[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 16th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16989 6378 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
168/10:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 216
7
168/10:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 216
7
175/23:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 216
2
175/23:25:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 216
3
176/18:02:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 216
3
Coasting Arc #1 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2019/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5544905
17 A = 6795668
45 meter
Y = -3223607
68 meter E =
0009666
Z = -2256952
01 I = 51
75079
XDOT = 4177
194900 Wp = 80
64382
YDOT = -3382
380051 meter/sec RA = 14
06725 deg
ZDOT = -5449
932453 TA = 124
35960
MA = 124
26812
Ha = 228
168 n
mi
Hp = 217
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18191946
09 X = -5497482
64
Y = -10576140
67 feet Y = -3285349
22 meter
Z = -7404698
18 Z = -2283772
59
XDOT = 13704
707676 XDOT = 4241
180157
YDOT = -11097
047411 feet/sec YDOT = -3335
309193 meter/sec
ZDOT = -17880
355816 ZDOT = -5429
486094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13110654
51 X = -3996127
50
Y = 16404326
41 feet Y = 5000038
69 meter
Z = -7525956
59 Z = -2293911
57
XDOT = -7766
029962 XDOT = -2367
085932
YDOT = -14339
873319 feet/sec YDOT = -4370
793388 meter/sec
ZDOT = -17787
173570 ZDOT = -5421
530504
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
52770381
00016717 00000-0 10270-3 0 9002
2 25544 51
6418 14
5055 0007873 43
8324 316
3451 15
51186134 14830
Satellite: ISS
Catalog Number: 25544
Epoch time: 19165
52770381 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 14
5055 deg
Eccentricity:
0007873
Arg of perigee: 43
8324 deg
Mean anomaly: 316
3451 deg
Mean motion: 15
51186134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 296
Coasting Arc #2 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2019/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5270367
21 A = 6794203
19 meter
Y = 3150033
41 meter E =
0020177
Z = 2882785
95 I = 51
71350
XDOT = -4741
567407 Wp = 68
49155
YDOT = 3283
943929 meter/sec RA = 9
11257 deg
ZDOT = 5059
023712 TA = 324
29098
MA = 324
42577
Ha = 228
093 n
mi
Hp = 216
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17291231
02 X = 5220747
86
Y = 10334755
28 feet Y = 3208692
44 meter
Z = 9457959
16 Z = 2908267
62
XDOT = -15556
323514 XDOT = -4802
511113
YDOT = 10774
094254 feet/sec YDOT = 3230
578816 meter/sec
ZDOT = 16597
846824 ZDOT = 5035
843290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12469449
43 X = 3800688
19
Y = -15751652
77 feet Y = -4801103
76 meter
Z = 9573144
42 Z = 2917894
42
XDOT = 7517
544144 XDOT = 2291
347455
YDOT = 16016
171360 feet/sec YDOT = 4881
729031 meter/sec
ZDOT = 16492
275431 ZDOT = 5026
845551
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
55848163
00016717 00000-0 10270-3 0 9011
2 25544 51
6417 9
3887 0007834 47
2492 312
9318 15
51218633 14996
Satellite: ISS
Catalog Number: 25544
Epoch time: 19166
55848163 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 9
3887 deg
Eccentricity:
0007834
Arg of perigee: 47
2492 deg
Mean anomaly: 312
9318 deg
Mean motion: 15
51218633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 331
Coasting Arc #3 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2019/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4918898
06 A = 6792573
82 meter
Y = -3131057
28 meter E =
0012639
Z = -3499635
29 I = 51
67332
