[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 27th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17270 6943 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
299/11:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 212
8
300/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 212
8
303/19:34:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 212
5
306/03:16:27
095 0
6 1
1 1
1
N/A 1
0 -0
1 222
6
000/00:02:54
191 -0
1 0
0 213
3
307/06:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2017/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1105698
58 A = 6781213
55 meter
Y = 5136228
49 meter E =
0011639
Z = -4297134
41 I = 51
96094
XDOT = -5344
292208 Wp = 88
13770
YDOT = 4148
368608 meter/sec RA = 117
63605 deg
ZDOT = 3592
017410 TA = 218
36298
MA = 218
44581
Ha = 222
451 n
mi
Hp = 213
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3627620
02 X = 1069055
64
Y = 16851143
35 feet Y = 5148388
12 meter
Z = -14098210
02 Z = -4291852
34
XDOT = -17533
767088 XDOT = -5407
731883
YDOT = 13610
133229 feet/sec YDOT = 4088
250513 meter/sec
ZDOT = 11784
834022 ZDOT = 3565
901571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11916824
91 X = -3632248
23
Y = -12479977
41 feet Y = -3803897
11 meter
Z = -14075497
60 Z = -4290211
67
XDOT = 7092
528347 XDOT = 2161
802640
YDOT = -19900
191161 feet/sec YDOT = -6065
578266 meter/sec
ZDOT = 11668
370521 ZDOT = 3556
519335
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 17296
50960565
00016717 00000-0 10270-3 0 9008
2 25544 51
6361 118
6222 0005032 48
5662 311
5922 15
54239099 1705
Satellite: ISS
Catalog Number: 25544
Epoch time: 17296
50960565 = yrday
fracday
Element set: 900
Inclination: 51
6361 deg
RA of node: 118
6222 deg
Eccentricity:
0005032
Arg of perigee: 48
5662 deg
Mean anomaly: 311
5922 deg
Mean motion: 15
54239099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 170
Checksum: 297
Coasting Arc #2 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2017/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -11754
71 A = 6785109
60 meter
Y = -6074753
40 meter E =
0016960
Z = 3009876
98 I = 51
98870
XDOT = 5267
105289 Wp = 84
57998
YDOT = -2494
267407 meter/sec RA = 112
67342 deg
ZDOT = -4987
903775 TA = 61
12276
MA = 60
95269
Ha = 222
421 n
mi
Hp = 212
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -38565
32 X = 41554
82
Y = -19930293
30 feet Y = -6074586
69 meter
Z = 9874924
48 Z = 3009949
54
XDOT = 17280
529165 XDOT = 5318
834762
YDOT = -8183
292017 feet/sec YDOT = -2435
077946 meter/sec
ZDOT = -16364
513698 ZDOT = -4962
191478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10711369
06 X = 3264825
29
Y = 16806578
65 feet Y = 5122645
17 meter
Z = 9876117
60 Z = 3010240
65
XDOT = -9122
478320 XDOT = -2780
531392
YDOT = 15412
557690 feet/sec YDOT = 4697
747584 meter/sec
ZDOT = -16250
058296 ZDOT = -4953
017769
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 17297
53836297
00016717 00000-0 10270-3 0 9017
2 25544 51
6364 113
4924 0004999 50
3199 309
8388 15
54258969 1867
Satellite: ISS
Catalog Number: 25544
Epoch time: 17297
53836297 = yrday
fracday
Element set: 901
Inclination: 51
6364 deg
RA of node: 113
4924 deg
Eccentricity:
0004999
Arg of perigee: 50
3199 deg
Mean anomaly: 309
8388 deg
Mean motion: 15
54258969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 186
Checksum: 358
Coasting Arc #3 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2017/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -917171
