[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 16th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 67 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
There are no maneuvers
Coasting Arc #1 (Orbit 3909)
---------------------------------------
Vector Time (GMT): 2013/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4866432
31 A = 6800967
52 meter
Y = 4501372
29 meter E =
0016366
Z = 1474919
62 I = 51
47829
XDOT = -4267
086339 Wp = 135
57665
YDOT = -2716
468107 meter/sec RA = 327
43352 deg
ZDOT = -5761
197516 TA = 28
30667
MA = 28
21783
Ha = 228
363 n
mi
Hp = 221
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15965985
26 X = -4923570
67
Y = 14768281
79 feet Y = 4446633
20 meter
Z = 4838975
14 Z = 1451140
51
XDOT = -13999
627098 XDOT = -4208
406848
YDOT = -8912
296939 feet/sec YDOT = -2763
856930 meter/sec
ZDOT = -18901
566653 ZDOT = -5781
784179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19795423
41 X = 6033645
06
Y = 9061766
77 feet Y = 2762026
51 meter
Z = 4738787
58 Z = 1444382
46
XDOT = -2208
941765 XDOT = -673
285450
YDOT = 14802
614806 feet/sec YDOT = 4511
836993 meter/sec
ZDOT = -18987
259426 ZDOT = -5787
316673
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 13196
53509099
00016717 00000-0 10270-3 0 9007
2 25544 51
6493 327
8479 0005141 188
2461 171
8606 15
49833570 39108
Satellite: ISS
Catalog Number: 25544
Epoch time: 13196
53509099 = yrday
fracday
Element set: 900
Inclination: 51
6493 deg
RA of node: 327
8479 deg
Eccentricity:
0005141
Arg of perigee: 188
2461 deg
Mean anomaly: 171
8606 deg
Mean motion: 15
49833570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3910
Checksum: 329
Coasting Arc #2 (Orbit 3924)
---------------------------------------
Vector Time (GMT): 2013/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4667817
65 A = 6801196
50 meter
Y = -4796234
94 meter E =
0005248
Z = -1204987
75 I = 51
45496
XDOT = 4203
787749 Wp = 62
76127
YDOT = 2631
221845 meter/sec RA = 322
46986 deg
ZDOT = 5833
295215 TA = 284
14418
MA = 284
20249
Ha = 228
204 n
mi
Hp = 221
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15314362
37 X = 4726956
76
Y = -15735678
94 feet Y = -4743705
70 meter
Z = -3953371
87 Z = -1182168
65
XDOT = 13791
954557 XDOT = 4145
715909
YDOT = 8632
617602 feet/sec YDOT = 2677
906143 meter/sec
ZDOT = 19138
107661 ZDOT = 5853
575932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20570468
99 X = -6269878
95
Y = -7729719
72 feet Y = -2356018
57 meter
Z = -3857158
86 Z = -1175662
02
XDOT = 1854
041283 XDOT = 565
111783
YDOT = -14489
231059 feet/sec YDOT = -4416
317627 meter/sec
ZDOT = 19222
532604 ZDOT = 5859
027938
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 13197
50228680
00016717 00000-0 10270-3 0 9010
2 25544 51
6504 323
0581 0004995 191
7505 168
3530 15
49853087 39255
Satellite: ISS
Catalog Number: 25544
Epoch time: 13197
50228680 = yrday
fracday
Element set: 901
Inclination: 51
6504 deg
RA of node: 323
0581 deg
Eccentricity:
0004995
Arg of perigee: 191
7505 deg
Mean anomaly: 168
3530 deg
Mean motion: 15
49853087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3925
Checksum: 319
Coasting Arc #3 (Orbit 3940)
---------------------------------------
Vector Time (GMT): 2013/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4452632
90 A = 6801434
07 meter
Y = 5049662
77 meter E =
0015809
Z = 897162
96 I = 51
43187
XDOT = -4140
879556 Wp = 142
66389
YDOT = -2594
266233 meter/sec RA = 317
50456 deg
ZDOT = -5907
010824 TA = 27
60959
MA = 27
52572
Ha = 228
057 n
mi
Hp = 221
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14608375
66 X = -4513126
56
Y = 16567135
06 feet Y = 4999532
29 meter
Z = 2943448
03 Z = 875386
01
