[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 11th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17868 1559 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
227/05:42:52
433 0
3 1
8 1
8
N/A 1
8 0
0 223
7
000/00:09:44
866 0
4 -0
0 222
9
227/08:44:52
374 0
6 1
8 1
8
N/A 1
7 -0
0 224
0
000/00:09:44
748 0
1 -0
0 223
6
234/03:38:33
000 0
0 0
0 0
0
N/A 0
0 0
0 226
3
000/00:00:00
000 0
0 0
0 223
3
235/16:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
5
000/00:00:00
000 0
0 0
0 223
1
236/05:30:59
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
8
Coasting Arc #1 (Orbit 2351)
---------------------------------------
Vector Time (GMT): 2019/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4179420
51 A = 6786293
90 meter
Y = 211251
12 meter E =
0009846
Z = -5350537
94 I = 52
00732
XDOT = -629
397508 Wp = 105
40104
YDOT = 7628
385656 meter/sec RA = 95
84680 deg
ZDOT = -193
286272 TA = 162
78008
MA = 162
74665
Ha = 224
834 n
mi
Hp = 221
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13712009
56 X = 4202737
31
Y = 693081
09 feet Y = 258119
02 meter
Z = -17554258
32 Z = -5330179
43
XDOT = -2064
952453 XDOT = -713
714665
YDOT = 25027
511996 feet/sec YDOT = 7620
875855 meter/sec
ZDOT = -634
141312 ZDOT = -196
547961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9608537
53 X = -2928682
24
Y = -9970965
08 feet Y = -3039150
16 meter
Z = -17461598
29 Z = -5322295
16
XDOT = 17906
383739 XDOT = 5457
865764
YDOT = -16134
238618 feet/sec YDOT = -4917
715931 meter/sec
ZDOT = -649
628869 ZDOT = -198
006879
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 19221
51645849
00016717 00000-0 10270-3 0 9004
2 25544 51
6438 96
6890 0006120 240
6868 119
3672 15
51067169 23522
Satellite: ISS
Catalog Number: 25544
Epoch time: 19221
51645849 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 96
6890 deg
Eccentricity:
0006120
Arg of perigee: 240
6868 deg
Mean anomaly: 119
3672 deg
Mean motion: 15
51067169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2352
Checksum: 320
Coasting Arc #2 (Orbit 2367)
---------------------------------------
Vector Time (GMT): 2019/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4147932
96 A = 6786393
89 meter
Y = -721354
19 meter E =
0003270
Z = 5324911
74 I = 52
00982
XDOT = 576
785927 Wp = 242
48940
YDOT = -7617
669374 meter/sec RA = 90
90484 deg
ZDOT = -584
393940 TA = 213
05415
MA = 213
07459
Ha = 224
726 n
mi
Hp = 221
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13608703
93 X = -4165423
42
Y = -2366647
62 feet Y = -767837
45 meter
Z = 17470182
89 Z = 5304720
36
XDOT = 1892
342281 XDOT = 664
764655
YDOT = -24992
353590 feet/sec YDOT = -7610
727389 meter/sec
ZDOT = -1917
302953 ZDOT = -581
379000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8577300
78 X = 2614361
28
Y = 10974013
09 feet Y = 3344879
19 meter
Z = 17378322
18 Z = 5296912
60
XDOT = -17402
265046 XDOT = -5304
210386
YDOT = 16605
973631 feet/sec YDOT = 5061
500763 meter/sec
ZDOT = -1902
921064 ZDOT = -580
010340
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 19222
54733683
00016717 00000-0 10270-3 0 9013
2 25544 51
6437 91
5741 0006135 244
5023 115
5494 15
51065118 23681
Satellite: ISS
Catalog Number: 25544
Epoch time: 19222
54733683 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 91
5741 deg
Eccentricity:
0006135
Arg of perigee: 244
5023 deg
Mean anomaly: 115
5494 deg
Mean motion: 15
51065118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 298
Coasting Arc #3 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2019/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4171357
65 A = 6786893
41 meter
Y = 1239888
24 meter E =
0009288
Z = -5215928
30 I = 52
00968
XDOT = -532
692535 Wp = 120
73385
YDOT = 7516
603126 meter/sec RA = 85
96273 deg
ZDOT = 1357
953215 TA = 162
28717
MA = 162
25476
Ha = 224