XDOT = 5262
834114 Wp = 63
91453
YDOT = -3210
119897 meter/sec RA = 4
15431 deg
ZDOT = -4532
448803 TA = 157
08022
MA = 157
02376
Ha = 228
304 n
mi
Hp = 216
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16138117
01 X = -4866520
74
Y = -10272497
64 feet Y = -3185770
35 meter
Z = -11481743
08 Z = -3523402
92
XDOT = 17266
516122 XDOT = 5320
355667
YDOT = -10531
889427 feet/sec YDOT = -3150
944757 meter/sec
ZDOT = -14870
238855 ZDOT = -4506
744671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12004490
11 X = -3658968
58
Y = 14811390
29 feet Y = 4514511
76 meter
Z = -11589149
55 Z = -3532372
78
XDOT = -7445
263099 XDOT = -2269
316193
YDOT = -17559
321727 feet/sec YDOT = -5352
081262 meter/sec
ZDOT = -14753
230428 ZDOT = -4496
784634
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
52483547
00016717 00000-0 10270-3 0 9021
2 25544 51
6401 4
5920 0008052 51
3769 308
8102 15
51206940 15141
Satellite: ISS
Catalog Number: 25544
Epoch time: 19167
52483547 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 4
5920 deg
Eccentricity:
0008052
Arg of perigee: 51
3769 deg
Mean anomaly: 308
8102 deg
Mean motion: 15
51206940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1514
Checksum: 286
Coasting Arc #4 (Orbit 1528)
---------------------------------------
Vector Time (GMT): 2019/168/10:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6787339
94 A = 6797801
30 meter
Y = 40740
14 meter E =
0020381
Z = 121585
52 I = 51
66165
XDOT = -147
893878 Wp = 49
50966
YDOT = 4756
378181 meter/sec RA = 359
53220 deg
ZDOT = 6012
611181 TA = 311
79876
MA = 311
97270
Ha = 228
337 n
mi
Hp = 216
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22268175
66 X = 6785789
33
Y = 133661
86 feet Y = 116632
23 meter
Z = 398902
62 Z = 154552
16
XDOT = -485
216135 XDOT = -230
276021
YDOT = 15604
915292 feet/sec YDOT = 4754
262554 meter/sec
ZDOT = 19726
414636 ZDOT = 6011
693583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11831627
86 X = 3606280
17
Y = -18861612
92 feet Y = -5749019
62 meter
Z = 548430
75 Z = 167161
69
XDOT = 11569
557865 XDOT = 3526
401237
YDOT = 7875
934770 feet/sec YDOT = 2400
584918 meter/sec
ZDOT = 19721
637328 ZDOT = 6011
155058
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
49118742
00016717 00000-0 10270-3 0 9031
2 25544 51
6420 359
7977 0008021 54
6491 305
5409 15
51216362 15292
Satellite: ISS
Catalog Number: 25544
Epoch time: 19168
49118742 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 359
7977 deg
Eccentricity:
0008021
Arg of perigee: 54
6491 deg
Mean anomaly: 305
5409 deg
Mean motion: 15
51216362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1529
Checksum: 317
Coasting Arc #5 (Orbit 1543)
---------------------------------------
Vector Time (GMT): 2019/169/10:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6671960
90 A = 6797174
02 meter
Y = -359498
50 meter E =
0012431
Z = -1248567
28 I = 51
62625
XDOT = 1339
887324 Wp = 102
65754
YDOT = -4770
901118 meter/sec RA = 354
57502 deg
ZDOT = -5838
084099 TA = 90
89282
MA = 90
75039
Ha = 228
324 n
mi
Hp = 216
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21889635
51 X = -6661380
19
Y = -1179457
01 feet Y = -434049
63 meter
Z = -4096349
35 Z = -1280951
45
XDOT = 4395
955787 XDOT = 1421
495400
YDOT = -15652
562723 feet/sec YDOT = -4755
460136 meter/sec
ZDOT = -19153
819221 ZDOT = -5831
378155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12118210
07 X = -3693630
43
Y = 18233805
35 feet Y = 5557663
87 meter
Z = -4243190
65 Z = -1293324
51
XDOT = -9857
897771 XDOT = -3004
687240
YDOT = -10963
444507 feet/sec YDOT = -3341
