[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 4th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20352 94 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
7
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 1311)
---------------------------------------
Vector Time (GMT): 2019/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965102
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4605290
39 A = 6788583
83 meter
Y = 1568618
71 meter E =
0011806
Z = -4742129
59 I = 51
99076
XDOT = 454
765099 Wp = 69
22977
YDOT = 7110
470982 meter/sec RA = 68
43173 deg
ZDOT = 2803
362861 TA = 228
40970
MA = 228
51094
Ha = 227
479 n
mi
Hp = 218
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15109220
43 X = 4610442
30
Y = 5146386
85 feet Y = 1620147
89 meter
Z = -15558167
95 Z = -4719745
75
XDOT = 1492
011481 XDOT = 361
602632
YDOT = 23328
316871 feet/sec YDOT = 7115
035114 meter/sec
ZDOT = 9197
384714 ZDOT = 2805
346874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9869370
59 X = 3008184
16
Y = -12669412
22 feet Y = -3861636
84 meter
Z = -15456776
77 Z = -4711225
56
XDOT = 21574
256642 XDOT = 6575
833424
YDOT = 5614
345039 feet/sec YDOT = 1711
252368 meter/sec
ZDOT = 9205
584513 ZDOT = 2805
862160
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
51112949
00016717 00000-0 10270-3 0 9009
2 25544 51
6430 69
1783 0007760 6
4780 353
6470 15
51167537 13126
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
51112949 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 69
1783 deg
Eccentricity:
0007760
Arg of perigee: 6
4780 deg
Mean anomaly: 353
6470 deg
Mean motion: 15
51167537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 299
Coasting Arc #2 (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 = -2192535
23 A = 6797893
18 meter
Y = -6412651
36 meter E =
0007931
Z = -533164
88 I = 52
01907
XDOT = 4623
501100 Wp = 93
92866
YDOT = -1087
885882 meter/sec RA = 67
60257 deg
ZDOT = -6006
066239 TA = 91
78184
MA = 91
69099
Ha = 227
385 n
mi
Hp = 218
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7193357
04 X = -2118074
32
Y = -21038882
40 feet Y = -6436753
39 meter
Z = -1749228
60 Z = -543635
76
XDOT = 15168
966862 XDOT = 4664
497008
YDOT = -3569
179402 feet/sec YDOT = -1035
952416 meter/sec
ZDOT = -19704
941730 ZDOT = -5983
507336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10388927
66 X = -3166545
15
Y = 19654090
50 feet Y = 5990566
78 meter
Z = -1796014
37 Z = -547425
18
XDOT = -11657
848427 XDOT = -3553
312201
YDOT = -7930
900492 feet/sec YDOT = -2417
338470 meter/sec
ZDOT = -19602
454983 ZDOT = -5974
828279
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
70440364
00016717 00000-0 10270-3 0 9016
2 25544 51
6425 68
2193 0007660 5
5344 354
5890 15
51141091 13156
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
70440364 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 68
2193 deg
Eccentricity:
0007660
Arg of perigee: 5
5344 deg
Mean anomaly: 354
5890 deg
Mean motion: 15
51141091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 286
Coasting Arc #3 (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 = -2631340
36 A = 6787081
55 meter
Y = 3661601
89 meter E =
0007295
Z = 5066540
01 I = 51
97347
XDOT = -4514
244039 Wp = 52
08600
YDOT = -5895
056347 meter/sec RA = 64
21316 deg
ZDOT = 1918
358212 TA = 19
41233
MA = 19
38457
Ha = 227
518 n
mi
Hp = 218
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8633006
43 X = -2696700
53
Y = 12013129
57 feet Y = 3631810
05 meter
Z = 16622506
60 Z = 5053599
73
XDOT = -14810
511939 XDOT = -4457
306733
YDOT = -19340
