[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 28th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
190/18:21:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
3
191/21:37:03
242 -0
6 0
9 0
9
N/A -0
7 -0
1 229
2
000/00:02:06
485 0
0 -0
1 221
6
193/01:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 221
7
Coasting Arc #1 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2020/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3144508
77 A = 6802819
77 meter
Y = -5998607
71 meter E =
0012397
Z = -585546
18 I = 51
33083
XDOT = 4489
764641 Wp = 49
65079
YDOT = 1782
182813 meter/sec RA = 301
63113 deg
ZDOT = 5944
807010 TA = 304
01548
MA = 304
13316
Ha = 229
228 n
mi
Hp = 221
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10316629
81 X = 3214197
49
Y = -19680471
48 feet Y = -5963053
83 meter
Z = -1921083
28 Z = -570103
17
XDOT = 14730
198955 XDOT = 4440
626003
YDOT = 5847
056473 feet/sec YDOT = 1832
114994 meter/sec
ZDOT = 19503
960006 ZDOT = 5966
497117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20379752
68 X = -6211748
62
Y = -8870671
54 feet Y = -2703780
69 meter
Z = -1849658
37 Z = -563775
87
XDOT = 4124
075944 XDOT = 1257
018348
YDOT = -13497
514881 feet/sec YDOT = -4114
042536 meter/sec
ZDOT = 19603
578637 ZDOT = 5975
170769
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 20178
50109083
00016717 00000-0 10270-3 0 9001
2 25544 51
6426 302
3694 0002348 94
5348 265
6070 15
49452107 33452
Satellite: ISS
Catalog Number: 25544
Epoch time: 20178
50109083 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 302
3694 deg
Eccentricity:
0002348
Arg of perigee: 94
5348 deg
Mean anomaly: 265
6070 deg
Mean motion: 15
49452107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 297
Coasting Arc #2 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2020/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2755850
97 A = 6802858
69 meter
Y = 6199801
61 meter E =
0014716
Z = 398267
53 I = 51
31446
XDOT = -4529
395332 Wp = 125
90704
YDOT = -1620
833133 meter/sec RA = 296
65956 deg
ZDOT = -5963
403413 TA = 49
78763
MA = 49
65894
Ha = 229
152 n
mi
Hp = 221
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9041505
80 X = -2826908
71
Y = 20340556
48 feet Y = 6168586
37 meter
Z = 1306651
98 Z = 384708
98
XDOT = -14860
220905 XDOT = -4481
967575
YDOT = -5317
694006 feet/sec YDOT = -1671
218164 meter/sec
ZDOT = -19564
971829 ZDOT = -5985
290210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21071724
24 X = 6422661
55
Y = 7185371
26 feet Y = 2190101
16 meter
Z = 1243897
81 Z = 379140
05
XDOT = -3449
657119 XDOT = -1051
455490
YDOT = 13608
401148 feet/sec YDOT = 4147
840670 meter/sec
ZDOT = -19665
507781 ZDOT = -5994
046772
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 20179
53302626
00016717 00000-0 10270-3 0 9014
2 25544 51
6426 297
2613 0002272 99
2071 260
9336 15
49465449 33610
Satellite: ISS
Catalog Number: 25544
Epoch time: 20179
53302626 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 297
2613 deg
Eccentricity:
0002272
Arg of perigee: 99
2071 deg
Mean anomaly: 260
9336 deg
Mean motion: 15
49465449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 308
Coasting Arc #3 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2020/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2319249
61 A = 6802902
10 meter
Y = -6384758
80 meter E =
0013123
Z = -255002
30 I = 51
30142
XDOT = 4578
583316 Wp = 51
87538
YDOT = 1433
366697 meter/sec RA = 291
68676 deg
ZDOT = 5971
933196 TA = 305
36959
MA = 305
49214
Ha = 229
214 n
mi
Hp = 221
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7609086
65 X = 2391712
16
Y = -20947371
39 feet Y = -6358418
10 meter
Z = -836621
72 Z = -243561
09
XDOT = 15021
598807 XDOT = 4533
206644
YDOT = 4702
646644 feet/sec YDOT = 1484
