[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 11th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
283/18:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
5
284/08:40:15
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
284/14:44:49
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
7
287/02:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
5
291/16:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 216
4
295/18:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 216
2
Coasting Arc #1 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2018/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1834270
07 A = 6780647
13 meter
Y = 4484893
32 meter E =
0007506
Z = -4750516
72 I = 51
73581
XDOT = -7160
799423 Wp = 117
24602
YDOT = -43
746365 meter/sec RA = 162
89315 deg
ZDOT = 2723
581839 TA = 179
67545
MA = 179
67496
Ha = 220
077 n
mi
Hp = 216
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6017946
42 X = -1861209
08
Y = 14714216
93 feet Y = 4464230
13 meter
Z = -15585684
77 Z = -4759493
04
XDOT = -23493
436428 XDOT = -7173
008033
YDOT = -143
524820 feet/sec YDOT = -123
891382 meter/sec
ZDOT = 8935
635954 ZDOT = 2688
766788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1032987
15 X = 314854
48
Y = -15823568
65 feet Y = -4823023
73 meter
Z = -15626421
27 Z = -4762933
20
XDOT = 21269
439239 XDOT = 6482
925080
YDOT = -7281
467528 feet/sec YDOT = -2219
391303 meter/sec
ZDOT = 8779
200003 ZDOT = 2675
900161
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 18283
51136211
00016717 00000-0 10270-3 0 9009
2 25544 51
6407 164
0271 0003871 272
9429 87
1281 15
53811555 16441
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
51136211 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 164
0271 deg
Eccentricity:
0003871
Arg of perigee: 272
9429 deg
Mean anomaly: 87
1281 deg
Mean motion: 15
53811555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1644
Checksum: 294
Coasting Arc #2 (Orbit 1647)
---------------------------------------
Vector Time (GMT): 2018/283/18:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1767901
17 A = 6778346
21 meter
Y = 3830787
45 meter E =
0011133
Z = -5314877
02 I = 51
73292
XDOT = -7149
158524 Wp = 87
05700
YDOT = 2718
104788 meter/sec RA = 161
66068 deg
ZDOT = -419
123108 TA = 178
94795
MA = 178
94560
Ha = 220
172 n
mi
Hp = 216
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5800200
70 X = 1750750
27
Y = 12568200
29 feet Y = 3850460
94 meter
Z = -17437260
58 Z = -5306331
02
XDOT = -23455
244502 XDOT = -7176
985862
YDOT = 8917
666628 feet/sec YDOT = 2638
002301 meter/sec
ZDOT = -1375
075815 ZDOT = -453
919835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9950039
11 X = -3032771
92
Y = 9691465
40 feet Y = 2953958
65 meter
Z = -17399202
94 Z = -5303277
06
XDOT = -15370
401194 XDOT = -4684
898284
YDOT = -18529
157391 feet/sec YDOT = -5647
687173 meter/sec
ZDOT = -1531
681931 ZDOT = -466
856653
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 18283
76862560
00016717 00000-0 10270-3 0 9010
2 25544 51
6376 162
7409 0003626 265
7767 94
2971 15
53813170 16481
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
76862560 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 162
7409 deg
Eccentricity:
0003626
Arg of perigee: 265
7767 deg
Mean anomaly: 94
2971 deg
Mean motion: 15
53813170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1648
Checksum: 335
Coasting Arc #3 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2018/284/08:40:15