736045 feet/sec YDOT = -5945
219770 meter/sec
ZDOT = 6293
826156 ZDOT = 1896
566733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3671903
24 X = -1119196
11
Y = 14398744
45 feet Y = 4388737
31 meter
Z = 16563365
98 Z = 5048513
95
XDOT = -19910
035578 XDOT = -6068
578844
YDOT = -12194
981179 feet/sec YDOT = -3717
030263 meter/sec
ZDOT = 6195
620926 ZDOT = 1888
425258
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
41308011
00016717 00000-0 10270-3 0 9028
2 25544 51
6416 64
7019 0007705 8
6055 351
5227 15
51192646 13262
Satellite: ISS
Catalog Number: 25544
Epoch time: 19155
41308011 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 64
7019 deg
Eccentricity:
0007705
Arg of perigee: 8
6055 deg
Mean anomaly: 351
5227 deg
Mean motion: 15
51192646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1326
Checksum: 284
Coasting Arc #4 (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 = 2889729
74 A = 6786419
78 meter
Y = -3193687
00 meter E =
0018564
Z = -5259756
78 I = 51
95530
XDOT = 4595
074965 Wp = 58
23227
YDOT = 6013
508088 meter/sec RA = 59
26710 deg
ZDOT = -1120
214008 TA = 201
01446
MA = 201
09085
Ha = 227
616 n
mi
Hp = 218
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9480740
61 X = 2950776
77
Y = -10477975
73 feet Y = -3161029
71 meter
Z = -17256419
87 Z = -5245571
81
XDOT = 15075
705265 XDOT = 4532
930086
YDOT = 19729
357244 feet/sec YDOT = 6064
546168 meter/sec
ZDOT = -3675
242808 ZDOT = -1098
042577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4802595
90 X = 1463831
23
Y = -13373024
83 feet Y = -4076097
97 meter
Z = -17191676
01 Z = -5240022
85
XDOT = 20574
708816 XDOT = 6271
171247
YDOT = 12013
091946 feet/sec YDOT = 3661
590425 meter/sec
ZDOT = -3575
336255 ZDOT = -1089
762490
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
37945690
00016717 00000-0 10270-3 0 9035
2 25544 51
6416 59
9056 0007827 12
9966 347
1386 15
51158190 13413
Satellite: ISS
Catalog Number: 25544
Epoch time: 19156
37945690 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 59
9056 deg
Eccentricity:
0007827
Arg of perigee: 12
9966 deg
Mean anomaly: 347
1386 deg
Mean motion: 15
51158190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 332
Coasting Arc #5 (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 = -3203488
48 A = 6785960
23 meter
Y = 2700052
06 meter E =
0008442
Z = 5333960
87 I = 51
93584
XDOT = -4653
552767 Wp = 33
04454
YDOT = -6087
327658 meter/sec RA = 54
32066 deg
ZDOT = 293
233239 TA = 54
21062
MA = 54
13218
Ha = 227
794 n
mi
Hp = 217
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10510132
80 X = -3259352
53
Y = 8858438
53 feet Y = 2663915
08 meter
Z = 17499871
61 Z = 5318264
34
XDOT = -15267
561572 XDOT = -4586
561034
YDOT = -19971
547433 feet/sec YDOT = -6138
992422 meter/sec
ZDOT = 962
051308 ZDOT = 270
789640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6167119
42 X = -1879738
00
Y = 12385500
85 feet Y = 3775100
66 meter
Z = 17428319
99 Z = 5312151
93
XDOT = -21112
652715 XDOT = -6435
136548
YDOT = -11693
155419 feet/sec YDOT = -3564
073772 meter/sec
ZDOT = 860
925464 ZDOT = 262
410081
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
41025683
00016717 00000-0 10270-3 0 9043
2 25544 51
6413 54
7910 0007883 16
2719 343
8684 15
51181268 13570
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41025683 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 54
7910 deg
Eccentricity:
0007883
Arg of perigee: 16
2719 deg
Mean anomaly: 343
8684 deg
Mean motion: 15
51181268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 317
Coasting Arc #6 (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 = 3986383