440 n
mi
Hp = 221
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13685556
58 X = 4182518
51
Y = 4067874
80 feet Y = 1286598
06 meter
Z = -17112625
65 Z = -5195638
54
XDOT = -1747
678920 XDOT = -623
301839
YDOT = 24660
771412 feet/sec YDOT = 7510
139461 meter/sec
ZDOT = 4455
227082 ZDOT = 1355
146090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7699643
66 X = -2346851
39
Y = -12153472
54 feet Y = -3704378
43 meter
Z = -17020358
80 Z = -5187805
36
XDOT = 16702
798476 XDOT = 5091
012976
YDOT = -16815
333046 feet/sec YDOT = -5125
313512 meter/sec
ZDOT = 4441
783764 ZDOT = 1353
855691
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 19223
51378452
00016717 00000-0 10270-3 0 9021
2 25544 51
6425 86
7787 0006123 248
4036 111
6463 15
51066108 23838
Satellite: ISS
Catalog Number: 25544
Epoch time: 19223
51378452 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 86
7787 deg
Eccentricity:
0006123
Arg of perigee: 248
4036 deg
Mean anomaly: 111
6463 deg
Mean motion: 15
51066108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2383
Checksum: 303
Coasting Arc #4 (Orbit 2398)
---------------------------------------
Vector Time (GMT): 2019/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4237470
43 A = 6787696
94 meter
Y = -1730581
04 meter E =
0001734
Z = 5013375
12 I = 52
00980
XDOT = 505
833603 Wp = 330
84868
YDOT = -7349
043067 meter/sec RA = 81
02222 deg
ZDOT = -2108
123038 TA = 139
59031
MA = 139
57743
Ha = 224
294 n
mi
Hp = 221
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13902462
05 X = -4242155
36
Y = -5677759
31 feet Y = -1777993
93 meter
Z = 16448081
11 Z = 4992779
99
XDOT = 1659
559065 XDOT = 598
215014
YDOT = -24111
033686 feet/sec YDOT = -7342
869809 meter/sec
ZDOT = -6916
414166 ZDOT = -2105
442030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7029737
83 X = 2142664
09
Y = 13385402
98 feet Y = 4079870
83 meter
Z = 16354465
66 Z = 4984841
13
XDOT = -15901
824897 XDOT = -4846
876229
YDOT = 16790
859264 feet/sec YDOT = 5117
853904 meter/sec
ZDOT = -6903
546227 ZDOT = -2104
200890
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 19224
54465848
00016717 00000-0 10270-3 0 9032
2 25544 51
6432 81
6643 0006283 253
1713 106
8749 15
51083067 23996
Satellite: ISS
Catalog Number: 25544
Epoch time: 19224
54465848 = yrday
fracday
Element set: 903
Inclination: 51
6432 deg
RA of node: 81
6643 deg
Eccentricity:
0006283
Arg of perigee: 253
1713 deg
Mean anomaly: 106
8749 deg
Mean motion: 15
51083067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2399
Checksum: 322
Coasting Arc #5 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2019/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4351543
23 A = 6788901
82 meter
Y = 2197763
23 meter E =
0006455
Z = -4730538
33 I = 52
00644
XDOT = -512
890928 Wp = 140
63798
YDOT = 7099
725748 meter/sec RA = 76
08008 deg
ZDOT = 2823
921553 TA = 157
27568
MA = 157
24709
Ha = 223
981 n
mi
Hp = 221
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14276716
63 X = 4349621
61
Y = 7210509
27 feet Y = 2246414
74 meter
Z = -15520138
87 Z = -4709405
18
XDOT = -1682
713017 XDOT = -605
960725
YDOT = 23293
063479 feet/sec YDOT = 7093
469714 meter/sec
ZDOT = 9264
834491 ZDOT = 2821
204488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6574014
64 X = -2003759
66
Y = -14682294
63 feet Y = -4475163
40 meter
Z = -15424115
79 Z = -4701270
49
XDOT = 15019
808428 XDOT = 4578
037609
YDOT = -16453
913311 feet/sec YDOT = -5015
152777 meter/sec
ZDOT = 9251
813790 ZDOT = 2819
952843
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 19225
51110121
00016717 00000-0 10270-3 0 9042
2 25544 51
6423 76
8674 0006209 256
5399 103
5060 15
51072251 24142
Satellite: ISS
Catalog Number: 25544
Epoch time: 19225
51110121 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 76
8674 deg
Eccentricity:
0006209
Arg of perigee: 256
5399 deg
Mean anomaly: 103
5060 deg
Mean motion: 15
51072251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2414
Checksum: 278
Coasting Arc #6 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2019/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4495508
55 A = 6790246
45 meter
Y = -2620067
01 meter E =
0003672
Z = 4361318
03 I = 52
00152
XDOT = 564
926867 Wp = 56
14276
YDOT = -6795
344918 meter/sec RA = 71
14078 deg
ZDOT = -3495
907691 TA = 69
25317
MA = 69
21383
Ha = 223
879 n
mi
Hp = 221
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14749043
79 X = -4487060
45
Y = -8596020
38 feet Y = -2670291
85 meter
Z = 14308786
19 Z = 4339501
48
XDOT = 1853
434604 XDOT = 657
853163
YDOT = -22294
438708 feet/sec YDOT = -6788
507813 meter/sec
ZDOT = -11469
513422 ZDOT = -3492
938074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6331868
33 X = 1929953
47
Y = 15942375
18 feet Y = 4859235
96 meter
Z = 14209691
70 Z = 4331114
03
XDOT = -14161
553277 XDOT = -4316
441439
YDOT = 15846
979710 feet/sec YDOT = 4830
159416 meter/sec
ZDOT = -11455
361777 ZDOT = -3491
594270
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 19226
54196996
00016717 00000-0 10270-3 0 9051
2 25544 51
6418 71
7526 0006238 261
3492 98
6952 15
51091406 24301
Satellite: ISS
Catalog Number: 25544
Epoch time: 19226
54196996 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 71
7526 deg
Eccentricity:
0006238
Arg of perigee: 261
3492 deg
Mean anomaly: 98
6952 deg
Mean motion: 15
51091406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2430
Checksum: 326
Coasting Arc #7 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2019/227/05:47:44
866
Vector Time (MET): N/A
Weight (LBS) : 937363
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4643925
82 A = 6791995
54 meter
Y = 2646205
61 meter E =
0002794
Z = -4192552
25 I = 51
99428
XDOT = -409
315434 Wp = 183
54784
YDOT = 6665
663924 meter/sec RA = 67
47946 deg
ZDOT = 3750
927651 TA = 124
89087
MA = 124
86461
Ha = 223
696 n
mi
Hp = 222
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15235977
11 X = 4634354
66
Y = 8681776
94 feet Y = 2698083
81 meter
Z = -13755092
70 Z = -4170017
54
XDOT = -1342
898404 XDOT = -502
041878
YDOT = 21868
976129 feet/sec YDOT = 6660
568140 meter/sec
ZDOT = 12306
193081 ZDOT = 3748
714303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16566432
79 X = 5049448
72
Y = -5988907
63 feet Y = -1825419
05 meter
Z = -13652732
85 Z = -4161352
97
XDOT = 15240
450591 XDOT = 4645
289340
YDOT = 14106
823837 feet/sec YDOT = 4299
759905 meter/sec
ZDOT = 12295
491361 ZDOT = 3747
665767
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 19227
25069482
00016717 00000-0 10270-3 0 9060
2 25544 51
6410 68
2365 0007427 268
2030 91
8270 15
50703300 24412
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
25069482 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 68
2365 deg
Eccentricity:
0007427
Arg of perigee: 268
2030 deg
Mean anomaly: 91
8270 deg
Mean motion: 15
50703300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 286
Coasting Arc #8 (Orbit 2442)
---------------------------------------
Vector Time (GMT): 2019/227/08:49:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4606849
25 A = 6790396
38 meter
Y = 1091235
37 meter E =
0004116
Z = -4870980
96 I = 51
98630
XDOT = 943
808231 Wp = 150
16830
YDOT = 7178
405818 meter/sec RA = 66
86244 deg
ZDOT = 2498
226235 TA = 144
30207
MA = 144
27454
Ha = 224
048 n
mi
Hp = 223
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15114334
81 X = 4617964
32
Y = 3580168
55 feet Y = 1142814
62 meter
Z = -15980908
67 Z = -4848576
13
XDOT = 3096
483697 XDOT = 851
332376
YDOT = 23551
200190 feet/sec YDOT = 7188
443043 meter/sec
ZDOT = 8196
280300 ZDOT = 2502
586300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2232469