313282 meter/sec
ZDOT = 19592
956681 ZDOT = 5994
063979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21641906
28 X = -6596453
03
Y = -5329573
46 feet Y = -1624453
99 meter
Z = -783608
87 Z = -238843
98
XDOT = 2695
119658 XDOT = 821
472472
YDOT = -13727
380030 feet/sec YDOT = -4184
105433 meter/sec
ZDOT = 19694
627936 ZDOT = 6002
922595
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 20180
50046308
00016717 00000-0 10270-3 0 9026
2 25544 51
6435 292
4729 0002379 97
8846 262
2574 15
49461858 33762
Satellite: ISS
Catalog Number: 25544
Epoch time: 20180
50046308 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 292
4729 deg
Eccentricity:
0002379
Arg of perigee: 97
8846 deg
Mean anomaly: 262
2574 deg
Mean motion: 15
49461858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 332
Coasting Arc #4 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2020/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1905243
72 A = 6802922
41 meter
Y = 6523905
96 meter E =
0014277
Z = 64157
00 I = 51
28921
XDOT = -4617
719472 Wp = 128
92373
YDOT = -1281
002722 meter/sec RA = 286
71342 deg
ZDOT = -5977
890681 TA = 50
38315
MA = 50
25721
Ha = 229
184 n
mi
Hp = 221
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6250799
60 X = -1978366
01
Y = 21403890
96 feet Y = 6502191
31 meter
Z = 210488
84 Z = 54725
29
XDOT = -15149
998269 XDOT = -4574
014611
YDOT = -4202
764836 feet/sec YDOT = -1332
396250 meter/sec
ZDOT = -19612
502234 ZDOT = -6000
215718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22014270
45 X = 6709949
63
Y = 3547879
60 feet Y = 1081393
70 meter
Z = 166722
00 Z = 50816
87
XDOT = -2049
378766 XDOT = -624
650648
YDOT = 13816
248325 feet/sec YDOT = 4211
192489 meter/sec
ZDOT = -19715
077694 ZDOT = -6009
155681
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 20181
53239362
00016717 00000-0 10270-3 0 9035
2 25544 51
6426 287
3650 0002382 103
6327 256
5088 15
49463702 33926
Satellite: ISS
Catalog Number: 25544
Epoch time: 20181
53239362 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 287
3650 deg
Eccentricity:
0002382
Arg of perigee: 103
6327 deg
Mean anomaly: 256
5088 deg
Mean motion: 15
49463702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 305
Coasting Arc #5 (Orbit 3407)
---------------------------------------
Vector Time (GMT): 2020/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1446512
94 A = 6802913
95 meter
Y = -6641231
52 meter E =
0013654
Z = 81128
55 I = 51
28140
XDOT = 4665
360684 Wp = 54
69061
YDOT = 1097
793051 meter/sec RA = 281
73930 deg
ZDOT = 5976
335236 TA = 306
18588
MA = 306
31209
Ha = 229
181 n
mi
Hp = 221
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4745777
38 X = 1520275
59
Y = -21788817
32 feet Y = -6624643
16 meter
Z = 266169
77 Z = 88333
36
XDOT = 15306
301458 XDOT = 4623
708467
YDOT = 3601
683237 feet/sec YDOT = 1149
730696 meter/sec
ZDOT = 19607
399067 ZDOT = 5998
896739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22240225
88 X = -6778820
85
Y = -1621217
78 feet Y = -494147
18 meter
Z = 299691
84 Z = 91346
07
XDOT = 1307
133624 XDOT = 398
414328
YDOT = -13907
123920 feet/sec YDOT = -4238
891371 meter/sec
ZDOT = 19711
075624 ZDOT = 6007
935850
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 20182
56432271
00016717 00000-0 10270-3 0 9044
2 25544 51
6433 282
2574 0002348 104
1535 255
9876 15
49465874 34080
Satellite: ISS
Catalog Number: 25544
Epoch time: 20182
56432271 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 282
2574 deg
Eccentricity:
0002348
Arg of perigee: 104
1535 deg
Mean anomaly: 255
9876 deg
Mean motion: 15
49465874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3408
Checksum: 318
Coasting Arc #6 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2020/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1017491