657886 meter/sec
ZDOT = -19122
786027 ZDOT = -5828
625181
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 19169
45753898
00016717 00000-0 10270-3 0 9046
2 25544 51
6421 355
0016 0007865 57
8267 302
3646 15
51188800 15447
Satellite: ISS
Catalog Number: 25544
Epoch time: 19169
45753898 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 355
0016 deg
Eccentricity:
0007865
Arg of perigee: 57
8267 deg
Mean anomaly: 302
3646 deg
Mean motion: 15
51188800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1544
Checksum: 327
Coasting Arc #6 (Orbit 1559)
---------------------------------------
Vector Time (GMT): 2019/170/10:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6494577
70 A = 6796105
49 meter
Y = 366044
09 meter E =
0021744
Z = 1930900
62 I = 51
58982
XDOT = -1950
447105 Wp = 65
06108
YDOT = 4869
038138 meter/sec RA = 349
61318 deg
ZDOT = 5596
812105 TA = 316
23332
MA = 316
40547
Ha = 228
247 n
mi
Hp = 216
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21307669
61 X = 6480622
62
Y = 1200932
06 feet Y = 438592
62 meter
Z = 6334975
79 Z = 1962414
81
XDOT = -6399
104675 XDOT = -2031
935134
YDOT = 15974
534572 feet/sec YDOT = 4846
770206 meter/sec
ZDOT = 18362
244438 ZDOT = 5587
140612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11527313
26 X = 3513525
08
Y = -17909473
29 feet Y = -5458807
46 meter
Z = 6477866
62 Z = 1974453
74
XDOT = 9378
988429 XDOT = 2858
715673
YDOT = 12709
239915 feet/sec YDOT = 3873
776326 meter/sec
ZDOT = 18317
751619 ZDOT = 5583
250694
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 19170
48830930
00016717 00000-0 10270-3 0 9055
2 25544 51
6419 349
8846 0007855 61
4917 298
7024 15
51237515 15602
Satellite: ISS
Catalog Number: 25544
Epoch time: 19170
48830930 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 349
8846 deg
Eccentricity:
0007855
Arg of perigee: 61
4917 deg
Mean anomaly: 298
7024 deg
Mean motion: 15
51237515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1560
Checksum: 331
Coasting Arc #7 (Orbit 1574)
---------------------------------------
Vector Time (GMT): 2019/171/10:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6251787
90 A = 6794800
66 meter
Y = -452262
68 meter E =
0011306
Z = -2633806
37 I = 51
55131
XDOT = 2549
314168 Wp = 86
50360
YDOT = -4991
803032 meter/sec RA = 344
64896 deg
ZDOT = -5212
784368 TA = 123
14215
MA = 123
03361
Ha = 228
408 n
mi
Hp = 216
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20511115
14 X = -6233472
48
Y = -1483801
45 feet Y = -522071
69 meter
Z = -8641097
00 Z = -2664130
51
XDOT = 8363
891626 XDOT = 2630
265029
YDOT = -16377
306536 feet/sec YDOT = -4962
841295 meter/sec
ZDOT = -17102
310917 ZDOT = -5200
205117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11078092
73 X = -3376602
66
Y = 17256550
90 feet Y = 5259796
72 meter
Z = -8778575
11 Z = -2675709
69
XDOT = -9076
920806 XDOT = -2766
645462
YDOT = -14467
074011 feet/sec YDOT = -4409
564159 meter/sec
ZDOT = -17044
620739 ZDOT = -5195
200401
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 19171
45465756
00016717 00000-0 10270-3 0 9064
2 25544 51
6405 345
0884 0008018 64
7751 295
4230 15
51209513 15757
Satellite: ISS
Catalog Number: 25544
Epoch time: 19171
45465756 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 345
0884 deg
Eccentricity:
0008018
Arg of perigee: 64
7751 deg
Mean anomaly: 295
4230 deg
Mean motion: 15
51209513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1575
Checksum: 315
Coasting Arc #8 (Orbit 1590)
---------------------------------------
