[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 27th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
152/21:55:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
1
153/10:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 216
2
153/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
3
155/13:34:21
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
4
156/18:50:00
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
5
160/01:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
6
Coasting Arc #1 (Orbit 1837)
---------------------------------------
Vector Time (GMT): 2017/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5757854
75 A = 6784702
92 meter
Y = 606861
32 meter E =
0011752
Z = 3532958
62 I = 51
84666
XDOT = 2166
755967 Wp = 115
87435
YDOT = -5807
917461 meter/sec RA = 145
33826 deg
ZDOT = 4512
259280 TA = 285
60926
MA = 285
73893
Ha = 221
624 n
mi
Hp = 215
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18890599
56 X = -5781374
56
Y = 1991014
84 feet Y = 542341
16 meter
Z = 11591071
59 Z = 3504931
21
XDOT = 7108
779420 XDOT = 2209
621870
YDOT = -19054
847314 feet/sec YDOT = -5783
448198 meter/sec
ZDOT = 14804
000263 ZDOT = 4522
888304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6715306
62 X = -2046825
46
Y = 17848719
06 feet Y = 5440289
57 meter
Z = 11467332
62 Z = 3495242
98
XDOT = -12591
937799 XDOT = -3838
022641
YDOT = -14314
894431 feet/sec YDOT = -4363
179823 meter/sec
ZDOT = 14851
792403 ZDOT = 4526
826324
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 17146
55696808
00016717 00000-0 10270-3 0 9003
2 25544 51
6360 146
1378 0005009 199
1516 160
9449 15
53939675 18385
Satellite: ISS
Catalog Number: 25544
Epoch time: 17146
55696808 = yrday
fracday
Element set: 900
Inclination: 51
6360 deg
RA of node: 146
1378 deg
Eccentricity:
0005009
Arg of perigee: 199
1516 deg
Mean anomaly: 160
9449 deg
Mean motion: 15
53939675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1838
Checksum: 342
Coasting Arc #2 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2017/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4955055
18 A = 6781094
76 meter
Y = 584068
58 meter E =
0007658
Z = -4598258
17 I = 51
86113
XDOT = -3550
007049 Wp = 98
87439
YDOT = 6061
268765 meter/sec RA = 140
36620 deg
ZDOT = -3061
062658 TA = 140
62752
MA = 140
57183
Ha = 221
578 n
mi
Hp = 215
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16256742
72 X = 4970492
04
Y = 1916235
51 feet Y = 639566
28 meter
Z = -15086148
85 Z = -4574150
20
XDOT = -11647
004755 XDOT = -3602
652590
YDOT = 19886
052380 feet/sec YDOT = 6021
276230 meter/sec
ZDOT = -10042
856491 ZDOT = -3078
434760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8800522
52 X = 2682399
26
Y = -13917608
68 feet Y = -4242087
12 meter
Z = -14979869
88 Z = -4565864
34
XDOT = 11904
682875 XDOT = 3628
547340
YDOT = 18401
044363 feet/sec YDOT = 5608
638322 meter/sec
ZDOT = -10120
457254 ZDOT = -3084
715371
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 17147
52162262
00016717 00000-0 10270-3 0 9014
2 25544 51
6365 141
3296 0004900 201
2244 158
8706 15
53923580 18535
Satellite: ISS
Catalog Number: 25544
Epoch time: 17147
52162262 = yrday
fracday
Element set: 901
Inclination: 51
6365 deg
RA of node: 141
3296 deg
Eccentricity:
0004900
Arg of perigee: 201
2244 deg
Mean anomaly: 158
8706 deg
Mean motion: 15
53923580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 293
Coasting Arc #3 (Orbit 1868)
---------------------------------------
Vector Time (GMT): 2017/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3934311
79 A = 6778560
25 meter
Y = -1851215
70 meter E =
0007004
Z = 5200389
88 I = 51
87763
XDOT = 4590
547865 Wp = 168
12638