59 A = 6802874
36 meter
Y = 6714840
66 meter E =
0013611
Z = -273684
03 I = 51
27550
XDOT = -4707
593773 Wp = 132
23579
YDOT = -948
471575 meter/sec RA = 276
76468 deg
ZDOT = -5969
349117 TA = 50
72265
MA = 50
60199
Ha = 229
137 n
mi
Hp = 221
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3338227
02 X = -1091173
92
Y = 22030317
11 feet Y = 6703050
40 meter
Z = -897913
49 Z = -278804
46
XDOT = -15444
861459 XDOT = -4667
642102
YDOT = -3111
783384 feet/sec YDOT = -1000
890867 meter/sec
ZDOT = -19584
478729 ZDOT = -5992
119910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22279980
11 X = 6790937
94
Y = -193827
54 feet Y = -59078
64 meter
Z = -921844
54 Z = -280978
22
XDOT = -666
491279 XDOT = -203
146542
YDOT = 13985
932796 feet/sec YDOT = 4262
912316 meter/sec
ZDOT = -19689
131275 ZDOT = -6001
247213
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 20183
53175372
00016717 00000-0 10270-3 0 9059
2 25544 51
6432 277
4688 0002323 109
8624 250
2776 15
49468815 34237
Satellite: ISS
Catalog Number: 25544
Epoch time: 20183
53175372 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 277
4688 deg
Eccentricity:
0002323
Arg of perigee: 109
8624 deg
Mean anomaly: 250
2776 deg
Mean motion: 15
49468815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 320
Coasting Arc #7 (Orbit 3438)
---------------------------------------
Vector Time (GMT): 2020/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 549531
39 A = 6802831
68 meter
Y = -6761611
47 meter E =
0014188
Z = 421634
27 I = 51
27339
XDOT = 4755
652474 Wp = 57
42268
YDOT = 766
688219 meter/sec RA = 271
78950 deg
ZDOT = 5957
341602 TA = 307
13798
MA = 307
26751
Ha = 229
144 n
mi
Hp = 221
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1802924
52 X = 623052
85
Y = -22183764
66 feet Y = -6755055
21 meter
Z = 1383314
54 Z = 424480
97
XDOT = 15602
534365 XDOT = 4717
788378
YDOT = 2515
381296 feet/sec YDOT = 819
656481 meter/sec
ZDOT = 19545
083997 ZDOT = 5980
350853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22154989
58 X = -6752840
82
Y = 2118713
85 feet Y = 645783
98 meter
Z = 1396781
55 Z = 425739
02
XDOT = -76
604652 XDOT = -23
349098
YDOT = -14055
016050 feet/sec YDOT = -4283
968892 meter/sec
ZDOT = 19650
850798 ZDOT = 5989
579323
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 20184
56367760
00016717 00000-0 10270-3 0 9068
2 25544 51
6440 272
3610 0002288 106
7568 253
3833 15
49469422 34398
Satellite: ISS
Catalog Number: 25544
Epoch time: 20184
56367760 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 272
3610 deg
Eccentricity:
0002288
Arg of perigee: 106
7568 deg
Mean anomaly: 253
3833 deg
Mean motion: 15
49469422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3439
Checksum: 320
Coasting Arc #8 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2020/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -117508
20 A = 6802735
56 meter
Y = 6768461
87 meter E =
0012835
Z = -615192
29 I = 51
27191
XDOT = -4802
528749 Wp = 134
45483
YDOT = -615
168329 meter/sec RA = 266
81522 deg
ZDOT = -5936
650821 TA = 52
20721
MA = 52
09105
Ha = 229
128 n
mi
Hp = 221
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -385525
58 X = -190198
19
Y = 22206239
72 feet Y = 6766741
50 meter
Z = -2018347
39 Z = -615938
27
XDOT = -15756
327918 XDOT = -4766
456135
YDOT = -2018
268796 feet/sec YDOT = -668
670728 meter/sec
ZDOT = -19477
200856 ZDOT = -5959
892013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21864304
84 X = 6664240
11
Y = -3899045
87 feet Y = -1188429
18 meter
Z = -2022140
96 Z = -616348
57
XDOT = 733
782521 XDOT = 223
656913
YDOT = 14125
839175 feet/sec YDOT = 4305
555780 meter/sec
ZDOT = -19584
052376 ZDOT = -5969
219164
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 20185