92 A = 6788092
93 meter
Y = 6565258
85 meter E =
0013357
Z = -1440174
78 I = 52
00986
XDOT = -4957
196062 Wp = 45
10953
YDOT = 575
324166 meter/sec RA = 107
72182 deg
ZDOT = 5821
740225 TA = 299
26325
MA = 299
39671
Ha = 222
536 n
mi
Hp = 212
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3009094
24 X = -983522
42
Y = 21539563
17 feet Y = 6554631
39 meter
Z = -4724982
87 Z = -1444791
52
XDOT = -16263
766609 XDOT = -4991
540834
YDOT = 1887
546475 feet/sec YDOT = 519
697514 meter/sec
ZDOT = 19100
197588 ZDOT = 5797
575747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9301840
33 X = -2835200
93
Y = -19654009
46 feet Y = -5990542
08 meter
Z = -4746427
21 Z = -1446711
01
XDOT = 11246
113085 XDOT = 3427
815268
YDOT = -9876
146468 feet/sec YDOT = -3010
249444 meter/sec
ZDOT = 18992
875550 ZDOT = 5789
028468
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 17298
50282162
00016717 00000-0 10270-3 0 9022
2 25544 51
6360 108
6837 0005092 57
2089 302
9554 15
54246946 2010
Satellite: ISS
Catalog Number: 25544
Epoch time: 17298
50282162 = yrday
fracday
Element set: 902
Inclination: 51
6360 deg
RA of node: 108
6837 deg
Eccentricity:
0005092
Arg of perigee: 57
2089 deg
Mean anomaly: 302
9554 deg
Mean motion: 15
54246946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 306
Coasting Arc #4 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2017/299/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -711269
26 A = 6788503
35 meter
Y = 6667493
05 meter E =
0014519
Z = -1024060
43 I = 52
02055
XDOT = -4842
161177 Wp = 45
58802
YDOT = 385
449338 meter/sec RA = 102
93693 deg
ZDOT = 5934
302571 TA = 303
36967
MA = 303
50853
Ha = 222
527 n
mi
Hp = 212
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2333560
55 X = -780799
60
Y = 21874977
20 feet Y = 6659150
36 meter
Z = -3359778
31 Z = -1027684
64
XDOT = -15886
355568 XDOT = -4874
937985
YDOT = 1264
597565 feet/sec YDOT = 331
117845 meter/sec
ZDOT = 19469
496624 ZDOT = 5910
700777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5922134
22 X = -1805066
51
Y = -21184274
15 feet Y = -6456966
76 meter
Z = -3376847
26 Z = -1029263
05
XDOT = 12872
128640 XDOT = 3923
424809
YDOT = -6653
222998 feet/sec YDOT = -2027
902370 meter/sec
ZDOT = 19364
690890 ZDOT = 5902
357783
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 17299
46727333
00016717 00000-0 10270-3 0 9033
2 25544 51
6365 103
8755 0005061 58
8506 301
3142 15
54256990 2160
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
46727333 = yrday
fracday
Element set: 903
Inclination: 51
6365 deg
RA of node: 103
8755 deg
Eccentricity:
0005061
Arg of perigee: 58
8506 deg
Mean anomaly: 301
3142 deg
Mean motion: 15
54256990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 307
Coasting Arc #5 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2017/300/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1528989
93 A = 6788535
41 meter
Y = -6566523
67 meter E =
0012451
Z = -770181
42 I = 52
02823
XDOT = 4470
514863 Wp = 115
44113
YDOT = 1733
016030 meter/sec RA = 97
99237 deg
ZDOT = -5980
904584 TA = 72
83663
MA = 72
70033
Ha = 222
531 n
mi
Hp = 212
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5016371
15 X = 1606046
14
Y = -21543712
84 feet Y = -6548994
64 meter
Z = -2526841
92 Z = -762566
60
XDOT = 14667
043514 XDOT = 4479
856358
YDOT = 5685
748130 feet/sec YDOT = 1783
060461 meter/sec
ZDOT = -19622
390367 ZDOT = -5959
165189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3646588
01 X = 1111480
03
