[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 30th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19998 2692 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
249/18:11:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 219
3
250/16:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 219
0
253/21:33:20
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 218
7
254/16:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 218
5
Coasting Arc #1 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2019/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6417221
09 A = 6798941
57 meter
Y = -1527506
04 meter E =
0001853
Z = -1650175
13 I = 51
67585
XDOT = 2522
180516 Wp = 65
97047
YDOT = -4430
140371 meter/sec RA = 1
98457 deg
ZDOT = -5711
810606 TA = 132
04888
MA = 132
03311
Ha = 227
553 n
mi
Hp = 221
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21053874
97 X = -6391647
66
Y = -5011502
76 feet Y = -1599124
93 meter
Z = -5413960
39 Z = -1681284
87
XDOT = 8274
870458 XDOT = 2599
276440
YDOT = -14534
581271 feet/sec YDOT = -4401
504493 meter/sec
ZDOT = -18739
536108 ZDOT = -5699
371794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17053280
79 X = 5197839
99
Y = 13267078
55 feet Y = 4043805
54 meter
Z = -5555359
52 Z = -1693273
58
XDOT = -12699
742374 XDOT = -3870
881475
YDOT = 8506
888271 feet/sec YDOT = 2592
899545 meter/sec
ZDOT = -18682
468678 ZDOT = -5694
416453
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 19240
52893346
00016717 00000-0 10270-3 0 9003
2 25544 51
6441 2
4132 0007438 335
9541 24
1262 15
50411315 26479
Satellite: ISS
Catalog Number: 25544
Epoch time: 19240
52893346 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 2
4132 deg
Eccentricity:
0007438
Arg of perigee: 335
9541 deg
Mean anomaly: 24
1262 deg
Mean motion: 15
50411315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 276
Coasting Arc #2 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2019/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6322249
84 A = 6798242
57 meter
Y = 1325289
80 meter E =
0015707
Z = 2085948
76 I = 51
64055
XDOT = -2778
040568 Wp = 41
46900
YDOT = 4527
436402 meter/sec RA = 357
03169 deg
ZDOT = 5531
073220 TA = 341
60321
MA = 341
65995
Ha = 227
603 n
mi
Hp = 220
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20742289
51 X = 6296828
02
Y = 4348063
66 feet Y = 1395847
57 meter
Z = 6843663
93 Z = 2116597
47
XDOT = -9114
306327 XDOT = -2855
327526
YDOT = 14853
793969 feet/sec YDOT = 4495
938408 meter/sec
ZDOT = 18146
565682 ZDOT = 5517
390985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17248702
76 X = -5257404
60
Y = -12235367
33 feet Y = -3729339
96 meter
Z = 6982979
80 Z = 2128412
24
XDOT = 13498
650345 XDOT = 4114
388625
YDOT = -8686
112733 feet/sec YDOT = -2647
527161 meter/sec
ZDOT = 18083
839464 ZDOT = 5511
954269
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 19241
56024551
00016717 00000-0 10270-3 0 9013
2 25544 51
6445 357
3016 0007394 340
1189 19
9673 15
50412854 26638
Satellite: ISS
Catalog Number: 25544
Epoch time: 19241
56024551 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 357
3016 deg
Eccentricity:
0007394
Arg of perigee: 340
1189 deg
Mean anomaly: 19
9673 deg
Mean motion: 15
50412854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2663
Checksum: 305
Coasting Arc #3 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2019/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6208087
56 A = 6797390
21 meter
Y = -1155203
37 meter E =
0004290
Z = -2523742
00 I = 51
60444
XDOT = 3012
880015 Wp = 25