53110521
00016717 00000-0 10270-3 0 9078
2 25544 51
6427 267
5731 0002326 112
1040 248
0357 15
49472552 34549
Satellite: ISS
Catalog Number: 25544
Epoch time: 20185
53110521 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 267
5731 deg
Eccentricity:
0002326
Arg of perigee: 112
1040 deg
Mean anomaly: 248
0357 deg
Mean motion: 15
49472552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 281
Coasting Arc #9 (Orbit 3469)
---------------------------------------
Vector Time (GMT): 2020/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -348784
14 A = 6802680
49 meter
Y = -6744662
24 meter E =
0014556
Z = 763266
67 I = 51
27461
XDOT = 4851
983074 Wp = 60
95525
YDOT = 427
271215 meter/sec RA = 261
84020 deg
ZDOT = 5913
883044 TA = 307
32101
MA = 307
45357
Ha = 229
126 n
mi
Hp = 221
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1144304
91 X = -277044
87
Y = -22128156
96 feet Y = -6748161
63 meter
Z = 2504155
73 Z = 761745
27
XDOT = 15918
579640 XDOT = 4818
118647
YDOT = 1401
808448 feet/sec YDOT = 481
338972 meter/sec
ZDOT = 19402
503426 ZDOT = 5937
369670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21397399
91 X = -6521927
49
Y = 5757543
93 feet Y = 1754899
39 meter
Z = 2497503
74 Z = 761239
14
XDOT = -1505
376806 XDOT = -458
838850
YDOT = -14170
445923 feet/sec YDOT = -4319
151917 meter/sec
ZDOT = 19510
505017 ZDOT = 5946
801929
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 20186
56302736
00016717 00000-0 10270-3 0 9084
2 25544 51
6426 262
4655 0002271 112
5177 247
6214 15
49463987 34708
Satellite: ISS
Catalog Number: 25544
Epoch time: 20186
56302736 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 262
4655 deg
Eccentricity:
0002271
Arg of perigee: 112
5177 deg
Mean anomaly: 247
6214 deg
Mean motion: 15
49463987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3470
Checksum: 316
Coasting Arc #10 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2020/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 772513
84 A = 6802480
28 meter
Y = 6685549
30 meter E =
0011953
Z = -956516
83 I = 51
27944
XDOT = -4902
883310 Wp = 136
63544
YDOT = -267
177836 meter/sec RA = 256
86573 deg
ZDOT = -5879
600983 TA = 53
75488
MA = 53
64447
Ha = 229
076 n
mi
Hp = 221
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2534494
24 X = 702342
76
Y = 21934216
86 feet Y = 6693795
94 meter
Z = -3138178
57 Z = -952933
40
XDOT = -16085
575164 XDOT = -4870
971978
YDOT = -876
567702 feet/sec YDOT = -321
825761 meter/sec
ZDOT = -19290
029472 ZDOT = -5903
339448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20791550
51 X = 6337264
60
Y = -7439497
07 feet Y = -2267558
71 meter
Z = -3122019
44 Z = -951591
52
XDOT = 2202
586902 XDOT = 671
348488
YDOT = 14224
076107 feet/sec YDOT = 4335
498397 meter/sec
ZDOT = -19399
209508 ZDOT = -5912
879058
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 20187
53045157
00016717 00000-0 10270-3 0 9094
2 25544 51
6419 257
6771 0002267 116
5563 243
5819 15
49483788 34856
Satellite: ISS
Catalog Number: 25544
Epoch time: 20187
53045157 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 257
6771 deg
Eccentricity:
0002267
Arg of perigee: 116
5563 deg
Mean anomaly: 243
5819 deg
Mean motion: 15
49483788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 344
Coasting Arc #11 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2020/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1223916
08 A = 6802421
41 meter
Y = -6593045
29 meter E =
0014954
Z = 1105428
27 I = 51
28776
XDOT = 4952
463021 Wp = 64
31781
YDOT = 70
100775 meter/sec RA = 251
89095 deg
ZDOT = 5845
728255 TA = 307
71382
MA = 307
84929
Ha = 229
116 n
mi
Hp = 221
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4015472
71 X = -1155469
15
Y = -21630726
02 feet Y = -6606349
49 meter