Y = 21821377
00 feet Y = 6651155
71 meter
Z = -2492062
27 Z = -759580
58
XDOT = -14252
254048 XDOT = -4344
087034
YDOT = 182
279042 feet/sec YDOT = 55
558652 meter/sec
ZDOT = -19526
159961 ZDOT = -5951
573556
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 17300
49601500
00016717 00000-0 10270-3 0 9047
2 25544 51
6372 98
7455 0005298 60
2011 299
9668 15
54315830 2329
Satellite: ISS
Catalog Number: 25544
Epoch time: 17300
49601500 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 98
7455 deg
Eccentricity:
0005298
Arg of perigee: 60
2011 deg
Mean anomaly: 299
9668 deg
Mean motion: 15
54315830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 300
Coasting Arc #6 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2017/300/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 532138
00 A = 6787868
90 meter
Y = 6561967
76 meter E =
0012677
Z = -1637962
04 I = 52
02931
XDOT = -4730
185369 Wp = 47
07194
YDOT = 1811
254290 meter/sec RA = 96
56045 deg
ZDOT = 5755
913380 TA = 295
09371
MA = 295
22522
Ha = 222
582 n
mi
Hp = 212
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1745859
59 X = 466677
33
Y = 21528765
63 feet Y = 6567552
44 meter
Z = -5373891
21 Z = -1635536
21
XDOT = -15518
980870 XDOT = -4778
047612
YDOT = 5942
435335 feet/sec YDOT = 1758
090670 meter/sec
ZDOT = 18884
230250 ZDOT = 5732
818921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16512515
53 X = -5033014
73
Y = 13927586
06 feet Y = 4245128
23 meter
Z = -5364108
44 Z = -1634980
25
XDOT = -12893
687319 XDOT = -3929
995895
YDOT = -8099
316258 feet/sec YDOT = -2468
671595 meter/sec
ZDOT = 18781
453040 ZDOT = 5724
586887
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 17300
75320002
00016717 00000-0 10270-3 0 9052
2 25544 51
6399 97
4658 0005061 61
3360 298
8301 15
54239149 2360
Satellite: ISS
Catalog Number: 25544
Epoch time: 17300
75320002 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 97
4658 deg
Eccentricity:
0005061
Arg of perigee: 61
3360 deg
Mean anomaly: 298
8301 deg
Mean motion: 15
54239149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 296
Coasting Arc #7 (Orbit 251)
---------------------------------------
Vector Time (GMT): 2017/301/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 302386
57 A = 6788864
77 meter
Y = -6776493
41 meter E =
0014529
Z = -142397
83 I = 52
03508
XDOT = 4707
819870 Wp = 116
22575
YDOT = 326
929345 meter/sec RA = 91
61643 deg
ZDOT = -6042
762485 TA = 65
29973
MA = 65
14854
Ha = 222
585 n
mi
Hp = 212
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 992081
92 X = 378832
36
Y = -22232589
94 feet Y = -6772684
49 meter
Z = -467184
47 Z = -140742
96
XDOT = 15445
603249 XDOT = 4733
167395
YDOT = 1072
602837 feet/sec YDOT = 379
716895 meter/sec
ZDOT = -19825
336237 ZDOT = -6019
831448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18484932
31 X = 5634207
37
Y = -12393034
87 feet Y = -3777397
03 meter
Z = -458810
67 Z = -139845
49
XDOT = 7477
555254 XDOT = 2279
158841
YDOT = 11823
806601 feet/sec YDOT = 3603
896252 meter/sec
ZDOT = -19723
601022 ZDOT = -6011
753591
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 17301
78193642
00016717 00000-0 10270-3 0 9065
2 25544 51
6392 92
3367 0005184 66
8735 293
2963 15
54284740 2524
Satellite: ISS
Catalog Number: 25544
Epoch time: 17301
78193642 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 92
3367 deg
Eccentricity:
0005184
Arg of perigee: 66
8735 deg
Mean anomaly: 293
2963 deg
Mean motion: 15
54284740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 252
