: 184
3688 deg
Mean anomaly: 175
7405 deg
Mean motion: 15
50987495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2130
Checksum: 323
Coasting Arc #5 (Orbit 2145)
---------------------------------------
Vector Time (GMT): 2019/208/04:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3474423
85 A = 6787915
46 meter
Y = -3000502
52 meter E =
0010845
Z = 4999630
59 I = 51
74310
XDOT = 6308
642842 Wp = 157
00292
YDOT = -3821
815935 meter/sec RA = 161
63501 deg
ZDOT = 2079
190563 TA = 272
72178
MA = 272
84591
Ha = 226
989 n
mi
Hp = 219
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11399028
37 X = -3464898
42
Y = -9844168
37 feet Y = -3039303
23 meter
Z = 16402987
51 Z = 4982776
07
XDOT = 20697
647118 XDOT = 6340
811124
YDOT = -12538
766192 feet/sec YDOT = -3751
088614 meter/sec
ZDOT = 6821
491350 ZDOT = 2109
913137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13389919
39 X = -4081247
43
Y = -7075073
47 feet Y = -2156482
39 meter
Z = 16326570
13 Z = 4976338
57
XDOT = 16877
413022 XDOT = 5144
235489
YDOT = -15791
317668 feet/sec YDOT = -4813
193625 meter/sec
ZDOT = 6961
410909 ZDOT = 2121
838045
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 19208
24370167
00016717 00000-0 10270-3 0 9041
2 25544 51
6410 162
5414 0006645 188
0207 172
0839 15
51020022 21460
Satellite: ISS
Catalog Number: 25544
Epoch time: 19208
24370167 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 162
5414 deg
Eccentricity:
0006645
Arg of perigee: 188
0207 deg
Mean anomaly: 172
0839 deg
Mean motion: 15
51020022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2146
Checksum: 275
Coasting Arc #6 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2019/209/04:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3003755
56 A = 6787150
76 meter
Y = 3170265
95 meter E =
0012977
Z = -5205241
04 I = 51
77068
XDOT = -6438
127793 Wp = 108
44498
YDOT = 3920
308129 meter/sec RA = 156
67735 deg
ZDOT = -1334
265507 TA = 148
77376
MA = 148
69661
Ha = 226
888 n
mi
Hp = 219
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9854841
07 X = 2993365
45
Y = 10401135
00 feet Y = 3203798
59 meter
Z = -17077562
46 Z = -5190674
88
XDOT = -21122
466512 XDOT = -6475
006243
YDOT = 12861
903312 feet/sec YDOT = 3848
106425 meter/sec
ZDOT = -4377
511505 ZDOT = -1365
628369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12145302
59 X = 3701888
23
Y = 7748764
82 feet Y = 2361823
52 meter
Z = -17011552
25 Z = -5185121
13
XDOT = -16889
613758 XDOT = -5147
954274
YDOT = 16597
220013 feet/sec YDOT = 5058
832660 meter/sec
ZDOT = -4520
374298 ZDOT = -1377
810086
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 19209
21017707
00016717 00000-0 10270-3 0 9058
2 25544 51
6402 157
7465 0006659 191
2753 168
8250 15
50984109 21611
Satellite: ISS
Catalog Number: 25544
Epoch time: 19209
21017707 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 157
7465 deg
Eccentricity:
0006659
Arg of perigee: 191
2753 deg
Mean anomaly: 168
8250 deg
Mean motion: 15
50984109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 313
Coasting Arc #7 (Orbit 2176)
---------------------------------------
Vector Time (GMT): 2019/210/04:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2566104
97 A = 6786538
64 meter
Y = -3361974
19 meter E =
0007648
Z = 5307340
28 I = 51
80007
XDOT = 6498
088879 Wp = 173
19855
YDOT = -4020
655702 meter/sec RA = 151
72124 deg
ZDOT = 587
425403 TA = 271
16044
MA = 271
24806
Ha = 226
741 n
mi
Hp = 219
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8418979
56 X = -2554099
50
Y = -11030099
06 feet Y = -3390603
75 meter
Z = 17412533
73 Z = 5294903
97
XDOT = 21319
189234 XDOT = 6539
712704
YDOT = -13191