42283
YDOT = -4646
927456 meter/sec RA = 352
07640 deg
ZDOT = -5283
808535 TA = 182
84059
MA = 182
84303
Ha = 227
805 n
mi
Hp = 220
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20367741
34 X = -6182449
65
Y = -3790037
29 feet Y = -1224483
37 meter
Z = -8279993
43 Z = -2553835
65
XDOT = 9884
776951 XDOT = 3090
284695
YDOT = -15245
824988 feet/sec YDOT = -4612
802813 meter/sec
ZDOT = -17335
329840 ZDOT = -5268
985113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17315139
26 X = 5277654
45
Y = 11274356
71 feet Y = 3436423
93 meter
Z = -8416792
40 Z = -2565438
32
XDOT = -14252
310363 XDOT = -4344
104199
YDOT = 8996
753593 feet/sec YDOT = 2742
210495 meter/sec
ZDOT = -17267
410781 ZDOT = -5263
106806
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 19242
52709954
00016717 00000-0 10270-3 0 9028
2 25544 51
6445 352
5100 0007417 343
2112 16
8792 15
50407285 26781
Satellite: ISS
Catalog Number: 25544
Epoch time: 19242
52709954 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 352
5100 deg
Eccentricity:
0007417
Arg of perigee: 343
2112 deg
Mean anomaly: 16
8792 deg
Mean motion: 15
50407285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2678
Checksum: 303
Coasting Arc #4 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2019/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6042478
18 A = 6796396
33 meter
Y = 998679
69 meter E =
0014515
Z = 2924811
62 I = 51
56933
XDOT = -3228
145173 Wp = 51
21340
YDOT = 4820
494015 meter/sec RA = 347
11750 deg
ZDOT = 5015
282512 TA = 342
16188
MA = 342
21278
Ha = 227
810 n
mi
Hp = 220
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19824403
49 X = 6016654
67
Y = 3276508
18 feet Y = 1066106
78 meter
Z = 9595838
65 Z = 2954100
48
XDOT = -10591
027469 XDOT = -3306
170508
YDOT = 15815
269078 feet/sec YDOT = 4783
958746 meter/sec
ZDOT = 16454
338950 ZDOT = 4999
411743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17181073
64 X = -5236791
24
Y = -10294670
34 feet Y = -3137815
52 meter
Z = 9728980
95 Z = 2965393
39
XDOT = 15005
357226 XDOT = 4573
632882
YDOT = -9537
228190 feet/sec YDOT = -2906
947152 meter/sec
ZDOT = 16381
650471 ZDOT = 4993
127064
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 19243
55840582
00016717 00000-0 10270-3 0 9036
2 25544 51
6454 347
3982 0007464 347
3279 12
7683 15
50426938 26940
Satellite: ISS
Catalog Number: 25544
Epoch time: 19243
55840582 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 347
3982 deg
Eccentricity:
0007464
Arg of perigee: 347
3279 deg
Mean anomaly: 12
7683 deg
Mean motion: 15
50426938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 340
Coasting Arc #5 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2019/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5868689
89 A = 6795408
78 meter
Y = -882699
93 meter E =
0008054
Z = -3321054
31 I = 51
53320
XDOT = 3404
396055 Wp = 25
59406
YDOT = -5004
512395 meter/sec RA = 342
15614 deg
ZDOT = -4682
979986 TA = 192
99273
MA = 193
01349
Ha = 228
093 n
mi
Hp = 220
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19254231
92 X = -5842251
42
Y = -2895997
14 feet Y = -948180
21 meter
Z = -10895847
47 Z = -3349497
65
XDOT = 11169
278397 XDOT = 3482
852048
YDOT = -16419
003920 feet/sec YDOT = -4966
003765 meter/sec
ZDOT = -15364
107565 ZDOT = -4666
251876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16946852
51 X = 5165400
64
Y = 9438334
08 feet Y = 2876804
23 meter
Z = -11025143
00 Z = -3360463
59
XDOT = -15626
187450 XDOT = -4762
861935
YDOT = 10188
890714 feet/sec YDOT = 3105
573890 meter/sec
ZDOT = -15287