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2821726
57 A = 6778767
12 meter
Y = -3301885
56 meter E =
0002124
Z = 5205277
32 I = 51
75459
XDOT = 6618
434739 Wp = 191
47792
YDOT = -3658
936533 meter/sec RA = 158
63977 deg
ZDOT = 1264
851876 TA = 246
38599
MA = 246
40830
Ha = 220
121 n
mi
Hp = 216
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9257633
11 X = -2809879
31
Y = -10832957
87 feet Y = -3333373
39 meter
Z = 17077681
50 Z = 5191599
10
XDOT = 21714
024735 XDOT = 6652
713966
YDOT = -12004
384951 feet/sec YDOT = -3584
732828 meter/sec
ZDOT = 4149
776495 ZDOT = 1297
086220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2472179
30 X = 753520
25
Y = 14107819
38 feet Y = 4300063
35 meter
Z = 17016512
99 Z = 5186633
16
XDOT = -23743
407120 XDOT = -7236
990490
YDOT = -1027
536700 feet/sec YDOT = -313
193186 meter/sec
ZDOT = 4294
966025 ZDOT = 1309
105644
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 18284
41177999
00016717 00000-0 10270-3 0 9029
2 25544 51
6386 159
5403 0003934 275
1771 84
8933 15
53836681 16588
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
41177999 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 159
5403 deg
Eccentricity:
0003934
Arg of perigee: 275
1771 deg
Mean anomaly: 84
8933 deg
Mean motion: 15
53836681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 351
Coasting Arc #4 (Orbit 1661)
---------------------------------------
Vector Time (GMT): 2018/284/14:44:49
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4915522
13 A = 6782378
45 meter
Y = -1673584
33 meter E =
0005822
Z = 4360266
55 I = 51
77214
XDOT = 4750
076114 Wp = 116
55117
YDOT = -4928
110568 meter/sec RA = 157
39200 deg
ZDOT = 3457
328664 TA = 298
39419
MA = 298
45286
Ha = 220
215 n
mi
Hp = 216
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16127041
12 X = -4917622
67
Y = -5490762
23 feet Y = -1728564
51 meter
Z = 14305336
44 Z = 4336383
14
XDOT = 15584
239218 XDOT = 4788
036320
YDOT = -16168
341760 feet/sec YDOT = -4874
779400 meter/sec
ZDOT = 11342
941811 ZDOT = 3480
495992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12772815
54 X = 3893154
18
Y = -11407896
67 feet Y = -3477126
91 meter
Z = 14198156
66 Z = 4327598
15
XDOT = 5590
134521 XDOT = 1703
873002
YDOT = 20531
548149 feet/sec YDOT = 6258
015876 meter/sec
ZDOT = 11447
505413 ZDOT = 3489
199650
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 18284
66904211
00016717 00000-0 10270-3 0 9032
2 25544 51
6368 158
2563 0004016 276
5256 83
5439 15
53787732 16620
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
66904211 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 158
2563 deg
Eccentricity:
0004016
Arg of perigee: 276
5256 deg
Mean anomaly: 83
5439 deg
Mean motion: 15
53787732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1662
Checksum: 326
Coasting Arc #5 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2018/285/14:44:49
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3672673
90 A = 6779424
64 meter
Y = 2594505
71 meter E =
0009636
Z = -5082214
62 I = 51
79212
XDOT = -5807
366592 Wp = 67
55307
YDOT = 4652
027645 meter/sec RA = 152
40992 deg
ZDOT = -1820
983100 TA = 184
83326
MA = 184
84257
Ha = 220
130 n
mi
Hp = 216
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12049455
06 X = 3668075
72
Y = 8512157
85 feet Y = 2635550
10 meter
Z = -16673932
48 Z = -5064384
97
XDOT = -19053
039999 XDOT = -5850
109670
YDOT = 15262
557889 feet/sec YDOT = 4586
846543 meter/sec
ZDOT = -5974
354001 ZDOT = -1849
297980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13287464