127631 feet/sec YDOT = -3947
756853 meter/sec
ZDOT = 1927
248696 ZDOT = 619
090886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11049042
25 X = -3367748
08
Y = -8509942
85 feet Y = -2593830
58 meter
Z = 17356214
20 Z = 5290174
09
XDOT = 16653
708841 XDOT = 5076
050455
YDOT = -17347
433482 feet/sec YDOT = -5287
497725 meter/sec
ZDOT = 2071
521694 ZDOT = 631
399812
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 19210
24107961
00016717 00000-0 10270-3 0 9066
2 25544 51
6410 152
6316 0006562 195
3032 164
7922 15
51023237 21772
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
24107961 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 152
6316 deg
Eccentricity:
0006562
Arg of perigee: 195
3032 deg
Mean anomaly: 164
7922 deg
Mean motion: 15
51023237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2177
Checksum: 282
Coasting Arc #8 (Orbit 2180)
---------------------------------------
Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602864
96 A = 6787315
89 meter
Y = -2598636
30 meter E =
0009275
Z = 5131859
94 I = 51
80920
XDOT = 5779
810369 Wp = 165
46262
YDOT = -4757
193581 meter/sec RA = 150
46393 deg
ZDOT = 1639
449799 TA = 268
68900
MA = 268
79527
Ha = 226
611 n
mi
Hp = 219
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11820423
10 X = -3598465
89
Y = -8525709
66 feet Y = -2638902
15 meter
Z = 16836810
82 Z = 5114369
13
XDOT = 18962
632443 XDOT = 5824
613676
YDOT = -15607
590490 feet/sec YDOT = -4692
309389 meter/sec
ZDOT = 5378
772305 ZDOT = 1667
633781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4654511
29 X = -1418695
04
Y = 13907253
05 feet Y = 4238930
73 meter
Z = 16757450
98 Z = 5107671
06
XDOT = -19452
943162 XDOT = -5929
257076
YDOT = -13183
836653 feet/sec YDOT = -4018
433412 meter/sec
ZDOT = 5507
271190 ZDOT = 1678
616259
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 19210
49880574
00016717 00000-0 10270-3 0 9072
2 25544 51
6400 151
3537 0006295 196
9410 163
1532 15
51033446 21810
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
49880574 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 151
3537 deg
Eccentricity:
0006295
Arg of perigee: 196
9410 deg
Mean anomaly: 163
1532 deg
Mean motion: 15
51033446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2181
Checksum: 296
Coasting Arc #9 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3166429
00 A = 6786743
13 meter
Y = 2864283
97 meter E =
0012885
Z = -5285376
51 I = 51
83565
XDOT = -5850
740163 Wp = 108
71794
YDOT = 4857
434954 meter/sec RA = 145
50920 deg
ZDOT = -878
541434 TA = 152
92220
MA = 152
85493
Ha = 226
468 n
mi
Hp = 220
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10388546
60 X = 3159837
38
Y = 9397257
11 feet Y = 2899657
02 meter
Z = -17340474
13 Z = -5270011
11
XDOT = -19195
341741 XDOT = -5900
355172
YDOT = 15936
466386 feet/sec YDOT = 4791
730568 meter/sec
ZDOT = -2882
353787 ZDOT = -907
081502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5685275
44 X = 1732871
95
Y = -12896506
95 feet Y = -3930855
32 meter
Z = -17270788
52 Z = -5264136
34
XDOT = 20146
323021 XDOT = 6140
599257
YDOT = 12890
076972 feet/sec YDOT = 3928
895461 meter/sec
ZDOT = -3012
504198 ZDOT = -918
211280
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 19211
46527621
00016717 00000-0 10270-3 0 9082
2 25544 51
6401 146
5576 0006178 199
6609 160
4304 15
51004723 21969
Satellite: ISS
Catalog Number: 25544
Epoch time: 19211
46527621 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 146
5576 deg
Eccentricity:
0006178
Arg of perigee: 199
6609 deg
Mean anomaly: 160
4304 deg
Mean motion: 15
51004723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 305