69 A = 6786331
62 meter
Y = -1547041
43 meter E =
0017426
Z = -5283080
17 I = 51
93646
XDOT = 3813
481280 Wp = 70
75479
YDOT = 6563
918447 meter/sec RA = 54
14013 deg
ZDOT = 963
551265 TA = 208
40056
MA = 208
49564
Ha = 227
743 n
mi
Hp = 218
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13078686
64 X = 4029049
11
Y = -5075595
24 feet Y = -1502223
38 meter
Z = -17332940
18 Z = -5263612
48
XDOT = 12511
421523 XDOT = 3735
117855
YDOT = 21535
165510 feet/sec YDOT = 6606
125132 meter/sec
ZDOT = 3161
257430 ZDOT = 981
886576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7665421
99 X = 2336420
62
Y = -11879229
39 feet Y = -3620789
12 meter
Z = -17244411
89 Z = -5256096
74
XDOT = 21917
915828 XDOT = 6680
580744
YDOT = 9473
626065 feet/sec YDOT = 2887
561224 meter/sec
ZDOT = 3243
682953 ZDOT = 988
674564
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
41025743
00016717 00000-0 10270-3 0 9051
2 25544 51
6417 54
7908 0007887 16
6924 343
4485 15
51161153 13573
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41025743 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 54
7908 deg
Eccentricity:
0007887
Arg of perigee: 16
6924 deg
Mean anomaly: 343
4485 deg
Mean motion: 15
51161153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 318
Coasting Arc #7 (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 = -4339668
58 A = 6787062
73 meter
Y = 1088881
70 meter E =
0012691
Z = 5100209
01 I = 51
91899
XDOT = -3729
400915 Wp = 33
93663
YDOT = -6456
546700 meter/sec RA = 49
19261 deg
ZDOT = -1782
425738 TA = 73
31298
MA = 73
17372
Ha = 227
891 n
mi
Hp = 217
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14237757
79 X = -4376296
08
Y = 3572446
51 feet Y = 1040146
84 meter
Z = 16732969
20 Z = 5079039
85
XDOT = -12235
567308 XDOT = -3648
266802
YDOT = -21182
895998 feet/sec YDOT = -6497
797526 meter/sec
ZDOT = -5847
853471 ZDOT = -1800
345699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9287984
46 X = -2830977
66
Y = 11507369
28 feet Y = 3507446
16 meter
Z = 16636771
81 Z = 5070888
05
XDOT = -21667
443536 XDOT = -6604
236790
YDOT = -8858
419762 feet/sec YDOT = -2700
046344 meter/sec
ZDOT = -5928
400260 ZDOT = -1806
976399
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
44105704
00016717 00000-0 10270-3 0 9062
2 25544 51
6420 49
6761 0007873 19
9151 340
2306 15
51170424 13736
Satellite: ISS
Catalog Number: 25544
Epoch time: 19158
44105704 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 49
6761 deg
Eccentricity:
0007873
Arg of perigee: 19
9151 deg
Mean anomaly: 340
2306 deg
Mean motion: 15
51170424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1373
Checksum: 292
Coasting Arc #8 (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 = 4702315
89 A = 6788130
49 meter
Y = -730165
73 meter E =
0014542
Z = -4851437
85 I = 51
90068
XDOT = 3583
104813 Wp = 74
88949
YDOT = 6269
141246 meter/sec RA = 44
24337 deg
ZDOT = 2539
462970 TA = 219
99180
MA = 220
09899
Ha = 227
911 n
mi
Hp = 217
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15427545
58 X = 4733696
76
Y = -2395556
85 feet Y = -677404
98 meter
Z = -15916790
86 Z = -4828519
80
XDOT = 11755
593219 XDOT = 3500
399968
YDOT = 20568
048707 feet/sec YDOT = 6308
747238 meter/sec
ZDOT = 8331
571423 ZDOT = 2556
668259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10746823
18 X = 3275631
70
Y = -11469802
91 feet Y = -3495995
93 meter
Z = -15812700
57 Z = -4819711
13
XDOT = 21060
799318 XDOT = 6419
331632
YDOT = 8186
127207 feet/sec YDOT = 2495
131573 meter/sec
ZDOT = 8408
891303 ZDOT = 2563
030069