513619 ZDOT = -4659
634151
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 19244
52525362
00016717 00000-0 10270-3 0 9041
2 25544 51
6450 342
6065 0007558 350
8896 9
2116 15
50407636 27097
Satellite: ISS
Catalog Number: 25544
Epoch time: 19244
52525362 = yrday
fracday
Element set: 904
Inclination: 51
6450 deg
RA of node: 342
6065 deg
Eccentricity:
0007558
Arg of perigee: 350
8896 deg
Mean anomaly: 9
2116 deg
Mean motion: 15
50407636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 312
Coasting Arc #6 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2019/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5650144
80 A = 6794254
25 meter
Y = 793979
77 meter E =
0012715
Z = 3673441
78 I = 51
49789
XDOT = -3555
521874 Wp = 59
05752
YDOT = 5234
258746 meter/sec RA = 337
19124 deg
ZDOT = 4332
691252 TA = 344
70920
MA = 344
74759
Ha = 228
048 n
mi
Hp = 220
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18537220
48 X = 5623002
89
Y = 2604920
51 feet Y = 857012
20 meter
Z = 12051974
33 Z = 3700821
96
XDOT = -11665
098013 XDOT = -3634
834339
YDOT = 17172
764914 feet/sec YDOT = 5194
055274 meter/sec
ZDOT = 14214
866313 ZDOT = 4315
226881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16520998
56 X = -5035600
36
Y = -8628752
28 feet Y = -2630043
69 meter
Z = 12176431
34 Z = 3711376
27
XDOT = 16198
343791 XDOT = 4937
255188
YDOT = -11045
909944 feet/sec YDOT = -3366
793351 meter/sec
ZDOT = 14134
912502 ZDOT = 4308
321331
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 19245
55655396
00016717 00000-0 10270-3 0 9057
2 25544 51
6447 337
4947 0007588 355
0063 5
1011 15
50437930 27257
Satellite: ISS
Catalog Number: 25544
Epoch time: 19245
55655396 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 337
4947 deg
Eccentricity:
0007588
Arg of perigee: 355
0063 deg
Mean anomaly: 5
1011 deg
Mean motion: 15
50437930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 318
Coasting Arc #7 (Orbit 2739)
---------------------------------------
Vector Time (GMT): 2019/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5439182
72 A = 6793257
58 meter
Y = -748162
43 meter E =
0011759
Z = -4013513
80 I = 51
46305
XDOT = 3651
378086 Wp = 33
02499
YDOT = -5458
152205 meter/sec RA = 332
22377 deg
ZDOT = -3926
756518 TA = 195
95296
MA = 195
99003
Ha = 228
318 n
mi
Hp = 219
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17845087
66 X = -5410916
89
Y = -2454601
14 feet Y = -808829
41 meter
Z = -13167696
18 Z = -4039866
59
XDOT = 11979
586896 XDOT = 3731
215333
YDOT = -17907
323506 feet/sec YDOT = -5416
873774 meter/sec
ZDOT = -12883
059441 ZDOT = -3908
825247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16051530
39 X = 4892506
46
Y = 7978208
69 feet Y = 2431758
01 meter
Z = -13287475
36 Z = -4050022
49
XDOT = -16555
924870 XDOT = -5046
245900
YDOT = 11966
862152 feet/sec YDOT = 3647
499584 meter/sec
ZDOT = -12800
970385 ZDOT = -3901
735773
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 19246
52339792
00016717 00000-0 10270-3 0 9065
2 25544 51
6438 332
7029 0007603 358
0567 2
0553 15
50409354 27409
Satellite: ISS
Catalog Number: 25544
Epoch time: 19246
52339792 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 332
7029 deg
Eccentricity:
0007603
Arg of perigee: 358
0567 deg
Mean anomaly: 2
0553 deg
Mean motion: 15
50409354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2740
Checksum: 308
Coasting Arc #8 (Orbit 2755)
---------------------------------------
Vector Time (GMT): 2019/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5192250
85 A = 6792084
63 meter
Y = 741424
