[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 10th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
107/20:48:33
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
3
109/09:19:21
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 441)
---------------------------------------
Vector Time (GMT): 2019/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5905409
93 A = 6792692
92 meter
Y = -2827242
11 meter E =
0006655
Z = -1803138
74 I = 51
57497
XDOT = 3531
562754 Wp = 49
02644
YDOT = 3785
382197 meter/sec RA = 347
03660 deg
ZDOT = 5648
715956 TA = 291
16254
MA = 291
23364
Ha = 223
786 n
mi
Hp = 217
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19374704
49 X = 5945344
82
Y = -9275728
72 feet Y = -2760980
50 meter
Z = -5915809
53 Z = -1774354
93
XDOT = 11586
491975 XDOT = 3461
532359
YDOT = 12419
232929 feet/sec YDOT = 3824
483347 meter/sec
ZDOT = 18532
532663 ZDOT = 5665
700898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16210721
75 X = 4941027
99
Y = -14147709
37 feet Y = -4312221
82 meter
Z = -5785321
07 Z = -1763365
86
XDOT = 13344
240762 XDOT = 4067
324584
YDOT = 7705
058111 feet/sec YDOT = 2348
501712 meter/sec
ZDOT = 18608
882802 ZDOT = 5671
987478
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 19098
50346308
00016717 00000-0 10270-3 0 9003
2 25544 51
6428 347
6260 0001594 164
6779 195
4422 15
52518374 4423
Satellite: ISS
Catalog Number: 25544
Epoch time: 19098
50346308 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 347
6260 deg
Eccentricity:
0001594
Arg of perigee: 164
6779 deg
Mean anomaly: 195
4422 deg
Mean motion: 15
52518374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 442
Checksum: 320
Coasting Arc #2 (Orbit 457)
---------------------------------------
Vector Time (GMT): 2019/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6254373
72 A = 6793993
06 meter
Y = 2556117
60 meter E =
0014440
Z = 637528
13 I = 51
54703
XDOT = -2339
388056 Wp = 132
33390
YDOT = -4218
169435 meter/sec RA = 342
06764 deg
ZDOT = -5960
908458 TA = 40
77653
MA = 40
66856
Ha = 223
816 n
mi
Hp = 217
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20519598
81 X = -6285588
91
Y = 8386212
61 feet Y = 2486002
31 meter
Z = 2091627
73 Z = 607070
44
XDOT = -7675
157663 XDOT = -2263
090261
YDOT = -13839
138565 feet/sec YDOT = -4243
903700 meter/sec
ZDOT = -19556
786279 ZDOT = -5972
087018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17291393
63 X = -5270416
78
Y = 13890590
92 feet Y = 4233852
11 meter
Z = 1953610
47 Z = 595460
47
XDOT = -10162
825587 XDOT = -3097
629239
YDOT = -9855
421943 feet/sec YDOT = -3003
932608 meter/sec
ZDOT = -19606
826616 ZDOT = -5976
160753
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 19099
53337353
00016717 00000-0 10270-3 0 9018
2 25544 51
6430 342
5047 0001697 167
2966 192
8229 15
52474872 4581
Satellite: ISS
Catalog Number: 25544
Epoch time: 19099
53337353 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 342
5047 deg
Eccentricity:
0001697
Arg of perigee: 167
2966 deg
Mean anomaly: 192
8229 deg
Mean motion: 15
52474872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 458
Checksum: 333
Coasting Arc #3 (Orbit 473)
---------------------------------------
Vector Time (GMT): 2019/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6385095
07 A = 6793849
70 meter
Y = -2244924
54 meter E =
0012336
Z = 524574
12 I = 51
51528
XDOT = 1143
529926 Wp = 56
42698
YDOT = 4669
760352 meter/sec RA = 337
09631 deg
ZDOT = 5970
613695 TA = 309
23834
MA = 309
34777
Ha = 223
656 n
mi
Hp = 217