Coasting Arc #10 (Orbit 2211)
---------------------------------------
Vector Time (GMT): 2019/212/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2770189
97 A = 6786411
30 meter
Y = -3146970
40 meter E =
0005950
Z = 5336679
88 I = 51
86209
XDOT = 5857
006674 Wp = 181
09840
YDOT = -4940
975481 meter/sec RA = 140
55857 deg
ZDOT = 120
861237 TA = 267
71862
MA = 267
78675
Ha = 226
359 n
mi
Hp = 220
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9088549
76 X = -2760715
78
Y = -10324706
04 feet Y = -3177896
24 meter
Z = 17508792
24 Z = 5323246
29
XDOT = 19215
901162 XDOT = 5911
235718
YDOT = -16210
549477 feet/sec YDOT = -4875
175119 meter/sec
ZDOT = 396
526368 ZDOT = 149
442869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6762475
22 X = -2061202
45
Y = 12066426
31 feet Y = 3677846
74 meter
Z = 17447904
81 Z = 5318121
39
XDOT = -20704
029036 XDOT = -6310
588050
YDOT = -12392
775417 feet/sec YDOT = -3777
317947 meter/sec
ZDOT = 526
894782 ZDOT = 160
597530
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 19212
49617634
00016717 00000-0 10270-3 0 9091
2 25544 51
6405 141
4442 0006154 204
1889 155
8974 15
51024014 22120
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
49617634 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 141
4442 deg
Eccentricity:
0006154
Arg of perigee: 204
1889 deg
Mean anomaly: 155
8974 deg
Mean motion: 15
51024014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2212
Checksum: 295
Coasting Arc #11 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2019/212/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1832352
12 A = 6792456
46 meter
Y = -5382307
10 meter E =
0010020
Z = 3704561
63 I = 51
89018
XDOT = 6259
848124 Wp = 116
22611
YDOT = -861
698868 meter/sec RA = 139
53577 deg
ZDOT = -4343
427071 TA = 19
84162
MA = 19
80268
Ha = 226
154 n
mi
Hp = 220
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6011653
94 X = 1874408
18
Y = -17658487
87 feet Y = -5361581
71 meter
Z = 12154073
59 Z = 3713563
85
XDOT = 20537
559461 XDOT = 6290
116093
YDOT = -2827
096023 feet/sec YDOT = -791
527136 meter/sec
ZDOT = -14250
088817 ZDOT = -4312
946386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5362646
74 X = -1634534
73
Y = 17838098
10 feet Y = 5437052
30 meter
Z = 12195407
25 Z = 3717160
13
XDOT = -19231
355437 XDOT = -5861
717137
YDOT = 3876
713573 feet/sec YDOT = 1181
622297 meter/sec
ZDOT = -14111
365556 ZDOT = -4301
144222
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 19212
68946894
00016717 00000-0 10270-3 0 9107
2 25544 51
6429 140
4865 0006085 205
5912 154
4939 15
51047312 22154
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
68946894 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 140
4865 deg
Eccentricity:
0006085
Arg of perigee: 205
5912 deg
Mean anomaly: 154
4939 deg
Mean motion: 15
51047312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 315
Coasting Arc #12 (Orbit 2227)
---------------------------------------
Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 435554
34 A = 6790430
86 meter
Y = -5202562
70 meter E =
0006718
Z = 4335146
24 I = 51
90281
XDOT = 6371
191637 Wp = 111
73170
YDOT = -2403
457573 meter/sec RA = 135
40450 deg
ZDOT = -3522
531742 TA = 13
99888
MA = 13
98027
Ha = 226
173 n
mi
Hp = 220
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1428984
04 X = 472641
35
Y = -17068775
27 feet Y = -5197485
04 meter
Z = 14222920
73 Z = 4337351
57
XDOT = 20902
859701 XDOT = 6414
704319
YDOT = -7885
359493 feet/sec YDOT = -2331
966832 meter/sec
ZDOT = -11556
862672 ZDOT = -3491
478233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14964249
24 X = -4561103
17
Y = 8316267
07 feet Y = 2534798
