[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 19th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
235/02:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
0
238/15:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
0
242/21:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
1
Coasting Arc #1 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2018/229/13:50:05
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4147277
22 A = 6785299
75 meter
Y = -4141928
15 meter E =
0017620
Z = 3405260
76 I = 52
00428
XDOT = 1937
932430 Wp = 83
60553
YDOT = -5784
085023 meter/sec RA = 71
95285 deg
ZDOT = -4652
661232 TA = 56
79276
MA = 56
62394
Ha = 223
429 n
mi
Hp = 213
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13606552
56 X = -4117193
64
Y = -13589003
10 feet Y = -4188137
60 meter
Z = 11172115
36 Z = 3385188
01
XDOT = 6358
046031 XDOT = 2025
067649
YDOT = -18976
656900 feet/sec YDOT = -5761
926599 meter/sec
ZDOT = -15264
636588 ZDOT = -4643
035762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11799510
64 X = 3596490
84
Y = 15250068
41 feet Y = 4648220
85 meter
Z = 11082526
86 Z = 3377954
19
XDOT = -7757
619181 XDOT = -2364
522326
YDOT = 17117
554401 feet/sec YDOT = 5217
430581 meter/sec
ZDOT = -15220
651976 ZDOT = -4639
254722
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 18229
61570960
00016717 00000-0 10270-3 0 9003
2 25544 51
6373 72
5716 0005431 68
0811 292
0919 15
53850627 8060
Satellite: ISS
Catalog Number: 25544
Epoch time: 18229
61570960 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 72
5716 deg
Eccentricity:
0005431
Arg of perigee: 68
0811 deg
Mean anomaly: 292
0919 deg
Mean motion: 15
53850627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 307
Coasting Arc #2 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2018/230/13:50:05
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3916488
36 A = 6788439
95 meter
Y = 5154837
97 meter E =
0011804
Z = -2036804
69 I = 52
00316
XDOT = -2880
771491 Wp = 55
41620
YDOT = 4384
873945 meter/sec RA = 67
00141 deg
ZDOT = 5587
580180 TA = 282
19835
MA = 282
33054
Ha = 223
508 n
mi
Hp = 213
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12849371
25 X = 3868448
11
Y = 16912198
07 feet Y = 5198366
23 meter
Z = -6682430
08 Z = -2017896
59
XDOT = -9451
350036 XDOT = -2956
731583
YDOT = 14386
069374 feet/sec YDOT = 4352
234473 meter/sec
ZDOT = 18331
955972 ZDOT = 5573
401978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10903170
79 X = -3323286
46
Y = -18258369
66 feet Y = -5565151
07 meter
Z = -6598216
52 Z = -2011136
39
XDOT = 9803
539684 XDOT = 2988
118896
YDOT = -12420
498845 feet/sec YDOT = -3785
768048 meter/sec
ZDOT = 18267
702529 ZDOT = 5567
995731
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 18230
58041819
00016717 00000-0 10270-3 0 9018
2 25544 51
6370 67
7646 0005624 74
0605 286
1167 15
53842621 8218
Satellite: ISS
Catalog Number: 25544
Epoch time: 18230
58041819 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 67
7646 deg
Eccentricity:
0005624
Arg of perigee: 74
0605 deg
Mean anomaly: 286
1167 deg
Mean motion: 15
53842621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 821
Checksum: 300
Coasting Arc #3 (Orbit 836)
---------------------------------------
Vector Time (GMT): 2018/231/13:50:05
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3462040
56 A = 6789960
25 meter
Y = -5819273
21 meter E =
0016572
Z = 424098
75 I = 51
99503
XDOT = 3867
052993 Wp = 114
35981
YDOT = -2752
469328 meter/sec RA = 62
05578 deg
ZDOT = -6022
342701 TA = 61
09004
MA = 60
92391