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
40742940
00016717 00000-0 10270-3 0 9079
2 25544 51
6427 44
8795 0007935 23
6417 336
5097 15
51175940 13882
Satellite: ISS
Catalog Number: 25544
Epoch time: 19159
40742940 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 44
8795 deg
Eccentricity:
0007935
Arg of perigee: 23
6417 deg
Mean anomaly: 336
5097 deg
Mean motion: 15
51175940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 335
Coasting Arc #9 (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 = -5088286
23 A = 6789618
48 meter
Y = 373226
97 meter E =
0016081
Z = 4475060
16 I = 51
88068
XDOT = -3346
656363 Wp = 49
74716
YDOT = -6065
791185 meter/sec RA = 39
29523 deg
ZDOT = -3281
460444 TA = 73
30565
MA = 73
12920
Ha = 228
085 n
mi
Hp = 217
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16693852
48 X = -5113818
82
Y = 1224497
95 feet Y = 316182
90 meter
Z = 14681955
91 Z = 4450281
35
XDOT = -10979
843711 XDOT = -3262
638808
YDOT = -19900
889715 feet/sec YDOT = -6102
745681 meter/sec
ZDOT = -10765
946338 ZDOT = -3297
513809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12262769
55 X = -3737692
16
Y = 11536854
52 feet Y = 3516433
26 meter
Z = 14569468
27 Z = 4440773
93
XDOT = -20171
622966 XDOT = -6148
310680
YDOT = -7679
138191 feet/sec YDOT = -2340
601321 meter/sec
ZDOT = -10838
056519 ZDOT = -3303
439627
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
43822581
00016717 00000-0 10270-3 0 9085
2 25544 51
6425 39
7645 0007995 27
7234 332
4342 15
51166025 14046
Satellite: ISS
Catalog Number: 25544
Epoch time: 19160
43822581 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 39
7645 deg
Eccentricity:
0007995
Arg of perigee: 27
7234 deg
Mean anomaly: 332
4342 deg
Mean motion: 15
51166025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 305
Coasting Arc #10 (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 = 5450511
20 A = 6791086
88 meter
Y = -131551
86 meter E =
0011714
Z = -4054572
19 I = 51
85996
XDOT = 3052
366625 Wp = 65
94208
YDOT = 5821
525501 meter/sec RA = 34
34644 deg
ZDOT = 3927
974276 TA = 244
70542
MA = 244
82682
Ha = 228
070 n
mi
Hp = 217
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17882254
60 X = 5471271
96
Y = -431600
58 feet Y = -70483
93 meter
Z = -13302402
20 Z = -4028045
31
XDOT = 10014
326199 XDOT = 2967
961947
YDOT = 19099
493115 feet/sec YDOT = 5855
186872 meter/sec
ZDOT = 12887
054710 ZDOT = 3942
597071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13475318
18 X = 4107276
98
Y = -11898126
52 feet Y = -3626548
96 meter
Z = -13182017
98 Z = -4017879
08
XDOT = 19024
102230 XDOT = 5798
546360
YDOT = 7245
391193 feet/sec YDOT = 2208
395236 meter/sec
ZDOT = 12952
694820 ZDOT = 3947
981381
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
40459663
00016717 00000-0 10270-3 0 9091
2 25544 51
6432 34
9686 0007954 30
9157 329
2461 15
51183312 14191
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
40459663 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 34
9686 deg
Eccentricity:
0007954
Arg of perigee: 30
9157 deg
Mean anomaly: 329
2461 deg
Mean motion: 15
51183312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1419
Checksum: 316
Coasting Arc #11 (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 = 3406466
45 A = 6786434
05 meter
Y = -2675024
82 meter E =
0018416
Z = -5239113
14 I = 51
84082
XDOT = 5712
509187 Wp = 75
31348
YDOT = 4947
459699 meter/sec RA = 33
75009 deg
ZDOT = 1196
216877 TA = 206
10885
MA = 206
20184
Ha = 227
984 n
mi
Hp = 217
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11176071
04 X = 3461574
81
Y = -8776328
14 feet Y = -2636622
