[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 11th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
345/16:37:50
609 1
9 3
1 3
1
N/A -2
4 -0
3 226
4
000/00:07:41
217 0
4 0
2 221
0
347/15:02:13
571 1
5 3
4 3
4
N/A -3
0 -0
3 226
3
000/00:08:27
142 0
4 0
2 222
9
Coasting Arc #1 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2013/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3657595
13 A = 6787204
45 meter
Y = -2350883
56 meter E =
0015436
Z = -5225272
27 I = 51
39825
XDOT = 5125
273707 Wp = 83
58825
YDOT = -5578
070193 meter/sec RA = 319
10742 deg
ZDOT = -1079
055987 TA = 176
02186
MA = 176
00958
Ha = 226
561 n
mi
Hp = 219
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11999984
04 X = -3605652
17
Y = -7712872
56 feet Y = -2391494
51 meter
Z = -17143281
73 Z = -5242914
49
XDOT = 16815
202452 XDOT = 5192
509776
YDOT = -18300
755228 feet/sec YDOT = -5520
380143 meter/sec
ZDOT = -3540
209930 ZDOT = -1053
994679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10093039
47 X = 3076358
43
Y = -9954058
61 feet Y = -3033997
06 meter
Z = -17217067
11 Z = -5247762
05
XDOT = 13522
841766 XDOT = 4121
762170
YDOT = 19644
996473 feet/sec YDOT = 5987
794925 meter/sec
ZDOT = -3433
855384 ZDOT = -1046
639121
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 13343
51793326
00016717 00000-0 10270-3 0 9007
2 25544 51
6476 319
6121 0001263 107
0836 253
0453 15
50876426 21909
Satellite: ISS
Catalog Number: 25544
Epoch time: 13343
51793326 = yrday
fracday
Element set: 900
Inclination: 51
6476 deg
RA of node: 319
6121 deg
Eccentricity:
0001263
Arg of perigee: 107
0836 deg
Mean anomaly: 253
0453 deg
Mean motion: 15
50876426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 290
Coasting Arc #2 (Orbit 2205)
---------------------------------------
Vector Time (GMT): 2013/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3317948
96 A = 6786757
03 meter
Y = 2650979
76 meter E =
0003723
Z = 5290667
86 I = 51
37423
XDOT = -5122
214034 Wp = 105
57062
YDOT = 5692
783628 meter/sec RA = 314
12459 deg
ZDOT = 358
647414 TA = 340
98942
MA = 341
00331
Ha = 226
355 n
mi
Hp = 219
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10885659
32 X = 3262357
75
Y = 8697440
14 feet Y = 2687772
17 meter
Z = 17357834
20 Z = 5306651
31
XDOT = -16805
164154 XDOT = -5187
233528
YDOT = 18677
111642 feet/sec YDOT = 5635
140211 meter/sec
ZDOT = 1176
664744 ZDOT = 333
606279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10664017
52 X = -3250392
54
Y = 8837406
99 feet Y = 2693641
65 meter
Z = 17424592
39 Z = 5311015
76
XDOT = -14326
337122 XDOT = -4366
667555
YDOT = -19405
600104 feet/sec YDOT = -5914
826912 meter/sec
ZDOT = 1070
383502 ZDOT = 326
252891
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 13344
54890564
00016717 00000-0 10270-3 0 9014
2 25544 51
6475 314
4982 0001163 108
4867 251
6410 15
50912873 22066
Satellite: ISS
Catalog Number: 25544
Epoch time: 13344
54890564 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 314
4982 deg
Eccentricity:
0001163
Arg of perigee: 108
4867 deg
Mean anomaly: 251
6410 deg
Mean motion: 15
50912873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2206
Checksum: 304
Coasting Arc #3 (Orbit 2220)
---------------------------------------
Vector Time (GMT): 2013/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3011119
97 A = 6786713
42 meter
Y = -3011604
92 meter E =
0015895
Z = -5298056
79 I = 51
35361
XDOT = 5057
006144 Wp = 94
29119
YDOT = -5729
437380 meter/sec RA = 309
13886 deg
ZDOT = 382
527680 TA = 179
37986
MA = 179
37789
Ha = 226
427 n
mi
Hp = 219
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9879002