62 meter E =
0010492
Z = 4304371
42 I = 51
43119
XDOT = -3722
495770 Wp = 63
01159
YDOT = 5716
133537 meter/sec RA = 327
25205 deg
ZDOT = 3503
816036 TA = 351
22011
MA = 351
23845
Ha = 228
261 n
mi
Hp = 219
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17034943
73 X = 5162665
87
Y = 2432495
47 feet Y = 799322
80 meter
Z = 14121953
48 Z = 4329521
55
XDOT = -12212
912630 XDOT = -3803
158165
YDOT = 18753
718953 feet/sec YDOT = 5674
055115 meter/sec
ZDOT = 11495
459436 ZDOT = 3485
537362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15414583
68 X = -4698365
11
Y = -7433405
35 feet Y = -2265701
95 meter
Z = 14236256
77 Z = 4339211
06
XDOT = 16836
141383 XDOT = 5131
655893
YDOT = -13045
374928 feet/sec YDOT = -3976
230278 meter/sec
ZDOT = 11411
774418 ZDOT = 3478
308843
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 19247
55469217
00016717 00000-0 10270-3 0 9076
2 25544 51
6444 327
5902 0007713 1
8609 358
2569 15
50447502 27567
Satellite: ISS
Catalog Number: 25544
Epoch time: 19247
55469217 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 327
5902 deg
Eccentricity:
0007713
Arg of perigee: 1
8609 deg
Mean anomaly: 358
2569 deg
Mean motion: 15
50447502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2756
Checksum: 327
Coasting Arc #9 (Orbit 2770)
---------------------------------------
Vector Time (GMT): 2019/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4970193
48 A = 6791208
05 meter
Y = -775179
25 meter E =
0015254
Z = -4577244
56 I = 51
39949
XDOT = 3729
269400 Wp = 42
10586
YDOT = -5949
281740 meter/sec RA = 322
27870 deg
ZDOT = -3036
704576 TA = 197
34215
MA = 197
39431
Ha = 228
591 n
mi
Hp = 219
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16306409
04 X = -4938922
09
Y = -2543239
00 feet Y = -830584
74 meter
Z = -15017206
55 Z = -4601311
91
XDOT = 12235
135826 XDOT = 3810
269443
YDOT = -19518
640880 feet/sec YDOT = -5907
125615 meter/sec
ZDOT = -9962
941523 ZDOT = -3018
392272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14804546
27 X = 4512425
70
Y = 7063680
23 feet Y = 2153009
74 meter
Z = -15126578
08 Z = -4610581
00
XDOT = -16846
508524 XDOT = -5134
815798
YDOT = 14116
307028 feet/sec YDOT = 4302
650382 meter/sec
ZDOT = -9879
089975 ZDOT = -3011
146624
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 19248
52153036
00016717 00000-0 10270-3 0 9084
2 25544 51
6435 322
7982 0007818 5
8092 354
3148 15
50413500 27716
Satellite: ISS
Catalog Number: 25544
Epoch time: 19248
52153036 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 322
7982 deg
Eccentricity:
0007818
Arg of perigee: 5
8092 deg
Mean anomaly: 354
3148 deg
Mean motion: 15
50413500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2771
Checksum: 304
Coasting Arc #10 (Orbit 2786)
---------------------------------------
Vector Time (GMT): 2019/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4723505
79 A = 6790194
98 meter
Y = 854618
54 meter E =
0008649
Z = 4794304
35 I = 51
37068
XDOT = -3713
958175 Wp = 60
67126
YDOT = 6203
857758 meter/sec RA = 317
30202 deg
ZDOT = 2553
902029 TA = 4
09784
MA = 4
09077
Ha = 228
513 n
mi
Hp = 219
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15497066
25 X = 4690310
12
Y = 2803866
60 feet Y = 907254
60 meter
Z = 15729344
96 Z = 4817168
67
XDOT = -12184
902149 XDOT = -3795
460885
YDOT = 20353
864034 feet/sec YDOT = 6161
870003 meter/sec
ZDOT = 8378
943666 ZDOT = 2535
662974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14069624
33 X = -4288421
49
Y = -6840126
80 feet Y = -2084870
65 meter
Z = 15833235
92 Z = 4825970