Checksum: 323
Coasting Arc #8 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2017/302/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1076792
21 A = 6787496
76 meter
Y = 6430037
88 meter E =
0019192
Z = 1855824
45 I = 52
03007
XDOT = -4572
745040 Wp = 67
11763
YDOT = -2413
449427 meter/sec RA = 86
67102 deg
ZDOT = 5669
720711 TA = 313
20385
MA = 313
36400
Ha = 222
674 n
mi
Hp = 212
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3532782
84 X = -1157629
41
Y = 21095924
80 feet Y = 6417544
56 meter
Z = 6088662
88 Z = 1850396
95
XDOT = -15002
444357 XDOT = -4572
958500
YDOT = -7918
141164 feet/sec YDOT = -2464
585876 meter/sec
ZDOT = 18601
445902 ZDOT = 5647
506998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18931372
80 X = -5770282
43
Y = 9971282
82 feet Y = 3039247
00 meter
Z = 6063584
46 Z = 1848180
54
XDOT = -2166
369284 XDOT = -660
309358
YDOT = -15443
382665 feet/sec YDOT = -4707
143036 meter/sec
ZDOT = 18503
212601 ZDOT = 5639
779201
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 17302
81066781
00016717 00000-0 10270-3 0 9074
2 25544 51
6391 87
2071 0005240 69
6553 290
5162 15
54262680 2687
Satellite: ISS
Catalog Number: 25544
Epoch time: 17302
81066781 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 87
2071 deg
Eccentricity:
0005240
Arg of perigee: 69
6553 deg
Mean anomaly: 290
5162 deg
Mean motion: 15
54262680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 305
Coasting Arc #9 (Orbit 282)
---------------------------------------
Vector Time (GMT): 2017/303/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1887851
34 A = 6783934
30 meter
Y = -5554272
76 meter E =
0010051
Z = -3417164
80 I = 52
01631
XDOT = 4295
727520 Wp = 81
27672
YDOT = 4313
659694 meter/sec RA = 81
71816 deg
ZDOT = -4648
376289 TA = 138
41084
MA = 138
33434
Ha = 222
653 n
mi
Hp = 212
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6193738
00 X = 1966419
59
Y = -18222679
66 feet Y = -5532722
44 meter
Z = -11211170
61 Z = -3407802
84
XDOT = 14093
594227 XDOT = 4269
751678
YDOT = 14152
426819 feet/sec YDOT = 4361
551903 meter/sec
ZDOT = -15250
578377 ZDOT = -4627
572001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18177542
05 X = 5540514
82
Y = -6399588
55 feet Y = -1950594
59 meter
Z = -11168752
04 Z = -3404235
62
XDOT = -2749
833613 XDOT = -838
149285
YDOT = 18586
670893 feet/sec YDOT = 5665
217288 meter/sec
ZDOT = -15158
899364 ZDOT = -4620
432526
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 17303
77509677
00016717 00000-0 10270-3 0 9087
2 25544 51
6398 82
3977 0005320 73
1491 287
0245 15
54295164 2838
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
77509677 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 82
3977 deg
Eccentricity:
0005320
Arg of perigee: 73
1491 deg
Mean anomaly: 287
0245 deg
Mean motion: 15
54295164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 283
Checksum: 329
Coasting Arc #10 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2017/303/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2336307
20 A = 6782352
19 meter
Y = -5026435
61 meter E =
0011885
Z = -3921083
99 I = 52
01183
XDOT = 4012
487711 Wp = 73
49426
YDOT = 5065
319939 meter/sec RA = 81
39362 deg
ZDOT = -4109
471459 TA = 153
62398
MA = 153
56343
Ha = 222
658 n
mi
Hp = 212
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7665049
87 X = 2411387
54
Y = -16490930
48 feet Y = -4999889
89 meter
Z = -12864448
79 Z = -3909552
04
XDOT = 13164
329760 XDOT = 3975