53 X = -2951483
00
Y = -9880593
56 feet Y = -3044943
52 meter
Z = -17382076
08 Z = -5312539
92
XDOT = 16591
227507 XDOT = 5118
839902
YDOT = -18797
366733 feet/sec YDOT = -5672
540998 meter/sec
ZDOT = 1255
012074 ZDOT = 407
244330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11491207
12 X = 3502519
93
Y = -7814729
76 feet Y = -2381929
63 meter
Z = -17442463
89 Z = -5316462
99
XDOT = 14905
510631 XDOT = 4543
199640
YDOT = 18881
287484 feet/sec YDOT = 5755
016425 meter/sec
ZDOT = 1359
928502 ZDOT = 414
506208
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 13345
51542191
00016717 00000-0 10270-3 0 9023
2 25544 51
6476 309
7030 0001190 111
8542 248
2736 15
50940034 22216
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
51542191 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 309
7030 deg
Eccentricity:
0001190
Arg of perigee: 111
8542 deg
Mean anomaly: 248
2736 deg
Mean motion: 15
50940034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2221
Checksum: 273
Coasting Arc #4 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2013/345/16:41:41
217
Vector Time (MET): N/A
Weight (LBS) : 901651
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1999791
92 A = 6789270
36 meter
Y = -4039463
26 meter E =
0011923
Z = -5087997
47 I = 51
35634
XDOT = 5604
312019 Wp = 105
44150
YDOT = -4924
269163 meter/sec RA = 308
15446 deg
ZDOT = 1706
996326 TA = 181
15022
MA = 181
15296
Ha = 226
355 n
mi
Hp = 221
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6560997
11 X = -1929756
79
Y = -13252832
20 feet Y = -4061434
40 meter
Z = -16692905
10 Z = -5097542
42
XDOT = 18386
850457 XDOT = 5650
667563
YDOT = -16155
738725 feet/sec YDOT = -4861
339058 meter/sec
ZDOT = 5600
381648 ZDOT = 1734
334199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 994788
28 X = 303211
47
Y = -14709728
90 feet Y = -4483525
37 meter
Z = -16732351
80 Z = -5100020
83
XDOT = 22884
577182 XDOT = 6975
219125
YDOT = -4953
622104 feet/sec YDOT = -1509
864017 meter/sec
ZDOT = 5716
181803 ZDOT = 1742
292214
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 13345
70872326
00016717 00000-0 10270-3 0 9031
2 25544 51
6511 308
7446 0001469 261
2377 98
8607 15
50388299 22249
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
70872326 = yrday
fracday
Element set: 903
Inclination: 51
6511 deg
RA of node: 308
7446 deg
Eccentricity:
0001469
Arg of perigee: 261
2377 deg
Mean anomaly: 98
8607 deg
Mean motion: 15
50388299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 324
Coasting Arc #5 (Orbit 2239)
---------------------------------------
Vector Time (GMT): 2013/346/16:41:41
217
Vector Time (MET): N/A
Weight (LBS) : 901651
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1916950
41 A = 6789755
67 meter
Y = 4263642
47 meter E =
0005229
Z = 4921892
06 I = 51
34013
XDOT = -5380
457896 Wp = 49
47166
YDOT = 4986
176294 meter/sec RA = 303
17437 deg
ZDOT = -2218
886198 TA = 62
31826
MA = 62
26521
Ha = 226
152 n
mi
Hp = 221
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6289207
38 X = 1845221
48
Y = 13988328
30 feet Y = 4284677
70 meter
Z = 16147939
82 Z = 4931030
53
XDOT = -17652
420917 XDOT = -5425
035676
YDOT = 16358
846110 feet/sec YDOT = 4925
759459 meter/sec
ZDOT = -7279
810360 ZDOT = -2245
132253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1331624
08 X = -405879
02
Y = 15239265
73 feet Y = 4644928
19 meter
Z = 16185641
05 Z = 4933383
39
XDOT = -22204
022916 XDOT = -6767
786185
YDOT = 5926
815559 feet/sec YDOT = 1806
493382 meter/sec
ZDOT = -7391
026026 ZDOT = -2252
784733
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 13346
74003436
