[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 17th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14504 3693 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
201/16:28:21
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
5
201/22:50:29
000 0
0 -0
0 0
0
N/A -0
0 0
0 227
4
000/00:00:58
000 0
0 -0
0 218
6
202/23:35:13
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
7
203/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 219
0
204/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
9
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
8
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
Coasting Arc #1 (Orbit 1994)
---------------------------------------
Vector Time (GMT): 2019/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3081042
45 A = 6786918
67 meter
Y = 3051063
12 meter E =
0019199
Z = -5237519
30 I = 51
42552
XDOT = -6142
347222 Wp = 114
63320
YDOT = -4443
464481 meter/sec RA = 209
72267 deg
ZDOT = 1019
950600 TA = 165
21486
MA = 165
15864
Ha = 227
916 n
mi
Hp = 218
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10108406
98 X = -3089490
89
Y = 10010049
61 feet Y = 3016562
23 meter
Z = -17183462
28 Z = -5252505
64
XDOT = -20152
057816 XDOT = -6097
156871
YDOT = -14578
295540 feet/sec YDOT = -4511
899984 meter/sec
ZDOT = 3346
294619 ZDOT = 990
223131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13219805
73 X = 4029396
79
Y = 5026621
87 feet Y = 1532114
35 meter
Z = -17251729
48 Z = -5258327
15
XDOT = -4688
314262 XDOT = -1428
998187
YDOT = 23407
362809 feet/sec YDOT = 7134
564184 meter/sec
ZDOT = 3211
651629 ZDOT = 978
911417
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 19198
51445789
00016717 00000-0 10270-3 0 9008
2 25544 51
6396 210
8143 0006832 151
2501 208
9027 15
50961524 19955
Satellite: ISS
Catalog Number: 25544
Epoch time: 19198
51445789 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 210
8143 deg
Eccentricity:
0006832
Arg of perigee: 151
2501 deg
Mean anomaly: 208
9027 deg
Mean motion: 15
50961524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1995
Checksum: 317
Coasting Arc #2 (Orbit 2010)
---------------------------------------
Vector Time (GMT): 2019/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3495406
93 A = 6787466
67 meter
Y = -2838196
07 meter E =
0007925
Z = 5071881
60 I = 51
45671
XDOT = 6073
501239 Wp = 113
71566
YDOT = 4340
731403 meter/sec RA = 204
74260 deg
ZDOT = -1757
593205 TA = 353
31714
MA = 353
32770
Ha = 227
723 n
mi
Hp = 218
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11467870
50 X = 3502248
84
Y = -9311666
91 feet Y = -2799070
34 meter
Z = 16640031
51 Z = 5088876
88
XDOT = 19926
185167 XDOT = 6033
047765
YDOT = 14241
244760 feet/sec YDOT = 4408
423578 meter/sec
ZDOT = -5766
381905 ZDOT = -1728
188794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13250680
96 X = -4038807
56
Y = -6329100
28 feet Y = -1929109
77 meter
Z = 16717409
70 Z = 5095466
48
XDOT = 3957
026354 XDOT = 1206
101633
YDOT = -23155
537327 feet/sec YDOT = -7057
807777 meter/sec
ZDOT = -5633
170378 ZDOT = -1716
990331
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 19199
54537797
00016717 00000-0 10270-3 0 9014
2 25544 51
6390 205
6987 0006804 153
9299 206
2196 15
50991253 20119
Satellite: ISS
Catalog Number: 25544
Epoch time: 19199
54537797 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 205
6987 deg
Eccentricity:
0006804
Arg of perigee: 153
9299 deg
Mean anomaly: 206
2196 deg
Mean motion: 15
50991253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2011
Checksum: 337
Coasting Arc #3 (Orbit 2025)
---------------------------------------
Vector Time (GMT): 2019/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3941758