XDOT = -13585
562849 XDOT = -4082
867529
YDOT = -8511
372155 feet/sec YDOT = -2640
247272 meter/sec
ZDOT = -19379
956773 ZDOT = -5926
986144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21158806
41 X = 6449204
19
Y = 6380597
10 feet Y = 1944805
99 meter
Z = 2851557
83 Z = 869154
83
XDOT = -1653
590763 XDOT = -504
014465
YDOT = 14246
041085 feet/sec YDOT = 4342
193323 meter/sec
ZDOT = -19463
109925 ZDOT = -5932
355905
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 13198
53395272
00016717 00000-0 10270-3 0 9027
2 25544 51
6501 317
9485 0005021 195
8877 164
2116 15
49866031 39411
Satellite: ISS
Catalog Number: 25544
Epoch time: 13198
53395272 = yrday
fracday
Element set: 902
Inclination: 51
6501 deg
RA of node: 317
9485 deg
Eccentricity:
0005021
Arg of perigee: 195
8877 deg
Mean anomaly: 164
2116 deg
Mean motion: 15
49866031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 322
Coasting Arc #4 (Orbit 3955)
---------------------------------------
Vector Time (GMT): 2013/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4207725
78 A = 6801561
05 meter
Y = -5306232
60 meter E =
0006550
Z = -610295
12 I = 51
41129
XDOT = 4087
764890 Wp = 56
22429
YDOT = 2563
305746 meter/sec RA = 312
53747 deg
ZDOT = 5946
347709 TA = 297
18193
MA = 297
24869
Ha = 227
909 n
mi
Hp = 221
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13804874
62 X = 4269713
14
Y = -17408899
60 feet Y = -5258832
49 meter
Z = -2002280
56 Z = -589704
43
XDOT = 13411
302132 XDOT = 4029
911971
YDOT = 8409
795756 feet/sec YDOT = 2608
693593 meter/sec
ZDOT = 19509
014792 ZDOT = 5966
065408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21673962
57 X = -6606223
79
Y = -4921828
30 feet Y = -1500173
27 meter
Z = -1915314
26 Z = -583787
79
XDOT = 1472
265341 XDOT = 448
746476
YDOT = -14040
811769 feet/sec YDOT = -4279
639427 meter/sec
ZDOT = 19591
097031 ZDOT = 5971
366375
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 13199
50112985
00016717 00000-0 10270-3 0 9034
2 25544 51
6509 313
1584 0004821 199
7543 160
3422 15
49878809 39566
Satellite: ISS
Catalog Number: 25544
Epoch time: 13199
50112985 = yrday
fracday
Element set: 903
Inclination: 51
6509 deg
RA of node: 313
1584 deg
Eccentricity:
0004821
Arg of perigee: 199
7543 deg
Mean anomaly: 160
3422 deg
Mean motion: 15
49878809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3956
Checksum: 334
Coasting Arc #5 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2013/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3953127
39 A = 6801638
69 meter
Y = 5516312
18 meter E =
0014847
Z = 288185
13 I = 51
39154
XDOT = -4042
392019 Wp = 149
85501
YDOT = -2578
060464 meter/sec RA = 307
56955 deg
ZDOT = -5980
932299 TA = 27
03270
MA = 26
95545
Ha = 227
752 n
mi
Hp = 221
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12969578
05 X = -4015918
10
Y = 18098137
09 feet Y = 5471754
70 meter
Z = 945489
28 Z = 268829
49
XDOT = -13262
441006 XDOT = -3984
209585
YDOT = -8458
203623 feet/sec YDOT = -2622
938987 meter/sec
ZDOT = -19622
481295 ZDOT = -6000
428752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21994144
85 X = 6703815
35
Y = 3486854
97 feet Y = 1062793
40 meter
Z = 863658
23 Z = 263243
03
XDOT = -1418
250165 XDOT = -432
282650
YDOT = 13934
648884 feet/sec YDOT = 4247
280980 meter/sec
ZDOT = -19703
639955 ZDOT = -6005
669458
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 13200
53277619
00016717 00000-0 10270-3 0 9047
2 25544 51
6509 308
0491 0004892 203
5390 156
5537 15
49894754 39727
Satellite: ISS
Catalog Number: 25544
Epoch time: 13200
53277619 = yrday
fracday
Element set: 904
Inclination: 51
6509 deg
RA of node: 308
0491 deg
Eccentricity:
0004892
Arg of perigee: 203