31
XDOT = 16764
760778 XDOT = 5109
899085
YDOT = -15287
036846 feet/sec YDOT = -4659
488831 meter/sec
ZDOT = 8295
410701 ZDOT = 2528
441182
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 19249
55282080
00016717 00000-0 10270-3 0 9091
2 25544 51
6434 317
6859 0007851 9
6459 350
4841 15
50447262 27873
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
55282080 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 317
6859 deg
Eccentricity:
0007851
Arg of perigee: 9
6459 deg
Mean anomaly: 350
4841 deg
Mean motion: 15
50447262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2787
Checksum: 338
Coasting Arc #11 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2019/249/18:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4797388
61 A = 6790362
58 meter
Y = 650162
39 meter E =
0009209
Z = 4752537
49 I = 51
36199
XDOT = -3478
308275 Wp = 60
65509
YDOT = 6299
901960 meter/sec RA = 316
02231 deg
ZDOT = 2649
830669 TA = 3
09254
MA = 3
08685
Ha = 228
644 n
mi
Hp = 219
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15739463
95 X = 4766676
64
Y = 2133078
70 feet Y = 703638
53 meter
Z = 15592314
59 Z = 4775766
73
XDOT = -11411
772556 XDOT = -3561
368451
YDOT = 20668
969684 feet/sec YDOT = 6260
540697 meter/sec
ZDOT = 8693
670173 ZDOT = 2632
732548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5491819
50 X = -1673906
58
Y = 14792477
02 feet Y = 4508746
99 meter
Z = 15697884
15 Z = 4784715
09
XDOT = -16592
261177 XDOT = -5057
321207
YDOT = -15300
763230 feet/sec YDOT = -4663
672633 meter/sec
ZDOT = 8615
319113 ZDOT = 2625
949266
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 19249
81064418
00016717 00000-0 10270-3 0 9105
2 25544 51
6404 316
4093 0008169 10
7773 349
3551 15
50447044 27910
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
81064418 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 316
4093 deg
Eccentricity:
0008169
Arg of perigee: 10
7773 deg
Mean anomaly: 349
3551 deg
Mean motion: 15
50447044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2791
Checksum: 309
Coasting Arc #12 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2019/250/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5433487
96 A = 6794062
99 meter
Y = 1618910
02 meter E =
0012259
Z = -3758795
45 I = 51
35282
XDOT = 1046
568379 Wp = 40
64687
YDOT = -6293
229870 meter/sec RA = 311
39329 deg
ZDOT = -4222
045331 TA = 184
38599
MA = 184
39675
Ha = 228
956 n
mi
Hp = 218
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17826404
07 X = -5432929
22
Y = 5311384
59 feet Y = 1558152
00 meter
Z = -12332006
06 Z = -3785187
81
XDOT = 3433
623291 XDOT = 1137
371540
YDOT = -20647
079626 feet/sec YDOT = -6281
018762 meter/sec
ZDOT = -13851
854760 ZDOT = -4216
740879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6262751
86 X = 1908886
77
Y = -17429608
08 feet Y = -5312544
54 meter
Z = -12452171
02 Z = -3795421
73
XDOT = 13248
317302 XDOT = 4038
087114
YDOT = 14641
836598 feet/sec YDOT = 4462
831795 meter/sec
ZDOT = -13827
144646 ZDOT = -4214
513688
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 19250
71302226
00016717 00000-0 10270-3 0 9119
2 25544 51
6408 311
9359 0008185 15
6662 344
4741 15
50421447 28050
Satellite: ISS
Catalog Number: 25544
Epoch time: 19250
71302226 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 311
9359 deg
Eccentricity:
0008185
Arg of perigee: 15
6662 deg
Mean anomaly: 344
4741 deg
Mean motion: 15
50421447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 293
Coasting Arc #13 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2019/251/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5197072