00016717 00000-0 10270-3 0 9045
2 25544 51
6510 303
6326 0001554 267
5950 92
5023 15
50451266 22406
Satellite: ISS
Catalog Number: 25544
Epoch time: 13346
74003436 = yrday
fracday
Element set: 904
Inclination: 51
6510 deg
RA of node: 303
6326 deg
Eccentricity:
0001554
Arg of perigee: 267
5950 deg
Mean anomaly: 92
5023 deg
Mean motion: 15
50451266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2240
Checksum: 275
Coasting Arc #6 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2013/347/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2575120
62 A = 6791095
33 meter
Y = -3740327
69 meter E =
0009076
Z = -5057805
90 I = 51
32282
XDOT = 4755
569569 Wp = 109
07534
YDOT = -5718
830640 meter/sec RA = 298
52700 deg
ZDOT = 1807
686356 TA = 178
53465
MA = 178
53199
Ha = 226
285 n
mi
Hp = 222
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8448558
48 X = -2508534
36
Y = -12271416
31 feet Y = -3768751
68 meter
Z = -16593851
38 Z = -5070154
26
XDOT = 15602
262365 XDOT = 4810
384013
YDOT = -18762
567717 feet/sec YDOT = -5665
344472 meter/sec
ZDOT = 5930
729515 ZDOT = 1830
921474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4470418
02 X = 1362583
41
Y = -14151901
65 feet Y = -4313499
62 meter
Z = -16645141
78 Z = -5073439
21
XDOT = 23338
447740 XDOT = 7113
558871
YDOT = 279
770359 feet/sec YDOT = 85
274005 meter/sec
ZDOT = 6029
406465 ZDOT = 1837
763091
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 13347
64241736
00016717 00000-0 10270-3 0 9053
2 25544 51
6507 299
1581 0004153 271
5768 88
4907 15
49802363 22540
Satellite: ISS
Catalog Number: 25544
Epoch time: 13347
64241736 = yrday
fracday
Element set: 905
Inclination: 51
6507 deg
RA of node: 299
1581 deg
Eccentricity:
0004153
Arg of perigee: 271
5768 deg
Mean anomaly: 88
4907 deg
Mean motion: 15
49802363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 327
Coasting Arc #7 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2013/348/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2681004
12 A = 6791324
05 meter
Y = 3788006
98 meter E =
0003939
Z = 4958708
35 I = 51
31013
XDOT = -4414
201970 Wp = 15
17727
YDOT = 5894
281617 meter/sec RA = 293
55075 deg
ZDOT = -2111
978873 TA = 95
52825
MA = 95
48333
Ha = 226
110 n
mi
Hp = 222
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8795945
29 X = 2614358
25
Y = 12427844
44 feet Y = 3817614
62 meter
Z = 16268728
18 Z = 4971570
98
XDOT = -14482
289927 XDOT = -4469
525544
YDOT = 19338
194281 feet/sec YDOT = 5844
610045 meter/sec
ZDOT = -6929
064543 ZDOT = -2133
556748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4126435
01 X = -1257737
39
Y = 14596251
90 feet Y = 4448937
58 meter
Z = 16322176
70 Z = 4974999
46
XDOT = -23046
216286 XDOT = -7024
486724
YDOT = 1350
730959 feet/sec YDOT = 411
702796 meter/sec
ZDOT = -7020
800746 ZDOT = -2139
940068
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 13348
67411560
00016717 00000-0 10270-3 0 9062
2 25544 51
6506 294
0489 0004233 275
8793 84
1875 15
49859395 22706
Satellite: ISS
Catalog Number: 25544
Epoch time: 13348
67411560 = yrday
fracday
Element set: 906
Inclination: 51
6506 deg
RA of node: 294
0489 deg
Eccentricity:
0004233
Arg of perigee: 275
8793 deg
Mean anomaly: 84
1875 deg
Mean motion: 15
49859395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 342
Coasting Arc #8 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2013/349/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2810694
94 A = 6791762
77 meter
Y = -3840574
42 meter E =
0007615
Z = -4852655
67 I = 51
30090
XDOT = 4063
044104 Wp = 112
00219
YDOT = -6022
278659 meter/sec RA = 288
57308 deg
ZDOT = 2413
171703 TA = 181