Vector Time (GMT): 2019/172/10:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5941045
29 A = 6793242
07 meter
Y = 537461
03 meter E =
0020224
Z = 3228871
96 I = 51
51419
XDOT = -3068
021691 Wp = 79
97708
YDOT = 5173
222837 meter/sec RA = 339
68067 deg
ZDOT = 4761
980752 TA = 317
47694
MA = 317
63340
Ha = 228
245 n
mi
Hp = 216
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19491618
40 X = 5918909
81
Y = 1763323
59 feet Y = 603773
69 meter
Z = 10593411
93 Z = 3257677
34
XDOT = -10065
687963 XDOT = -3148
772926
YDOT = 16972
515870 feet/sec YDOT = 5138
461821 meter/sec
ZDOT = 15623
296431 ZDOT = 4746
882291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10549740
11 X = 3215560
78
Y = -16399755
42 feet Y = -4998645
45 meter
Z = 10723986
21 Z = 3268671
00
XDOT = 9145
352956 XDOT = 2787
503581
YDOT = 16100
744138 feet/sec YDOT = 4907
506813 meter/sec
ZDOT = 15554
167036 ZDOT = 4740
910113
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 19172
48542626
00016717 00000-0 10270-3 0 9071
2 25544 51
6402 339
9724 0007799 69
0892 291
1094 15
51232982 15913
Satellite: ISS
Catalog Number: 25544
Epoch time: 19172
48542626 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 339
9724 deg
Eccentricity:
0007799
Arg of perigee: 69
0892 deg
Mean anomaly: 291
1094 deg
Mean motion: 15
51232982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1591
Checksum: 338
Coasting Arc #9 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2019/173/10:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5585098
54 A = 6791529
21 meter
Y = -717489
38 meter E =
0014253
Z = -3812273
33 I = 51
47740
XDOT = 3532
888703 Wp = 73
26105
YDOT = -5348
263253 meter/sec RA = 334
70761 deg
ZDOT = -4178
211241 TA = 152
51112
MA = 152
43566
Ha = 228
444 n
mi
Hp = 216
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18323814
12 X = -5558142
58
Y = -2353967
77 feet Y = -779794
61 meter
Z = -12507458
44 Z = -3839337
98
XDOT = 11590
842200 XDOT = 3612
727145
YDOT = -17546
795451 feet/sec YDOT = -5308
309031 meter/sec
ZDOT = -13708
042130 ZDOT = -4160
856810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10266218
40 X = -3129143
37
Y = 15258601
36 feet Y = 4650821
69 meter
Z = -12630110
41 Z = -3849657
65
XDOT = -9354
126395 XDOT = -2851
137725
YDOT = -17550
377177 feet/sec YDOT = -5349
354964 meter/sec
ZDOT = -13628
671414 ZDOT = -4154
019047
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 19173
45177197
00016717 00000-0 10270-3 0 9087
2 25544 51
6400 335
1756 0008035 72
4556 287
7473 15
51227178 16063
Satellite: ISS
Catalog Number: 25544
Epoch time: 19173
45177197 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 335
1756 deg
Eccentricity:
0008035
Arg of perigee: 72
4556 deg
Mean anomaly: 287
7473 deg
Mean motion: 15
51227178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 324
Coasting Arc #10 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2019/174/10:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5185698
69 A = 6789928
68 meter
Y = 916213
23 meter E =
0017033
Z = 4272096
79 I = 51
44223
XDOT = -3916
818730 Wp = 93
06526
YDOT = 5561
041567 meter/sec RA = 329
73089 deg
ZDOT = 3548
651501 TA = 320
60895
MA = 320
73269
Ha = 228
315 n
mi
Hp = 216
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17013447
14 X = 5154316
65
Y = 3005948
91 feet Y = 974027
35 meter
Z = 14016065
59 Z = 4297210
63
XDOT = -12850
455150 XDOT = -3995
949992
YDOT = 18244
887031 feet/sec YDOT = 5516
798062 meter/sec
ZDOT = 11642
557417 ZDOT = 3529
433743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10019970
05 X = 3054086
87
Y = -13960336
77 feet Y = -4255110