YDOT = -5996
346449 meter/sec RA = 135
38843 deg
ZDOT = 1331
383230 TA = 269
08337
MA = 269
16362
Ha = 221
463 n
mi
Hp = 215
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12907847
08 X = -3938579
70
Y = -6073542
32 feet Y = -1895236
38 meter
Z = 17061646
59 Z = 5181267
49
XDOT = 15060
852577 XDOT = 4650
792158
YDOT = -19673
052654 feet/sec YDOT = -5944
675163 meter/sec
ZDOT = 4368
055215 ZDOT = 1353
828369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10947393
86 X = -3336765
65
Y = 9301476
08 feet Y = 2835089
91 meter
Z = 16977553
64 Z = 5174758
35
XDOT = -10934
953481 XDOT = -3332
973821
YDOT = -21067
375932 feet/sec YDOT = -6421
336184 meter/sec
ZDOT = 4468
052497 ZDOT = 1361
862401
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 17148
55058288
00016717 00000-0 10270-3 0 9021
2 25544 51
6369 136
2017 0004829 206
2859 153
8049 15
53924932 18694
Satellite: ISS
Catalog Number: 25544
Epoch time: 17148
55058288 = yrday
fracday
Element set: 902
Inclination: 51
6369 deg
RA of node: 136
2017 deg
Eccentricity:
0004829
Arg of perigee: 206
2859 deg
Mean anomaly: 153
8049 deg
Mean motion: 15
53924932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1869
Checksum: 339
Coasting Arc #4 (Orbit 1883)
---------------------------------------
Vector Time (GMT): 2017/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2777702
97 A = 6778045
59 meter
Y = 3170979
34 meter E =
0013345
Z = -5318637
98 I = 51
89838
XDOT = -5268
590960 Wp = 113
07523
YDOT = 5532
251310 meter/sec RA = 130
40803 deg
ZDOT = 542
760100 TA = 162
11512
MA = 162
06811
Ha = 221
242 n
mi
Hp = 215
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9113198
73 X = 2767873
19
Y = 10403475
53 feet Y = 3201987
16 meter
Z = -17449599
68 Z = -5305168
23
XDOT = -17285
403413 XDOT = -5332
698939
YDOT = 18150
430808 feet/sec YDOT = 5472
975846 meter/sec
ZDOT = 1780
708991 ZDOT = 517
011804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13230201
69 X = 4032565
48
Y = -4277626
32 feet Y = -1303820
50 meter
Z = -17390655
53 Z = -5300671
80
XDOT = 9372
816934 XDOT = 2856
834601
YDOT = 22161
495057 feet/sec YDOT = 6754
823693 meter/sec
ZDOT = 1666
186567 ZDOT = 507
853666
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 17149
51523002
00016717 00000-0 10270-3 0 9030
2 25544 51
6369 131
3945 0004791 210
0722 150
0156 15
53921794 18848
Satellite: ISS
Catalog Number: 25544
Epoch time: 17149
51523002 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 131
3945 deg
Eccentricity:
0004791
Arg of perigee: 210
0722 deg
Mean anomaly: 150
0156 deg
Mean motion: 15
53921794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1884
Checksum: 292
Coasting Arc #5 (Orbit 1899)
---------------------------------------
Vector Time (GMT): 2017/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1598457
32 A = 6779664
28 meter
Y = -4389435
09 meter E =
0002980
Z = 4910705
50 I = 51
92452
XDOT = 5599
210315 Wp = 99
28809
YDOT = -4680
363084 meter/sec RA = 125
43087 deg
ZDOT = -2360
226163 TA = 13
72719
MA = 13
71908
Ha = 221
127 n
mi
Hp = 215
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5244282
55 X = -1573108
51
Y = -14401033
76 feet Y = -4407168
88 meter
Z = 16111238
52 Z = 4903001
82
XDOT = 18370
112582 XDOT = 5662
596040
YDOT = -15355
521928 feet/sec YDOT = -4617
394276 meter/sec
ZDOT = -7743
524156 ZDOT = -2332
873437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15348839
32 X = -4678326
23
Y = -614270
90 feet Y = -187229
77 meter
Z = 16077937
75 Z = 4900555
43
XDOT = -7114
356982 XDOT = -2168
456008
YDOT = -21796
701782 feet/sec YDOT = -6643
634703 meter/sec
ZDOT = -7622
037084 ZDOT = -2323
196903
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 17150
54418471