20 meter
Z = 14233323
77 Z = 4338317
08
XDOT = -17556
119399 XDOT = -5351
105193
YDOT = -12041
943194 feet/sec YDOT = -3670
384285 meter/sec
ZDOT = -11415
407463 ZDOT = -3479
416195
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 19213
52707547
00016717 00000-0 10270-3 0 9112
2 25544 51
6418 136
3300 0006191 208
2432 151
8384 15
51015828 22281
Satellite: ISS
Catalog Number: 25544
Epoch time: 19213
52707547 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 136
3300 deg
Eccentricity:
0006191
Arg of perigee: 208
2432 deg
Mean anomaly: 151
8384 deg
Mean motion: 15
51015828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2228
Checksum: 287
Coasting Arc #13 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2019/214/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -684004
34 A = 6791912
39 meter
Y = 5518612
74 meter E =
0007606
Z = -3907862
49 I = 51
93131
XDOT = -6081
713736 Wp = 156
79409
YDOT = 2163
441558 meter/sec RA = 130
46023 deg
ZDOT = 4115
598108 TA = 156
29171
MA = 156
25665
Ha = 225
980 n
mi
Hp = 220
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2244108
73 X = -726682
51
Y = 18105684
84 feet Y = 5510725
32 meter
Z = -12821071
15 Z = -3911288
38
XDOT = -19953
129054 XDOT = -6125
444707
YDOT = 7097
905373 feet/sec YDOT = 2095
186813 meter/sec
ZDOT = 13502
618464 ZDOT = 4085
950131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16140654
09 X = 4919671
37
Y = -8480628
49 feet Y = -2584895
56 meter
Z = -12837053
36 Z = -3912733
86
XDOT = 16587
907117 XDOT = 5055
994089
YDOT = 11316
167114 feet/sec YDOT = 3449
167736 meter/sec
ZDOT = 13367
558757 ZDOT = 4074
431909
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 19214
49354001
00016717 00000-0 10270-3 0 9123
2 25544 51
6423 131
5344 0006106 211
7706 148
3077 15
51024194 22434
Satellite: ISS
Catalog Number: 25544
Epoch time: 19214
49354001 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 131
5344 deg
Eccentricity:
0006106
Arg of perigee: 211
7706 deg
Mean anomaly: 148
3077 deg
Mean motion: 15
51024194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 271
Coasting Arc #14 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2019/215/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 872082
09 A = 6793465
06 meter
Y = -5806439
27 meter E =
0010191
Z = 3404135
59 I = 51
95701
XDOT = 5802
250244 Wp = 119
39892
YDOT = -1860
281369 meter/sec RA = 125
52055 deg
ZDOT = -4653
935079 TA = 21
04219
MA = 21
00029
Ha = 225
879 n
mi
Hp = 220
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2861161
70 X = 920411
55
Y = -19049997
59 feet Y = -5796416
90 meter
Z = 11168423
86 Z = 3408488
95
XDOT = 19036
254081 XDOT = 5845
226890
YDOT = -6103
285331 feet/sec YDOT = -1795
156094 meter/sec
ZDOT = -15268
815875 ZDOT = -4625
646288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17126031
30 X = -5220014
34
Y = 8794058
70 feet Y = 2680429
09 meter
Z = 11188651
83 Z = 3410301
08
XDOT = -15442
241604 XDOT = -4706
795241
YDOT = -10787
274123 feet/sec YDOT = -3287
961153 meter/sec
ZDOT = -15139
949772 ZDOT = -4614
656690
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 19215
52443392
00016717 00000-0 10270-3 0 9131
2 25544 51
6421 126
4205 0006058 215
4295 144
6455 15
51019330 22593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19215
52443392 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 126
4205 deg
Eccentricity:
0006058
Arg of perigee: 215
4295 deg
Mean anomaly: 144
6455 deg
Mean motion: 15
51019330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 288
Coasting Arc #15 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2019/216/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1002817