Z = 3626733
18 Z = 1099648
11
XDOT = 16248
238258 XDOT = 4922
916421
YDOT = 229
989418 feet/sec YDOT = 125
316461 meter/sec
ZDOT = 19178
898473 ZDOT = 5869
713163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20006277
42 X = -6097913
36
Y = 9162488
92 feet Y = 2792726
62 meter
Z = 3600442
11 Z = 1097414
75
XDOT = -3014
205503 XDOT = -918
729837
YDOT = -14233
604879 feet/sec YDOT = -4338
402767 meter/sec
ZDOT = 19289
233243 ZDOT = 5879
358293
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 20188
56236958
00016717 00000-0 10270-3 0 9101
2 25544 51
6419 252
5689 0002247 113
7083 246
4303 15
49462783 35013
Satellite: ISS
Catalog Number: 25544
Epoch time: 20188
56236958 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 252
5689 deg
Eccentricity:
0002247
Arg of perigee: 113
7083 deg
Mean anomaly: 246
4303 deg
Mean motion: 15
49462783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 318
Coasting Arc #12 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2020/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1627773
96 A = 6802132
71 meter
Y = 6471436
96 meter E =
0011057
Z = -1297646
06 I = 51
29764
XDOT = -5004
958472 Wp = 137
28491
YDOT = 103
863557 meter/sec RA = 246
91760 deg
ZDOT = -5797
406995 TA = 56
87321
MA = 56
76715
Ha = 229
082 n
mi
Hp = 221
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5340465
74 X = 1561590
53
Y = 21231748
54 feet Y = 6489270
04 meter
Z = -4257368
95 Z = -1289898
83
XDOT = -16420
467427 XDOT = -4977
588064
YDOT = 340
759703 feet/sec YDOT = 48
048522 meter/sec
ZDOT = -19020
364157 ZDOT = -5821
652104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19115993
90 X = 5826554
94
Y = -10685804
21 feet Y = -3257033
12 meter
Z = -4221999
10 Z = -1286865
33
XDOT = 3768
682026 XDOT = 1148
694282
YDOT = 14252
398530 feet/sec YDOT = 4344
131072 meter/sec
ZDOT = -19131
914511 ZDOT = -5831
407543
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 20189
52979085
00016717 00000-0 10270-3 0 9114
2 25544 51
6407 247
7805 0002321 117
4412 242
6975 15
49494187 35168
Satellite: ISS
Catalog Number: 25544
Epoch time: 20189
52979085 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 247
7805 deg
Eccentricity:
0002321
Arg of perigee: 117
4412 deg
Mean anomaly: 242
6975 deg
Mean motion: 15
49494187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 326
Coasting Arc #13 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2020/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2054337
77 A = 6802078
28 meter
Y = -6314695
28 meter E =
0015170
Z = 1444773
98 I = 51
31075
XDOT = 5051
269360 Wp = 68
47691
YDOT = -317
214027 meter/sec RA = 241
94445 deg
ZDOT = 5752
561419 TA = 307
32843
MA = 307
46656
Ha = 229
120 n
mi
Hp = 221
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6739953
32 X = -1990590
02
Y = -20717504
22 feet Y = -6337312
12 meter
Z = 4740072
11 Z = 1434948
98
XDOT = 16572
406037 XDOT = 5026
499092
YDOT = -1040
728435 feet/sec YDOT = -260
866429 meter/sec
ZDOT = 18873
233002 ZDOT = 5777
037766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18048392
80 X = -5501150
12
Y = 12219724
84 feet Y = 3724572
13 meter
Z = 4695112
08 Z = 1431070
16
XDOT = -4640
312918 XDOT = -1414
367377
YDOT = -14203
791149 feet/sec YDOT = -4329
315542 meter/sec
ZDOT = 18985
865660 ZDOT = 5786
891853
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 20190
56170781
00016717 00000-0 10270-3 0 9127
2 25544 51
6401 242
6724 0002287 118
5722 241
5658 15
49458680 35325
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
56170781 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 242
6724 deg
Eccentricity:
0002287
Arg of perigee: 118
5722 deg
Mean anomaly: 241
5658 deg
Mean motion: 15
49458680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 306