00016717 00000-0 10270-3 0 9049
2 25544 51
6370 126
2668 0004840 215
2593 144
8240 15
53946216 19003
Satellite: ISS
Catalog Number: 25544
Epoch time: 17150
54418471 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 126
2668 deg
Eccentricity:
0004840
Arg of perigee: 215
2593 deg
Mean anomaly: 144
8240 deg
Mean motion: 15
53946216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1900
Checksum: 296
Coasting Arc #6 (Orbit 1914)
---------------------------------------
Vector Time (GMT): 2017/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 470419
41 A = 6783002
01 meter
Y = 5434765
59 meter E =
0006986
Z = -4038903
20 I = 51
95459
XDOT = -5600
051660 Wp = 147
60213
YDOT = 3422
816012 meter/sec RA = 120
46153 deg
ZDOT = 3950
923403 TA = 163
32065
MA = 163
29767
Ha = 220
929 n
mi
Hp = 216
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1543370
76 X = 429230
49
Y = 17830595
77 feet Y = 5439796
17 meter
Z = -13250994
74 Z = -4036717
64
XDOT = -18372
872900 XDOT = -5657
101931
YDOT = 11229
711327 feet/sec YDOT = 3359
873131 meter/sec
ZDOT = 12962
347124 ZDOT = 3923
581791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17169773
95 X = 5233347
10
Y = 5073792
10 feet Y = 1546491
83 meter
Z = -13242224
00 Z = -4036229
88
XDOT = 3985
707990 XDOT = 1214
843795
YDOT = 20048
761937 feet/sec YDOT = 6110
862638 meter/sec
ZDOT = 12841
095289 ZDOT = 3913
965844
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 17151
50882605
00016717 00000-0 10270-3 0 9051
2 25544 51
6379 121
4594 0004732 218
9063 141
1750 15
53932781 19153
Satellite: ISS
Catalog Number: 25544
Epoch time: 17151
50882605 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 121
4594 deg
Eccentricity:
0004732
Arg of perigee: 218
9063 deg
Mean anomaly: 141
1750 deg
Mean motion: 15
53932781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1915
Checksum: 308
Coasting Arc #7 (Orbit 1930)
---------------------------------------
Vector Time (GMT): 2017/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 551050
31 A = 6786585
62 meter
Y = -6167621
00 meter E =
0011587
Z = 2760532
19 I = 51
98233
XDOT = 5358
336285 Wp = 120
62719
YDOT = -1840
926657 meter/sec RA = 115
50272 deg
ZDOT = -5172
318829 TA = 28
25216
MA = 28
18936
Ha = 220
769 n
mi
Hp = 216
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1807907
86 X = 606567
98
Y = -20234977
04 feet Y = -6161148
56 meter
Z = 9056864
13 Z = 2763343
45
XDOT = 17579
843455 XDOT = 5403
648403
YDOT = -6039
785619 feet/sec YDOT = -1780
752401 meter/sec
ZDOT = -16969
549963 ZDOT = -5146
179708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18309752
47 X = -5580812
55
Y = -8788208
88 feet Y = -2678646
07 meter
Z = 9070279
13 Z = 2764621
08
XDOT = -38
956446 XDOT = -11
873925
YDOT = -17348
540670 feet/sec YDOT = -5287
835196 meter/sec
ZDOT = -16853
850670 ZDOT = -5137
053684
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 17152
53777331
00016717 00000-0 10270-3 0 9065
2 25544 51
6378 116
3312 0004672 223
7280 136
3503 15
53957509 19316
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
53777331 = yrday
fracday
Element set: 906
Inclination: 51
6378 deg
RA of node: 116
3312 deg
Eccentricity:
0004672
Arg of perigee: 223
7280 deg
Mean anomaly: 136
3503 deg
Mean motion: 15
53957509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1931
Checksum: 305
Coasting Arc #8 (Orbit 1936)
---------------------------------------
Vector Time (GMT): 2017/152/21:55:46
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1604232
45 A = 6781712
78 meter
Y = 4924157
09 meter E =
0008471
Z = -4386858
90 I = 51
97072
XDOT = -4975
174440 Wp = 143
65391
YDOT = 4695
086162 meter/sec RA = 113
44563 deg
ZDOT = 3447
524797 TA = 161
20574