94 A = 6788552
87 meter
Y = 2682629
21 meter E =
0016915
Z = -4848049
24 I = 51
49056
XDOT = -5897
057764 Wp = 125
46358
YDOT = -4203
529710 meter/sec RA = 199
76644 deg
ZDOT = 2465
169015 TA = 168
87390
MA = 168
83645
Ha = 227
768 n
mi
Hp = 218
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12932279
99 X = -3947915
31
Y = 8801276
93 feet Y = 2638515
76 meter
Z = -15905673
37 Z = -4867211
09
XDOT = -19347
302374 XDOT = -5861
588564
YDOT = -13791
107971 feet/sec YDOT = -4269
276678 meter/sec
ZDOT = 8087
824853 ZDOT = 2436
609676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13545862
39 X = 4128778
86
Y = 7644214
22 feet Y = 2329956
50 meter
Z = -15992885
54 Z = -4874631
51
XDOT = -3289
044987 XDOT = -1002
500912
YDOT = 22502
515400 feet/sec YDOT = 6858
766694 meter/sec
ZDOT = 7958
415419 ZDOT = 2425
725020
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 19200
51186468
00016717 00000-0 10270-3 0 9020
2 25544 51
6388 200
9040 0006705 157
0745 203
0706 15
50961095 20264
Satellite: ISS
Catalog Number: 25544
Epoch time: 19200
51186468 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 200
9040 deg
Eccentricity:
0006705
Arg of perigee: 157
0745 deg
Mean anomaly: 203
0706 deg
Mean motion: 15
50961095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2026
Checksum: 288
Coasting Arc #4 (Orbit 2041)
---------------------------------------
Vector Time (GMT): 2019/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4352829
87 A = 6789670
42 meter
Y = -2568586
05 meter E =
0010477
Z = 4523456
71 I = 51
52530
XDOT = 5680
133638 Wp = 106
43934
YDOT = 4084
013515 meter/sec RA = 194
79321 deg
ZDOT = -3143
677213 TA = 15
14693
MA = 15
11559
Ha = 227
481 n
mi
Hp = 218
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14280937
88 X = 4359257
05
Y = -8427119
58 feet Y = -2519874
09 meter
Z = 14840737
25 Z = 4544616
08
XDOT = 18635
609048 XDOT = 5649
312786
YDOT = 13398
994472 feet/sec YDOT = 4147
360691 meter/sec
ZDOT = -10313
901617 ZDOT = -3116
160345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13959756
10 X = -4254933
66
Y = -8787469
02 feet Y = -2678420
56 meter
Z = 14937021
49 Z = 4552804
15
XDOT = 2769
112646 XDOT = 844
025535
YDOT = -21736
123557 feet/sec YDOT = -6625
170460 meter/sec
ZDOT = -10189
195531 ZDOT = -3105
666798
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 19201
54278260
00016717 00000-0 10270-3 0 9037
2 25544 51
6376 195
7890 0006626 161
9077 198
2311 15
50996805 20421
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
54278260 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 195
7890 deg
Eccentricity:
0006626
Arg of perigee: 161
9077 deg
Mean anomaly: 198
2311 deg
Mean motion: 15
50996805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2042
Checksum: 322
Coasting Arc #5 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2019/201/16:28:21
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 167044
59 A = 6786624
45 meter
Y = -4271645
05 meter E =
0009124
Z = 5267859
92 I = 51
52349
XDOT = 7527
234909 Wp = 149
55835
YDOT = 1240
869243 meter/sec RA = 193
89770 deg
ZDOT = 759
235183 TA = 293
12618
MA = 293
22230
Ha = 227
487 n
mi
Hp = 218
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 548046
56 X = 189211
13
Y = -14014583
48 feet Y = -4269653
52 meter
Z = 17283004
99 Z = 5268724
83
XDOT = 24695
652589 XDOT = 7509
111852
YDOT = 4071
093316 feet/sec YDOT = 1324
942675 meter/sec
ZDOT = 2490
929077 ZDOT = 795
754999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 635506
82 X = 193702
48
Y = 14005683
34 feet Y = 4268932
28 meter
Z = 17287224
53 Z = 5269146
04
XDOT = -23895
227247 XDOT = -7283
265265