Coasting Arc #14 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2020/190/18:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 964251
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 927378
62 A = 6795441
06 meter
Y = -5242082
36 meter E =
0012360
Z = 4215732
01 I = 51
29211
XDOT = 5519
295531 Wp = 107
32926
YDOT = 3896
611782 meter/sec RA = 240
64055 deg
ZDOT = 3618
700742 TA = 305
38023
MA = 305
49564
Ha = 229
120 n
mi
Hp = 221
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3042580
77 X = 965451
06
Y = -17198432
92 feet Y = -5231499
43 meter
Z = 13831141
78 Z = 4220328
53
XDOT = 18107
924969 XDOT = 5457
735061
YDOT = 12784
159389 feet/sec YDOT = 3957
987793 meter/sec
ZDOT = 11872
377761 ZDOT = 3645
361741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3562663
93 X = 1085899
96
Y = 17080976
53 feet Y = 5206281
64 meter
Z = 13852492
28 Z = 4222239
65
XDOT = -20213
136946 XDOT = -6160
964141
YDOT = -5544
814339 feet/sec YDOT = -1690
059411 meter/sec
ZDOT = 11994
903928 ZDOT = 3656
046717
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 20190
81968764
00016717 00000-0 10270-3 0 9132
2 25544 51
6395 241
3962 0002272 113
9774 246
1614 15
49449830 35361
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
81968764 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 241
3962 deg
Eccentricity:
0002272
Arg of perigee: 113
9774 deg
Mean anomaly: 246
1614 deg
Mean motion: 15
49449830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 327
Coasting Arc #15 (Orbit 3550)
---------------------------------------
Vector Time (GMT): 2020/191/18:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 964251
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -631614
96 A = 6795144
15 meter
Y = 5213230
74 meter E =
0010323
Z = -4322555
21 I = 51
30914
XDOT = -5807
297870 Wp = 78
36129
YDOT = -3576
025858 meter/sec RA = 235
66634 deg
ZDOT = -3469
340403 TA = 156
14914
MA = 156
10128
Ha = 229
187 n
mi
Hp = 221
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2072227
58 X = -668867
84
Y = 17103775
38 feet Y = 5205959
77 meter
Z = -14181611
58 Z = -4325713
17
XDOT = -19052
814534 XDOT = -5750
026341
YDOT = -11732
368300 feet/sec YDOT = -3640
646582 meter/sec
ZDOT = -11382
350404 ZDOT = -3497
410738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4718444
22 X = -1438181
80
Y = -16557533
91 feet Y = -5046736
33 meter
Z = -14196327
75 Z = -4327040
70
XDOT = 20812
677753 XDOT = 6343
704179
YDOT = 3924
620243 feet/sec YDOT = 1196
224250 meter/sec
ZDOT = -11511
395241 ZDOT = -3508
673270
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 20191
78715295
00016717 00000-0 10270-3 0 9149
2 25544 51
6401 236
6065 0002277 111
5091 248
6302 15
49429923 35510
Satellite: ISS
Catalog Number: 25544
Epoch time: 20191
78715295 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 236
6065 deg
Eccentricity:
0002277
Arg of perigee: 111
5091 deg
Mean anomaly: 248
6302 deg
Mean motion: 15
49429923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3551
Checksum: 303
Coasting Arc #16 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2020/191/21:38:06
485
Vector Time (MET): N/A
Weight (LBS) : 964155
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4018607
38 A = 6791774
53 meter
Y = 1596702
58 meter E =
0015925
Z = -5251338
65 I = 51
30139
XDOT = -3768
595028 Wp = 99
21785
YDOT = -6597
692256 meter/sec RA = 234
95556 deg
ZDOT = 877
651997 TA = 179
23798
MA = 179
23555
Ha = 229
168 n
mi
Hp = 221
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13184407
43 X = -4010656
02
Y = 5238525
52 feet Y = 1551808
69 meter
Z = -17228801
35 Z = -5270839
60
XDOT = -12364
156915 XDOT = -3698
800625
YDOT = -21645
971969 feet/sec YDOT = -6639
445227 meter/sec
ZDOT = 2879
435686 ZDOT = 859