MA = 161
17445
Ha = 220
831 n
mi
Hp = 216
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5263229
84 X = 1570359
28
Y = 16155371
04 feet Y = 4941907
59 meter
Z = -14392581
68 Z = -4379147
96
XDOT = -16322
750787 XDOT = -5044
052793
YDOT = 15403
825991 feet/sec YDOT = 4639
065046 meter/sec
ZDOT = 11310
776892 ZDOT = 3423
189875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14272848
20 X = -4350364
13
Y = -9270333
61 feet Y = -2825597
68 meter
Z = -14359342
89 Z = -4376727
71
XDOT = 2508
167244 XDOT = 764
489376
YDOT = -21230
425396 feet/sec YDOT = -6471
033661 meter/sec
ZDOT = 11202
572559 ZDOT = 3414
544116
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 17152
92362774
00016717 00000-0 10270-3 0 9070
2 25544 51
6367 114
4048 0004926 221
3045 138
7736 15
53959676 19371
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
92362774 = yrday
fracday
Element set: 907
Inclination: 51
6367 deg
RA of node: 114
4048 deg
Eccentricity:
0004926
Arg of perigee: 221
3045 deg
Mean anomaly: 138
7736 deg
Mean motion: 15
53959676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1937
Checksum: 335
Coasting Arc #9 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2017/153/10:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4573803
28 A = 6780298
84 meter
Y = 1562746
01 meter E =
0007641
Z = 4755189
05 I = 51
97319
XDOT = 422
056063 Wp = 153
95240
YDOT = -7146
134679 meter/sec RA = 110
83753 deg
ZDOT = 2746
111572 TA = 268
95947
MA = 269
04701
Ha = 220
686 n
mi
Hp = 216
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15005916
28 X = -4614036
86
Y = 5127119
45 feet Y = 1511373
39 meter
Z = 15601013
94 Z = 4732873
20
XDOT = 1384
698369 XDOT = 488
595323
YDOT = -23445
323751 feet/sec YDOT = -7141
043089 meter/sec
ZDOT = 9009
552402 ZDOT = 2748
322972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5263636
48 X = -1604356
40
Y = 15060925
39 feet Y = 4590570
06 meter
Z = 15502231
15 Z = 4725080
05
XDOT = -16556
044605 XDOT = -5046
282396
YDOT = -15099
351537 feet/sec YDOT = -4602
282348 meter/sec
ZDOT = 9020
489680 ZDOT = 2749
445254
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 17153
50240790
00016717 00000-0 10270-3 0 9089
2 25544 51
6371 111
5242 0004847 227
5420 132
5323 15
53978450 19462
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
50240790 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 111
5242 deg
Eccentricity:
0004847
Arg of perigee: 227
5420 deg
Mean anomaly: 132
5323 deg
Mean motion: 15
53978450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 295
Coasting Arc #10 (Orbit 1946)
---------------------------------------
Vector Time (GMT): 2017/153/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4299567
34 A = 6778289
10 meter
Y = 203656
36 meter E =
0010533
Z = -5245025
55 I = 51
96916
XDOT = -1761
058046 Wp = 95
42072
YDOT = 7364
677590 meter/sec RA = 110
33346 deg
ZDOT = -1160
620341 TA = 163
50704
MA = 163
47274
Ha = 220
648 n
mi
Hp = 216
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14106192
06 X = 4322448
33
Y = 668163
91 feet Y = 251865
29 meter
Z = -17208089
07 Z = -5224083
89
XDOT = -5777
749494 XDOT = -1837
643165
YDOT = 24162
328050 feet/sec YDOT = 7344
556104 meter/sec
ZDOT = -3807
809517 ZDOT = -1169
360619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1203739
03 X = 366899
66
Y = -14182895
15 feet Y = -4322946
44 meter
Z = -17115663
12 Z = -5216854
12
XDOT = 22892
971840 XDOT = 6977
777817
YDOT = 6574
403689 feet/sec YDOT = 2003
878244 meter/sec
ZDOT = -3847
609696 ZDOT = -1172
751435
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 17153
56671801
00016717 00000-0 10270-3 0 9097
2 25544 51
6387 111
2033 0004725 227
8497 132
2255 15
53963408 19475