95 A = 6794872
08 meter
Y = 6085284
87 meter E =
0002611
Z = -2855764
11 I = 51
98048
XDOT = -5512
627222 Wp = 174
99531
YDOT = 1487
072121 meter/sec RA = 120
58246 deg
ZDOT = 5102
382548 TA = 152
77165
MA = 152
75796
Ha = 225
687 n
mi
Hp = 220
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3290085
15 X = -1056919
39
Y = 19964845
37 feet Y = 6073768
19 meter
Z = -9369304
81 Z = -2860766
65
XDOT = -18086
047316 XDOT = -5553
630424
YDOT = 4878
845542 feet/sec YDOT = 1425
196722 meter/sec
ZDOT = 16740
100222 ZDOT = 5075
505242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17970105
06 X = 5477288
02
Y = -9276829
97 feet Y = -2827577
77 meter
Z = -9392514
76 Z = -2862838
50
XDOT = 14068
200261 XDOT = 4287
987440
YDOT = 10419
330360 feet/sec YDOT = 3175
811894 meter/sec
ZDOT = 16617
674135 ZDOT = 5065
067076
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 19216
49089531
00016717 00000-0 10270-3 0 9140
2 25544 51
6422 121
6250 0006119 219
4255 140
6451 15
51036196 22747
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
49089531 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 121
6250 deg
Eccentricity:
0006119
Arg of perigee: 219
4255 deg
Mean anomaly: 140
6451 deg
Mean motion: 15
51036196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 291
Coasting Arc #16 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2019/216/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3799862
17 A = 6798139
43 meter
Y = 5584567
80 meter E =
0007183
Z = 743144
55 I = 51
99207
XDOT = -3550
824411 Wp = 65
08208
YDOT = -3217
016748 meter/sec RA = 119
29983 deg
ZDOT = 5976
792061 TA = 302
89593
MA = 302
96502
Ha = 225
769 n
mi
Hp = 220
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12466739
39 X = -3865637
71
Y = 18322072
83 feet Y = 5541707
29 meter
Z = 2438138
29 Z = 724526
89
XDOT = -11649
686389 XDOT = -3543
618290
YDOT = -10554
516890 feet/sec YDOT = -3256
684329 meter/sec
ZDOT = 19608
897837 ZDOT = 5959
561283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3030243
24 X = -923618
14
Y = -21962319
57 feet Y = -6694115
00 meter
Z = 2352999
66 Z = 717194
30
XDOT = 14215
166762 XDOT = 4332
782829
YDOT = 146
531527 feet/sec YDOT = 44
662809 meter/sec
ZDOT = 19530
715502 ZDOT = 5952
962085
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 19216
81304773
00016717 00000-0 10270-3 0 9155
2 25544 51
6386 120
0225 0006376 219
2328 140
8362 15
51027541 22797
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
81304773 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 120
0225 deg
Eccentricity:
0006376
Arg of perigee: 219
2328 deg
Mean anomaly: 140
8362 deg
Mean motion: 15
51027541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 296
Coasting Arc #17 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2019/217/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3715499
48 A = 6797409
84 meter
Y = -5501413
05 meter E =
0011263
Z = -1427148
92 I = 52
00643
XDOT = 3300
960158 Wp = 175
11510
YDOT = 3736
263094 meter/sec RA = 114
36703 deg
ZDOT = -5823
063729 TA = 20
35258
MA = 20
30773
Ha = 225
550 n
mi
Hp = 220
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12189958
91 X = 3783673
92
Y = -18049255
41 feet Y = -5459482
52 meter
Z = -4682247
13 Z = -1408935
14
XDOT = 10829
921777 XDOT = 3287
219665
YDOT = 12258
081016 feet/sec YDOT = 3773
099973 meter/sec
ZDOT = -19104
539793 ZDOT = -5807
062469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3412273
85 X = 1040061
07
Y = 21529057
25 feet Y = 6562056
65 meter
Z = -4598938
84 Z = -1401756
56
XDOT = -14806
386247 XDOT = -4512
986528
YDOT = -1708
587848 feet/sec YDOT = -520
777576 meter/sec