02 X = -4050019
03
Y = 6614186
79 feet Y = 2016004
13 meter
Z = -16594036
75 Z = -5057862
40
XDOT = -3837
851917 XDOT = -1169
777264
YDOT = -23026
022271 feet/sec YDOT = -7018
331588 meter/sec
ZDOT = -6102
048739 ZDOT = -1859
904456
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 18285
63377243
00016717 00000-0 10270-3 0 9040
2 25544 51
6362 153
4483 0003859 279
1009 80
9706 15
53811675 16779
Satellite: ISS
Catalog Number: 25544
Epoch time: 18285
63377243 = yrday
fracday
Element set: 904
Inclination: 51
6362 deg
RA of node: 153
4483 deg
Eccentricity:
0003859
Arg of perigee: 279
1009 deg
Mean anomaly: 80
9706 deg
Mean motion: 15
53811675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 333
Coasting Arc #6 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2018/286/14:44:49
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2275652
06 A = 6778384
70 meter
Y = -3519124
97 meter E =
0001478
Z = 5328732
50 I = 51
81699
XDOT = 6452
390288 Wp = 300
10675
YDOT = -4141
966603 meter/sec RA = 147
42509 deg
ZDOT = 20
862917 TA = 149
69919
MA = 149
69064
Ha = 220
332 n
mi
Hp = 216
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7466050
08 X = -2262015
79
Y = -11545685
59 feet Y = -3544496
42 meter
Z = 17482718
16 Z = 5317711
21
XDOT = 21169
259476 XDOT = 6498
126011
YDOT = -13589
129274 feet/sec YDOT = -4069
555771 meter/sec
ZDOT = 68
447890 ZDOT = 52
318285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13742604
94 X = 4188745
99
Y = -1379778
98 feet Y = -420556
63 meter
Z = 17433508
35 Z = 5313733
34
XDOT = 2151
160111 XDOT = 655
673602
YDOT = 24051
655091 feet/sec YDOT = 7330
944472 meter/sec
ZDOT = 210
235501 ZDOT = 64
079781
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 18286
66281663
00016717 00000-0 10270-3 0 9055
2 25544 51
6360 148
3203 0003795 283
2931 76
7798 15
53773551 16931
Satellite: ISS
Catalog Number: 25544
Epoch time: 18286
66281663 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 148
3203 deg
Eccentricity:
0003795
Arg of perigee: 283
2931 deg
Mean anomaly: 76
7798 deg
Mean motion: 15
53773551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 340
Coasting Arc #7 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2018/287/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 614794
62 A = 6779376
30 meter
Y = 4449497
48 meter E =
0009509
Z = -5086362
43 I = 51
83549
XDOT = -6802
157713 Wp = 102
75295
YDOT = 3017
916325 meter/sec RA = 145
00073 deg
ZDOT = 1818
674238 TA = 184
81732
MA = 184
82648
Ha = 220
295 n
mi
Hp = 216
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2017042
70 X = 589700
74
Y = 14598088
85 feet Y = 4456232
04 meter
Z = -16687540
80 Z = -5083437
04
XDOT = -22316
790398 XDOT = -6844
233669
YDOT = 9901
300280 feet/sec YDOT = 2941
614684 meter/sec
ZDOT = 5966
778996 ZDOT = 1785
528779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13476496
94 X = 4107636
27
Y = 5998441
15 feet Y = 1828324
86 meter
Z = -16674813
68 Z = -5082483
21
XDOT = -3134
125478 XDOT = -955
281446
YDOT = 23205
669576 feet/sec YDOT = 7073
088087 meter/sec
ZDOT = 5817
488495 ZDOT = 1773
170493
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 18287
11302105
00016717 00000-0 10270-3 0 9062
2 25544 51
6375 146
0799 0003734 285
7772 74
2968 15
53791641 17006
Satellite: ISS
Catalog Number: 25544
Epoch time: 18287
11302105 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 146
0799 deg
Eccentricity:
0003734
Arg of perigee: 285
7772 deg
Mean anomaly: 74
2968 deg
Mean motion: 15