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20948474
63 X = 6407175
78
Y = -7365237
99 feet Y = -2173398
47 meter
Z = 1721043
71 Z = 555644
50
XDOT = 3751
738601 XDOT = 1062
224127
YDOT = 15320
736062 feet/sec YDOT = 4682
093587 meter/sec
ZDOT = 19588
627607 ZDOT = 5975
971040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17742320
37 X = 5407859
25
Y = -13333833
88 feet Y = -4064152
57 meter
Z = 1861787
58 Z = 567472
85
XDOT = 7098
585038 XDOT = 2163
648720
YDOT = 12224
096862 feet/sec YDOT = 3725
904723 meter/sec
ZDOT = 19612
293757 ZDOT = 5977
827137
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 19100
56327679
00016717 00000-0 10270-3 0 9025
2 25544 51
6425 337
3824 0001456 172
9585 187
1587 15
52528395 4745
Satellite: ISS
Catalog Number: 25544
Epoch time: 19100
56327679 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 337
3824 deg
Eccentricity:
0001456
Arg of perigee: 172
9585 deg
Mean anomaly: 187
1587 deg
Mean motion: 15
52528395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 474
Checksum: 334
Coasting Arc #4 (Orbit 488)
---------------------------------------
Vector Time (GMT): 2019/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6318284
50 A = 6792825
00 meter
Y = 1813125
36 meter E =
0008848
Z = -1697921
19 I = 51
48062
XDOT = 46
027156 Wp = 147
62112
YDOT = -5142
164996 meter/sec RA = 332
12325 deg
ZDOT = -5683
404630 TA = 51
02095
MA = 50
94216
Ha = 223
616 n
mi
Hp = 217
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20729279
87 X = -6329842
19
Y = 5948574
01 feet Y = 1742405
25 meter
Z = -5570607
59 Z = -1728641
33
XDOT = 151
007731 XDOT = 131
131882
YDOT = -16870
620067 feet/sec YDOT = -5141
174467 meter/sec
ZDOT = -18646
340650 ZDOT = -5682
974315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17728372
52 X = -5403607
94
Y = 12215737
93 feet Y = 3723356
92 meter
Z = -5709711
05 Z = -1740319
93
XDOT = -4209
646120 XDOT = -1283
100137
YDOT = -14792
047498 feet/sec YDOT = -4508
616077 meter/sec
ZDOT = -18643
786595 ZDOT = -5682
626154
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 19101
52881119
00016717 00000-0 10270-3 0 9037
2 25544 51
6418 332
5814 0001586 179
7333 180
3820 15
52485422 4897
Satellite: ISS
Catalog Number: 25544
Epoch time: 19101
52881119 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 332
5814 deg
Eccentricity:
0001586
Arg of perigee: 179
7333 deg
Mean anomaly: 180
3820 deg
Mean motion: 15
52485422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 489
Checksum: 308
Coasting Arc #5 (Orbit 504)
---------------------------------------
Vector Time (GMT): 2019/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6063296
58 A = 6790700
35 meter
Y = -1304191
74 meter E =
0013108
Z = 2752771
16 I = 51
44515
XDOT = -1132
127313 Wp = 85
10684
YDOT = 5591
484282 meter/sec RA = 327
14390 deg
ZDOT = 5122
750598 TA = 306
14324
MA = 306
26448
Ha = 223
480 n
mi
Hp = 217
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19892705
32 X = 6064058
33
Y = -4278844
31 feet Y = -1236383
45 meter
Z = 9031401
43 Z = 2782226
30
XDOT = -3714
328456 XDOT = -1219
452267
YDOT = 18344
764705 feet/sec YDOT = 5578
335804 meter/sec
ZDOT = 16806
924535 ZDOT = 5117
039012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17263163
09 X = 5261812
11
Y = -10657651
69 feet Y = -3248452
23 meter
Z = 9164720
73 Z = 2793406
88
XDOT = 1744
695790 XDOT = 531
783277
YDOT = 17311
452644 feet/sec YDOT = 5276
530766 meter/sec
ZDOT = 16780
447308 ZDOT = 5114
680340
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 19102
55870929