ZDOT = -19031
993302 ZDOT = -5800
951558
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 19217
77950529
00016717 00000-0 10270-3 0 9168
2 25544 51
6397 115
2268 0006134 223
8136 136
2529 15
51068236 22949
Satellite: ISS
Catalog Number: 25544
Epoch time: 19217
77950529 = yrday
fracday
Element set: 916
Inclination: 51
6397 deg
RA of node: 115
2268 deg
Eccentricity:
0006134
Arg of perigee: 223
8136 deg
Mean anomaly: 136
2529 deg
Mean motion: 15
51068236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 321
Coasting Arc #18 (Orbit 2309)
---------------------------------------
Vector Time (GMT): 2019/218/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933877
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3608085
23 A = 6796554
18 meter
Y = 5372302
82 meter E =
0008521
Z = 2068338
85 I = 52
01559
XDOT = -3113
628944 Wp = 86
19573
YDOT = -4242
168085 meter/sec RA = 109
43384 deg
ZDOT = 5567
899878 TA = 296
52594
MA = 296
61328
Ha = 225
488 n
mi
Hp = 221
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11837549
96 X = -3677938
44
Y = 17625665
42 feet Y = 5331564
06 meter
Z = 6785888
61 Z = 2050642
74
XDOT = -10215
318057 XDOT = -3093
005871
YDOT = -13917
874296 feet/sec YDOT = -4276
871662 meter/sec
ZDOT = 18267
388052 ZDOT = 5552
825208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3730370
28 X = -1137016
86
Y = -20927689
82 feet Y = -6378759
86 meter
Z = 6704930
37 Z = 2043662
78
XDOT = 15582
450645 XDOT = 4749
530956
YDOT = 3073
554640 feet/sec YDOT = 936
819454 meter/sec
ZDOT = 18199
101984 ZDOT = 5547
086285
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 19218
81039226
00016717 00000-0 10270-3 0 9177
2 25544 51
6392 110
1111 0006290 225
5154 134
5484 15
51041866 23107
Satellite: ISS
Catalog Number: 25544
Epoch time: 19218
81039226 = yrday
fracday
Element set: 917
Inclination: 51
6392 deg
RA of node: 110
1111 deg
Eccentricity:
0006290
Arg of perigee: 225
5154 deg
Mean anomaly: 134
5484 deg
Mean motion: 15
51041866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2310
Checksum: 278
Coasting Arc #19 (Orbit 2324)
---------------------------------------
Vector Time (GMT): 2019/219/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933877
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3506417
73 A = 6795268
96 meter
Y = -5153372
22 meter E =
0006905
Z = -2695450
02 I = 52
02165
XDOT = 2979
458899 Wp = 185
73829
YDOT = 4754
665463 meter/sec RA = 104
50148 deg
ZDOT = -5219
991022 TA = 24
49645
MA = 24
46366
Ha = 225
380 n
mi
Hp = 221
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11503995
17 X = 3576876
50
Y = -16907389
17 feet Y = -5113766
94 meter
Z = -8843339
95 Z = -2678246
34
XDOT = 9775
127623 XDOT = 2951
425025
YDOT = 15599
296137 feet/sec YDOT = 4787
827290 meter/sec
ZDOT = -17125
954797 ZDOT = -5205
585983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3807044
90 X = 1160387
29
Y = 20126951
28 feet Y = 6134694
75 meter
Z = -8764622
99 Z = -2671457
09
XDOT = -16560
887774 XDOT = -5047
758594
YDOT = -4288
917263 feet/sec YDOT = -1307
261982 meter/sec
ZDOT = -17060
763815 ZDOT = -5200
120811
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 19219
77684677
00016717 00000-0 10270-3 0 9180
2 25544 51
6394 105
3162 0006206 229
5741 130
4869 15
51052351 23253
Satellite: ISS
Catalog Number: 25544
Epoch time: 19219
77684677 = yrday
fracday
Element set: 918
Inclination: 51
6394 deg
RA of node: 105
3162 deg
Eccentricity:
0006206
Arg of perigee: 229
5741 deg
Mean anomaly: 130
4869 deg
Mean motion: 15
51052351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2325
Checksum: 317
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