YDOT = -2228
481924 feet/sec YDOT = -679
241290 meter/sec
ZDOT = 2656
726183 ZDOT = 809
770141
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 19201
73608012
00016717 00000-0 10270-3 0 9041
2 25544 51
6399 194
8309 0006510 163
7125 196
4236 15
51022518 20458
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
73608012 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 194
8309 deg
Eccentricity:
0006510
Arg of perigee: 163
7125 deg
Mean anomaly: 196
4236 deg
Mean motion: 15
51022518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 293
Coasting Arc #6 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2019/201/22:50:58
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4747586
75 A = 6790793
02 meter
Y = -2377985
01 meter E =
0011735
Z = 4221184
52 I = 51
54453
XDOT = 5322
692856 Wp = 108
03024
YDOT = 4149
190707 meter/sec RA = 192
54375 deg
ZDOT = -3644
244645 TA = 19
34642
MA = 19
30191
Ha = 227
368 n
mi
Hp = 218
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15576072
00 X = 4753321
45
Y = -7801788
10 feet Y = -2324862
42 meter
Z = 13849030
58 Z = 4244259
80
XDOT = 17462
903072 XDOT = 5293
601184
YDOT = 13612
830405 feet/sec YDOT = 4208
550416 meter/sec
ZDOT = -11956
183220 ZDOT = -3618
459854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10438370
31 X = 3181615
27
Y = 13842096
58 feet Y = 4219071
04 meter
Z = 13954008
45 Z = 4253181
78
XDOT = -9253
857582 XDOT = -2820
575791
YDOT = 18929
134581 feet/sec YDOT = 5769
600220 meter/sec
ZDOT = -11839
339709 ZDOT = -3608
630743
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 19201
99380842
00016717 00000-0 10270-3 0 9058
2 25544 51
6385 193
5494 0006552 165
8952 194
2383 15
50995604 20498
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
99380842 = yrday
fracday
Element set: 905
Inclination: 51
6385 deg
RA of node: 193
5494 deg
Eccentricity:
0006552
Arg of perigee: 165
8952 deg
Mean anomaly: 194
2383 deg
Mean motion: 15
50995604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 340
Coasting Arc #7 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2019/202/22:50:58
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5129573
31 A = 6792279
73 meter
Y = 2352650
64 meter E =
0010896
Z = -3793150
22 I = 51
58204
XDOT = -4960
975310 Wp = 138
03189
YDOT = -4027
887418 meter/sec RA = 187
57536 deg
ZDOT = 4209
714624 TA = 176
57103
MA = 176
56356
Ha = 227
480 n
mi
Hp = 218
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16829308
76 X = -5137075
39
Y = 7718670
07 feet Y = 2295246
45 meter
Z = -12444718
56 Z = -3818085
40
XDOT = -16276
165716 XDOT = -4936
013710
YDOT = -13214
853734 feet/sec YDOT = -4083
225231 meter/sec
ZDOT = 13811
399684 ZDOT = 4185
676846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10840148
61 X = -3304077
30
Y = -14915041
66 feet Y = -4546104
70 meter
Z = -12558153
98 Z = -3827725
33
XDOT = 8674
343170 XDOT = 2643
939798
YDOT = -17844
092696 feet/sec YDOT = -5438
879454 meter/sec
ZDOT = 13702
465899 ZDOT = 4176
511606
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 19202
96029324
00016717 00000-0 10270-3 0 9062
2 25544 51
6382 188
7531 0006700 167
9369 192
1944 15
50994826 20645
Satellite: ISS
Catalog Number: 25544
Epoch time: 19202
96029324 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 188
7531 deg
Eccentricity:
0006700
Arg of perigee: 167
9369 deg
Mean anomaly: 192
1944 deg
Mean motion: 15
50994826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 331
Coasting Arc #8 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2019/202/23:35:13
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4423470
98 A = 6790650
37 meter
Y = -2848629
40 meter E =
0011277
Z = 4281544