65 meter
Z = 14129840
92 Z = 4306775
51
XDOT = 9853
415969 XDOT = 3003
321187
YDOT = 18810
566227 feet/sec YDOT = 5733
460586 meter/sec
ZDOT = 11554
724123 ZDOT = 3521
879913
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 19174
48253694
00016717 00000-0 10270-3 0 9099
2 25544 51
6399 330
0593 0007923 76
2581 283
9451 15
51224118 16221
Satellite: ISS
Catalog Number: 25544
Epoch time: 19174
48253694 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 330
0593 deg
Eccentricity:
0007923
Arg of perigee: 76
2581 deg
Mean anomaly: 283
9451 deg
Mean motion: 15
51224118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 324
Coasting Arc #11 (Orbit 1636)
---------------------------------------
Vector Time (GMT): 2019/175/10:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4772212
27 A = 6788387
87 meter
Y = -1212038
33 meter E =
0018962
Z = -4691455
59 I = 51
40827
XDOT = 4215
806559 Wp = 74
70435
YDOT = -5728
416960 meter/sec RA = 324
75053 deg
ZDOT = -2813
087019 TA = 167
24936
MA = 167
20133
Ha = 228
551 n
mi
Hp = 216
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15656864
40 X = -4735515
91
Y = -3976503
71 feet Y = -1265198
84 meter
Z = -15391914
66 Z = -4714548
05
XDOT = 13831
386347 XDOT = 4293
214343
YDOT = -18794
018896 feet/sec YDOT = -5680
839721 meter/sec
ZDOT = -9229
288120 ZDOT = -2792
421000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10092185
00 X = -3076097
99
Y = 12484704
23 feet Y = 3805337
85 meter
Z = -15496482
95 Z = -4723328
00
XDOT = -10392
996491 XDOT = -3167
785330
YDOT = -19721
078089 feet/sec YDOT = -6010
984601 meter/sec
ZDOT = -9134
882075 ZDOT = -2784
312057
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 19175
44887910
00016717 00000-0 10270-3 0 9102
2 25544 51
6393 325
2633 0008207 80
8728 279
3352 15
51227115 16371
Satellite: ISS
Catalog Number: 25544
Epoch time: 19175
44887910 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 325
2633 deg
Eccentricity:
0008207
Arg of perigee: 80
8728 deg
Mean anomaly: 279
3352 deg
Mean motion: 15
51227115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1637
Checksum: 317
Coasting Arc #12 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2019/175/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5573073
91 A = 6797557
66 meter
Y = -3847672
92 meter E =
0020359
Z = 491267
53 I = 51
42474
XDOT = 2355
936675 Wp = 62
66568
YDOT = 4197
373122 meter/sec RA = 322
06180 deg
ZDOT = 5966
549098 TA = 302
64437
MA = 302
84065
Ha = 228
489 n
mi
Hp = 216
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18284363
21 X = 5613299
19
Y = -12623598
81 feet Y = -3785126
04 meter
Z = 1611770
10 Z = 518436
56
XDOT = 7729
451034 XDOT = 2279
843338
YDOT = 13770
909194 feet/sec YDOT = 4223
292738 meter/sec
ZDOT = 19575
292316 ZDOT = 5977
808937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9055306
26 X = 2760057
35
Y = 20279563
63 feet Y = 6181210
99 meter
Z = 1735429
39 Z = 528958
88
XDOT = -13453
936779 XDOT = -4100
759930
YDOT = 4280
702475 feet/sec YDOT = 1304
758114 meter/sec
ZDOT = 19625
844845 ZDOT = 5981
957509
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 19176
02868161
00016717 00000-0 10270-3 0 9115
2 25544 51
6394 322
3891 0008167 83
1218 277
0862 15
51263029 16466
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
02868161 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 322
3891 deg
Eccentricity:
0008167
Arg of perigee: 83
1218 deg
Mean anomaly: 277
0862 deg
Mean motion: 15
51263029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 315