Ha = 223
375 n
mi
Hp = 213
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11358400
80 X = -3398770
57
Y = -19092103
71 feet Y = -5857634
38 meter
Z = 1391400
11 Z = 407435
15
XDOT = 12687
181735 XDOT = 3926
797577
YDOT = -9030
411182 feet/sec YDOT = -2708
891184 meter/sec
ZDOT = -19758
342194 ZDOT = -6003
412962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9487875
05 X = 2891904
31
Y = 20092348
29 feet Y = 6124147
76 meter
Z = 1317366
35 Z = 401533
26
XDOT = -12158
581721 XDOT = -3705
935709
YDOT = 7071
711938 feet/sec YDOT = 2155
457799 meter/sec
ZDOT = -19672
965635 ZDOT = -5996
319926
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 18231
60943648
00016717 00000-0 10270-3 0 9024
2 25544 51
6372 62
6368 0005537 75
0301 285
1464 15
53888175 8372
Satellite: ISS
Catalog Number: 25544
Epoch time: 18231
60943648 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 62
6368 deg
Eccentricity:
0005537
Arg of perigee: 75
0301 deg
Mean anomaly: 285
1464 deg
Mean motion: 15
53888175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 837
Checksum: 320
Coasting Arc #4 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2018/232/13:50:05
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2824233
57 A = 6789497
97 meter
Y = 6053251
98 meter E =
0019005
Z = 1170884
73 I = 51
97808
XDOT = -4789
059936 Wp = 64
60299
YDOT = 1081
437954 meter/sec RA = 57
11015 deg
ZDOT = 5894
217260 TA = 308
05739
MA = 308
22873
Ha = 223
471 n
mi
Hp = 213
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9265858
18 X = 2750647
05
Y = 19859750
60 feet Y = 6084423
06 meter
Z = 3841485
34 Z = 1184425
07
XDOT = -15712
138896 XDOT = -4829
427636
YDOT = 3548
024785 feet/sec YDOT = 1027
657601 meter/sec
ZDOT = 19337
983135 ZDOT = 5870
855882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7651062
56 X = -2332043
87
Y = -20524686
35 feet Y = -6255924
40 meter
Z = 3901451
43 Z = 1189162
40
XDOT = 14573
473877 XDOT = 4441
994838
YDOT = -1735
920510 feet/sec YDOT = -529
108572 meter/sec
ZDOT = 19232
932428 ZDOT = 5862
197804
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 18232
63845482
00016717 00000-0 10270-3 0 9036
2 25544 51
6384 57
5090 0005634 81
9078 278
2713 15
53866302 8531
Satellite: ISS
Catalog Number: 25544
Epoch time: 18232
63845482 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 57
5090 deg
Eccentricity:
0005634
Arg of perigee: 81
9078 deg
Mean anomaly: 278
2713 deg
Mean motion: 15
53866302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 853
Checksum: 321
Coasting Arc #5 (Orbit 867)
---------------------------------------
Vector Time (GMT): 2018/233/13:50:05
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1911377
30 A = 6786940
76 meter
Y = -5922514
29 meter E =
0009968
Z = -2713435
26 I = 51
95030
XDOT = 5596
295203 Wp = 101
57565
YDOT = 568
513521 meter/sec RA = 52
15990 deg
ZDOT = -5201
052638 TA = 108
92427
MA = 108
81620
Ha = 223
495 n
mi
Hp = 212
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6270922
89 X = -1831827
79
Y = -19430821
15 feet Y = -5943443
81 meter
Z = -8902346
64 Z = -2722526
80
XDOT = 18360
548567 XDOT = 5614
785637
YDOT = 1865
201841 feet/sec YDOT = 631
198609 meter/sec
ZDOT = -17063
820990 ZDOT = -5173
823222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5006533
45 X = 1525991
39
Y = 19776302
81 feet Y = 6027817
10 meter
Z = -8942344
80 Z = -2725626
69
XDOT = -16882
026870 XDOT = -5145
641790
YDOT = -3360
052068 feet/sec YDOT = -1024
143870 meter/sec
ZDOT = -16941
630483 ZDOT = -5163
808971
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 18233