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
56671801 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 111
2033 deg
Eccentricity:
0004725
Arg of perigee: 227
8497 deg
Mean anomaly: 132
2255 deg
Mean motion: 15
53963408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1947
Checksum: 316
Coasting Arc #11 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2017/154/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3784841
33 A = 6777933
76 meter
Y = -1873068
02 meter E =
0001858
Z = 5302409
19 I = 51
97931
XDOT = 2557
340529 Wp = 216
93782
YDOT = -7193
280997 meter/sec RA = 105
35913 deg
ZDOT = -717
169850 TA = 239
87134
MA = 239
88976
Ha = 220
522 n
mi
Hp = 216
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12417458
42 X = -3789371
60
Y = -6145236
28 feet Y = -1915418
34 meter
Z = 17396355
61 Z = 5284012
34
XDOT = 8390
224834 XDOT = 2641
071304
YDOT = -23600
003270 feet/sec YDOT = -7164
214870 meter/sec
ZDOT = -2352
919454 ZDOT = -704
544060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6400701
11 X = -1950933
70
Y = 12401490
79 feet Y = 3779974
39 meter
Z = 17315439
43 Z = 5277745
94
XDOT = -22517
591469 XDOT = -6863
361880
YDOT = -8423
377223 feet/sec YDOT = -2567
445378 meter/sec
ZDOT = -2295
975984 ZDOT = -699
813480
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 17154
59565808
00016717 00000-0 10270-3 0 9102
2 25544 51
6394 106
0760 0004789 233
4536 126
6176 15
53982864 19633
Satellite: ISS
Catalog Number: 25544
Epoch time: 17154
59565808 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 106
0760 deg
Eccentricity:
0004789
Arg of perigee: 233
4536 deg
Mean anomaly: 126
6176 deg
Mean motion: 15
53982864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 339
Coasting Arc #12 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2017/155/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3216964
32 A = 6779884
46 meter
Y = 3485419
14 meter E =
0009441
Z = -4853179
77 I = 51
99362
XDOT = -3200
015124 Wp = 130
65924
YDOT = 6483
276131 meter/sec RA = 100
38573 deg
ZDOT = 2532
193758 TA = 164
15900
MA = 164
12945
Ha = 220
296 n
mi
Hp = 216
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10554344
88 X = 3201324
98
Y = 11435102
17 feet Y = 3521306
31 meter
Z = -15922505
81 Z = -4837590
33
XDOT = -10498
737283 XDOT = -3284
575273
YDOT = 21270
590980 feet/sec YDOT = 6447
018411 meter/sec
ZDOT = 8307
722304 ZDOT = 2516
443978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11470003
61 X = 3496057
10
Y = -10619014
11 feet Y = -3236675
50 meter
Z = -15854258
27 Z = -4832377
92
XDOT = 20460
829276 XDOT = 6236
460763
YDOT = 9788
908911 feet/sec YDOT = 2983
659436 meter/sec
ZDOT = 8237
086298 ZDOT = 2510
663904
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 17155
56028628
00016717 00000-0 10270-3 0 9115
2 25544 51
6396 101
2676 0004645 236
3230 123
7480 15
53977566 19787
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
56028628 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 101
2676 deg
Eccentricity:
0004645
Arg of perigee: 236
3230 deg
Mean anomaly: 123
7480 deg
Mean motion: 15
53977566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 326
Coasting Arc #13 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2017/155/13:34:21
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3076852
59 A = 6786921
78 meter
Y = 5446303
12 meter E =
0009412
Z = 2624221
58 I = 52
01726
XDOT = -3366
036505 Wp = 86
97518
YDOT = -4445
160146 meter/sec RA = 100
34329 deg
ZDOT = 5263
118474 TA = 302
41861
MA = 302
50962
Ha = 220
325 n
mi
Hp = 216
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10094660
72 X = -3150273
22
Y = 17868448
56 feet Y = 5411484
97 meter
Z = 8609650
85 Z = 2609097