5390 deg
Mean anomaly: 156
5537 deg
Mean motion: 15
49894754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 328
Coasting Arc #6 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2013/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3670934
95 A = 6801626
54 meter
Y = -5722402
81 meter E =
0007843
Z = 11958
75 I = 51
37440
XDOT = 4015
564998 Wp = 56
40022
YDOT = 2594
430714 meter/sec RA = 302
59974 deg
ZDOT = 5983
226902 TA = 303
72878
MA = 303
80350
Ha = 227
611 n
mi
Hp = 221
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12043749
85 X = 3734593
18
Y = -18774287
45 feet Y = -5680996
17 meter
Z = 39234
76 Z = 29945
50
XDOT = 13174
425846 XDOT = 3957
190510
YDOT = 8511
911791 feet/sec YDOT = 2639
008137 meter/sec
ZDOT = 19630
009520 ZDOT = 6002
592478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22217955
02 X = -6772032
69
Y = -1968878
87 feet Y = -600114
28 meter
Z = 115368
17 Z = 35164
22
XDOT = 1349
826310 XDOT = 411
427059
YDOT = -13891
657431 feet/sec YDOT = -4234
177185 meter/sec
ZDOT = 19710
624710 ZDOT = 6007
798412
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 13201
56441257
00016717 00000-0 10270-3 0 9053
2 25544 51
6516 302
9395 0004670 208
0175 152
0724 15
49906621 39889
Satellite: ISS
Catalog Number: 25544
Epoch time: 13201
56441257 = yrday
fracday
Element set: 905
Inclination: 51
6516 deg
RA of node: 302
9395 deg
Eccentricity:
0004670
Arg of perigee: 208
0175 deg
Mean anomaly: 152
0724 deg
Mean motion: 15
49906621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 306
Coasting Arc #7 (Orbit 4002)
---------------------------------------
Vector Time (GMT): 2013/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3387527
36 A = 6801534
83 meter
Y = 5878439
52 meter E =
0013442
Z = -344049
54 I = 51
35796
XDOT = -4003
261847 Wp = 157
05706
YDOT = -2651
246236 meter/sec RA = 297
62972 deg
ZDOT = -5974
137319 TA = 26
66067
MA = 26
59162
Ha = 227
447 n
mi
Hp = 222
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11113934
92 X = -3451338
31
Y = 19286218
89 feet Y = 5840201
30 meter
Z = -1128771
47 Z = -360659
84
XDOT = -13134
061178 XDOT = -3944
297271
YDOT = -8698
314421 feet/sec YDOT = -2695
682830 meter/sec
ZDOT = -19600
188055 ZDOT = -5993
441569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22249594
06 X = 6781676
27
Y = 519116
49 feet Y = 158226
71 meter
Z = -1199164
64 Z = -365505
38
XDOT = -1371
391990 XDOT = -418
000279
YDOT = 13966
688180 feet/sec YDOT = 4257
046557 meter/sec
ZDOT = -19680
546336 ZDOT = -5998
630523
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 13202
53156251
00016717 00000-0 10270-3 0 9069
2 25544 51
6510 298
1501 0004756 211
3170 148
7698 15
49920480 40035
Satellite: ISS
Catalog Number: 25544
Epoch time: 13202
53156251 = yrday
fracday
Element set: 906
Inclination: 51
6510 deg
RA of node: 298
1501 deg
Eccentricity:
0004756
Arg of perigee: 211
3170 deg
Mean anomaly: 148
7698 deg
Mean motion: 15
49920480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4003
Checksum: 288
Coasting Arc #8 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2013/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3080824
45 A = 6801353
88 meter
Y = -6024226
96 meter E =
0008873
Z = 653071
37 I = 51
34455
XDOT = 4016
157921 Wp = 60
34123
YDOT = 2703
481329 meter/sec RA = 292
65768 deg
ZDOT = 5935
488299 TA = 306
72546
MA = 306
80692
Ha = 227
308 n
mi
Hp = 222
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10107691
77 X = 3144787
32
Y = -19764524
16 feet Y = -5989417
67 meter
Z = 2142622
62 Z = 668192
17
XDOT = 13176
371132 XDOT = 3956
796155
YDOT = 8869
689399 feet/sec YDOT = 2748
060039 meter/sec
ZDOT = 19473
386809 ZDOT = 5954