00016717 00000-0 10270-3 0 9049
2 25544 51
6420 327
4592 0001360 185
4944 174
6193 15
52523157 5054
Satellite: ISS
Catalog Number: 25544
Epoch time: 19102
55870929 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 327
4592 deg
Eccentricity:
0001360
Arg of perigee: 185
4944 deg
Mean anomaly: 174
6193 deg
Mean motion: 15
52523157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 505
Checksum: 307
Coasting Arc #6 (Orbit 519)
---------------------------------------
Vector Time (GMT): 2019/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5654504
05 A = 6788080
77 meter
Y = 650065
34 meter E =
0005421
Z = -3703544
89 I = 51
40853
XDOT = 2118
773046 Wp = 91
02614
YDOT = -5981
677600 meter/sec RA = 322
15801 deg
ZDOT = -4290
388837 TA = 133
22289
MA = 133
17761
Ha = 223
439 n
mi
Hp = 217
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18551522
46 X = -5643363
27
Y = 2132760
29 feet Y = 586894
95 meter
Z = -12150737
83 Z = -3730985
27
XDOT = 6951
355139 XDOT = 2206
344695
YDOT = -19624
926508 feet/sec YDOT = -5957
494421 meter/sec
ZDOT = -14076
078862 ZDOT = -4279
883855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16553206
98 X = -5045417
49
Y = 8465639
12 feet Y = 2580326
80 meter
Z = -12274867
61 Z = -3741379
65
XDOT = 342
912510 XDOT = 104
519733
YDOT = -19643
290427 feet/sec YDOT = -5987
274922 meter/sec
ZDOT = -14027
896188 ZDOT = -4275
702758
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 19103
52423495
00016717 00000-0 10270-3 0 9050
2 25544 51
6414 322
6571 0001370 191
8695 168
2424 15
52522791 5202
Satellite: ISS
Catalog Number: 25544
Epoch time: 19103
52423495 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 322
6571 deg
Eccentricity:
0001370
Arg of perigee: 191
8695 deg
Mean anomaly: 168
2424 deg
Mean motion: 15
52522791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 520
Checksum: 296
Coasting Arc #7 (Orbit 535)
---------------------------------------
Vector Time (GMT): 2019/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5125228
88 A = 6785565
51 meter
Y = 87864
66 meter E =
0009435
Z = 4441481
44 I = 51
37346
XDOT = -2943
454244 Wp = 118
49914
YDOT = 6283
876035 meter/sec RA = 317
16599 deg
ZDOT = 3262
565275 TA = 298
45342
MA = 298
54845
Ha = 223
414 n
mi
Hp = 217
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16815055
37 X = 5102291
24
Y = 288269
89 feet Y = 145050
46 meter
Z = 14571789
49 Z = 4466322
09
XDOT = -9657
002114 XDOT = -3029
351255
YDOT = 20616
391191 feet/sec YDOT = 6250
480101 meter/sec
ZDOT = 10703
954314 ZDOT = 3248
058276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15661166
74 X = 4773523
62
Y = -5854225
31 feet Y = -1784367
87 meter
Z = 14684077
70 Z = 4475706
88
XDOT = -1927
318408 XDOT = -587
446651
YDOT = 21605
647745 feet/sec YDOT = 6585
401433 meter/sec
ZDOT = 10637
659126 ZDOT = 3242
358502
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 19104
55412808
00016717 00000-0 10270-3 0 9061
2 25544 51
6405 317
5355 0001270 188
2716 171
8415 15
52505912 5361
Satellite: ISS
Catalog Number: 25544
Epoch time: 19104
55412808 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 317
5355 deg
Eccentricity:
0001270
Arg of perigee: 188
2716 deg
Mean anomaly: 171
8415 deg
Mean motion: 15
52505912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 536
Checksum: 296
Coasting Arc #8 (Orbit 550)
---------------------------------------
Vector Time (GMT): 2019/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4518035
37 A = 6783342
67 meter
Y = -947450
30 meter E =
0011990
Z = -4981170
87 I = 51
34152