16 A = 6792876
26 meter
Y = -1551381
82 meter E =
0013841
Z = 4074850
87 I = 51
32817
XDOT = -1041
635616 Wp = 66
77984
YDOT = 6567
254602 meter/sec RA = 306
41572 deg
ZDOT = 3823
788346 TA = 343
51663
MA = 343
56158
Ha = 228
817 n
mi
Hp = 218
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17050761
68 X = 5194240
72
Y = -5089835
37 feet Y = -1493280
25 meter
Z = 13368933
31 Z = 4100089
23
XDOT = -3417
439686 XDOT = -1133
568811
YDOT = 21546
110900 feet/sec YDOT = 6555
092346 meter/sec
ZDOT = 12545
237355 ZDOT = 3818
505096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5688743
08 X = -1733928
89
Y = 16768647
62 feet Y = 5111083
80 meter
Z = 13483839
78 Z = 4109874
36
XDOT = -14300
950605 XDOT = -4358
929744
YDOT = -14932
630942 feet/sec YDOT = -4551
465911 meter/sec
ZDOT = 12520
612085 ZDOT = 3816
282564
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 19251
74430700
00016717 00000-0 10270-3 0 9123
2 25544 51
6410 306
8241 0008210 18
1672 341
9771 15
50456599 28213
Satellite: ISS
Catalog Number: 25544
Epoch time: 19251
74430700 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 306
8241 deg
Eccentricity:
0008210
Arg of perigee: 18
1672 deg
Mean anomaly: 341
9771 deg
Mean motion: 15
50456599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 290
Coasting Arc #14 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2019/252/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4998033
53 A = 6791909
03 meter
Y = 1446663
70 meter E =
0015912
Z = -4382002
82 I = 51
30505
XDOT = 990
035923 Wp = 46
60022
YDOT = -6794
839095 meter/sec RA = 301
43489 deg
ZDOT = -3369
480963 TA = 189
02297
MA = 189
05160
Ha = 229
158 n
mi
Hp = 218
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16397747
79 X = -4992553
98
Y = 4746271
99 feet Y = 1390802
67 meter
Z = -14376649
66 Z = -4406267
85
XDOT = 3248
149355 XDOT = 1082
311078
YDOT = -22292
779182 feet/sec YDOT = -6783
251976 meter/sec
ZDOT = -11054
727570 ZDOT = -3364
447469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5309502
48 X = 1618336
36
Y = -16125567
92 feet Y = -4915073
10 meter
Z = -14487115
95 Z = -4415672
94
XDOT = 15326
600764 XDOT = 4671
547913
YDOT = 14965
511630 feet/sec YDOT = 4561
487945 meter/sec
ZDOT = -11031
234105 ZDOT = -3362
320155
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 19252
71113679
00016717 00000-0 10270-3 0 9135
2 25544 51
6403 302
0310 0008354 22
4741 337
6774 15
50427547 28366
Satellite: ISS
Catalog Number: 25544
Epoch time: 19252
71113679 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 302
0310 deg
Eccentricity:
0008354
Arg of perigee: 22
4741 deg
Mean anomaly: 337
6774 deg
Mean motion: 15
50427547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 295
Coasting Arc #15 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2019/253/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4787700
64 A = 6790816
64 meter
Y = -1297003
63 meter E =
0011516
Z = 4626655
57 I = 51
28495
XDOT = -902
094652 Wp = 69
58872
YDOT = 7041
010691 meter/sec RA = 296
45327 deg
ZDOT = 2905
377984 TA = 351
35847
MA = 351
37828
Ha = 228
965 n
mi
Hp = 218
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15707679
25 X = 4779374
83
Y = -4255261
24 feet Y = -1243510
52 meter
Z = 15179316
18 Z = 4649891
97
XDOT = -2959
628125 XDOT = -994
874761
YDOT = 23100
428777 feet/sec YDOT = 7030
404201 meter/sec
ZDOT = 9532
079999 ZDOT = 2900
770332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5057407
53 X = -1541497
82
Y = 15363554
92 feet Y = 4682811