60315712
00016717 00000-0 10270-3 0 9043
2 25544 51
6379 52
7020 0005728 84
1883 275
9922 15
53865951 8689
Satellite: ISS
Catalog Number: 25544
Epoch time: 18233
60315712 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 52
7020 deg
Eccentricity:
0005728
Arg of perigee: 84
1883 deg
Mean anomaly: 275
9922 deg
Mean motion: 15
53865951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 868
Checksum: 326
Coasting Arc #6 (Orbit 883)
---------------------------------------
Vector Time (GMT): 2018/234/13:50:05
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 820039
97 A = 6783412
53 meter
Y = 5442975
01 meter E =
0016499
Z = 3951636
63 I = 51
91780
XDOT = -6196
681680 Wp = 96
24965
YDOT = -2019
453458 meter/sec RA = 47
19997 deg
ZDOT = 4051
292540 TA = 311
55860
MA = 311
69996
Ha = 223
432 n
mi
Hp = 213
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2690419
86 X = 739919
51
Y = 17857529
55 feet Y = 5451697
26 meter
Z = 12964687
11 Z = 3955425
47
XDOT = -20330
320473 XDOT = -6193
317778
YDOT = -6625
503471 feet/sec YDOT = -2088
730254 meter/sec
ZDOT = 13291
642193 ZDOT = 4021
199845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1811677
13 X = -552199
19
Y = -17956224
47 feet Y = -5473057
22 meter
Z = 12980934
53 Z = 3956588
84
XDOT = 18795
732271 XDOT = 5728
939196
YDOT = 7653
391450 feet/sec YDOT = 2332
753714 meter/sec
ZDOT = 13156
801065 ZDOT = 4010
192965
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 18234
63217091
00016717 00000-0 10270-3 0 9059
2 25544 51
6383 47
5744 0005563 89
4175 270
7615 15
53877890 8843
Satellite: ISS
Catalog Number: 25544
Epoch time: 18234
63217091 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 47
5744 deg
Eccentricity:
0005563
Arg of perigee: 89
4175 deg
Mean anomaly: 270
7615 deg
Mean motion: 15
53877890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 884
Checksum: 336
Coasting Arc #7 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2018/235/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -857225
64 A = 6779748
06 meter
Y = 4575741
27 meter E =
0011485
Z = 4920299
60 I = 51
89437
XDOT = -6320
718428 Wp = 105
22424
YDOT = -3684
522475 meter/sec RA = 44
62558 deg
ZDOT = 2317
857216 TA = 322
16508
MA = 322
24575
Ha = 223
417 n
mi
Hp = 213
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2812420
07 X = -932228
95
Y = 15012274
52 feet Y = 4565735
81 meter
Z = 16142715
22 Z = 4915953
40
XDOT = -20737
265183 XDOT = -6290
306051
YDOT = -12088
328331 feet/sec YDOT = -3755
035078 meter/sec
ZDOT = 7604
518425 ZDOT = 2287
227742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1744775
02 X = -531807
43
Y = 15194879
48 feet Y = 4631399
27 meter
Z = 16122553
93 Z = 4914154
44
XDOT = -20555
283980 XDOT = -6265
250557
YDOT = -10309
618905 feet/sec YDOT = -3142
371842 meter/sec
ZDOT = 7467
504467 ZDOT = 2276
095361
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 18235
14667665
00016717 00000-0 10270-3 0 9063
2 25544 51
6387 45
0150 0005472 86
1333 274
0445 15
53893201 8921
Satellite: ISS
Catalog Number: 25544
Epoch time: 18235
14667665 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 45
0150 deg
Eccentricity:
0005472
Arg of perigee: 86
1333 deg
Mean anomaly: 274
0445 deg
Mean motion: 15
53893201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 308
Coasting Arc #8 (Orbit 906)
---------------------------------------
Vector Time (GMT): 2018/236/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2214351
72 A = 6778244
51 meter
Y = -3591782
02 meter E =
0020344
Z = -5322350
72 I = 51
86483
XDOT = 6131