08
XDOT = -11043
426853 XDOT = -3341
645310
YDOT = -14583
858748 feet/sec YDOT = -4482
665439 meter/sec
ZDOT = 17267
449061 ZDOT = 5246
826063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18819204
96 X = 5736093
67
Y = 8257258
95 feet Y = 2516812
53 meter
Z = 8541950
36 Z = 2603586
47
XDOT = -12754
314313 XDOT = -3887
515003
YDOT = 11225
503170 feet/sec YDOT = 3421
533366 meter/sec
ZDOT = 17196
259350 ZDOT = 5241
419850
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 17155
62459499
00016717 00000-0 10270-3 0 9127
2 25544 51
6397 100
9474 0004641 236
5206 123
5503 15
53969023 19795
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
62459499 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 100
9474 deg
Eccentricity:
0004641
Arg of perigee: 236
5206 deg
Mean anomaly: 123
5503 deg
Mean motion: 15
53969023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 326
Coasting Arc #14 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2017/156/13:34:21
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3495260
65 A = 6783217
31 meter
Y = -4274415
17 meter E =
0002307
Z = -3941717
34 I = 52
01090
XDOT = 2643
545198 Wp = 101
18874
YDOT = 5923
957505 meter/sec RA = 95
38864 deg
ZDOT = -4082
292941 TA = 126
30592
MA = 126
28461
Ha = 220
210 n
mi
Hp = 216
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11467390
58 X = 3561945
68
Y = -14023671
82 feet Y = -4234955
61 meter
Z = -12932143
50 Z = -3924576
62
XDOT = 8673
048551 XDOT = 2596
935505
YDOT = 19435
556119 feet/sec YDOT = 5953
259150 meter/sec
ZDOT = -13393
349544 ZDOT = -4069
563966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15310025
40 X = -4666495
74
Y = -9784590
99 feet Y = -2982343
33 meter
Z = -12855724
61 Z = -3918424
86
XDOT = 17528
783098 XDOT = 5342
773088
YDOT = -9913
398578 feet/sec YDOT = -3021
603886 meter/sec
ZDOT = -13338
155728 ZDOT = -4065
469866
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 17156
58921983
00016717 00000-0 10270-3 0 9136
2 25544 51
6406 96
1403 0004633 240
6825 119
3865 15
53992189 19948
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
58921983 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 96
1403 deg
Eccentricity:
0004633
Arg of perigee: 240
6825 deg
Mean anomaly: 119
3865 deg
Mean motion: 15
53992189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
Checksum: 338
Coasting Arc #15 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2017/156/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1532447
34 A = 6789003
70 meter
Y = 6472525
31 meter E =
0008869
Z = 1338033
28 I = 52
02805
XDOT = -4410
234654 Wp = 59
05647
YDOT = -2258
735517 meter/sec RA = 94
28692 deg
ZDOT = 5851
060957 TA = 315
43118
MA = 315
50246
Ha = 220
122 n
mi
Hp = 216
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5027714
38 X = -1611210
52
Y = 21235319
25 feet Y = 6454947
94 meter
Z = 4389872
97 Z = 1330398
29
XDOT = -14469
273800 XDOT = -4413
071054
YDOT = -7410
549597 feet/sec YDOT = -2308
070119 meter/sec
ZDOT = 19196
394215 ZDOT = 5829
630037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6517015
93 X = 1986386
46
Y = -20833860
35 feet Y = -6350160
63 meter
Z = 4355048
39 Z = 1327418
75
XDOT = 12526
077670 XDOT = 3817
948474
YDOT = 7928
041498 feet/sec YDOT = 2416
467049 meter/sec
ZDOT = 19102
148968 ZDOT = 5822
335006
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 17156
84645078
00016717 00000-0 10270-3 0 9144
2 25544 51
6378 94
8564 0004930 241
0910 118
9748 15
53983973 19989
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
84645078 = yrday
fracday
Element set: 914
Inclination: 51
6378 deg
RA of node: 94
8564 deg
Eccentricity:
0004930
Arg of perigee: 241
0910 deg
Mean anomaly: 118
9748 deg