20 X = 680456
61
Y = -15476555
29 feet Y = -4717254
05 meter
Z = -15878995
03 Z = -4839917
68
XDOT = 22066
355884 XDOT = 6725
825273
YDOT = -5254
744589 feet/sec YDOT = -1601
646151 meter/sec
ZDOT = 8215
460373 ZDOT = 2504
072322
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 19227
37958233
00016717 00000-0 10270-3 0 9075
2 25544 51
6432 67
5985 0009000 269
8656 90
1463 15
50369099 24437
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
37958233 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 67
5985 deg
Eccentricity:
0009000
Arg of perigee: 269
8656 deg
Mean anomaly: 90
1463 deg
Mean motion: 15
50369099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2443
Checksum: 336
Coasting Arc #9 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2019/228/08:49:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4786739
82 A = 6791126
18 meter
Y = -1230007
77 meter E =
0004419
Z = 4660959
02 I = 51
97555
XDOT = -1095
301736 Wp = 340
03837
YDOT = -6976
889637 meter/sec RA = 61
92712 deg
ZDOT = -2962
820065 TA = 139
39069
MA = 139
35772
Ha = 224
852 n
mi
Hp = 224
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15704526
97 X = -4795269
61
Y = -4035458
57 feet Y = -1283584
14 meter
Z = 15291860
29 Z = 4637686
64
XDOT = -3593
509633 XDOT = -1002
811329
YDOT = -22890
057865 feet/sec YDOT = -6988
620937 meter/sec
ZDOT = -9720
538272 ZDOT = -2967
915849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2357455
83 X = -718552
54
Y = 16142660
87 feet Y = 4920283
03 meter
Z = 15186012
85 Z = 4628696
72
XDOT = -21218
387969 XDOT = -6467
364653
YDOT = 6076
956649 feet/sec YDOT = 1852
256387 meter/sec
ZDOT = -9743
079256 ZDOT = -2969
690557
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 19228
41091599
00016717 00000-0 10270-3 0 9085
2 25544 51
6438 62
4866 0009110 274
3605 85
6505 15
50409001 24593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19228
41091599 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 62
4866 deg
Eccentricity:
0009110
Arg of perigee: 274
3605 deg
Mean anomaly: 85
6505 deg
Mean motion: 15
50409001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2459
Checksum: 312
Coasting Arc #10 (Orbit 2473)
---------------------------------------
Vector Time (GMT): 2019/229/08:49:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4986475
74 A = 6792155
35 meter
Y = 1336010
31 meter E =
0001968
Z = -4414490
69 I = 51
96184
XDOT = 1208
792085 Wp = 200
95299
YDOT = 6753
572997 meter/sec RA = 56
99027 deg
ZDOT = 3407
073645 TA = 103
44056
MA = 103
41862
Ha = 225
305 n
mi
Hp = 224
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16359828
56 X = 4992608
21
Y = 4383235
93 feet Y = 1391806
79 meter
Z = -14483237
17 Z = -4390253
87
XDOT = 3965
853296 XDOT = 1116
632502
YDOT = 22157
391724 feet/sec YDOT = 6766
575331 meter/sec
ZDOT = 11178
063140 ZDOT = 3412
721421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2345534
82 X = 714919
01
Y = -16868190
14 feet Y = -5141424
36 meter
Z = -14373014
09 Z = -4380894
70
XDOT = 20289
320182 XDOT = 6184
184792
YDOT = -6731
051693 feet/sec YDOT = -2051
624556 meter/sec
ZDOT = 11203
130379 ZDOT = 3414
714139
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 19229
37779039
00016717 00000-0 10270-3 0 9094
2 25544 51
6437 57
6933 0009088 278
0200 81
9919 15
50377272 24748
Satellite: ISS
Catalog Number: 25544
Epoch time: 19229
37779039 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 57
6933 deg
Eccentricity:
0009088
Arg of perigee: 278
0200 deg
Mean anomaly: 81
9919 deg
Mean motion: 15
50377272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2474
Checksum: 346
Coasting Arc #11 (Orbit 2489)
---------------------------------------
Vector Time (GMT): 2019/230/08:49:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5203979
17 A = 6793072
16 meter
Y = -1411237