854096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22171192
02 X = -6757779
33
Y = 980291
18 feet Y = 298792
75 meter
Z = 2206797
11 Z = 672631
76
XDOT = 1340
112673 XDOT = 408
466343
YDOT = -14116
415189 feet/sec YDOT = -4302
683350 meter/sec
ZDOT = 19554
003951 ZDOT = 5960
060404
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 13203
56317991
00016717 00000-0 10270-3 0 9074
2 25544 51
6515 293
0405 0004554 216
1842 143
9001 15
49935391 40191
Satellite: ISS
Catalog Number: 25544
Epoch time: 13203
56317991 = yrday
fracday
Element set: 907
Inclination: 51
6515 deg
RA of node: 293
0405 deg
Eccentricity:
0004554
Arg of perigee: 216
1842 deg
Mean anomaly: 143
9001 deg
Mean motion: 15
49935391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 299
Coasting Arc #9 (Orbit 4033)
---------------------------------------
Vector Time (GMT): 2013/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2782525
14 A = 6801082
90 meter
Y = 6118545
63 meter E =
0011566
Z = -990010
61 I = 51
33157
XDOT = -4048
942381 Wp = 164
05634
YDOT = -2788
157135 meter/sec RA = 287
68551 deg
ZDOT = -5878
939043 TA = 26
69993
MA = 26
64042
Ha = 227
133 n
mi
Hp = 222
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9129019
50 X = -2845928
16
Y = 20073968
60 feet Y = 6087075
24 meter
Z = -3248066
31 Z = -1003681
09
XDOT = -13283
931697 XDOT = -3988
906065
YDOT = -9147
497163 feet/sec YDOT = -2833
098851 meter/sec
ZDOT = -19287
857752 ZDOT = -5898
462358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21916155
37 X = 6680044
16
Y = -2367379
83 feet Y = -721577
37 meter
Z = -3306175
04 Z = -1007722
15
XDOT = -1354
327391 XDOT = -412
798989
YDOT = 14389
387090 feet/sec YDOT = 4385
885185 meter/sec
ZDOT = -19369
130471 ZDOT = -5903
710967
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 13204
53031256
00016717 00000-0 10270-3 0 9080
2 25544 51
6502 288
2509 0004598 219
4555 140
6262 15
49947196 40349
Satellite: ISS
Catalog Number: 25544
Epoch time: 13204
53031256 = yrday
fracday
Element set: 908
Inclination: 51
6502 deg
RA of node: 288
2509 deg
Eccentricity:
0004598
Arg of perigee: 219
4555 deg
Mean anomaly: 140
6262 deg
Mean motion: 15
49947196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4034
Checksum: 313
Coasting Arc #10 (Orbit 4049)
---------------------------------------
Vector Time (GMT): 2013/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2467105
17 A = 6800730
43 meter
Y = -6197749
24 meter E =
0009543
Z = 1302782
57 I = 51
32229
XDOT = 4110
981696 Wp = 66
53778
YDOT = 2861
114937 meter/sec RA = 282
71131 deg
ZDOT = 5796
013666 TA = 307
67524
MA = 307
76176
Ha = 227
001 n
mi
Hp = 222
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8094177
07 X = 2529897
97
Y = -20333822
96 feet Y = -6169809
48 meter
Z = 4274221
03 Z = 1314919
49
XDOT = 13487
472756 XDOT = 4050
527730
YDOT = 9386
860028 feet/sec YDOT = 2906
748235 meter/sec
ZDOT = 19015
792869 ZDOT = 5815
837293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21548639
35 X = -6568025
27
Y = 3767181
14 feet Y = 1148236
81 meter
Z = 4325911
74 Z = 1318537
90
XDOT = 1277
761061 XDOT = 389
461571
YDOT = -14734
276527 feet/sec YDOT = -4491
007485 meter/sec
ZDOT = 19098
319703 ZDOT = 5821
167845
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 13205
56191133
00016717 00000-0 10270-3 0 9096
2 25544 51
6504 283
1409 0004444 224
4979 135
5815 15
49963671 40501
Satellite: ISS
Catalog Number: 25544
Epoch time: 13205
56191133 = yrday
fracday
Element set: 909
Inclination: 51
6504 deg
RA of node: 283
1409 deg
Eccentricity:
0004444
Arg of perigee: 224
4979 deg
Mean anomaly: 135
5815 deg
Mean motion: 15
49963671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4050
Checksum: 311