20 I = 51
57724
XDOT = 5764
201266 Wp = 109
53608
YDOT = 3597
231665 meter/sec RA = 187
42356 deg
ZDOT = -3557
984298 TA = 16
79042
MA = 16
75312
Ha = 227
426 n
mi
Hp = 218
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14512700
08 X = 4434199
41
Y = -9345896
97 feet Y = -2799103
33 meter
Z = 14047061
02 Z = 4303057
27
XDOT = 18911
421476 XDOT = 5740
829998
YDOT = 11801
941157 feet/sec YDOT = 3661
560564 meter/sec
ZDOT = -11673
176832 ZDOT = -3530
040981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14126789
90 X = 4305845
56
Y = 9779439
20 feet Y = 2980773
07 meter
Z = 14144983
32 Z = 4311390
92
XDOT = -2977
712044 XDOT = -907
606631
YDOT = 21020
877161 feet/sec YDOT = 6407
163359 meter/sec
ZDOT = -11546
471239 ZDOT = -3519
364434
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 19203
02472587
00016717 00000-0 10270-3 0 9074
2 25544 51
6381 188
4329 0006774 168
5248 191
6058 15
50972107 20659
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
02472587 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 188
4329 deg
Eccentricity:
0006774
Arg of perigee: 168
5248 deg
Mean anomaly: 191
6058 deg
Mean motion: 15
50972107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 327
Coasting Arc #9 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2019/203/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4015156
76 A = 6791231
01 meter
Y = -3532970
02 meter E =
0014077
Z = 4181932
64 I = 51
61057
XDOT = 6177
533213 Wp = 129
02004
YDOT = -2611
339509 meter/sec RA = 183
06401 deg
ZDOT = 3707
992827 TA = 282
78188
MA = 282
93916
Ha = 227
387 n
mi
Hp = 218
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13173086
48 X = -3995664
88
Y = -11591109
00 feet Y = -3577761
58 meter
Z = 13720251
44 Z = 4162475
92
XDOT = 20267
497417 XDOT = 6188
263724
YDOT = -8567
386842 feet/sec YDOT = -2542
198212 meter/sec
ZDOT = 12165
330798 ZDOT = 3738
026455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14932987
42 X = 4551574
57
Y = -9343525
96 feet Y = -2847906
71 meter
Z = 13632084
37 Z = 4155059
32
XDOT = 1677
479536 XDOT = 511
295763
YDOT = 20711
634463 feet/sec YDOT = 6312
906184 meter/sec
ZDOT = 12301
958007 ZDOT = 3749
636801
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 19203
92677539
00016717 00000-0 10270-3 0 9088
2 25544 51
6403 183
9605 0006305 171
3430 188
7831 15
50971563 20792
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
92677539 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 183
9605 deg
Eccentricity:
0006305
Arg of perigee: 171
3430 deg
Mean anomaly: 188
7831 deg
Mean motion: 15
50971563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 324
Coasting Arc #10 (Orbit 2087)
---------------------------------------
Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 69492
32 A = 6786505
71 meter
Y = -4212544
88 meter E =
0007261
Z = 5317493
65 I = 51
61261
XDOT = 7665
907477 Wp = 153
35548
YDOT = 62
313949 meter/sec RA = 180
12743 deg
ZDOT = -57
134968 TA = 297
15229
MA = 297
22631
Ha = 227
359 n
mi
Hp = 218
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 227993
18 X = 90763
93
Y = -13820685
29 feet Y = -4211649
13 meter
Z = 17445845
32 Z = 5317882
64
XDOT = 25150
615083 XDOT = 7664
918449
YDOT = 204
442089 feet/sec YDOT = 148
033984 meter/sec
ZDOT = -187
450682 ZDOT = -19
899710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13376836
27 X = -4077259
70
Y = 3471634
91 feet Y = 1058154
32 meter
Z = 17447889
39 Z = 5318116
69
XDOT = -6062
158947 XDOT = -1847
746047
YDOT = -23370
938481 feet/sec YDOT = -7123
462049 meter/sec
ZDOT = -18
268024 ZDOT = -5
568094
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 19204
50666393