49 meter E =
0004565
Z = 4133814
68 I = 51
94563
XDOT = -1278
212252 Wp = 17
67089
YDOT = -6510
245419 meter/sec RA = 52
05398 deg
ZDOT = -3826
302078 TA = 111
73364
MA = 111
68504
Ha = 225
513 n
mi
Hp = 224
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17073422
48 X = -5207890
99
Y = -4630044
26 feet Y = -1469453
79 meter
Z = 13562384
12 Z = 4108526
66
XDOT = -4193
609750 XDOT = -1186
732065
YDOT = -21359
072898 feet/sec YDOT = -6524
027911 meter/sec
ZDOT = -12553
484507 ZDOT = -3832
288663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2201299
29 X = -670956
02
Y = 17640842
33 feet Y = 5376928
74 meter
Z = 13447389
76 Z = 4098764
40
XDOT = -19296
113783 XDOT = -5881
455481
YDOT = 7195
271465 feet/sec YDOT = 2193
118743 meter/sec
ZDOT = -12580
108778 ZDOT = -3834
417156
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 19230
40911982
00016717 00000-0 10270-3 0 9107
2 25544 51
6432 52
5813 0009100 282
6804 77
3329 15
50410805 24902
Satellite: ISS
Catalog Number: 25544
Epoch time: 19230
40911982 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 52
5813 deg
Eccentricity:
0009100
Arg of perigee: 282
6804 deg
Mean anomaly: 77
3329 deg
Mean motion: 15
50410805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2490
Checksum: 283
Coasting Arc #12 (Orbit 2504)
---------------------------------------
Vector Time (GMT): 2019/231/08:49:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5426096
66 A = 6794199
70 meter
Y = 1442547
83 meter E =
0003182
Z = -3822440
09 I = 51
92722
XDOT = 1307
257778 Wp = 289
40005
YDOT = 6261
762959 meter/sec RA = 47
11650 deg
ZDOT = 4216
995139 TA = 24
96740
MA = 24
95201
Ha = 225
827 n
mi
Hp = 223
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17802154
39 X = 5428129
46
Y = 4732768
48 feet Y = 1503237
49 meter
Z = -12540813
95 Z = -3796077
59
XDOT = 4288
903470 XDOT = 1216
656214
YDOT = 20543
841729 feet/sec YDOT = 6275
875210 meter/sec
ZDOT = 13835
285889 ZDOT = 4223
124940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1886561
37 X = 575023
91
Y = -18405133
63 feet Y = -5609884
73 meter
Z = -12420940
19 Z = -3785902
57
XDOT = 18297
630223 XDOT = 5577
117692
YDOT = -7483
882376 feet/sec YDOT = -2281
087348 meter/sec
ZDOT = 13862
576660 ZDOT = 4225
313366
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 19231
37599145
00016717 00000-0 10270-3 0 9118
2 25544 51
6427 47
7884 0009157 285
4248 74
5891 15
50378688 25057
Satellite: ISS
Catalog Number: 25544
Epoch time: 19231
37599145 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 47
7884 deg
Eccentricity:
0009157
Arg of perigee: 285
4248 deg
Mean anomaly: 74
5891 deg
Mean motion: 15
50378688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2505
Checksum: 349
Coasting Arc #13 (Orbit 2520)
---------------------------------------
Vector Time (GMT): 2019/232/08:49:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5655629
46 A = 6795149
93 meter
Y = -1444493
20 meter E =
0004872
Z = 3478908
65 I = 51
90833
XDOT = -1285
567227 Wp = 47
54807
YDOT = -6005
324600 meter/sec RA = 42
17869 deg
ZDOT = -4576
148341 TA = 91
87245
MA = 91
81666
Ha = 225
937 n
mi
Hp = 223
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18555214
77 X = -5655954
85
Y = -4739150
91 feet Y = -1507740
12 meter
Z = 11413742
30 Z = 3451435
22
XDOT = -4217
740245 XDOT = -1196
090210
YDOT = -19702
508529 feet/sec YDOT = -6019
200590 meter/sec
ZDOT = -15013
610044 ZDOT = -4582
175548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1447216
13 X = -441111
48
Y = 19170214
55 feet Y = 5843081
40 meter
Z = 11288821
87 Z = 3440832
91
XDOT = -17297
634433 XDOT = -5272
318975
YDOT = 7565
293153 feet/sec YDOT = 2305
901353 meter/sec
ZDOT = -15040
448779 ZDOT = -4584
328788
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 19232
40731677
00016717 00000-0 10270-3 0 9122