Coasting Arc #11 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2013/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2170246
37 A = 6800267
88 meter
Y = 6226761
75 meter E =
0009240
Z = -1638724
30 I = 51
31374
XDOT = -4195
919540 Wp = 170
35644
YDOT = -2956
101643 meter/sec RA = 277
73686 deg
ZDOT = -5689
219457 TA = 27
64080
MA = 27
59171
Ha = 226
815 n
mi
Hp = 222
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7120230
89 X = -2231753
76
Y = 20429008
35 feet Y = 6202148
82 meter
Z = -5376392
05 Z = -1649416
16
XDOT = -13766
140224 XDOT = -4134
915779
YDOT = -9698
496204 feet/sec YDOT = -3002
681811 meter/sec
ZDOT = -18665
418166 ZDOT = -5709
454369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21033232
84 X = 6410929
37
Y = -5015216
02 feet Y = -1528637
84 meter
Z = -5422027
85 Z = -1652634
09
XDOT = -1199
752448 XDOT = -365
684546
YDOT = 15191
062446 feet/sec YDOT = 4630
235834 meter/sec
ZDOT = -18749
659304 ZDOT = -5714
896156
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 13206
52902708
00016717 00000-0 10270-3 0 9103
2 25544 51
6490 278
3506 0004409 227
9417 132
1359 15
49977890 40655
Satellite: ISS
Catalog Number: 25544
Epoch time: 13206
52902708 = yrday
fracday
Element set: 910
Inclination: 51
6490 deg
RA of node: 278
3506 deg
Eccentricity:
0004409
Arg of perigee: 227
9417 deg
Mean anomaly: 132
1359 deg
Mean motion: 15
49977890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4065
Checksum: 322
Coasting Arc #12 (Orbit 4080)
---------------------------------------
Vector Time (GMT): 2013/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1863766
25 A = 6799767
62 meter
Y = -6237669
53 meter E =
0009829
Z = 1949255
25 I = 51
30906
XDOT = 4311
468701 Wp = 74
27725
YDOT = 3032
068537 meter/sec RA = 272
76093 deg
ZDOT = 5559
447713 TA = 307
28359
MA = 307
37316
Ha = 226
705 n
mi
Hp = 222
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6114718
66 X = 1923909
90
Y = -20464795
04 feet Y = -6216491
47 meter
Z = 6395194
38 Z = 1958455
07
XDOT = 14145
238520 XDOT = 4250
237151
YDOT = 9947
731421 feet/sec YDOT = 3079
939633 meter/sec
ZDOT = 18239
657852 ZDOT = 5580
243441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20414739
60 X = -6222412
63
Y = 6239451
11 feet Y = 1901784
70 meter
Z = 6434577
55 Z = 1961259
24
XDOT = 998
097737 XDOT = 304
220190
YDOT = -15703
895288 feet/sec YDOT = -4786
547284 meter/sec
ZDOT = 18326
240993 ZDOT = 5585
838255
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 13207
56060789
00016717 00000-0 10270-3 0 9113
2 25544 51
6491 273
2401 0004296 232
8466 127
2292 15
49989277 40818
Satellite: ISS
Catalog Number: 25544
Epoch time: 13207
56060789 = yrday
fracday
Element set: 911
Inclination: 51
6491 deg
RA of node: 273
2401 deg
Eccentricity:
0004296
Arg of perigee: 232
8466 deg
Mean anomaly: 127
2292 deg
Mean motion: 15
49989277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4081
Checksum: 325
Coasting Arc #13 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2013/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1585839
61 A = 6799112
56 meter
Y = 6202648
77 meter E =
0006559
Z = -2277728
23 I = 51
30608
XDOT = -4449
755679 Wp = 174
74877
YDOT = -3118
136353 meter/sec RA = 267
78477 deg
ZDOT = -5400
785098 TA = 30
68459
MA = 30
64625
Ha = 226
518 n
mi
Hp = 222
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5202885
86 X = -1644016
66
Y = 20349897
53 feet Y = 6184589
66 meter
Z = -7472861
66 Z = -2285573
19
XDOT = -14598
935955 XDOT = -4388
322055
YDOT = -10230
106144 feet/sec YDOT = -3167
552736 meter/sec
ZDOT = -17719
111215 ZDOT = -5422
252189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19689216
50 X = 6001273
19
Y = -7281366