00016717 00000-0 10270-3 0 9090
2 25544 51
6382 181
0838 0006530 172
2537 187
8716 15
50987895 20880
Satellite: ISS
Catalog Number: 25544
Epoch time: 19204
50666393 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 181
0838 deg
Eccentricity:
0006530
Arg of perigee: 172
2537 deg
Mean anomaly: 187
8716 deg
Mean motion: 15
50987895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2088
Checksum: 344
Coasting Arc #11 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2019/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -580525
42 A = 6786765
49 meter
Y = 4241823
64 meter E =
0016965
Z = -5279806
64 I = 51
64666
XDOT = -7607
148831 Wp = 118
64694
YDOT = -9
425452 meter/sec RA = 175
16062 deg
ZDOT = 822
923967 TA = 159
27028
MA = 159
20138
Ha = 227
260 n
mi
Hp = 219
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1904610
97 X = -602269
43
Y = 13916744
22 feet Y = 4235210
54 meter
Z = -17322200
25 Z = -5282679
14
XDOT = -24957
837373 XDOT = -7610
475329
YDOT = -30
923399 feet/sec YDOT = -94
512584 meter/sec
ZDOT = 2699
881782 ZDOT = 785
963534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13869649
65 X = 4227469
21
Y = -2115203
50 feet Y = -644714
03 meter
Z = -17335531
92 Z = -5283870
13
XDOT = 6697
432117 XDOT = 2041
377309
YDOT = 23005
850274 feet/sec YDOT = 7012
183164 meter/sec
ZDOT = 2531
924442 ZDOT = 771
730570
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
47314528
00016717 00000-0 10270-3 0 9109
2 25544 51
6382 176
2890 0006511 175
6156 184
5053 15
50972193 21038
Satellite: ISS
Catalog Number: 25544
Epoch time: 19205
47314528 = yrday
fracday
Element set: 910
Inclination: 51
6382 deg
RA of node: 176
2890 deg
Eccentricity:
0006511
Arg of perigee: 175
6156 deg
Mean anomaly: 184
5053 deg
Mean motion: 15
50972193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 301
Coasting Arc #12 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2019/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1049086
63 A = 6787236
11 meter
Y = -4302667
64 meter E =
0005386
Z = 5139046
74 I = 51
68193
XDOT = 7504
907416 Wp = 134
45643
YDOT = -39
484114 meter/sec RA = 170
19640 deg
ZDOT = -1567
783928 TA = 330
63581
MA = 330
66607
Ha = 227
097 n
mi
Hp = 219
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3441885
26 X = 1072159
85
Y = -14116363
66 feet Y = -4290807
39 meter
Z = 16860389
56 Z = 5144198
50
XDOT = 24622
399659 XDOT = 7512
406534
YDOT = -129
541058 feet/sec YDOT = 44
483077 meter/sec
ZDOT = -5143
648057 ZDOT = -1531
309924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14471963
71 X = -4411054
54
Y = 938562
03 feet Y = 286073
71 meter
Z = 16884087
21 Z = 5146269
78
XDOT = -7255
822788 XDOT = -2211
574786
YDOT = -22488
526828 feet/sec YDOT = -6854
502977 meter/sec
ZDOT = -4977
877251 ZDOT = -1517
256986
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
50405627
00016717 00000-0 10270-3 0 9116
2 25544 51
6384 171
1739 0006458 180
1621 179
9529 15
50997564 21196
Satellite: ISS
Catalog Number: 25544
Epoch time: 19206
50405627 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 171
1739 deg
Eccentricity:
0006458
Arg of perigee: 180
1621 deg
Mean anomaly: 179
9529 deg
Mean motion: 15
50997564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 326
Coasting Arc #13 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2019/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1519689
20 A = 6788210
12 meter
Y = 4425386
70 meter E =
0015001
Z = -4931263
46 I = 51
71805
XDOT = -7300
356898 Wp = 131
10595
YDOT = 53
075416 meter/sec RA = 165
23496 deg
ZDOT = 2292
348222 TA = 161
35680
MA = 161
30179
Ha = 226
996 n
mi
Hp = 219
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4985856