Coasting Arc #13 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2019/175/23:25:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4579965
79 A = 6787762
17 meter
Y = 1311270
62 meter E =
0014180
Z = 4823804
58 I = 51
39184
XDOT = -4292
394428 Wp = 98
95390
YDOT = 5857
825976 meter/sec RA = 322
02220 deg
ZDOT = 2474
663658 TA = 326
62268
MA = 326
71200
Ha = 228
346 n
mi
Hp = 216
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15026134
48 X = 4541531
17
Y = 4302068
95 feet Y = 1362271
57 meter
Z = 15826130
51 Z = 4845959
01
XDOT = -14082
658884 XDOT = -4369
599767
YDOT = 19218
589159 feet/sec YDOT = 5809
393458 meter/sec
ZDOT = 8118
975257 ZDOT = 2453
626058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6011948
45 X = -1832441
89
Y = 14316570
43 feet Y = 4363690
67 meter
Z = 15926431
13 Z = 4854376
21
XDOT = -16397
356649 XDOT = -4997
914307
YDOT = -15841
233247 feet/sec YDOT = -4828
407894 meter/sec
ZDOT = 8022
877136 ZDOT = 2445
372951
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 19176
02868284
00016717 00000-0 10270-3 0 9122
2 25544 51
6396 322
3889 0008029 81
3689 278
8371 15
51235808 16462
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
02868284 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 322
3889 deg
Eccentricity:
0008029
Arg of perigee: 81
3689 deg
Mean anomaly: 278
8371 deg
Mean motion: 15
51235808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 348
Coasting Arc #14 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2019/176/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3784571
66 A = 6786235
73 meter
Y = 2174906
67 meter E =
0011361
Z = 5186621
75 I = 51
36880
XDOT = -4954
145329 Wp = 97
61251
YDOT = 5732
491752 meter/sec RA = 318
15104 deg
ZDOT = 1207
378896 TA = 340
74416
MA = 340
78706
Ha = 228
349 n
mi
Hp = 216
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12416573
68 X = 3734776
31
Y = 7135520
58 feet Y = 2216949
42 meter
Z = 17016475
57 Z = 5204885
02
XDOT = -16253
757642 XDOT = -5023
744248
YDOT = 18807
387639 feet/sec YDOT = 5676
701743 meter/sec
ZDOT = 3961
216849 ZDOT = 1183
145167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12681068
90 X = -3865189
80
Y = -6439033
87 feet Y = -1962617
52 meter
Z = 17099027
21 Z = 5211783
49
XDOT = 14735
511296 XDOT = 4491
383843
YDOT = -18762
143884 feet/sec YDOT = -5718
701456 meter/sec
ZDOT = 3850
653330 ZDOT = 1173
679135
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 19176
80175379
00016717 00000-0 10270-3 0 9135
2 25544 51
6417 318
5512 0007980 85
6466 274
5596 15
51234676 16588
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
80175379 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 318
5512 deg
Eccentricity:
0007980
Arg of perigee: 85
6466 deg
Mean anomaly: 274
5596 deg
Mean motion: 15
51234676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 347
Coasting Arc #15 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2019/177/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3374143
08 A = 6785924
18 meter
Y = -2601430
90 meter E =
0022859
Z = -5301624
48 I = 51
34402
XDOT = 5010
819031 Wp = 87
40914
YDOT = -5764
808992 meter/sec RA = 313
16220 deg
ZDOT = -360
696566 TA = 179
12983
MA = 179
12584
Ha = 228
554 n
mi
Hp = 216
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11070023
24 X = -3319050
03
Y = -8534878
28 feet Y = -2638854
29 meter
Z = -17393781
12 Z = -5317881
29
XDOT = 16439
694983 XDOT = 5076
662424
YDOT = -18913
415328 feet/sec YDOT = -5708
406306 meter/sec
ZDOT = -1183
387683 ZDOT = -336
196618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11546607
66 X = 3519406
02
Y = 7714045