XDOT = 3609
967257 Wp = 80
19576
YDOT = -6432
438236 meter/sec RA = 312
16696 deg
ZDOT = -2053
065307 TA = 169
73323
MA = 169
70872
Ha = 223
373 n
mi
Hp = 217
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14822950
68 X = -4482909
21
Y = -3108432
74 feet Y = -997778
01 meter
Z = -16342424
10 Z = -5003032
37
XDOT = 11843
724597 XDOT = 3691
600940
YDOT = -21103
799987 feet/sec YDOT = -6391
612726 meter/sec
ZDOT = -6735
778567 ZDOT = -2035
330852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14784441
21 X = -4506297
68
Y = 2750653
96 feet Y = 838399
33 meter
Z = -16441144
96 Z = -5011260
98
XDOT = 3119
339653 XDOT = 950
774726
YDOT = -22967
860274 feet/sec YDOT = -7000
603812 meter/sec
ZDOT = -6654
893984 ZDOT = -2028
411686
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 19105
51964780
00016717 00000-0 10270-3 0 9070
2 25544 51
6393 312
7336 0001403 199
3792 160
7307 15
52541304 5517
Satellite: ISS
Catalog Number: 25544
Epoch time: 19105
51964780 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 312
7336 deg
Eccentricity:
0001403
Arg of perigee: 199
3792 deg
Mean anomaly: 160
7307 deg
Mean motion: 15
52541304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 551
Checksum: 301
Coasting Arc #9 (Orbit 566)
---------------------------------------
Vector Time (GMT): 2019/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3867477
12 A = 6782215
44 meter
Y = 1857765
33 meter E =
0003534
Z = 5250902
52 I = 51
31629
XDOT = -4114
214850 Wp = 139
57595
YDOT = 6426
463303 meter/sec RA = 307
16313 deg
ZDOT = 753
659505 TA = 303
17355
MA = 303
20744
Ha = 223
277 n
mi
Hp = 217
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12688573
21 X = 3820909
63
Y = 6095030
61 feet Y = 1900754
17 meter
Z = 17227370
48 Z = 5269576
05
XDOT = -13498
080216 XDOT = -4189
432475
YDOT = 21084
197188 feet/sec YDOT = 6380
034758 meter/sec
ZDOT = 2472
636170 ZDOT = 733
491023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13960514
53 X = 4255164
83
Y = 587247
31 feet Y = 178992
98 meter
Z = 17311578
69 Z = 5276569
19
XDOT = -3961
188461 XDOT = -1207
370243
YDOT = 23703
538716 feet/sec YDOT = 7224
838601 meter/sec
ZDOT = 2380
768272 ZDOT = 725
658169
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 19106
54953399
00016717 00000-0 10270-3 0 9089
2 25544 51
6396 307
6114 0001361 200
6475 159
4622 15
52517811 5672
Satellite: ISS
Catalog Number: 25544
Epoch time: 19106
54953399 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 307
6114 deg
Eccentricity:
0001361
Arg of perigee: 200
6475 deg
Mean anomaly: 159
4622 deg
Mean motion: 15
52517811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 567
Checksum: 315
Coasting Arc #10 (Orbit 581)
---------------------------------------
Vector Time (GMT): 2019/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3219144
90 A = 6782073
37 meter
Y = -2819679
88 meter E =
0014343
Z = -5273966
95 I = 51
29477
XDOT = 4455
953452 Wp = 99
80400
YDOT = -6196
662155 meter/sec RA = 302
15537 deg
ZDOT = 592
133348 TA = 175
89026
MA = 175
87846
Ha = 223
356 n
mi
Hp = 217
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10561499
01 X = -3161757
04
Y = -9250918
24 feet Y = -2855358
17 meter
Z = -17303041
19 Z = -5289464
82
XDOT = 14619
269857 XDOT = 4522
038845
YDOT = -20330
256415 feet/sec YDOT = -6146
463009 meter/sec
ZDOT = 1942
694710 ZDOT = 613
939824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13337640
52 X = -4065312
83
Y = -4100419
44 feet Y = -1249807
85 meter
Z = -17372791
66 Z = -5295226
90
XDOT = 4585
016597 XDOT = 1397