339043 Wp = 86
44662
YDOT = 4550
084702 meter/sec RA = 39
64527 deg
ZDOT = -520
176610 TA = 178
59878
MA = 178
59307
Ha = 223
480 n
mi
Hp = 213
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7264933
46 X = 2280204
14
Y = -11784061
75 feet Y = -3566651
48 meter
Z = -17461780
57 Z = -5311434
38
XDOT = 20115
941741 XDOT = 6082
529744
YDOT = 14928
099415 feet/sec YDOT = 4618
376663 meter/sec
ZDOT = -1706
616173 ZDOT = -490
511849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6230264
02 X = 1898984
47
Y = -12431987
58 feet Y = -3789269
81 meter
Z = -17412255
62 Z = -5307255
51
XDOT = 20544
822705 XDOT = 6262
061960
YDOT = 12498
385498 feet/sec YDOT = 3809
507900 meter/sec
ZDOT = -1574
063369 ZDOT = -479
774515
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 18236
11137547
00016717 00000-0 10270-3 0 9073
2 25544 51
6390 40
2067 0005595 88
3100 271
8693 15
53851781 9075
Satellite: ISS
Catalog Number: 25544
Epoch time: 18236
11137547 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 40
2067 deg
Eccentricity:
0005595
Arg of perigee: 88
3100 deg
Mean anomaly: 271
8693 deg
Mean motion: 15
53851781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 907
Checksum: 312
Coasting Arc #9 (Orbit 922)
---------------------------------------
Vector Time (GMT): 2018/237/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3543815
81 A = 6778742
41 meter
Y = 2513425
59 meter E =
0009553
Z = 5195919
08 I = 51
84023
XDOT = -5569
175571 Wp = 75
13490
YDOT = -5112
849784 meter/sec RA = 34
66378 deg
ZDOT = -1320
734718 TA = 27
53257
MA = 27
48200
Ha = 223
626 n
mi
Hp = 213
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11626692
30 X = -3596896
81
Y = 8246146
93 feet Y = 2473499
55 meter
Z = 17046978
62 Z = 5178575
78
XDOT = -18271
573396 XDOT = -5505
173049
YDOT = -16774
441547 feet/sec YDOT = -5174
770341 meter/sec
ZDOT = -4333
119153 ZDOT = -1347
631726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10742960
32 X = -3274454
31
Y = 9509399
45 feet Y = 2898464
95 meter
Z = 16968751
25 Z = 5172075
38
XDOT = -19311
634679 XDOT = -5886
186250
YDOT = -13844
486069 feet/sec YDOT = -4219
799354 meter/sec
ZDOT = -4453
157071 ZDOT = -1357
322275
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 18237
14038509
00016717 00000-0 10270-3 0 9086
2 25544 51
6389 35
0798 0005661 91
2999 268
8802 15
53857577 9234
Satellite: ISS
Catalog Number: 25544
Epoch time: 18237
14038509 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 35
0798 deg
Eccentricity:
0005661
Arg of perigee: 91
2999 deg
Mean anomaly: 268
8802 deg
Mean motion: 15
53857577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 923
Checksum: 354
Coasting Arc #10 (Orbit 937)
---------------------------------------
Vector Time (GMT): 2018/238/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4761626
10 A = 6781237
59 meter
Y = -1463706
39 meter E =
0015466
Z = -4615912
21 I = 51
82093
XDOT = 4571
014569 Wp = 104
40314
YDOT = 5343
916928 meter/sec RA = 29
68362 deg
ZDOT = 3025
491406 TA = 195
75544
MA = 195
80361
Ha = 223
463 n
mi
Hp = 213
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15622132
88 X = 4800061
04
Y = -4802186
31 feet Y = -1410243
91 meter
Z = -15144068
93 Z = -4592688
88
XDOT = 14996
766959 XDOT = 4496
221708
YDOT = 17532
535852 feet/sec YDOT = 5394
615132 meter/sec
ZDOT = 9926
152907 ZDOT = 3047
513495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14971486
75 X = 4563309
16
Y = -6791170
16 feet Y = -2069948
67 meter
Z = -15039595
91 Z = -4584068
83
XDOT = 16572
123749 XDOT = 5051
183319
YDOT = 14369