67 meter
Z = -17188691
41 Z = -5222432
26
XDOT = 18741
828042 XDOT = 5650
950173
YDOT = 16231
823159 feet/sec YDOT = 5010
996663 meter/sec
ZDOT = 3924
596053 ZDOT = 1223
817018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7694113
64 X = -2345165
84
Y = -12055564
38 feet Y = -3674536
02 meter
Z = -17112673
51 Z = -5215942
89
XDOT = 17016
407732 XDOT = 5186
601077
YDOT = -16570
340671 feet/sec YDOT = -5050
639836 meter/sec
ZDOT = 4049
227545 ZDOT = 1234
204556
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
53344438
00016717 00000-0 10270-3 0 9100
2 25544 51
6429 34
3293 0007916 30
1730 329
9876 15
51187896 14213
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
53344438 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 34
3293 deg
Eccentricity:
0007916
Arg of perigee: 30
1730 deg
Mean anomaly: 329
9876 deg
Mean motion: 15
51187896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 317
Coasting Arc #12 (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 = -3893551
49 A = 6787258
30 meter
Y = 2369062
13 meter E =
0013595
Z = 5024501
52 I = 51
81636
XDOT = -5572
839280 Wp = 42
55287
YDOT = -4867
404243 meter/sec RA = 28
79527 deg
ZDOT = -2010
526634 TA = 67
00574
MA = 66
86239
Ha = 228
080 n
mi
Hp = 217
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12774119
07 X = -3944159
92
Y = 7772513
54 feet Y = 2325238
26 meter
Z = 16484585
05 Z = 5005465
38
XDOT = -18283
593437 XDOT = -5508
230352
YDOT = -15969
174027 feet/sec YDOT = -4929
362195 meter/sec
ZDOT = -6596
215991 ZDOT = -2037
440989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6779104
62 X = 2066271
09
Y = 13434416
74 feet Y = 4094810
22 meter
Z = 16397921
10 Z = 4998086
35
XDOT = -16320
875834 XDOT = -4974
602954
YDOT = 16487
360080 feet/sec YDOT = 5025
347352 meter/sec
ZDOT = -6717
732452 ZDOT = -2047
564851
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
56423772
00016717 00000-0 10270-3 0 9114
2 25544 51
6437 29
2138 0007872 32
6782 327
4855 15
51208439 14372
Satellite: ISS
Catalog Number: 25544
Epoch time: 19162
56423772 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 29
2138 deg
Eccentricity:
0007872
Arg of perigee: 32
6782 deg
Mean anomaly: 327
4855 deg
Mean motion: 15
51208439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 320
Coasting Arc #13 (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 = 4354755
96 A = 6788497
19 meter
Y = -2162887
48 meter E =
0015232
Z = -4748891
87 I = 51
78962
XDOT = 5345
312070 Wp = 78
98990
YDOT = 4733
809976 meter/sec RA = 23
83880 deg
ZDOT = 2755
995511 TA = 218
23241
MA = 218
34053
Ha = 228
126 n
mi
Hp = 217
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14287257
10 X = 4401685
94
Y = -7096087
54 feet Y = -2113926
66 meter
Z = -15580353
89 Z = -4727624
21
XDOT = 17537
113091 XDOT = 5278
592810
YDOT = 15530
872625 feet/sec YDOT = 4793
211665 meter/sec
ZDOT = 9041
980024 ZDOT = 2781
799624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6245988
81 X = -1903777
39
Y = -14780849
64 feet Y = -4505202
97 meter
Z = -15483594
84 Z = -4719399
71
XDOT = 15446
156303 XDOT = 4707
988441
YDOT = -16085
272361 feet/sec YDOT = -4902
791016 meter/sec
ZDOT = 9158
461648 ZDOT = 2791
499110
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
53060667
00016717 00000-0 10270-3 0 9123
2 25544 51
6428 24
4169 0007935 36
8443 323
3252 15
51189196 14524
Satellite: ISS
Catalog Number: 25544
Epoch time: 19163
53060667 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 24
4169 deg
Eccentricity:
0007935
Arg of perigee: 36
8443 deg
Mean anomaly: 323
3252 deg
Mean motion: 15