96 X = -1545109
00
Y = 14518985
22 feet Y = 4408250
78 meter
Z = -16178685
88 Z = -4938706
83
XDOT = -23951
302158 XDOT = -7311
542718
YDOT = 174
131942 feet/sec YDOT = -28
625054 meter/sec
ZDOT = 7520
827500 ZDOT = 2256
858856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15314312
20 X = 4667802
36
Y = 161475
93 feet Y = 49217
86 meter
Z = -16212814
24 Z = -4941665
78
XDOT = 7580
461610 XDOT = 2310
524699
YDOT = 21660
678120 feet/sec YDOT = 6602
174691 meter/sec
ZDOT = 7359
509100 ZDOT = 2243
178374
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
47053344
00016717 00000-0 10270-3 0 9129
2 25544 51
6388 166
3786 0006332 183
1470 176
9643 15
50981451 21343
Satellite: ISS
Catalog Number: 25544
Epoch time: 19207
47053344 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 166
3786 deg
Eccentricity:
0006332
Arg of perigee: 183
1470 deg
Mean anomaly: 176
9643 deg
Mean motion: 15
50981451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 316
Coasting Arc #14 (Orbit 2149)
---------------------------------------
Vector Time (GMT): 2019/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1933383
14 A = 6789307
96 meter
Y = -4568540
22 meter E =
0007173
Z = 4628125
57 I = 51
75335
XDOT = 7063
430430 Wp = 112
77507
YDOT = -34
061347 meter/sec RA = 160
27731 deg
ZDOT = -2983
374125 TA = 6
92761
MA = 6
91770
Ha = 226
805 n
mi
Hp = 219
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6343120
52 X = 1961845
45
Y = -14988649
00 feet Y = -4546761
13 meter
Z = 15184139
02 Z = 4637585
79
XDOT = 23173
984349 XDOT = 7077
777828
YDOT = -111
749825 feet/sec YDOT = 45
007440 meter/sec
ZDOT = -9787
972850 ZDOT = -2949
027997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16202013
59 X = -4938373
74
Y = -1035484
75 feet Y = -315615
75 meter
Z = 15227454
86 Z = 4641328
24
XDOT = -7728
550713 XDOT = -2355
662257
YDOT = -20761
849789 feet/sec YDOT = -6328
211816 meter/sec
ZDOT = -9631
829464 ZDOT = -2935
781621
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
50144141
00016717 00000-0 10270-3 0 9131
2 25544 51
6382 161
2639 0006290 187
8398 172
2656 15
51004598 21501
Satellite: ISS
Catalog Number: 25544
Epoch time: 19208
50144141 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 161
2639 deg
Eccentricity:
0006290
Arg of perigee: 187
8398 deg
Mean anomaly: 172
2656 deg
Mean motion: 15
51004598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2150
Checksum: 306
Coasting Arc #15 (Orbit 2164)
---------------------------------------
Vector Time (GMT): 2019/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2317599
39 A = 6790756
83 meter
Y = 4759542
02 meter E =
0011121
Z = -4264700
52 I = 51
78944
XDOT = -6743
406470 Wp = 144
63227
YDOT = -37
051225 meter/sec RA = 155
32277 deg
ZDOT = 3619
162411 TA = 162
38851
MA = 162
34992
Ha = 226
737 n
mi
Hp = 219
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7603672
54 X = -2349934
35
Y = 15615295
33 feet Y = 4733444
73 meter
Z = -13991799
59 Z = -4276036
39
XDOT = -22124
036976 XDOT = -6760
070695
YDOT = -121
559137 feet/sec YDOT = -112
554357 meter/sec
ZDOT = 11873
892423 ZDOT = 3586
365275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17239120
12 X = 5254483
81
Y = 1735472
11 feet Y = 528971
90 meter
Z = -14043668
12 Z = -4280510
04
XDOT = 7583
520544 XDOT = 2311
457062
YDOT = 19657
024407 feet/sec YDOT = 5991
461039 meter/sec
ZDOT = 11724
772348 ZDOT = 3573
710612
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
46791695
00016717 00000-0 10270-3 0 9140
2 25544 51
6386 156
4686 0006288 191
6211 168
4796 15
50986891 21659
Satellite: ISS
Catalog Number: 25544
Epoch time: 19209
46791695 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 156