221737 feet/sec YDOT = 4379
738785 meter/sec
ZDOT = 10024
262849 ZDOT = 3055
395316
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 18238
10507997
00016717 00000-0 10270-3 0 9096
2 25544 51
6391 30
2726 0005552 95
2165 264
9622 15
53856992 9386
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
10507997 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 30
2726 deg
Eccentricity:
0005552
Arg of perigee: 95
2165 deg
Mean anomaly: 264
9622 deg
Mean motion: 15
53856992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 938
Checksum: 336
Coasting Arc #11 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2018/238/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1521818
57 A = 6778020
31 meter
Y = 3916480
08 meter E =
0008061
Z = 5311851
24 I = 51
79767
XDOT = -6957
996766 Wp = 102
76078
YDOT = -3216
210715 meter/sec RA = 27
01846 deg
ZDOT = 375
694732 TA = 343
65469
MA = 343
68067
Ha = 223
401 n
mi
Hp = 213
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4992843
07 X = -1591302
37
Y = 12849344
10 feet Y = 3899073
85 meter
Z = 17427333
47 Z = 5304289
91
XDOT = -22828
073379 XDOT = -6923
339975
YDOT = -10551
872424 feet/sec YDOT = -3293
826054 meter/sec
ZDOT = 1232
594264 ZDOT = 341
980130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -214714
52 X = -65444
99
Y = -13827128
43 feet Y = -4214508
74 meter
Z = 17392828
83 Z = 5301334
23
XDOT = 24128
392445 XDOT = 7354
334017
YDOT = 995
129728 feet/sec YDOT = 303
315541 meter/sec
ZDOT = 1081
691923 ZDOT = 329
699698
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 18238
68389378
00016717 00000-0 10270-3 0 9102
2 25544 51
6416 27
3850 0005500 102
5327 257
6442 15
53907541 9470
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
68389378 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 27
3850 deg
Eccentricity:
0005500
Arg of perigee: 102
5327 deg
Mean anomaly: 257
6442 deg
Mean motion: 15
53907541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 947
Checksum: 316
Coasting Arc #12 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2018/239/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3057810
22 A = 6778800
88 meter
Y = -3160979
70 meter E =
0019304
Z = -5175672
61 I = 51
77017
XDOT = 6450
744816 Wp = 101
74845
YDOT = 3851
147106 meter/sec RA = 22
03239 deg
ZDOT = 1459
866521 TA = 182
30042
MA = 182
30931
Ha = 223
398 n
mi
Hp = 213
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10032185
77 X = 3118070
25
Y = -10370668
32 feet Y = -3126448
59 meter
Z = -16980553
17 Z = -5160672
45
XDOT = 21163
860945 XDOT = 6400
109631
YDOT = 12634
997068 feet/sec YDOT = 3923
000790 meter/sec
ZDOT = 4789
588324 ZDOT = 1491
078296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5154664
52 X = -1571141
74
Y = 13561803
57 feet Y = 4133637
73 meter
Z = -16912764
89 Z = -5155010
74
XDOT = -23431
318158 XDOT = -7141
865775
YDOT = -2762
053928 feet/sec YDOT = -841
874037 meter/sec
ZDOT = 4929
152060 ZDOT = 1502
405548
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 18239
64858586
00016717 00000-0 10270-3 0 9112
2 25544 51
6418 22
5789 0005611 104
1611 256
0165 15
53890675 9628
Satellite: ISS
Catalog Number: 25544
Epoch time: 18239
64858586 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 22
5789 deg
Eccentricity:
0005611
Arg of perigee: 104
1611 deg
Mean anomaly: 256
0165 deg
Mean motion: 15
53890675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 962
Checksum: 324
Coasting Arc #13 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2018/240/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4456627
42 A = 6781450