509876
YDOT = 16618
503738 feet/sec YDOT = 5109
983284 meter/sec
ZDOT = -13482
517911 ZDOT = -4090
069859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14572724
26 X = 4441766
36
Y = -10939556
94 feet Y = -3334376
96 meter
Z = -12812479
14 Z = -3905243
64
XDOT = 3125
249484 XDOT = 952
576043
YDOT = 19827
009983 feet/sec YDOT = 6043
272643 meter/sec
ZDOT = -13397
182510 ZDOT = -4083
461229
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 17303
83939133
00016717 00000-0 10270-3 0 9099
2 25544 51
6407 82
0777 0005397 72
9879 287
1865 15
54307816 2843
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
83939133 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 82
0777 deg
Eccentricity:
0005397
Arg of perigee: 72
9879 deg
Mean anomaly: 287
1865 deg
Mean motion: 15
54307816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 346
Coasting Arc #11 (Orbit 299)
---------------------------------------
Vector Time (GMT): 2017/304/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3063734
57 A = 6778776
18 meter
Y = 3559093
86 meter E =
0011571
Z = 4879648
10 I = 51
99202
XDOT = -3504
292415 Wp = 101
02597
YDOT = -6376
621854 meter/sec RA = 76
42572 deg
ZDOT = 2443
699754 TA = 325
10324
MA = 325
17905
Ha = 222
833 n
mi
Hp = 212
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10051622
62 X = -3127009
03
Y = 11676817
12 feet Y = 3524479
66 meter
Z = 16009344
15 Z = 4864611
17
XDOT = -11497
022360 XDOT = -3444
597416
YDOT = -20920
675374 feet/sec YDOT = -6415
475288 meter/sec
ZDOT = 8017
387645 ZDOT = 2426
822110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14346339
62 X = -4372764
32
Y = 5806568
79 feet Y = 1769842
17 meter
Z = 15942037
94 Z = 4859133
16
XDOT = -390
043277 XDOT = -118
885191
YDOT = -22836
356925 feet/sec YDOT = -6960
521591 meter/sec
ZDOT = 7943
471972 ZDOT = 2421
170257
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 17304
86811122
00016717 00000-0 10270-3 0 9102
2 25544 51
6388 76
9479 0005517 76
5551 283
6217 15
54304255 3008
Satellite: ISS
Catalog Number: 25544
Epoch time: 17304
86811122 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 76
9479 deg
Eccentricity:
0005517
Arg of perigee: 76
5551 deg
Mean anomaly: 283
6217 deg
Mean motion: 15
54304255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 300
Checksum: 304
Coasting Arc #12 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2017/305/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3777849
67 A = 6776950
20 meter
Y = -1846579
64 meter E =
0020017
Z = -5331892
03 I = 51
97796
XDOT = 2788
072095 Wp = 84
39184
YDOT = 7111
368368 meter/sec RA = 71
44983 deg
ZDOT = -487
073078 TA = 180
97274
MA = 180
97664
Ha = 222
655 n
mi
Hp = 212
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12394519
92 X = 3824118
19
Y = -6058332
16 feet Y = -1804074
83 meter
Z = -17493084
09 Z = -5313427
44
XDOT = 9147
218161 XDOT = 2710
709677
YDOT = 23331
261051 feet/sec YDOT = 7142
113901 meter/sec
ZDOT = -1598
008785 ZDOT = -473
717574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13899556
85 X = 4236584
93
Y = 28780
24 feet Y = 8772
22 meter
Z = -17410829
82 Z = -5306820
93
XDOT = -1979
861003 XDOT = -603
461634
YDOT = 23971
896972 feet/sec YDOT = 7306
634197 meter/sec
ZDOT = -1539
859062 ZDOT = -469
349042
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 17305
83253157
00016717 00000-0 10270-3 0 9119
2 25544 51
6397 72
1395 0005285 79
5291 280
6457 15
54295030 3158
Satellite: ISS
Catalog Number: 25544
Epoch time: 17305