53791641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 322
Coasting Arc #8 (Orbit 1715)
---------------------------------------
Vector Time (GMT): 2018/288/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 784083
90 A = 6782082
88 meter
Y = -5128960
94 meter E =
0006953
Z = 4365549
00 I = 51
87062
XDOT = 6557
447651 Wp = 51
00677
YDOT = -1951
272473 meter/sec RA = 140
02398 deg
ZDOT = -3462
298832 TA = 74
06281
MA = 73
98621
Ha = 220
247 n
mi
Hp = 216
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2572453
75 X = 820173
22
Y = -16827299
67 feet Y = -5119990
84 meter
Z = 14322667
33 Z = 4369445
70
XDOT = 21513
935864 XDOT = 6595
598254
YDOT = -6401
812576 feet/sec YDOT = -1877
729342 meter/sec
ZDOT = -11359
248138 ZDOT = -3430
351784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13089898
63 X = -3989801
10
Y = -10858806
76 feet Y = -3309764
30 meter
Z = 14340683
44 Z = 4371040
31
XDOT = 4954
359594 XDOT = 1510
088804
YDOT = -20818
402963 feet/sec YDOT = -6345
449223 meter/sec
ZDOT = -11215
424931 ZDOT = -3418
461519
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 18288
14206082
00016717 00000-0 10270-3 0 9074
2 25544 51
6366 140
9521 0003854 290
0526 70
0211 15
53834548 17167
Satellite: ISS
Catalog Number: 25544
Epoch time: 18288
14206082 = yrday
fracday
Element set: 907
Inclination: 51
6366 deg
RA of node: 140
9521 deg
Eccentricity:
0003854
Arg of perigee: 290
0526 deg
Mean anomaly: 70
0211 deg
Mean motion: 15
53834548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1716
Checksum: 295
Coasting Arc #9 (Orbit 1730)
---------------------------------------
Vector Time (GMT): 2018/289/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2001291
18 A = 6785709
44 meter
Y = 5605204
80 meter E =
0002491
Z = -3257938
08 I = 51
90794
XDOT = -5956
149754 Wp = 31
45942
YDOT = 649
865945 meter/sec RA = 135
05827 deg
ZDOT = 4780
545115 TA = 290
94393
MA = 290
97059
Ha = 220
440 n
mi
Hp = 216
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6565915
93 X = -2047995
83
Y = 18389779
54 feet Y = 5582563
73 meter
Z = -10688773
24 Z = -3267773
42
XDOT = -19541
173735 XDOT = -5986
195748
YDOT = 2132
106118 feet/sec YDOT = 583
092307 meter/sec
ZDOT = 15684
203132 ZDOT = 4751
538810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12595772
78 X = 3839191
54
Y = 14889007
44 feet Y = 4538169
47 meter
Z = -10733549
39 Z = -3271585
85
XDOT = -6989
348132 XDOT = -2130
353311
YDOT = 17116
824987 feet/sec YDOT = 5217
208256 meter/sec
ZDOT = 15553
710424 ZDOT = 4740
770937
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 18289
10678410
00016717 00000-0 10270-3 0 9080
2 25544 51
6373 136
1456 0003679 295
6649 64
4123 15
53812650 17317
Satellite: ISS
Catalog Number: 25544
Epoch time: 18289
10678410 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 136
1456 deg
Eccentricity:
0003679
Arg of perigee: 295
6649 deg
Mean anomaly: 64
4123 deg
Mean motion: 15
53812650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1731
Checksum: 321
Coasting Arc #10 (Orbit 1746)
---------------------------------------
Vector Time (GMT): 2018/290/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3010175
62 A = 6788700
41 meter
Y = -5798046
27 meter E =
0010086
Z = 1829388
30 I = 51
94034
XDOT = 5091
132366 Wp = 111
19288
YDOT = 847
175828 meter/sec RA = 130
10211 deg
ZDOT = -5670
638494 TA = 48
77934
MA = 48
69244
Ha = 220
478 n
mi
Hp = 216
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9875904
26 X = 3065900
95
Y = -19022461
52 feet Y = -5764072
75 meter