514763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -920583
41 X = -280593
82
Y = -14047103
34 feet Y = -4281557
10 meter
Z = -17318595
75 Z = -5278707
99
XDOT = 23397
035813 XDOT = 7131
416516
YDOT = -4981
604672 feet/sec YDOT = -1518
393104 meter/sec
ZDOT = 2796
203171 ZDOT = 852
282727
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 20191
91614823
00016717 00000-0 10270-3 0 9150
2 25544 51
6424 235
9693 0001596 120
8428 239
2879 15
49272948 35534
Satellite: ISS
Catalog Number: 25544
Epoch time: 20191
91614823 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 235
9693 deg
Eccentricity:
0001596
Arg of perigee: 120
8428 deg
Mean anomaly: 239
2879 deg
Mean motion: 15
49272948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 338
Coasting Arc #17 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2020/192/21:38:06
485
Vector Time (MET): N/A
Weight (LBS) : 964155
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3927347
60 A = 6791740
83 meter
Y = -1829496
99 meter E =
0004365
Z = 5226795
22 I = 51
32170
XDOT = 4253
214511 Wp = 77
17831
YDOT = 6298
189260 meter/sec RA = 229
98486 deg
ZDOT = -989
650455 TA = 22
35226
MA = 22
33324
Ha = 228
936 n
mi
Hp = 221
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12884998
68 X = 3922125
33
Y = -6002286
73 feet Y = -1785608
32 meter
Z = 17148278
27 Z = 5245859
55
XDOT = 13954
115849 XDOT = 4187
277250
YDOT = 20663
350590 feet/sec YDOT = 6345
383161 meter/sec
ZDOT = -3246
884694 ZDOT = -969
149843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1979964
63 X = 603493
22
Y = 13968234
07 feet Y = 4257517
74 meter
Z = 17236074
42 Z = 5253555
48
XDOT = -22841
609130 XDOT = -6962
122463
YDOT = 7134
717130 feet/sec YDOT = 2174
661781 meter/sec
ZDOT = -3152
741887 ZDOT = -960
955727
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 20192
94821543
00016717 00000-0 10270-3 0 9164
2 25544 51
6422 230
8621 0001506 124
7687 235
3605 15
49301859 35693
Satellite: ISS
Catalog Number: 25544
Epoch time: 20192
94821543 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 230
8621 deg
Eccentricity:
0001506
Arg of perigee: 124
7687 deg
Mean anomaly: 235
3605 deg
Mean motion: 15
49301859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 311
Coasting Arc #18 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2020/193/01:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964155
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4735285
97 A = 6793441
14 meter
Y = 471545
56 meter E =
0013405
Z = -4860977
17 I = 51
32671
XDOT = -3121
893620 Wp = 109
97186
YDOT = -6556
054756 meter/sec RA = 229
15715 deg
ZDOT = 2406
139166 TA = 183
78174
MA = 183
79188
Ha = 229
153 n
mi
Hp = 221
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15535715
11 X = -4716595
52
Y = 1547065
50 feet Y = 418697
21 meter
Z = -15948087
82 Z = -4883933
53
XDOT = -10242
433138 XDOT = -3060
037298
YDOT = -21509
365998 feet/sec YDOT = -6590
620380 meter/sec
ZDOT = 7894
157368 ZDOT = 2391
124040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11476332
17 X = -3497986
05
Y = -10424211
03 feet Y = -3177299
52 meter
Z = -16053752
99 Z = -4893183
91
XDOT = 8324
429147 XDOT = 2537
286004
YDOT = -21211
119491 feet/sec YDOT = -6465
149221 meter/sec
ZDOT = 7825
264389 ZDOT = 2385
140586
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 20193
07722406
00016717 00000-0 10270-3 0 9178
2 25544 51
6383 230
2207 0001622 128
0230 232
1067 15
49264856 35718
Satellite: ISS
Catalog Number: 25544
Epoch time: 20193
07722406 = yrday
fracday
Element set: 917
Inclination: 51
6383 deg
RA of node: 230
2207 deg
Eccentricity:
0001622
Arg of perigee: 128
0230 deg
Mean anomaly: 232
1067 deg
Mean motion: 15
49264856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 280
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