83253157 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 72
1395 deg
Eccentricity:
0005285
Arg of perigee: 79
5291 deg
Mean anomaly: 280
6457 deg
Mean motion: 15
54295030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 311
Coasting Arc #13 (Orbit 319)
---------------------------------------
Vector Time (GMT): 2017/306/03:17:54
191
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3808592
84 A = 6777413
85 meter
Y = -1748642
92 meter E =
0019087
Z = -5342809
61 I = 51
97615
XDOT = 2848
092229 Wp = 85
23120
YDOT = 7098
731162 meter/sec RA = 69
85204 deg
ZDOT = -292
445260 TA = 181
98505
MA = 181
99264
Ha = 222
569 n
mi
Hp = 213
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12495383
34 X = 3853816
99
Y = -5737017
44 feet Y = -1705800
13 meter
Z = -17528902
91 Z = -5324198
20
XDOT = 9344
134610 XDOT = 2769
921235
YDOT = 23289
800400 feet/sec YDOT = 7130
143374 meter/sec
ZDOT = -959
466075 ZDOT = -278
800111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5782981
08 X = -1762652
63
Y = -12589845
50 feet Y = -3837384
91 meter
Z = -17446011
90 Z = -5317544
43
XDOT = 22338
481988 XDOT = 6808
769310
YDOT = -9010
749886 feet/sec YDOT = -2746
476565 meter/sec
ZDOT = -900
034375 ZDOT = -274
330477
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 17306
15400530
00016717 00000-0 10270-3 0 9125
2 25544 51
6414 70
5372 0004313 76
9171 283
2463 15
54118829 3206
Satellite: ISS
Catalog Number: 25544
Epoch time: 17306
15400530 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 70
5372 deg
Eccentricity:
0004313
Arg of perigee: 76
9171 deg
Mean anomaly: 283
2463 deg
Mean motion: 15
54118829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 320
Checksum: 275
Coasting Arc #14 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2017/307/03:17:54
191
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4416635
70 A = 6778165
98 meter
Y = 42525
69 meter E =
0009098
Z = 5135266
88 I = 51
96743
XDOT = -1978
320941 Wp = 65
77825
YDOT = -7231
838508 meter/sec RA = 64
87524 deg
ZDOT = -1635
676734 TA = 39
95572
MA = 39
88880
Ha = 222
653 n
mi
Hp = 213
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14490274
59 X = -4441728
33
Y = 139519
99 feet Y = -7004
18 meter
Z = 16847988
45 Z = 5113750
64
XDOT = -6490
554267 XDOT = -1889
360002
YDOT = -23726
504291 feet/sec YDOT = -7253
464119 meter/sec
ZDOT = -5366
393484 ZDOT = -1645
070632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 443605
81 X = 135211
05
Y = 14594516
12 feet Y = 4448408
51 meter
Z = 16752478
96 Z = 5106155
59
XDOT = -22523
767040 XDOT = -6865
244194
YDOT = 6913
388242 feet/sec YDOT = 2107
200736 meter/sec
ZDOT = -5406
914763 ZDOT = -1648
027620
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 17307
18285180
00016717 00000-0 10270-3 0 9132
2 25544 51
6420 65
4084 0004252 79
2514 280
9117 15
54155495 3362
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
18285180 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 65
4084 deg
Eccentricity:
0004252
Arg of perigee: 79
2514 deg
Mean anomaly: 280
9117 deg
Mean motion: 15
54155495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 298
Coasting Arc #15 (Orbit 337)
---------------------------------------
Vector Time (GMT): 2017/307/06:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 552733
06 A = 6786068
57 meter
Y = 6159091
05 meter E =
0017596
Z = 2775321
91 I = 51
98984
XDOT = -5366
453130 Wp = 79
37566
YDOT = -1855
045612 meter/sec RA = 64
33739 deg
ZDOT = 5161
063326 TA = 311