Z = 6001930
12 Z = 1844146
43
XDOT = 16703
190177 XDOT = 5108
825922
YDOT = 2779
448254 feet/sec YDOT = 904
207114 meter/sec
ZDOT = -18604
457002 ZDOT = -5645
864307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11765209
78 X = -3586035
94
Y = -17892994
96 feet Y = -5453784
86 meter
Z = 6068876
54 Z = 1849793
57
XDOT = 9359
897914 XDOT = 2852
896884
YDOT = -12450
581603 feet/sec YDOT = -3794
937273 meter/sec
ZDOT = -18493
129956 ZDOT = -5636
706010
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 18290
13581818
00016717 00000-0 10270-3 0 9091
2 25544 51
6367 131
0175 0003909 301
2117 58
8653 15
53846415 17470
Satellite: ISS
Catalog Number: 25544
Epoch time: 18290
13581818 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 131
0175 deg
Eccentricity:
0003909
Arg of perigee: 301
2117 deg
Mean anomaly: 58
8653 deg
Mean motion: 15
53846415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1747
Checksum: 315
Coasting Arc #11 (Orbit 1761)
---------------------------------------
Vector Time (GMT): 2018/291/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739933
26 A = 6790079
97 meter
Y = 5653440
92 meter E =
0011389
Z = -252315
46 I = 51
96507
XDOT = -4065
613810 Wp = 24
91326
YDOT = -2425
078622 meter/sec RA = 125
15450 deg
ZDOT = 6034
217799 TA = 332
37988
MA = 332
44033
Ha = 220
509 n
mi
Hp = 216
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12270122
26 X = -3801648
03
Y = 18548034
52 feet Y = 5611273
31 meter
Z = -827806
62 Z = -270633
12
XDOT = -13338
627985 XDOT = -4067
505103
YDOT = -7956
294690 feet/sec YDOT = -2470
553421 meter/sec
ZDOT = 19797
302489 ZDOT = 6014
463770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10500961
13 X = 3200692
95
Y = 19600282
56 feet Y = 5974166
12 meter
Z = -910762
02 Z = -277600
26
XDOT = -11967
277000 XDOT = -3647
626030
YDOT = 7312
265933 feet/sec YDOT = 2228
778657 meter/sec
ZDOT = 19708
703214 ZDOT = 6007
212740
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 18291
10053725
00016717 00000-0 10270-3 0 9102
2 25544 51
6362 126
2113 0003704 301
6446 58
4344 15
53859029 17620
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
10053725 = yrday
fracday
Element set: 910
Inclination: 51
6362 deg
RA of node: 126
2113 deg
Eccentricity:
0003704
Arg of perigee: 301
6446 deg
Mean anomaly: 58
4344 deg
Mean motion: 15
53859029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1762
Checksum: 286
Coasting Arc #12 (Orbit 1770)
---------------------------------------
Vector Time (GMT): 2018/291/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 496782
33 A = 6782850
79 meter
Y = 5326737
69 meter E =
0004071
Z = -4173651
88 I = 51
95378
XDOT = -5691
178727 Wp = 101
15323
YDOT = 3482
292759 meter/sec RA = 122
29965 deg
ZDOT = 3769
302578 TA = 207
48829
MA = 207
50982
Ha = 220
507 n
mi
Hp = 216
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1629863
30 X = 457453
96
Y = 17476173
53 feet Y = 5332072
93 meter
Z = -13693083
60 Z = -4171334
48
XDOT = -18671
846216 XDOT = -5748
005191
YDOT = 11424
845009 feet/sec YDOT = 3418
332519 meter/sec
ZDOT = 12366
478275 ZDOT = 3741
518301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17534181
30 X = -5344418
46
Y = 946613
01 feet Y = 288527
65 meter
Z = -13683202
99 Z = -4170640
27
XDOT = -10516
374464 XDOT = -3205
390937
YDOT = -17961
918486 feet/sec YDOT = -5474
792755 meter/sec
ZDOT = 12241
156886 ZDOT = 3731
104619
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 18291
67936751
00016717 00000-0 10270-3 0 9114
2 25544 51
6387 123
3231 0003784 298