51189196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 311
Coasting Arc #14 (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 = -4829627
90 A = 6789966
58 meter
Y = 1964617
62 meter E =
0017018
Z = 4342794
39 I = 51
76341
XDOT = -5029
029218 Wp = 57
33741
YDOT = -4621
048822 meter/sec RA = 18
88308 deg
ZDOT = -3483
391683 TA = 68
09455
MA = 67
91369
Ha = 228
214 n
mi
Hp = 217
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15845235
89 X = -4872332
92
Y = 6445595
88 feet Y = 1910370
04 meter
Z = 14248013
09 Z = 4319230
19
XDOT = -16499
439692 XDOT = -4960
061044
YDOT = -15160
921332 feet/sec YDOT = -4676
900904 meter/sec
ZDOT = -11428
450403 ZDOT = -3507
654071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5785584
24 X = 1763446
08
Y = 16192160
54 feet Y = 4935370
53 meter
Z = 14140864
03 Z = 4310135
36
XDOT = -14643
469148 XDOT = -4463
329396
YDOT = 15363
055992 feet/sec YDOT = 4682
659466 meter/sec
ZDOT = -11537
938081 ZDOT = -3516
763527
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
56139803
00016717 00000-0 10270-3 0 9137
2 25544 51
6424 19
3017 0007962 39
8931 320
2804 15
51211691 14682
Satellite: ISS
Catalog Number: 25544
Epoch time: 19164
56139803 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 19
3017 deg
Eccentricity:
0007962
Arg of perigee: 39
8931 deg
Mean anomaly: 320
2804 deg
Mean motion: 15
51211691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 303
Coasting Arc #15 (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 = 5242786
72 A = 6791596
05 meter
Y = -1868244
22 meter E =
0012210
Z = -3898775
68 I = 51
73552
XDOT = 4644
966309 Wp = 70
49831
YDOT = 4490
724842 meter/sec RA = 13
92650 deg
ZDOT = 4108
779409 TA = 242
55445
MA = 242
67868
Ha = 228
226 n
mi
Hp = 217
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17200743
84 X = 5282226
56
Y = -6129410
18 feet Y = -1809394
63 meter
Z = -12791258
80 Z = -3873212
43
XDOT = 15239
390776 XDOT = 4574
446175
YDOT = 14733
349219 feet/sec YDOT = 4542
273222 meter/sec
ZDOT = 13480
247404 ZDOT = 4131
172475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5714859
08 X = -1741889
05
Y = -17427991
07 feet Y = -5312051
68 meter
Z = -12675057
11 Z = -3863357
41
XDOT = 13821
697412 XDOT = 4212
853371
YDOT = -14374
868329 feet/sec YDOT = -4381
459867 meter/sec
ZDOT = 13581
259578 ZDOT = 4139
567920
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
52776656
00016717 00000-0 10270-3 0 9148
2 25544 51
6411 14
5056 0007823 44
3106 315
8670 15
51185206 14839
Satellite: ISS
Catalog Number: 25544
Epoch time: 19165
52776656 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 14
5056 deg
Eccentricity:
0007823
Arg of perigee: 44
3106 deg
Mean anomaly: 315
8670 deg
Mean motion: 15
51185206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 301
Coasting Arc #16 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2019/166/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5644160
86 A = 6793228
51 meter
Y = 1770566
91 meter E =
0018989
Z = 3329807
93 I = 51
70935
XDOT = -4165
384948 Wp = 74
36857
YDOT = -4406
189735 meter/sec RA = 8
96899 deg
ZDOT = -4690
298639 TA = 66
95079
MA = 66
75067
Ha = 228
238 n
mi
Hp = 216
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18517588
12 X = -5679714
83
Y = 5808946
54 feet Y = 1707250
61 meter
Z = 10924566
71 Z = 3302304
44
XDOT = -13665
961114 XDOT = -4093
021061
YDOT = -14456
003068 feet/sec YDOT = -4452
364607 meter/sec
ZDOT = -15388
118893 ZDOT = -4710
357636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5684437
18 X = 1732616
45
Y = 18629206
83 feet Y = 5678182
24 meter
Z = 10799579