513059
YDOT = -23579
253069 feet/sec YDOT = -7186
956335 meter/sec
ZDOT = 2041
923715 ZDOT = 622
378348
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 19107
51504728
00016717 00000-0 10270-3 0 9096
2 25544 51
6375 302
8083 0001364 200
8632 159
2465 15
52554721 5822
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
51504728 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 302
8083 deg
Eccentricity:
0001364
Arg of perigee: 200
8632 deg
Mean anomaly: 159
2465 deg
Mean motion: 15
52554721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 582
Checksum: 302
Coasting Arc #11 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:48:33
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2638302
94 A = 6793426
78 meter
Y = 6164656
53 meter E =
0013984
Z = 1042667
77 I = 51
32889
XDOT = -4819
711423 Wp = 129
32224
YDOT = -1062
602144 meter/sec RA = 300
31835 deg
ZDOT = -5868
805759 TA = 39
32805
MA = 39
22658
Ha = 223
330 n
mi
Hp = 217
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8655849
54 X = -2712106
54
Y = 20225251
07 feet Y = 6134740
60 meter
Z = 3420826
01 Z = 1029672
03
XDOT = -15812
701520 XDOT = -4778
963288
YDOT = -3486
227508 feet/sec YDOT = -1116
272174 meter/sec
ZDOT = -19254
612070 ZDOT = -5892
119218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15906432
78 X = 4848280
71
Y = -15210941
48 feet Y = -4636294
96 meter
Z = 3361431
01 Z = 1024564
17
XDOT = 11955
499084 XDOT = 3644
036121
YDOT = 8191
248044 feet/sec YDOT = 2496
692404 meter/sec
ZDOT = -19359
875886 ZDOT = -5900
890170
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 19107
90125264
00016717 00000-0 10270-3 0 9105
2 25544 51
6400 300
8889 0001430 199
6372 160
4725 15
52568403 5884
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90125264 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 300
8889 deg
Eccentricity:
0001430
Arg of perigee: 199
6372 deg
Mean anomaly: 160
4725 deg
Mean motion: 15
52568403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 303
Coasting Arc #12 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2019/108/20:48:33
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2997350
79 A = 6794026
69 meter
Y = -6090068
65 meter E =
0011145
Z = 129047
74 I = 51
31376
XDOT = 4246
567387 Wp = 49
23323
YDOT = 2223
835356 meter/sec RA = 295
33274 deg
ZDOT = 5981
506783 TA = 312
16216
MA = 312
25677
Ha = 223
387 n
mi
Hp = 217
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9833828
05 X = 3064602
05
Y = -19980540
18 feet Y = -6056174
14 meter
Z = 423384
97 Z = 143771
71
XDOT = 13932
307701 XDOT = 4192
329023
YDOT = 7296
047755 feet/sec YDOT = 2271
020622 meter/sec
ZDOT = 19624
366087 ZDOT = 6002
003362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16618149
71 X = -5065212
03
Y = 14822343
12 feet Y = 4517850
18 meter
Z = 490570
76 Z = 149525
97
XDOT = -8966
331178 XDOT = -2732
937743
YDOT = -10736
406574 feet/sec YDOT = -3272
456724 meter/sec
ZDOT = 19716
773777 ZDOT = 6009
672647
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 19108
93113276
00016717 00000-0 10270-3 0 9110
2 25544 51
6393 295
7668 0001332 205
9029 154
2056 15
52510855 6048
Satellite: ISS
Catalog Number: 25544
Epoch time: 19108
93113276 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 295
7668 deg
Eccentricity:
0001332
Arg of perigee: 205
9029 deg
Mean anomaly: 154
2056 deg
Mean motion: 15
52510855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 302
Coasting Arc #13 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2019/109/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4463532