4686 deg
Eccentricity:
0006288
Arg of perigee: 191
6211 deg
Mean anomaly: 168
4796 deg
Mean motion: 15
50986891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2165
Checksum: 363
Coasting Arc #16 (Orbit 2180)
---------------------------------------
Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3610317
24 A = 6787332
64 meter
Y = -2592510
43 meter E =
0009306
Z = 5129720
50 I = 51
80917
XDOT = 5773
935778 Wp = 165
22306
YDOT = -4761
417413 meter/sec RA = 150
46460 deg
ZDOT = 1647
910405 TA = 268
84474
MA = 268
95136
Ha = 226
624 n
mi
Hp = 219
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11844872
82 X = -3605975
72
Y = -8505611
64 feet Y = -2632859
93 meter
Z = 16829791
67 Z = 5112193
36
XDOT = 18943
358852 XDOT = 5818
745658
YDOT = -15621
448206 feet/sec YDOT = -4696
598879 meter/sec
ZDOT = 5406
530200 ZDOT = 1676
065867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4628146
67 X = -1410659
10
Y = 13924696
46 feet Y = 4244247
48 meter
Z = 16750266
15 Z = 5105481
12
XDOT = -19459
218066 XDOT = -5931
169667
YDOT = -13163
093812 feet/sec YDOT = -4012
110994 meter/sec
ZDOT = 5534
899676 ZDOT = 1687
037421
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
49882080
00016717 00000-0 10270-3 0 9155
2 25544 51
6400 151
3539 0006296 196
6718 163
4227 15
51030929 21818
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
49882080 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 151
3539 deg
Eccentricity:
0006296
Arg of perigee: 196
6718 deg
Mean anomaly: 163
4227 deg
Mean motion: 15
51030929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2181
Checksum: 307
Coasting Arc #17 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3174831
93 A = 6786757
00 meter
Y = 2857336
49 meter E =
0012899
Z = -5284120
66 I = 51
83561
XDOT = -5844
980692 Wp = 108
66779
YDOT = 4862
586092 meter/sec RA = 145
50989 deg
ZDOT = -888
209442 TA = 152
87938
MA = 152
81194
Ha = 226
482 n
mi
Hp = 220
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10416115
26 X = 3168311
27
Y = 9374463
55 feet Y = 2892803
91 meter
Z = -17336353
86 Z = -5268714
26
XDOT = -19176
445841 XDOT = -5894
606770
YDOT = 15953
366442 feet/sec YDOT = 4796
946051 meter/sec
ZDOT = -2914
072974 ZDOT = -916
721560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5655080
27 X = 1723668
47
Y = -12915644
72 feet Y = -3936688
51 meter
Z = -17266481
33 Z = -5262823
51
XDOT = 20155
084818 XDOT = 6143
269853
YDOT = 12868
879667 feet/sec YDOT = 3922
434523 meter/sec
ZDOT = -3044
096616 ZDOT = -927
840649
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
46529296
00016717 00000-0 10270-3 0 9161
2 25544 51
6402 146
5578 0006179 199
3841 160
7076 15
51001971 21969
Satellite: ISS
Catalog Number: 25544
Epoch time: 19211
46529296 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 146
5578 deg
Eccentricity:
0006179
Arg of perigee: 199
3841 deg
Mean anomaly: 160
7076 deg
Mean motion: 15
51001971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 324
Coasting Arc #18 (Orbit 2211)
---------------------------------------
Vector Time (GMT): 2019/212/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2779520
65 A = 6786420
20 meter
Y = -3139091
25 meter E =
0005983
Z = 5336465
18 I = 51
86203
XDOT = 5851
428459 Wp = 180
81746
YDOT = -4947
315395 meter/sec RA = 140
55930 deg
ZDOT = 131
733862 TA = 267
89600
MA = 267
96452
Ha = 226
372 n
mi
Hp = 220
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9119162
24 X = -2770132
83
Y = -10298855
81 feet Y = -3170121
92 meter
Z = 17508087
86 Z = 5322986
07
XDOT = 19197
599930 XDOT = 5905
676000
YDOT = -16231
349720 feet/sec YDOT = -4881
577310 meter/sec
ZDOT = 432