50 feet Y = -2219360
51 meter
Z = -7506561
66 Z = -2287999
99
XDOT = -752
005025 XDOT = -229
211132
YDOT = 16300
064135 feet/sec YDOT = 4968
259548 meter/sec
ZDOT = -17808
497320 ZDOT = -5428
029983
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 13208
52770706
00016717 00000-0 10270-3 0 9128
2 25544 51
6486 268
4491 0004209 236
6091 123
4657 15
50011556 40964
Satellite: ISS
Catalog Number: 25544
Epoch time: 13208
52770706 = yrday
fracday
Element set: 912
Inclination: 51
6486 deg
RA of node: 268
4491 deg
Eccentricity:
0004209
Arg of perigee: 236
6091 deg
Mean anomaly: 123
4657 deg
Mean motion: 15
50011556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4096
Checksum: 306
Coasting Arc #14 (Orbit 4111)
---------------------------------------
Vector Time (GMT): 2013/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1306445
57 A = 6798496
67 meter
Y = -6148763
54 meter E =
0009714
Z = 2579290
32 I = 51
30600
XDOT = 4617
384432 Wp = 83
18050
YDOT = 3178
473892 meter/sec RA = 262
80802 deg
ZDOT = 5222
519378 TA = 305
92161
MA = 306
01172
Ha = 226
442 n
mi
Hp = 222
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4286238
75 X = 1362575
91
Y = -20173108
71 feet Y = -6133840
26 meter
Z = 8462238
58 Z = 2585773
02
XDOT = 15148
899056 XDOT = 4556
129529
YDOT = 10428
063951 feet/sec YDOT = 3229
765771 meter/sec
ZDOT = 17134
249927 ZDOT = 5244
801303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18881212
15 X = -5754993
46
Y = 8267500
78 feet Y = 2519934
24 meter
Z = 8490223
68 Z = 2587820
18
XDOT = 358
463181 XDOT = 109
259578
YDOT = -16925
767049 feet/sec YDOT = -5158
973796 meter/sec
ZDOT = 17227
043523 ZDOT = 5250
802866
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 13209
55927066
00016717 00000-0 10270-3 0 9136
2 25544 51
6485 263
3385 0004099 241
2321 118
8418 15
50012880 41127
Satellite: ISS
Catalog Number: 25544
Epoch time: 13209
55927066 = yrday
fracday
Element set: 913
Inclination: 51
6485 deg
RA of node: 263
3385 deg
Eccentricity:
0004099
Arg of perigee: 241
2321 deg
Mean anomaly: 118
8418 deg
Mean motion: 15
50012880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4112
Checksum: 297
Coasting Arc #15 (Orbit 4126)
---------------------------------------
Vector Time (GMT): 2013/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1064615
42 A = 6797676
68 meter
Y = 6056182
99 meter E =
0003705
Z = -2893378
30 I = 51
30893
XDOT = -4803
983138 Wp = 172
48615
YDOT = -3236
739632 meter/sec RA = 257
83120 deg
ZDOT = -5011
592638 TA = 40
57130
MA = 40
54369
Ha = 226
269 n
mi
Hp = 222
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3492832
73 X = -1118202
71
Y = 19869366
77 feet Y = 6043978
28 meter
Z = -9492710
97 Z = -2898679
99
XDOT = -15761
099533 XDOT = -4743
087407
YDOT = -10619
224516 feet/sec YDOT = -3290
120130 meter/sec
ZDOT = -16442
233064 ZDOT = -5034
781979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18016363
86 X = 5491387
70
Y = -9053429
84 feet Y = -2759485
41 meter
Z = -9515735
36 Z = -2900396
14
XDOT = 111
936768 XDOT = 34
118327
YDOT = 17591
208704 feet/sec YDOT = 5361
800413 meter/sec
ZDOT = -16538
823132 ZDOT = -5041
033291
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 13210
52635339
00016717 00000-0 10270-3 0 9145
2 25544 51
6490 258
5474 0004033 245
3127 114
7604 15
50044447 41277
Satellite: ISS
Catalog Number: 25544
Epoch time: 13210
52635339 = yrday
fracday
Element set: 914
Inclination: 51
6490 deg
RA of node: 258
5474 deg
Eccentricity:
0004033
Arg of perigee: 245
3127 deg
Mean anomaly: 114
7604 deg
Mean motion: 15
50044447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4127
Checksum: 286
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