93504
MA = 312
08490
Ha = 222
527 n
mi
Hp = 213
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1813428
69 X = 470337
82
Y = 20206991
63 feet Y = 6164811
53 meter
Z = 9105386
83 Z = 2777806
55
XDOT = -17606
473523 XDOT = -5370
381339
YDOT = -6086
107652 feet/sec YDOT = -1915
078663 meter/sec
ZDOT = 16932
622459 ZDOT = 5134
984524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13628762
64 X = 4154046
85
Y = -15022821
96 feet Y = -4578956
13 meter
Z = 9115412
94 Z = 2778377
86
XDOT = 6485
577690 XDOT = 1976
804080
YDOT = 16136
634358 feet/sec YDOT = 4918
446152 meter/sec
ZDOT = 16817
170437 ZDOT = 5125
873549
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 17307
31145697
00016717 00000-0 10270-3 0 9146
2 25544 51
6398 64
7658 0004163 79
7619 280
4003 15
54125028 3387
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
31145697 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 64
7658 deg
Eccentricity:
0004163
Arg of perigee: 79
7619 deg
Mean anomaly: 280
4003 deg
Mean motion: 15
54125028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 338
Checksum: 317
Coasting Arc #16 (Orbit 352)
---------------------------------------
Vector Time (GMT): 2017/308/06:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 535465
71 A = 6782280
75 meter
Y = -5387625
20 meter E =
0011537
Z = -4096575
27 I = 51
96078
XDOT = 5598
819165 Wp = 75
51264
YDOT = 3500
969189 meter/sec RA = 59
37780 deg
ZDOT = -3878
799197 TA = 154
49359
MA = 154
43662
Ha = 222
571 n
mi
Hp = 213
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1756777
26 X = 615571
58
Y = -17675935
69 feet Y = -5381189
46 meter
Z = -13440207
56 Z = -4093779
34
XDOT = 18368
829283 XDOT = 5578
096189
YDOT = 11486
119388 feet/sec YDOT = 3563
463038 meter/sec
ZDOT = -12725
719151 ZDOT = -3851
651413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14033395
09 X = -4277378
82
Y = 10906243
52 feet Y = 3324223
02 meter
Z = -13426906
67 Z = -4092521
15
XDOT = -3690
934760 XDOT = -1124
996915
YDOT = -20242
985818 feet/sec YDOT = -6170
062077 meter/sec
ZDOT = -12605
802069 ZDOT = -3842
248471
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 17308
27599763
00016717 00000-0 10270-3 0 9150
2 25544 51
6385 59
9578 0004246 83
7114 276
4522 15
54114880 3539
Satellite: ISS
Catalog Number: 25544
Epoch time: 17308
27599763 = yrday
fracday
Element set: 915
Inclination: 51
6385 deg
RA of node: 59
9578 deg
Eccentricity:
0004246
Arg of perigee: 83
7114 deg
Mean anomaly: 276
4522 deg
Mean motion: 15
54114880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 333
Coasting Arc #17 (Orbit 368)
---------------------------------------
Vector Time (GMT): 2017/309/06:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1704989
19 A = 6779038
03 meter
Y = 4289131
69 meter E =
0010123
Z = 4957826
37 I = 51
93290
XDOT = -5568
586099 Wp = 108
00554
YDOT = -4789
971228 meter/sec RA = 54
40674 deg
ZDOT = 2222
124399 TA = 320
37757
MA = 320
45151
Ha = 222
683 n
mi
Hp = 213
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5593796
56 X = -1776908
15
Y = 14071954
36 feet Y = 4269663
21 meter
Z = 16265834
53 Z = 4949369
10
XDOT = -18269
639433 XDOT = -5525
403824
YDOT = -15715
128702 feet/sec YDOT = -4852
001513 meter/sec
ZDOT = 7290
434380 ZDOT = 2195
177955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14003055
20 X = 4268131
23
Y = -5870949
45 feet Y = -1789465
39 meter
Z = 16227576
22 Z = 4946165
23
XDOT = 1326
978144 XDOT = 404
462938
YDOT = 23049
250342 feet/sec YDOT = 7025