54 meter
Z = 15285087
00 Z = 4658894
52
XDOT = -16482
227394 XDOT = -5023
782910
YDOT = -14893
901011 feet/sec YDOT = -4539
661028 meter/sec
ZDOT = 9510
520470 ZDOT = 2898
806639
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 19253
74241869
00016717 00000-0 10270-3 0 9143
2 25544 51
6399 296
9196 0008254 24
8905 335
2642 15
50462784 28528
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
74241869 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 296
9196 deg
Eccentricity:
0008254
Arg of perigee: 24
8905 deg
Mean anomaly: 335
2642 deg
Mean motion: 15
50462784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 345
Coasting Arc #16 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2019/253/21:33:20
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -593649
93 A = 6797137
62 meter
Y = 6223768
82 meter E =
0017492
Z = 2659300
92 I = 51
30554
XDOT = -5391
395234 Wp = 74
67772
YDOT = 1708
155661 meter/sec RA = 295
36833 deg
ZDOT = -5168
188568 TA = 75
22317
MA = 75
02941
Ha = 229
228 n
mi
Hp = 218
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1947670
37 X = -676119
04
Y = 20419189
05 feet Y = 6216669
23 meter
Z = 8724740
54 Z = 2656216
61
XDOT = -17688
304574 XDOT = -5384
991749
YDOT = 5604
185241 feet/sec YDOT = 1647
900827 meter/sec
ZDOT = -16955
999239 ZDOT = -5194
362149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16502644
22 X = -5030005
96
Y = 12192344
22 feet Y = 3716226
52 meter
Z = 8710182
25 Z = 2654863
55
XDOT = -15045
168850 XDOT = -4585
767465
YDOT = -8087
870791 feet/sec YDOT = -2465
183017 meter/sec
ZDOT = -17075
159760 ZDOT = -5204
508695
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 19253
93578600
00016717 00000-0 10270-3 0 9151
2 25544 51
6430 295
9623 0008312 26
2611 333
8960 15
50428024 28552
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
93578600 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 295
9623 deg
Eccentricity:
0008312
Arg of perigee: 26
2611 deg
Mean anomaly: 333
8960 deg
Mean motion: 15
50428024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 307
Coasting Arc #17 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2019/254/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1580083
14 A = 6792749
62 meter
Y = -5131577
21 meter E =
0012301
Z = -4167276
07 I = 51
27737
XDOT = 4952
129384 Wp = 66
93604
YDOT = -4517
482975 meter/sec RA = 291
36976 deg
ZDOT = 3698
625984 TA = 241
26225
MA = 241
38590
Ha = 229
269 n
mi
Hp = 218
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5183999
80 X = -1502340
86
Y = -16835883
23 feet Y = -5148812
40 meter
Z = -13672165
57 Z = -4174762
27
XDOT = 16247
143649 XDOT = 4984
311479
YDOT = -14821
138368 feet/sec YDOT = -4461
924594 meter/sec
ZDOT = 12134
599685 ZDOT = 3722
759733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17227583
16 X = 5250967
35
Y = 3551191
74 feet Y = 1082403
24 meter
Z = -13705777
80 Z = -4177521
07
XDOT = 5579
847339 XDOT = 1700
737469
YDOT = 20019
069369 feet/sec YDOT = 6101
812344 meter/sec
ZDOT = 12244
713926 ZDOT = 3732
188805
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 19254
70924480
00016717 00000-0 10270-3 0 9169
2 25544 51
6403 292
1267 0008405 28
6998 331
4614 15
50426952 28673
Satellite: ISS
Catalog Number: 25544
Epoch time: 19254
70924480 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 292
1267 deg
Eccentricity:
0008405
Arg of perigee: 28
6998 deg
Mean anomaly: 331
4614 deg
Mean motion: 15
50426952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 326
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