35 Z = 3291711
79
XDOT = -13189
552211 XDOT = -4020
175514
YDOT = 13050
201964 feet/sec YDOT = 3977
701559 meter/sec
ZDOT = -15478
544708 ZDOT = -4717
860427
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 19166
55855558
00016717 00000-0 10270-3 0 9152
2 25544 51
6418 9
3890 0007870 46
5003 313
6802 15
51217804 14996
Satellite: ISS
Catalog Number: 25544
Epoch time: 19166
55855558 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 9
3890 deg
Eccentricity:
0007870
Arg of perigee: 46
5003 deg
Mean anomaly: 313
6802 deg
Mean motion: 15
51217804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 322
Coasting Arc #17 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2019/167/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5956839
82 A = 6794802
72 meter
Y = -1761991
20 meter E =
0012772
Z = -2751179
33 I = 51
67925
XDOT = 3650
974965 Wp = 53
25455
YDOT = 4337
294828 meter/sec RA = 4
01124 deg
ZDOT = 5151
294216 TA = 275
67110
MA = 275
81673
Ha = 228
373 n
mi
Hp = 216
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19543437
72 X = 5989463
94
Y = -5780811
02 feet Y = -1695194
73 meter
Z = -9026178
90 Z = -2722164
17
XDOT = 11978
264321 XDOT = 3577
180508
YDOT = 14229
969908 feet/sec YDOT = 4377
709043 meter/sec
ZDOT = 16900
571575 ZDOT = 5168
850923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5986388
52 X = -1824651
22
Y = -19541994
09 feet Y = -5956399
80 meter
Z = -8894338
58 Z = -2710994
40
XDOT = 12681
090825 XDOT = 3865
196484
YDOT = -11576
341671 feet/sec YDOT = -3528
468941 meter/sec
ZDOT = 16979
649396 ZDOT = 5175
397136
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 19167
52492178
00016717 00000-0 10270-3 0 9166
2 25544 51
6398 4
5925 0007911 52
1407 308
0459 15
51180131 15142
Satellite: ISS
Catalog Number: 25544
Epoch time: 19167
52492178 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 4
5925 deg
Eccentricity:
0007911
Arg of perigee: 52
1407 deg
Mean anomaly: 308
0459 deg
Mean motion: 15
51180131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1514
Checksum: 302
Coasting Arc #18 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2019/168/12:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 931378
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6233952
82 A = 6796058
09 meter
Y = 1733630
83 meter E =
0019305
Z = 2060803
43 I = 51
65054
XDOT = -3050
287830 Wp = 90
90358
YDOT = -4331
904748 meter/sec RA = 359
05348 deg
ZDOT = -5538
360443 TA = 66
33084
MA = 66
12834
Ha = 228
272 n
mi
Hp = 216
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20452601
11 X = -6262885
70
Y = 5687765
19 feet Y = 1663756
23 meter
Z = 6761166
13 Z = 2030451
26
XDOT = -10007
506005 XDOT = -2974
718235
YDOT = -14212
285917 feet/sec YDOT = -4365
591607 meter/sec
ZDOT = -18170
473894 ZDOT = -5552
994897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6253220
99 X = 1905981
76
Y = 20332301
47 feet Y = 6197285
49 meter
Z = 6623267
82 Z = 2018772
03
XDOT = -12451
913514 XDOT = -3795
343239
YDOT = 9818
771200 feet/sec YDOT = 2992
761462 meter/sec
ZDOT = -18236
293854 ZDOT = -5558
422367
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 19168
55570894
00016717 00000-0 10270-3 0 9173
2 25544 51
6398 359
4764 0007853 54
0773 306
1106 15
51227416 15301
Satellite: ISS
Catalog Number: 25544
Epoch time: 19168
55570894 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 359
4764 deg
Eccentricity:
0007853
Arg of perigee: 54
0773 deg
Mean anomaly: 306
1106 deg
Mean motion: 15
51227416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 328
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