72 meter
Y = 2362332
82 meter E =
0013760
Z = 4521930
73 I = 51
74782
XDOT = -5507
805175 Wp = 82
56942
YDOT = -4303
192054 meter/sec RA = 17
04782 deg
ZDOT = -3170
212390 TA = 39
21593
MA = 39
11632
Ha = 223
503 n
mi
Hp = 213
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14621481
04 X = -4504677
38
Y = 7750435
78 feet Y = 2312227
43 meter
Z = 14835730
74 Z = 4500165
31
XDOT = -18070
226951 XDOT = -5443
877281
YDOT = -14118
084168 feet/sec YDOT = -4364
426963 meter/sec
ZDOT = -10400
959286 ZDOT = -3196
811494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10170644
64 X = 3100012
48
Y = -13164885
31 feet Y = -4012657
04 meter
Z = 14737694
92 Z = 4492049
41
XDOT = 21278
731392 XDOT = 6485
757328
YDOT = 4625
588814 feet/sec YDOT = 1409
879471 meter/sec
ZDOT = -10519
740386 ZDOT = -3206
416870
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 18240
67758830
00016717 00000-0 10270-3 0 9129
2 25544 51
6417 17
4514 0005591 107
5090 252
6674 15
53888968 9787
Satellite: ISS
Catalog Number: 25544
Epoch time: 18240
67758830 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 17
4514 deg
Eccentricity:
0005591
Arg of perigee: 107
5090 deg
Mean anomaly: 252
6674 deg
Mean motion: 15
53888968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 978
Checksum: 340
Coasting Arc #14 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2018/241/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5605674
00 A = 6785035
12 meter
Y = -1608017
76 meter E =
0010249
Z = -3478807
81 I = 51
72748
XDOT = 4131
439433 Wp = 101
61008
YDOT = 4561
196304 meter/sec RA = 12
07040 deg
ZDOT = 4558
345047 TA = 217
65555
MA = 217
72734
Ha = 223
351 n
mi
Hp = 213
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18391318
91 X = 5640136
79
Y = -5275648
82 feet Y = -1545138
83 meter
Z = -11413411
46 Z = -3451493
73
XDOT = 13554
591316 XDOT = 4057
985923
YDOT = 14964
554804 feet/sec YDOT = 4606
986603 meter/sec
ZDOT = 14955
200285 ZDOT = 4578
235225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14390502
13 X = -4386225
05
Y = 12719084
30 feet Y = 3876776
89 meter
Z = -11290588
38 Z = -3441371
34
XDOT = -17663
090292 XDOT = -5383
709921
YDOT = -6657
549216 feet/sec YDOT = -2029
221001 meter/sec
ZDOT = 15043
820713 ZDOT = 4585
356553
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 18241
64227616
00016717 00000-0 10270-3 0 9131
2 25544 51
6414 12
6453 0005492 111
8828 248
2909 15
53880377 9935
Satellite: ISS
Catalog Number: 25544
Epoch time: 18241
64227616 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 12
6453 deg
Eccentricity:
0005492
Arg of perigee: 111
8828 deg
Mean anomaly: 248
2909 deg
Mean motion: 15
53880377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 320
Coasting Arc #15 (Orbit 1008)
---------------------------------------
Vector Time (GMT): 2018/242/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6401708
99 A = 6788307
16 meter
Y = 844897
34 meter E =
0019492
Z = 2063888
91 I = 51
70615
XDOT = -2422
171723 Wp = 111
56031
YDOT = -4715
685227 meter/sec RA = 7
09929 deg
ZDOT = -5547
492111 TA = 45
61492
MA = 45
45546
Ha = 223
384 n
mi
Hp = 213
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21002982
24 X = -6420706
33
Y = 2771972
90 feet Y = 773202
94 meter
Z = 6771289
09 Z = 2032745
51
XDOT = -7946
757623 XDOT = -2342
312882
YDOT = -15471
408225 feet/sec YDOT = -4742
325553 meter/sec
ZDOT = -18200
433435 ZDOT = -5559
063811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17596708
01 X = 5363476
60
Y = -11876019
53 feet Y = -3619810
75 meter
Z = 6631401
03 Z = 2021251
03