82024
MA = 181
82301
Ha = 226
209 n
mi
Hp = 222
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9221440
08 X = -2743966
84
Y = -12600309
78 feet Y = -3871631
83 meter
Z = -15920786
33 Z = -4866148
16
XDOT = 13330
197190 XDOT = 4118
361971
YDOT = -19758
132083 feet/sec YDOT = -5976
534047 meter/sec
ZDOT = 7917
229996 ZDOT = 2433
043519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3730226
64 X = 1136973
08
Y = -15102944
10 feet Y = -4603377
36 meter
Z = -15976879
85 Z = -4869752
98
XDOT = 22560
202058 XDOT = 6876
349587
YDOT = -2891
870879 feet/sec YDOT = -881
442244 meter/sec
ZDOT = 8001
811926 ZDOT = 2438
952275
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 13349
64131540
00016717 00000-0 10270-3 0 9078
2 25544 51
6513 289
2585 0004217 279
0714 80
9959 15
49864751 22853
Satellite: ISS
Catalog Number: 25544
Epoch time: 13349
64131540 = yrday
fracday
Element set: 907
Inclination: 51
6513 deg
RA of node: 289
2585 deg
Eccentricity:
0004217
Arg of perigee: 279
0714 deg
Mean anomaly: 80
9959 deg
Mean motion: 15
49864751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 335
Coasting Arc #9 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2013/350/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2944408
03 A = 6792121
30 meter
Y = 3901365
31 meter E =
0005322
Z = 4715866
08 I = 51
29376
XDOT = -3725
763165 Wp = 31
01291
YDOT = 6113
816911 meter/sec RA = 283
59519 deg
ZDOT = -2725
784839 TA = 86
14333
MA = 86
08248
Ha = 226
106 n
mi
Hp = 222
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9660131
34 X = 2877654
78
Y = 12799754
94 feet Y = 3933917
82 meter
Z = 15472001
58 Z = 4730008
07
XDOT = -12223
632431 XDOT = -3780
611143
YDOT = 20058
454433 feet/sec YDOT = 6071
846670 meter/sec
ZDOT = -8942
863645 ZDOT = -2744
016905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3329031
55 X = -1014688
82
Y = 15628364
36 feet Y = 4763525
46 meter
Z = 15530823
33 Z = 4733794
95
XDOT = -21965
924571 XDOT = -6695
213809
YDOT = 4304
283989 feet/sec YDOT = 1311
945760 meter/sec
ZDOT = -9020
562870 ZDOT = -2749
467563
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 13350
67297408
00016717 00000-0 10270-3 0 9080
2 25544 51
6513 284
1492 0004294 283
5568 76
5104 15
49924915 23017
Satellite: ISS
Catalog Number: 25544
Epoch time: 13350
67297408 = yrday
fracday
Element set: 908
Inclination: 51
6513 deg
RA of node: 284
1492 deg
Eccentricity:
0004294
Arg of perigee: 283
5568 deg
Mean anomaly: 76
5104 deg
Mean motion: 15
49924915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 321
Coasting Arc #10 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/351/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3105923
45 A = 6792696
20 meter
Y = -3956118
14 meter E =
0005731
Z = -4571161
76 I = 51
28948
XDOT = 3389
191140 Wp = 112
82048
YDOT = -6160
325143 meter/sec RA = 278
61642 deg
ZDOT = 3029
509071 TA = 187
64655
MA = 187
65529
Ha = 226
196 n
mi
Hp = 222
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10190037
55 X = -3039248
95
Y = -12979390
23 feet Y = -3990477
26 meter
Z = -14997249
88 Z = -4586088
54
XDOT = 11119
393503 XDOT = 3443
108835
YDOT = -20211
040497 feet/sec YDOT = -6122
123906 meter/sec
ZDOT = 9939
334221 ZDOT = 3046
103755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2834852
10 X = 864062
92
Y = -16198699
74 feet Y = -4937363
68 meter
Z = -15059371
84 Z = -4590096
54
XDOT = 21218
164313 XDOT = 6467
296483
YDOT = -5590
170847 feet/sec YDOT = -1703
884074 meter/sec
ZDOT = 10010
151357 ZDOT = 3051
094134
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 13351
64013704
00016717 00000-0 10270-3 0 9094