9260 61
1513 15
53822198 17712
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
67936751 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 123
3231 deg
Eccentricity:
0003784
Arg of perigee: 298
9260 deg
Mean anomaly: 61
1513 deg
Mean motion: 15
53822198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1771
Checksum: 320
Coasting Arc #13 (Orbit 1786)
---------------------------------------
Vector Time (GMT): 2018/292/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 527843
04 A = 6786474
49 meter
Y = -6075439
03 meter E =
0009989
Z = 2969448
77 I = 51
98317
XDOT = 5445
203627 Wp = 88
40587
YDOT = -1987
549598 meter/sec RA = 117
34008 deg
ZDOT = -5019
616612 TA = 57
83606
MA = 57
73921
Ha = 220
597 n
mi
Hp = 216
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1731768
49 X = 581316
88
Y = -19932542
75 feet Y = -6069237
13 meter
Z = 9742285
98 Z = 2972143
18
XDOT = 17864
841297 XDOT = 5491
407187
YDOT = -6520
832015 feet/sec YDOT = -1926
399558 meter/sec
ZDOT = -16468
558437 ZDOT = -4993
053047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19879515
98 X = 6059276
47
Y = 2204901
80 feet Y = 672054
07 meter
Z = 9755033
11 Z = 2973334
09
XDOT = 6194
725260 XDOT = 1888
152259
YDOT = 16694
047363 feet/sec YDOT = 5088
345636 meter/sec
ZDOT = -16348
868003 ZDOT = -4983
134967
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 18292
70839587
00016717 00000-0 10270-3 0 9129
2 25544 51
6392 118
1951 0003684 303
1622 56
9177 15
53822083 17877
Satellite: ISS
Catalog Number: 25544
Epoch time: 18292
70839587 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 118
1951 deg
Eccentricity:
0003684
Arg of perigee: 303
1622 deg
Mean anomaly: 56
9177 deg
Mean motion: 15
53822083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1787
Checksum: 330
Coasting Arc #14 (Orbit 1801)
---------------------------------------
Vector Time (GMT): 2018/293/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1388334
31 A = 6789215
94 meter
Y = 6466286
52 meter E =
0009137
Z = -1510021
57 I = 52
00677
XDOT = -5011
132720 Wp = 13
57465
YDOT = 274
390474 meter/sec RA = 112
39066 deg
ZDOT = 5798
029315 TA = 330
01911
MA = 330
07141
Ha = 220
739 n
mi
Hp = 216
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4554902
58 X = -1453203
95
Y = 21214850
79 feet Y = 6450398
37 meter
Z = -4954139
02 Z = -1516923
80
XDOT = -16440
724146 XDOT = -5041
992734
YDOT = 900
231213 feet/sec YDOT = 218
180438 meter/sec
ZDOT = 19022
405889 ZDOT = 5773
611674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21169050
04 X = -6452326
45
Y = -4730009
47 feet Y = -1441706
89 meter
Z = -4985865
63 Z = -1519691
84
XDOT = -1083
737389 XDOT = -330
323156
YDOT = -15031
303474 feet/sec YDOT = -4581
541299 meter/sec
ZDOT = 18912
538235 ZDOT = 5764
541654
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 18293
67310695
00016717 00000-0 10270-3 0 9131
2 25544 51
6393 113
3884 0003757 309
2742 50
8077 15
53829979 18022
Satellite: ISS
Catalog Number: 25544
Epoch time: 18293
67310695 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 113
3884 deg
Eccentricity:
0003757
Arg of perigee: 309
2742 deg
Mean anomaly: 50
8077 deg
Mean motion: 15
53829979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1802
Checksum: 337
Coasting Arc #15 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2018/294/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2119371
20 A = 6790137
54 meter
Y = -6445682
85 meter E =
0008169
Z = -114384
78 I = 52
02114
XDOT = 4451
751059 Wp = 137
35579