411504 meter/sec
ZDOT = 7171
638297 ZDOT = 2185
915353
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 17309
30483647
00016717 00000-0 10270-3 0 9169
2 25544 51
6393 54
8289 0004247 86
9386 273
2253 15
54091295 3695
Satellite: ISS
Catalog Number: 25544
Epoch time: 17309
30483647 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 54
8289 deg
Eccentricity:
0004247
Arg of perigee: 86
9386 deg
Mean anomaly: 273
2253 deg
Mean motion: 15
54091295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 369
Checksum: 338
Coasting Arc #18 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2017/310/06:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2946558
48 A = 6777356
28 meter
Y = -2990919
23 meter E =
0019160
Z = -5336749
65 I = 51
90704
XDOT = 5159
566294 Wp = 88
25213
YDOT = 5645
180234 meter/sec RA = 49
42632 deg
ZDOT = -315
452950 TA = 178
74857
MA = 178
74377
Ha = 222
566 n
mi
Hp = 213
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9667186
62 X = 3005708
81
Y = -9812727
12 feet Y = -2957637
95 meter
Z = -17509021
15 Z = -5322292
16
XDOT = 16927
710939 XDOT = 5097
589267
YDOT = 18520
932525 feet/sec YDOT = 5702
531499 meter/sec
ZDOT = -1034
950625 ZDOT = -290
539065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13854959
03 X = -4222991
51
Y = 212096
91 feet Y = 64647
14 meter
Z = -17444341
70 Z = -5317035
35
XDOT = 794
844966 XDOT = 242
268746
YDOT = -24073
136902 feet/sec YDOT = -7337
492128 meter/sec
ZDOT = -925
333770 ZDOT = -282
041733
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 17310
26936466
00016717 00000-0 10270-3 0 9179
2 25544 51
6385 50
0197 0004334 91
1983 268
9666 15
54139373 3846
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
26936466 = yrday
fracday
Element set: 917
Inclination: 51
6385 deg
RA of node: 50
0197 deg
Eccentricity:
0004334
Arg of perigee: 91
1983 deg
Mean anomaly: 268
9666 deg
Mean motion: 15
54139373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 329
Coasting Arc #19 (Orbit 399)
---------------------------------------
Vector Time (GMT): 2017/311/06:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4121361
75 A = 6778274
35 meter
Y = 1597082
64 meter E =
0008782
Z = 5132319
00 I = 51
88747
XDOT = -4385
411218 Wp = 73
05735
YDOT = -6084
887992 meter/sec RA = 44
44480 deg
ZDOT = -1623
290274 TA = 32
56522
MA = 32
51108
Ha = 222
725 n
mi
Hp = 213
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13521528
04 X = -4163845
33
Y = 5239772
45 feet Y = 1550757
04 meter
Z = 16838316
94 Z = 5112195
09
XDOT = -14387
832080 XDOT = -4309
157101
YDOT = -19963
543282 feet/sec YDOT = -6133
502235 meter/sec
ZDOT = -5325
755492 ZDOT = -1644
408755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13521952
52 X = 4121491
13
Y = 5518423
64 feet Y = 1682015
52 meter
Z = 16748720
95 Z = 5105010
15
XDOT = -2814
789885 XDOT = -857
947957
YDOT = 23390
316636 feet/sec YDOT = 7129
368511 meter/sec
ZDOT = -5418
439374 ZDOT = -1651
540321
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 17311
29819064
00016717 00000-0 10270-3 0 9188
2 25544 51
6381 44
8912 0004293 95
4077 264
7565 15
54119586 4008
Satellite: ISS
Catalog Number: 25544
Epoch time: 17311
29819064 = yrday
fracday
Element set: 918
Inclination: 51
6381 deg
RA of node: 44
8912 deg
Eccentricity:
0004293
Arg of perigee: 95
4077 deg
Mean anomaly: 264
7565 deg
Mean motion: 15
54119586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 400
Checksum: 320
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