2 25544 51
6515 279
3588 0004320 286
4290 73
6385 15
49925483 23161
Satellite: ISS
Catalog Number: 25544
Epoch time: 13351
64013704 = yrday
fracday
Element set: 909
Inclination: 51
6515 deg
RA of node: 279
3588 deg
Eccentricity:
0004320
Arg of perigee: 286
4290 deg
Mean anomaly: 73
6385 deg
Mean motion: 15
49925483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 319
Coasting Arc #11 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/352/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3271982
93 A = 6793178
19 meter
Y = 4017316
85 meter E =
0006676
Z = 4392147
95 I = 51
28798
XDOT = -3076
629883 Wp = 44
84816
YDOT = 6168
723638 meter/sec RA = 273
63783 deg
ZDOT = -3342
537154 TA = 79
18641
MA = 79
11127
Ha = 226
170 n
mi
Hp = 222
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10734852
13 X = 3205481
43
Y = 13180173
39 feet Y = 4053533
96 meter
Z = 14409934
23 Z = 4407881
79
XDOT = -10093
930062 XDOT = -3129
144173
YDOT = 20238
594613 feet/sec YDOT = 6134
025529 meter/sec
ZDOT = -10966
329247 ZDOT = -3357
610005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2326833
34 X = -709218
80
Y = 16782353
59 feet Y = 5115261
37 meter
Z = 14475450
93 Z = 4412117
44
XDOT = -20393
585741 XDOT = -6215
964934
YDOT = 6708
817252 feet/sec YDOT = 2044
847498 meter/sec
ZDOT = -11030
741834 ZDOT = -3362
170111
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 13352
67175666
00016717 00000-0 10270-3 0 9106
2 25544 51
6515 274
2493 0004390 291
1030 68
9651 15
49988361 23327
Satellite: ISS
Catalog Number: 25544
Epoch time: 13352
67175666 = yrday
fracday
Element set: 910
Inclination: 51
6515 deg
RA of node: 274
2493 deg
Eccentricity:
0004390
Arg of perigee: 291
1030 deg
Mean anomaly: 68
9651 deg
Mean motion: 15
49988361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 317
Coasting Arc #12 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2013/353/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3466398
92 A = 6793873
91 meter
Y = -4060523
77 meter E =
0003598
Z = -4205204
31 I = 51
28855
XDOT = 2775
131311 Wp = 105
53647
YDOT = -6137
937920 meter/sec RA = 268
65848 deg
ZDOT = 3640
856574 TA = 201
99901
MA = 202
01446
Ha = 226
242 n
mi
Hp = 222
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11372699
88 X = -3400308
00
Y = -13321928
39 feet Y = -4098917
32 meter
Z = -13796602
05 Z = -4221883
51
XDOT = 9104
761520 XDOT = 2825
874657
YDOT = -20137
591602 feet/sec YDOT = -6106
621260 meter/sec
ZDOT = 11945
067500 ZDOT = 3654
460495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1692363
99 X = 515832
55
Y = -17378880
48 feet Y = -5297082
77 meter
Z = -13866099
82 Z = -4226387
23
XDOT = 19468
429657 XDOT = 5933
977360
YDOT = -7676
883044 feet/sec YDOT = -2339
913952 meter/sec
ZDOT = 12003
289613 ZDOT = 3658
602674
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 13353
63888345
00016717 00000-0 10270-3 0 9119
2 25544 51
6508 269
4584 0004423 293
4808 66
5877 15
49983678 23477
Satellite: ISS
Catalog Number: 25544
Epoch time: 13353
63888345 = yrday
fracday
Element set: 911
Inclination: 51
6508 deg
RA of node: 269
4584 deg
Eccentricity:
0004423
Arg of perigee: 293
4808 deg
Mean anomaly: 66
5877 deg
Mean motion: 15
49983678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 360
Coasting Arc #13 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/354/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3664264
81 A = 6794457
41 meter
Y = 4107616
51 meter E =
0007904
Z = 3980501
63 I = 51
29267
XDOT = -2508
185757 Wp = 57
93711
YDOT = 6069
657043 meter/sec RA = 263
67994 deg
ZDOT = -3944
667958 TA = 73
39304
MA = 73
30626
Ha = 226
277 n
mi