57 A = 6789445
47 meter
Y = -3964887
86 meter E =
0011917
Z = 3223079
24 I = 51
29297
XDOT = 1697
899636 Wp = 91
35126
YDOT = 5780
014593 meter/sec RA = 292
75198 deg
ZDOT = 4743
431376 TA = 306
14914
MA = 306
25935
Ha = 223
157 n
mi
Hp = 217
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14644135
73 X = 4491881
18
Y = -13008162
26 feet Y = -3914814
79 meter
Z = 10574406
96 Z = 3244830
83
XDOT = 5570
536865 XDOT = 1610
098394
YDOT = 18963
302469 feet/sec YDOT = 5798
511077 meter/sec
ZDOT = 15562
438897 ZDOT = 4751
465619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17264147
13 X = 5262112
05
Y = -9138632
95 feet Y = -2785455
32 meter
Z = 10673129
39 Z = 3253169
84
XDOT = 98
681141 XDOT = 30
078012
YDOT = 18462
628932 feet/sec YDOT = 5627
409298 meter/sec
ZDOT = 15598
151376 ZDOT = 4754
316539
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 19109
44606848
00016717 00000-0 10270-3 0 9120
2 25544 51
6406 293
2073 0001224 220
6044 139
5017 15
52549456 6128
Satellite: ISS
Catalog Number: 25544
Epoch time: 19109
44606848 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 293
2073 deg
Eccentricity:
0001224
Arg of perigee: 220
6044 deg
Mean anomaly: 139
5017 deg
Mean motion: 15
52549456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 292
Coasting Arc #14 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2019/110/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4440956
70 A = 6786697
93 meter
Y = 3102972
79 meter E =
0006354
Z = -4094124
89 I = 51
27166
XDOT = -1092
538649 Wp = 75
44251
YDOT = -6563
828078 meter/sec RA = 287
75297 deg
ZDOT = -3793
081572 TA = 155
16721
MA = 155
13661
Ha = 223
118 n
mi
Hp = 217
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14570067
91 X = -4455437
64
Y = 10180356
92 feet Y = 3053229
76 meter
Z = -13432168
26 Z = -4115733
05
XDOT = -3584
444386 XDOT = -1000
633865
YDOT = -21534
869021 feet/sec YDOT = -6575
531897 meter/sec
ZDOT = -12444
493345 ZDOT = -3798
165304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16383545
92 X = -4993704
80
Y = 6698076
13 feet Y = 2041573
60 meter
Z = -13530147
43 Z = -4123988
94
XDOT = 1872
820458 XDOT = 570
835676
YDOT = -20579
743167 feet/sec YDOT = -6272
705717 meter/sec
ZDOT = -12466
796919 ZDOT = -3799
879701
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 19110
41157265
00016717 00000-0 10270-3 0 9134
2 25544 51
6401 288
4045 0001280 227
0375 133
0670 15
52561677 6277
Satellite: ISS
Catalog Number: 25544
Epoch time: 19110
41157265 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 288
4045 deg
Eccentricity:
0001280
Arg of perigee: 227
0375 deg
Mean anomaly: 133
0670 deg
Mean motion: 15
52561677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 285
Coasting Arc #15 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2019/111/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4372729
98 A = 6784345
10 meter
Y = -2115083
99 meter E =
0007335
Z = 4733085
26 I = 51
25402
XDOT = 572
369806 Wp = 126
28614
YDOT = 7166
238643 meter/sec RA = 282
74921 deg
ZDOT = 2666
434805 TA = 297
19701
MA = 297
27175
Ha = 223
099 n
mi
Hp = 217
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14346226
98 X = 4373065
37
Y = -6939251
93 feet Y = -2066183
12 meter
Z = 15528494
95 Z = 4754327
55
XDOT = 1877
853693 XDOT = 479
240070
YDOT = 23511
281638 feet/sec YDOT = 7172
118602 meter/sec
ZDOT = 8748
145687 ZDOT = 2668
988905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15365544
57 X = 4683417
99
Y = -3856144
80 feet Y = -1175352
94 meter