YDOT = 1566
403187 meter/sec RA = 107
44702 deg
ZDOT = -6041
556120 TA = 43
86951
MA = 43
80466
Ha = 220
752 n
mi
Hp = 216
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6953317
60 X = 2191846
74
Y = -21147253
43 feet Y = -6421577
34 meter
Z = -375278
16 Z = -103912
82
XDOT = 14605
482476 XDOT = 4463
251413
YDOT = 5139
118066 feet/sec YDOT = 1616
249512 meter/sec
ZDOT = -19821
378346 ZDOT = -6019
902916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21198028
10 X = 6461158
96
Y = 6799422
57 feet Y = 2072464
00 meter
Z = -327482
26 Z = -99816
59
XDOT = -4532
986560 XDOT = -1381
654303
YDOT = 13228
759779 feet/sec YDOT = 4032
125981 meter/sec
ZDOT = -19724
137941 ZDOT = -6011
917245
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 18294
70213031
00016717 00000-0 10270-3 0 9143
2 25544 51
6388 108
2609 0003755 311
3030 48
7799 15
53848325 18186
Satellite: ISS
Catalog Number: 25544
Epoch time: 18294
70213031 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 108
2609 deg
Eccentricity:
0003755
Arg of perigee: 311
3030 deg
Mean anomaly: 48
7799 deg
Mean motion: 15
53848325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 313
Coasting Arc #16 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2018/295/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2691556
64 A = 6788924
04 meter
Y = 5985545
74 meter E =
0013333
Z = 1706411
94 I = 52
02728
XDOT = -3834
832303 Wp = 48
61909
YDOT = -3363
679045 meter/sec RA = 102
50321 deg
ZDOT = 5729
650389 TA = 329
99672
MA = 330
07306
Ha = 220
946 n
mi
Hp = 216
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8830566
40 X = -2766577
65
Y = 19637617
27 feet Y = 5955027
57 meter
Z = 5598464
36 Z = 1693154
27
XDOT = -12581
470812 XDOT = -3824
765879
YDOT = -11035
692405 feet/sec YDOT = -3406
505999 meter/sec
ZDOT = 18798
065582 ZDOT = 5711
046484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19850040
59 X = -6050292
37
Y = -8382258
74 feet Y = -2554912
46 meter
Z = 5538171
66 Z = 1688034
72
XDOT = 10107
458310 XDOT = 3080
753293
YDOT = -11526
145084 feet/sec YDOT = -3513
169022 meter/sec
ZDOT = 18714
738986 ZDOT = 5704
252443
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 18295
73115051
00016717 00000-0 10270-3 0 9151
2 25544 51
6401 103
1330 0003766 317
4416 42
6444 15
53853795 18349
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
73115051 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 103
1330 deg
Eccentricity:
0003766
Arg of perigee: 317
4416 deg
Mean anomaly: 42
6444 deg
Mean motion: 15
53853795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 294
Coasting Arc #17 (Orbit 1834)
---------------------------------------
Vector Time (GMT): 2018/295/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4041147
23 A = 6783136
14 meter
Y = -3591503
88 meter E =
0006716
Z = -4103882
36 I = 52
00744
XDOT = 1735
083750 Wp = 39
12271
YDOT = 6378
411791 meter/sec RA = 102
00891 deg
ZDOT = -3871
871905 TA = 190
97935
MA = 190
99402
Ha = 220
914 n
mi
Hp = 216
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13258357
04 X = 4100942
99
Y = -11783149
21 feet Y = -3545978
99 meter
Z = -13464180
96 Z = -4084105
90
XDOT = 5692
531989 XDOT = 1682
437519
YDOT = 20926
547872 feet/sec YDOT = 6397
519991 meter/sec
ZDOT = -12702
991813 ZDOT = -3863
571742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17518211
68 X = 5339550
92
Y = 3183897
36 feet Y = 970451
91 meter
Z = -13374821
97 Z = -4076645
74
XDOT = -12621
868805 XDOT = -3847
145612
YDOT = 16216
223987 feet/sec YDOT = 4942