2 25544 51
6439 42
6763 0009290 290
1432 69
8719 15
50415798 25214
Satellite: ISS
Catalog Number: 25544
Epoch time: 19232
40731677 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 42
6763 deg
Eccentricity:
0009290
Arg of perigee: 290
1432 deg
Mean anomaly: 69
8719 deg
Mean motion: 15
50415798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2521
Checksum: 320
Coasting Arc #14 (Orbit 2535)
---------------------------------------
Vector Time (GMT): 2019/233/08:49:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5873410
71 A = 6796255
48 meter
Y = 1399453
00 meter E =
0006487
Z = -3110301
27 I = 51
88504
XDOT = 1223
880667 Wp = 319
56596
YDOT = 5761
373985 meter/sec RA = 37
23886 deg
ZDOT = 4902
508915 TA = 4
83887
MA = 4
83260
Ha = 226
264 n
mi
Hp = 223
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19269720
16 X = 5872433
14
Y = 4591381
23 feet Y = 1465128
06 meter
Z = -10204400
49 Z = -3081773
00
XDOT = 4015
356518 XDOT = 1135
550816
YDOT = 18902
145621 feet/sec YDOT = 5774
566540 meter/sec
ZDOT = 16084
346834 ZDOT = 4908
239334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 838217
13 X = 255488
58
Y = -19857764
25 feet Y = -6052646
54 meter
Z = -10074684
97 Z = -3070763
98
XDOT = 16370
421898 XDOT = 4989
704595
YDOT = -7483
738644 feet/sec YDOT = -2281
043539 meter/sec
ZDOT = 16109
848563 ZDOT = 4910
281842
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 19233
37418325
00016717 00000-0 10270-3 0 9132
2 25544 51
6427 37
8826 0009236 293
2410 66
7768 15
50383172 25363
Satellite: ISS
Catalog Number: 25544
Epoch time: 19233
37418325 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 37
8826 deg
Eccentricity:
0009236
Arg of perigee: 293
2410 deg
Mean anomaly: 66
7768 deg
Mean motion: 15
50383172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2536
Checksum: 319
Coasting Arc #15 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2019/234/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4355427
99 A = 6798448
77 meter
Y = 4793830
10 meter E =
0010258
Z = 2043051
86 I = 51
87088
XDOT = -4855
133592 Wp = 28
33087
YDOT = 2035
796269 meter/sec RA = 33
40826 deg
ZDOT = 5570
827239 TA = 354
15316
MA = 354
16512
Ha = 226
277 n
mi
Hp = 223
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14289461
91 X = 4291574
32
Y = 15727789
04 feet Y = 4842178
57 meter
Z = 6702926
04 Z = 2064053
65
XDOT = -15928
915985 XDOT = -4904
597506
YDOT = 6679
121619 feet/sec YDOT = 1981
226282 meter/sec
ZDOT = 18276
992254 ZDOT = 5547
122723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19396456
04 X = 5912039
80
Y = 8604974
80 feet Y = 2622796
32 meter
Z = 6798028
33 Z = 2072039
04
XDOT = -11338
892825 XDOT = -3456
094533
YDOT = 11198
546841 feet/sec YDOT = 3413
317077 meter/sec
ZDOT = 18168
889815 ZDOT = 5537
877616
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 19234
21213467
00016717 00000-0 10270-3 0 9147
2 25544 51
6422 33
7298 0009030 297
0425 62
9804 15
50375872 25497
Satellite: ISS
Catalog Number: 25544
Epoch time: 19234
21213467 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 33
7298 deg
Eccentricity:
0009030
Arg of perigee: 297
0425 deg
Mean anomaly: 62
9804 deg
Mean motion: 15
50375872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 308
Coasting Arc #16 (Orbit 2563)
---------------------------------------
Vector Time (GMT): 2019/235/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4375392
88 A = 6797591
21 meter
Y = -4578679
76 meter E =
0003978
Z = -2468092
96 I = 51
84070
XDOT = 5111
388152 Wp = 285
92657
YDOT = -2001
554857 meter/sec RA = 28
46869 deg
ZDOT = -5339
979794 TA = 281
57684
MA = 281
62150
Ha = 226
475 n
mi
Hp = 223
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14354963
53 X = -4311878
98
Y = -15021915
23 feet Y = -4627253
36 meter
Z = -8097417
86 Z = -2489192
66
XDOT = 16769