Z = 15624717
22 Z = 4762413
81
XDOT = -3343
582333 XDOT = -1019
123895
YDOT = 22261
979500 feet/sec YDOT = 6785
451352 meter/sec
ZDOT = 8758
963304 ZDOT = 2669
732015
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 19111
44144328
00016717 00000-0 10270-3 0 9145
2 25544 51
6397 283
2824 0001114 225
7939 134
3121 15
52539073 6434
Satellite: ISS
Catalog Number: 25544
Epoch time: 19111
44144328 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 283
2824 deg
Eccentricity:
0001114
Arg of perigee: 225
7939 deg
Mean anomaly: 134
3121 deg
Mean motion: 15
52539073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 293
Coasting Arc #16 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2019/112/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4310002
50 A = 6782509
57 meter
Y = 1007035
31 meter E =
0012710
Z = -5150600
52 I = 51
24112
XDOT = -101
510127 Wp = 81
95966
YDOT = -7528
793887 meter/sec RA = 277
74014 deg
ZDOT = -1388
280459 TA = 174
60120
MA = 174
58749
Ha = 223
070 n
mi
Hp = 217
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14140428
14 X = -4295923
99
Y = 3303921
61 feet Y = 958916
61 meter
Z = -16898295
68 Z = -5171503
01
XDOT = -333
038475 XDOT = -10
569873
YDOT = -24700
767345 feet/sec YDOT = -7529
420552 meter/sec
ZDOT = -4554
725916 ZDOT = -1388
552756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14398381
93 X = -4388626
81
Y = 590700
34 feet Y = 180045
46 meter
Z = -16992871
27 Z = -5179427
16
XDOT = 4417
004423 XDOT = 1346
302948
YDOT = -23262
667507 feet/sec YDOT = -7090
461056 meter/sec
ZDOT = -4555
204002 ZDOT = -1388
426180
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 19112
40694199
00016717 00000-0 10270-3 0 9159
2 25544 51
6388 278
4800 0001299 233
0262 127
0771 15
52579220 6583
Satellite: ISS
Catalog Number: 25544
Epoch time: 19112
40694199 = yrday
fracday
Element set: 915
Inclination: 51
6388 deg
RA of node: 278
4800 deg
Eccentricity:
0001299
Arg of perigee: 233
0262 deg
Mean anomaly: 127
0771 deg
Mean motion: 15
52579220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 316
Coasting Arc #17 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2019/113/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4243259
26 A = 6781932
06 meter
Y = 148594
27 meter E =
0001575
Z = 5287238
64 I = 51
23640
XDOT = -327
528178 Wp = 120
81734
YDOT = 7660
304720 meter/sec RA = 272
72889 deg
ZDOT = 46
765514 TA = 328
72980
MA = 328
73916
Ha = 222
945 n
mi
Hp = 217
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13921454
26 X = 4215599
50
Y = 487514
01 feet Y = 195890
57 meter
Z = 17346583
46 Z = 5307783
87
XDOT = -1074
567513 XDOT = -413
390704
YDOT = 25132
233332 feet/sec YDOT = 7656
161982 meter/sec
ZDOT = 153
430164 ZDOT = 44
966135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13514606
22 X = 4119251
98
Y = 2858338
68 feet Y = 871221
63 meter
Z = 17439433
34 Z = 5315539
28
XDOT = -5178
386288 XDOT = -1578
372141
YDOT = 23586
204011 feet/sec YDOT = 7189
074983 meter/sec
ZDOT = 144
543386 ZDOT = 44
056824
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 19113
43680574
00016717 00000-0 10270-3 0 9166
2 25544 51
6396 273
3578 0001279 236
0507 124
0523 15
52555204 6747
Satellite: ISS
Catalog Number: 25544
Epoch time: 19113
43680574 = yrday
fracday
Element set: 916
Inclination: 51
6396 deg
RA of node: 273
3578 deg
Eccentricity:
0001279
Arg of perigee: 236
0507 deg
Mean anomaly: 124
0523 deg
Mean motion: 15
52555204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 307
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