197710 ZDOT = 160
288442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6728066
32 X = -2050714
62
Y = 12086945
82 feet Y = 3684101
09 meter
Z = 17446992
74 Z = 5317843
39
XDOT = -20716
158388 XDOT = -6314
285077
YDOT = -12370
981071 feet/sec YDOT = -3770
675030 meter/sec
ZDOT = 562
443509 ZDOT = 171
432781
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
49619494
00016717 00000-0 10270-3 0 9176
2 25544 51
6406 141
4444 0006154 203
9168 156
1698 15
51021376 22125
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
49619494 = yrday
fracday
Element set: 917
Inclination: 51
6406 deg
RA of node: 141
4444 deg
Eccentricity:
0006154
Arg of perigee: 203
9168 deg
Mean anomaly: 156
1698 deg
Mean motion: 15
51021376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2212
Checksum: 305
Coasting Arc #19 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2019/212/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1822211
27 A = 6792442
37 meter
Y = -5380873
83 meter E =
0010020
Z = 3711611
75 I = 51
89004
XDOT = 6263
664058 Wp = 116
14714
YDOT = -872
802205 meter/sec RA = 139
53640 deg
ZDOT = -4335
717600 TA = 19
81522
MA = 19
77632
Ha = 226
167 n
mi
Hp = 220
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5978383
42 X = 1864217
80
Y = -17653785
52 feet Y = -5360262
11 meter
Z = 12177203
92 Z = 3720564
60
XDOT = 20550
078931 XDOT = 6294
018457
YDOT = -2863
524295 feet/sec YDOT = -802
587319 meter/sec
ZDOT = -14224
795277 ZDOT = -4305
218170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5329388
63 X = -1624397
65
Y = 17832328
93 feet Y = 5435293
86 meter
Z = 12218312
83 Z = 3724141
75
XDOT = -19242
955197 XDOT = -5865
252744
YDOT = 3911
090851 feet/sec YDOT = 1192
100491 meter/sec
ZDOT = -14085
985960 ZDOT = -4293
408521
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
68948789
00016717 00000-0 10270-3 0 9180
2 25544 51
6430 140
4867 0006084 205
3162 154
7692 15
51044598 22154
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
68948789 = yrday
fracday
Element set: 918
Inclination: 51
6430 deg
RA of node: 140
4867 deg
Eccentricity:
0006084
Arg of perigee: 205
3162 deg
Mean anomaly: 154
7692 deg
Mean motion: 15
51044598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 328
Coasting Arc #20 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 424367
62 A = 6790417
19 meter
Y = -5198306
12 meter E =
0006714
Z = 4341335
93 I = 51
90267
XDOT = 6372
198389 Wp = 111
74636
YDOT = -2415
077676 meter/sec RA = 135
40518 deg
ZDOT = -3512
766582 TA = 13
87004
MA = 13
85160
Ha = 226
187 n
mi
Hp = 220
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1392282
22 X = 461377
80
Y = -17054810
11 feet Y = -5193353
99 meter
Z = 14243228
12 Z = 4343486
73
XDOT = 20906
162693 XDOT = 6415
793503
YDOT = -7923
483188 feet/sec YDOT = -2343
575216 meter/sec
ZDOT = -11524
824744 ZDOT = -3481
707983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14932258
99 X = -4551352
54
Y = 8339260
53 feet Y = 2541806
61 meter
Z = 14253382
77 Z = 4344431
07
XDOT = -17587
926314 XDOT = -5360
799940
YDOT = -12025
792568 feet/sec YDOT = -3665
461575 meter/sec
ZDOT = -11383
345556 ZDOT = -3469
643726
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
52709600
00016717 00000-0 10270-3 0 9192
2 25544 51
6419 136
3302 0006191 207
9625 152
1194 15
51012802 22275
Satellite: ISS
Catalog Number: 25544
Epoch time: 19213
52709600 = yrday
fracday
Element set: 919
Inclination: 51
6419 deg
RA of node: 136
3302 deg
Eccentricity:
0006191
Arg of perigee: 207
9625 deg
Mean anomaly: 152
1194 deg
Mean motion: 15
51012802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 281
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