XDOT = 13043
410376 XDOT = 3975
631483
YDOT = 9069
362016 feet/sec YDOT = 2764
341543 meter/sec
ZDOT = -18251
689848 ZDOT = -5563
115066
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 18242
67127385
00016717 00000-0 10270-3 0 9148
2 25544 51
6416 7
5178 0005559 113
7755 246
3981 15
53886047 10096
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
67127385 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 7
5178 deg
Eccentricity:
0005559
Arg of perigee: 113
7755 deg
Mean anomaly: 246
3981 deg
Mean motion: 15
53886047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1009
Checksum: 328
Coasting Arc #16 (Orbit 1012)
---------------------------------------
Vector Time (GMT): 2018/242/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -491179
20 A = 6778301
56 meter
Y = -4245128
33 meter E =
0019738
Z = -5278485
85 I = 51
66086
XDOT = 7609
581432 Wp = 91
05609
YDOT = 122
665364 meter/sec RA = 5
75029 deg
ZDOT = -809
722467 TA = 171
20926
MA = 171
17464
Ha = 223
394 n
mi
Hp = 213
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1611480
31 X = -418032
43
Y = -13927586
39 feet Y = -4250212
45 meter
Z = -17317866
96 Z = -5280693
84
XDOT = 24965
818345 XDOT = 7611
577393
YDOT = 402
445421 feet/sec YDOT = 207
772074 meter/sec
ZDOT = -2656
569772 ZDOT = -772
752986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10363095
89 X = 3158671
63
Y = -9426482
00 feet Y = -2873191
71 meter
Z = -17327167
34 Z = -5281320
61
XDOT = 13728
261151 XDOT = 4184
373999
YDOT = 19652
567741 feet/sec YDOT = 5990
102647 meter/sec
ZDOT = -2490
677930 ZDOT = -759
158633
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 18242
92852333
00016717 00000-0 10270-3 0 9155
2 25544 51
6389 6
2368 0005611 111
1609 249
0144 15
53871018 10139
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
92852333 = yrday
fracday
Element set: 915
Inclination: 51
6389 deg
RA of node: 6
2368 deg
Eccentricity:
0005611
Arg of perigee: 111
1609 deg
Mean anomaly: 249
0144 deg
Mean motion: 15
53871018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1013
Checksum: 288
Coasting Arc #17 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2018/243/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1221410
36 A = 6778458
01 meter
Y = 4125861
54 meter E =
0008168
Z = 5230562
30 I = 51
62769
XDOT = -7548
504886 Wp = 91
06529
YDOT = -919
707466 meter/sec RA =
75407 deg
ZDOT = -1035
969921 TA = 8
85645
MA = 8
84205
Ha = 223
358 n
mi
Hp = 213
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4007251
84 X = -1292863
45
Y = 13536291
13 feet Y = 4111803
69 meter
Z = 17160637
48 Z = 5224455
30
XDOT = -24765
435977 XDOT = -7532
627242
YDOT = -3017
412946 feet/sec YDOT = -1004
031366 meter/sec
ZDOT = -3398
851447 ZDOT = -1072
599350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13279500
67 X = -4047591
80
Y = 4889194
05 feet Y = 1490226
35 meter
Z = 17132640
40 Z = 5222028
79
XDOT = -12177
960673 XDOT = -3711
842413
YDOT = -20576
360821 feet/sec YDOT = -6271
674778 meter/sec
ZDOT = -3563
088544 ZDOT = -1086
029388
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 18243
95751821
00016717 00000-0 10270-3 0 9160
2 25544 51
6381 1
1096 0005495 114
7648 245
4077 15
53879292 10299
Satellite: ISS
Catalog Number: 25544
Epoch time: 18243
95751821 = yrday
fracday
Element set: 916
Inclination: 51
6381 deg
RA of node: 1
1096 deg
Eccentricity:
0005495
Arg of perigee: 114
7648 deg
Mean anomaly: 245
4077 deg
Mean motion: 15
53879292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 323
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