705071 meter/sec
ZDOT = -12666
347511 ZDOT = -3860
702721
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 18295
79546390
00016717 00000-0 10270-3 0 9162
2 25544 51
6390 102
8148 0003941 317
3735 42
7111 15
53839226 18353
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
79546390 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 102
8148 deg
Eccentricity:
0003941
Arg of perigee: 317
3735 deg
Mean anomaly: 42
7111 deg
Mean motion: 15
53839226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 319
Coasting Arc #18 (Orbit 1850)
---------------------------------------
Vector Time (GMT): 2018/296/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4145861
99 A = 6779852
01 meter
Y = 2086842
32 meter E =
0003194
Z = 4939366
01 I = 52
00287
XDOT = -912
903254 Wp = 95
42834
YDOT = -7259
792422 meter/sec RA = 97
04402 deg
ZDOT = 2299
390203 TA = 332
20242
MA = 332
21949
Ha = 221
164 n
mi
Hp = 215
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13601909
43 X = -4192882
95
Y = 6846595
55 feet Y = 2040217
90 meter
Z = 16205269
05 Z = 4919111
98
XDOT = -2995
089417 XDOT = -842
823885
YDOT = -23818
216609 feet/sec YDOT = -7269
609119 meter/sec
ZDOT = 7543
931111 ZDOT = 2295
126320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13976293
53 X = -4259974
27
Y = -6285172
80 feet Y = -1915720
67 meter
Z = 16113918
76 Z = 4911522
44
XDOT = 16060
816486 XDOT = 4895
336865
YDOT = -16407
046574 feet/sec YDOT = -5000
867796 meter/sec
ZDOT = 7525
558317 ZDOT = 2293
790175
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 18296
82448001
00016717 00000-0 10270-3 0 9178
2 25544 51
6393 97
6868 0004027 322
3783 37
7087 15
53866494 18512
Satellite: ISS
Catalog Number: 25544
Epoch time: 18296
82448001 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 97
6868 deg
Eccentricity:
0004027
Arg of perigee: 322
3783 deg
Mean anomaly: 37
7087 deg
Mean motion: 15
53866494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1851
Checksum: 344
Coasting Arc #19 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2018/297/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 944248
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4181578
03 A = 6778309
22 meter
Y = -423931
00 meter E =
0013214
Z = -5328962
37 I = 51
99961
XDOT = 121
504934 Wp = 70
74325
YDOT = 7640
736874 meter/sec RA = 92
07368 deg
ZDOT = -509
285472 TA = 194
39708
MA = 194
43477
Ha = 221
195 n
mi
Hp = 216
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13719088
02 X = 4211893
78
Y = -1390849
74 feet Y = -377000
52 meter
Z = -17483472
33 Z = -5308575
48
XDOT = 398
638234 XDOT = 38
528964
YDOT = 25068
034362 feet/sec YDOT = 7641
631647 meter/sec
ZDOT = -1670
884093 ZDOT = -508
897244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9998367
22 X = 3047502
33
Y = 9663375
40 feet Y = 2945396
82 meter
Z = -17391707
02 Z = -5300992
30
XDOT = -18168
924393 XDOT = -5537
888155
YDOT = 15774
113954 feet/sec YDOT = 4807
949933 meter/sec
ZDOT = -1670
010483 ZDOT = -509
019195
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 18297
78918306
00016717 00000-0 10270-3 0 9185
2 25544 51
6386 92
8801 0004020 326
3876 33
7021 15
53831204 18669
Satellite: ISS
Catalog Number: 25544
Epoch time: 18297
78918306 = yrday
fracday
Element set: 918
Inclination: 51
6386 deg
RA of node: 92
8801 deg
Eccentricity:
0004020
Arg of perigee: 326
3876 deg
Mean anomaly: 33
7021 deg
Mean motion: 15
53831204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 318
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