Mean motion: 15
53983973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1998
Checksum: 357
Coasting Arc #16 (Orbit 2012)
---------------------------------------
Vector Time (GMT): 2017/157/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2183051
30 A = 6786233
72 meter
Y = -5740583
97 meter E =
0004113
Z = -2880928
65 I = 52
02066
XDOT = 4022
528938 Wp = 183
81990
YDOT = 4083
207741 meter/sec RA = 89
33876 deg
ZDOT = -5091
728014 TA = 28
78026
MA = 28
75757
Ha = 220
012 n
mi
Hp = 216
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7162241
79 X = 2261076
09
Y = -18833936
91 feet Y = -5715735
05 meter
Z = -9451865
65 Z = -2870135
00
XDOT = 13197
273419 XDOT = 4001
303925
YDOT = 13396
350856 feet/sec YDOT = 4128
072237 meter/sec
ZDOT = -16705
144402 ZDOT = -5072
238676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8196966
10 X = -2498435
27
Y = 18432096
61 feet Y = 5618103
05 meter
Z = -9403202
25 Z = -2866096
05
XDOT = -11244
791324 XDOT = -3427
412396
YDOT = -13473
325084 feet/sec YDOT = -4106
669485 meter/sec
ZDOT = -16619
792794 ZDOT = -5065
712844
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 17157
81107198
00016717 00000-0 10270-3 0 9159
2 25544 51
6381 90
0483 0004837 245
6418 114
4230 15
53994713 20130
Satellite: ISS
Catalog Number: 25544
Epoch time: 17157
81107198 = yrday
fracday
Element set: 915
Inclination: 51
6381 deg
RA of node: 90
0483 deg
Eccentricity:
0004837
Arg of perigee: 245
6418 deg
Mean anomaly: 114
4230 deg
Mean motion: 15
53994713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2013
Checksum: 303
Coasting Arc #17 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2017/158/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2785278
72 A = 6782545
62 meter
Y = 4604995
12 meter E =
0007040
Z = 4125978
36 I = 52
00706
XDOT = -3562
791699 Wp = 126
75575
YDOT = -5600
840577 meter/sec RA = 84
38146 deg
ZDOT = 3837
376415 TA = 283
78065
MA = 283
85898
Ha = 219
864 n
mi
Hp = 216
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9138053
53 X = -2856608
21
Y = 15108251
70 feet Y = 4573448
92 meter
Z = 13536674
40 Z = 4112275
46
XDOT = -11688
949144 XDOT = -3518
537169
YDOT = -18375
461210 feet/sec YDOT = -5640
435145 meter/sec
ZDOT = 12589
817633 ZDOT = 3820
176065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9749518
43 X = 2971653
22
Y = -14777237
44 feet Y = -4504101
97 meter
Z = 13475347
47 Z = 4107285
91
XDOT = 10042
956506 XDOT = 3061
093143
YDOT = 18064
169694 feet/sec YDOT = 5505
958923 meter/sec
ZDOT = 12514
849623 ZDOT = 3814
526165
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 17158
83999600
00016717 00000-0 10270-3 0 9160
2 25544 51
6381 84
9195 0004941 248
9173 111
1451 15
54001951 20292
Satellite: ISS
Catalog Number: 25544
Epoch time: 17158
83999600 = yrday
fracday
Element set: 916
Inclination: 51
6381 deg
RA of node: 84
9195 deg
Eccentricity:
0004941
Arg of perigee: 248
9173 deg
Mean anomaly: 111
1451 deg
Mean motion: 15
54001951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 316
Coasting Arc #18 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2017/159/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3372174
45 A = 6779289
84 meter
Y = -3140303
69 meter E =
0007729
Z = -4979571
35 I = 51
99167
XDOT = 2998
165166 Wp = 76
36198
YDOT = 6700
337583 meter/sec RA = 79
41532 deg
ZDOT = -2196
200754 TA = 172
31111
MA = 172
29926
Ha = 219
861 n
mi
Hp = 216
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11063564
46 X = 3431228
11
Y = -10302833
64 feet Y = -3102262
90 meter
Z = -16337176
34 Z = -4963047
17
XDOT = 9836
499887 XDOT = 2933
685589
YDOT = 21982
734854 feet/sec YDOT = 6733
504863 meter/sec
ZDOT = -7205
383051 ZDOT = -2181