646169 XDOT = 5159
328819
YDOT = -6566
781028 feet/sec YDOT = -1944
127675 meter/sec
ZDOT = -17519
618747 ZDOT = -5315
034206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19295371
43 X = -5881229
21
Y = -7606240
07 feet Y = -2318381
97 meter
Z = -8192975
32 Z = -2497218
88
XDOT = 11998
263279 XDOT = 3657
070648
YDOT = -11659
727276 feet/sec YDOT = -3553
884874 meter/sec
ZDOT = -17405
874995 ZDOT = -5305
310698
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 19235
17899781
00016717 00000-0 10270-3 0 9153
2 25544 51
6432 28
9380 0009100 300
4712 59
5540 15
50388521 25643
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
17899781 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 28
9380 deg
Eccentricity:
0009100
Arg of perigee: 300
4712 deg
Mean anomaly: 59
5540 deg
Mean motion: 15
50388521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2564
Checksum: 310
Coasting Arc #17 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2019/235/16:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4348602
49 A = 6790599
77 meter
Y = -2079856
74 meter E =
0002836
Z = -4784858
38 I = 51
80211
XDOT = 5267
764597 Wp = 72
17516
YDOT = 4878
764824 meter/sec RA = 25
79707 deg
ZDOT = 2668
952377 TA = 224
13210
MA = 224
15473
Ha = 226
464 n
mi
Hp = 223
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14267068
54 X = 4394778
97
Y = -6823676
98 feet Y = -2030969
39 meter
Z = -15698354
28 Z = -4763622
42
XDOT = 17282
692248 XDOT = 5199
853080
YDOT = 16006
446274 feet/sec YDOT = 4937
292939 meter/sec
ZDOT = 8756
405436 ZDOT = 2694
376223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7424498
27 X = -2262987
07
Y = 14071977
31 feet Y = 4289138
68 meter
Z = -15601487
72 Z = -4755333
46
XDOT = -22352
948177 XDOT = -6813
178604
YDOT = -1965
594215 feet/sec YDOT = -599
113117 meter/sec
ZDOT = 8871
605664 ZDOT = 2704
065406
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 19235
69465568
00016717 00000-0 10270-3 0 9163
2 25544 51
6437 26
3799 0008933 299
6616 60
3645 15
50415220 25721
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
69465568 = yrday
fracday
Element set: 916
Inclination: 51
6437 deg
RA of node: 26
3799 deg
Eccentricity:
0008933
Arg of perigee: 299
6616 deg
Mean anomaly: 60
3645 deg
Mean motion: 15
50415220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 338
Coasting Arc #18 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2019/236/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3569570
11 A = 6789416
17 meter
Y = 2803841
00 meter E =
0008925
Z = 5054050
07 I = 51
78297
XDOT = -6075
632556 Wp = 340
76687
YDOT = -4243
573712 meter/sec RA = 23
10184 deg
ZDOT = -1929
634922 TA = 127
97961
MA = 127
89896
Ha = 226
686 n
mi
Hp = 222
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11711188
04 X = -3625207
86
Y = 9198953
42 feet Y = 2763612
39 meter
Z = 16581529
09 Z = 5036575
40
XDOT = -19933
177678 XDOT = -6018
355078
YDOT = -13922
485932 feet/sec YDOT = -4311
195421 meter/sec
ZDOT = -6330
823234 ZDOT = -1959
008914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 511469
39 X = 155895
87
Y = 14971702
68 feet Y = 4563374
98 meter
Z = 16501705
79 Z = 5029719
93
XDOT = -21853
847465 XDOT = -6661
052707
YDOT = 7897
550405 feet/sec YDOT = 2407
173364 meter/sec
ZDOT = -6464
061417 ZDOT = -1970
245920
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 19236
27477070
00016717 00000-0 10270-3 0 9170
2 25544 51
6448 23
5072 0009320 304
1489 55
8778 15
50435969 25815
Satellite: ISS
Catalog Number: 25544
Epoch time: 19236
27477070 = yrday
fracday
Element set: 917
Inclination: 51
6448 deg
RA of node: 23
5072 deg
Eccentricity:
0009320
Arg of perigee: 304
1489 deg
Mean anomaly: 55
8778 deg
Mean motion: 15
50435969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 329
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