61 feet Y = 2351241
10 meter
Z = -17467184
52 Z = -5323997
84
XDOT = -14460
747574 XDOT = -4407
635861
YDOT = 19221
267769 feet/sec YDOT = 5858
642416 meter/sec
ZDOT = -1071
627830 ZDOT = -326
632163
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 19177
76809162
00016717 00000-0 10270-3 0 9146
2 25544 51
6424 313
7549 0008067 88
3405 271
8670 15
51205274 16735
Satellite: ISS
Catalog Number: 25544
Epoch time: 19177
76809162 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 313
7549 deg
Eccentricity:
0008067
Arg of perigee: 88
3405 deg
Mean anomaly: 271
8670 deg
Mean motion: 15
51205274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 325
Coasting Arc #16 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2019/178/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2975482
01 A = 6785833
19 meter
Y = 3046532
15 meter E =
0010754
Z = 5273995
81 I = 51
32138
XDOT = -5034
405981 Wp = 85
27470
YDOT = 5768
814851 meter/sec RA = 308
17242 deg
ZDOT = -490
319081 TA = 9
43104
MA = 9
41086
Ha = 228
410 n
mi
Hp = 216
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9762080
09 X = 2915575
48
Y = 9995184
21 feet Y = 3079470
45 meter
Z = 17303135
85 Z = 5288304
50
XDOT = -16517
079990 XDOT = -5096
158650
YDOT = 18926
557909 feet/sec YDOT = 5712
171374 meter/sec
ZDOT = -1608
658403 ZDOT = -514
923652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10507200
18 X = -3202594
61
Y = -9086456
47 feet Y = -2769551
93 meter
Z = 17367656
11 Z = 5293661
58
XDOT = 14070
550839 XDOT = 4288
703896
YDOT = -19570
697802 feet/sec YDOT = -5965
148690 meter/sec
ZDOT = -1720
880410 ZDOT = -524
524349
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 19178
79884824
00016717 00000-0 10270-3 0 9159
2 25544 51
6416 308
6395 0008138 91
6750 268
5333 15
51247010 16897
Satellite: ISS
Catalog Number: 25544
Epoch time: 19178
79884824 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 308
6395 deg
Eccentricity:
0008138
Arg of perigee: 91
6750 deg
Mean anomaly: 268
5333 deg
Mean motion: 15
51247010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 340
Coasting Arc #17 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2019/179/18:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2644129
43 A = 6786487
59 meter
Y = -3532202
30 meter E =
0021956
Z = -5175935
91 I = 51
30403
XDOT = 4969
195000 Wp = 98
09079
YDOT = -5659
360805 meter/sec RA = 303
18067 deg
ZDOT = 1325
412276 TA = 184
72965
MA = 184
75042
Ha = 228
553 n
mi
Hp = 216
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8674965
31 X = -2579292
91
Y = -11588590
23 feet Y = -3561407
53 meter
Z = -16981417
03 Z = -5188623
18
XDOT = 16303
133203 XDOT = 5025
672135
YDOT = -18567
456710 feet/sec YDOT = -5603
476193 meter/sec
ZDOT = 4348
465473 ZDOT = 1349
687197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9754134
43 X = 2973060
18
Y = 10604914
65 feet Y = 3232377
99 meter
Z = -17038533
32 Z = -5193344
96
XDOT = -13415
338441 XDOT = -4088
995157
YDOT = 19493
901130 feet/sec YDOT = 5941
741064 meter/sec
ZDOT = 4459
169980 ZDOT = 1359
155010
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 19179
76518327
00016717 00000-0 10270-3 0 9160
2 25544 51
6423 303
8432 0008092 94
9665 265
2410 15
51209277 17045
Satellite: ISS
Catalog Number: 25544
Epoch time: 19179
76518327 = yrday
fracday
Element set: 916
Inclination: 51
6423 deg
RA of node: 303
8432 deg
Eccentricity:
0008092
Arg of perigee: 94
9665 deg
Mean anomaly: 265
2410 deg
Mean motion: 15
51209277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 319
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