792147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11351773
11 X = -3460020
45
Y = 10103736
10 feet Y = 3079618
76 meter
Z = -16263638
40 Z = -4957156
99
XDOT = -8753
540216 XDOT = -2668
079058
YDOT = -21326
832334 feet/sec YDOT = -6500
418495 meter/sec
ZDOT = -7142
951926 ZDOT = -2177
171747
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 17159
80461051
00016717 00000-0 10270-3 0 9173
2 25544 51
6377 80
1122 0004701 250
1709 109
8937 15
54002244 20445
Satellite: ISS
Catalog Number: 25544
Epoch time: 17159
80461051 = yrday
fracday
Element set: 917
Inclination: 51
6377 deg
RA of node: 80
1122 deg
Eccentricity:
0004701
Arg of perigee: 250
1709 deg
Mean anomaly: 109
8937 deg
Mean motion: 15
54002244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 282
Coasting Arc #19 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2017/160/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3518509
29 A = 6778609
33 meter
Y = 2706084
80 meter E =
0004622
Z = 5124766
31 I = 51
99162
XDOT = -2834
072264 Wp = 186
46771
YDOT = -6917
433595 meter/sec RA = 77
97410 deg
ZDOT = 1702
577101 TA = 247
13780
MA = 247
18661
Ha = 219
804 n
mi
Hp = 216
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11543665
65 X = -3573401
80
Y = 8878230
98 feet Y = 2666430
83 meter
Z = 16813537
75 Z = 5107541
34
XDOT = -9298
137350 XDOT = -2764
779445
YDOT = -22694
992110 feet/sec YDOT = -6948
738903 meter/sec
ZDOT = 5585
882876 ZDOT = 1688
977264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11397591
53 X = -3473985
90
Y = -9205577
80 feet Y = -2805860
11 meter
Z = 16736979
97 Z = 5101431
49
XDOT = 19150
215507 XDOT = 5836
985687
YDOT = -13635
384516 feet/sec YDOT = -4156
065201 meter/sec
ZDOT = 5527
066452 ZDOT = 1684
649855
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 17160
12614616
00016717 00000-0 10270-3 0 9188
2 25544 51
6415 78
5113 0005020 251
0422 109
0187 15
54019416 20499
Satellite: ISS
Catalog Number: 25544
Epoch time: 17160
12614616 = yrday
fracday
Element set: 918
Inclination: 51
6415 deg
RA of node: 78
5113 deg
Eccentricity:
0005020
Arg of perigee: 251
0422 deg
Mean anomaly: 109
0187 deg
Mean motion: 15
54019416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 271
Coasting Arc #20 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2017/161/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4054689
62 A = 6777770
90 meter
Y = -1024012
36 meter E =
0010141
Z = -5342426
53 I = 51
98036
XDOT = 2102
288319 Wp = 99
08916
YDOT = 7364
701735 meter/sec RA = 72
99995 deg
ZDOT = 182
657335 TA = 172
65257
MA = 172
63770
Ha = 219
629 n
mi
Hp = 216
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13302787
47 X = 4091790
13
Y = -3359620
59 feet Y = -978461
86 meter
Z = -17527646
09 Z = -5322639
98
XDOT = 6897
271388 XDOT = 2018
890779
YDOT = 24162
407266 feet/sec YDOT = 7387
744616 meter/sec
ZDOT = 599
269472 ZDOT = 192
668187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6666692
50 X = 2032007
87
Y = 12118938
48 feet Y = 3693852
45 meter
Z = -17440072
36 Z = -5315734
05
XDOT = -20727
170912 XDOT = -6317
641694
YDOT = 12332
209205 feet/sec YDOT = 3758
857366 meter/sec
ZDOT = 642
140600 ZDOT = 195
724455
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 17161
09075509
00016717 00000-0 10270-3 0 9198
2 25544 51
6411 73
7041 0004996 255
7990 104
2608 15
53989585 20648
Satellite: ISS
Catalog Number: 25544
Epoch time: 17161
09075509 = yrday
fracday
Element set: 919
Inclination: 51
6411 deg
RA of node: 73
7041 deg
Eccentricity:
0004996
Arg of perigee: 255
7990 deg
Mean anomaly: 104
2608 deg
Mean motion: 15
53989585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 330
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