Hp = 222
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12021866
19 X = 3598724
16
Y = 13476432
13 feet Y = 4148225
87 meter
Z = 13059388
54 Z = 3998143
30
XDOT = -8228
955896 XDOT = -2556
709622
YDOT = 19913
572976 feet/sec YDOT = 6041
337926 meter/sec
ZDOT = -12941
824008 ZDOT = -3956
969760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1038572
85 X = -316557
01
Y = 17975938
82 feet Y = 5479066
15 meter
Z = 13132939
82 Z = 4002920
06
XDOT = -18508
505744 XDOT = -5641
392551
YDOT = 8447
870707 feet/sec YDOT = 2574
910991 meter/sec
ZDOT = -12994
549672 ZDOT = -3960
738740
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 13354
67046473
00016717 00000-0 10270-3 0 9123
2 25544 51
6507 264
3487 0004506 298
2620 61
8075 15
50048136 23638
Satellite: ISS
Catalog Number: 25544
Epoch time: 13354
67046473 = yrday
fracday
Element set: 912
Inclination: 51
6507 deg
RA of node: 264
3487 deg
Eccentricity:
0004506
Arg of perigee: 298
2620 deg
Mean anomaly: 61
8075 deg
Mean motion: 15
50048136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 305
Coasting Arc #14 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2013/355/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3887287
04 A = 6795239
14 meter
Y = -4124987
59 meter E =
0002128
Z = -3748994
10 I = 51
29816
XDOT = 2261
498382 Wp = 63
43630
YDOT = -5971
473395 meter/sec RA = 258
70063 deg
ZDOT = 4228
245341 TA = 251
58047
MA = 251
60361
Ha = 226
330 n
mi
Hp = 222
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12753566
41 X = -3822660
16
Y = -13533423
85 feet Y = -4168096
11 meter
Z = -12299849
40 Z = -3767721
33
XDOT = 7419
614114 XDOT = 2307
565154
YDOT = -19591
448146 feet/sec YDOT = -5945
926593 meter/sec
ZDOT = 13872
196000 ZDOT = 4239
342886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 237669
90 X = 72441
79
Y = -18542451
27 feet Y = -5651739
15 meter
Z = -12377977
48 Z = -3772807
54
XDOT = 17509
259749 XDOT = 5336
822371
YDOT = -9061
630511 feet/sec YDOT = -2761
984980 meter/sec
ZDOT = 13919
831241 ZDOT = 4242
764562
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 13355
63755624
00016717 00000-0 10270-3 0 9136
2 25544 51
6494 259
5570 0004494 300
2133 59
8573 15
50038851 23780
Satellite: ISS
Catalog Number: 25544
Epoch time: 13355
63755624 = yrday
fracday
Element set: 913
Inclination: 51
6494 deg
RA of node: 259
5570 deg
Eccentricity:
0004494
Arg of perigee: 300
2133 deg
Mean anomaly: 59
8573 deg
Mean motion: 15
50038851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 320
Coasting Arc #15 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2013/356/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4110678
09 A = 6795880
80 meter
Y = 4143478
48 meter E =
0008917
Z = 3476688
18 I = 51
30789
XDOT = -2059
434883 Wp = 70
75523
YDOT = 5839
154791 meter/sec RA = 253
72292 deg
ZDOT = -4511
660897 TA = 68
27473
MA = 68
17983
Ha = 226
406 n
mi
Hp = 222
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13486476
67 X = 4047150
61
Y = 13594089
52 feet Y = 4189091
32 meter
Z = 11406457
28 Z = 3496503
24
XDOT = -6756
676125 XDOT = -2102
660305
YDOT = 19157
331993 feet/sec YDOT = 5815
883435 meter/sec
ZDOT = -14802
037065 ZDOT = -4521
770038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 581276
72 X = 177173
14
Y = 19090642
78 feet Y = 5818827
92 meter
Z = 11489171
68 Z = 3501899
53
XDOT = -16525
424645 XDOT = -5036
949432
YDOT = 9461
813026 feet/sec YDOT = 2883
960610 meter/sec
ZDOT = -14845
484514 ZDOT = -4524
903680
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 13356
66910010
00016717 00000-0 10270-3 0 9143
2 25544 51
6494 254
4468 0004619 304
9388 55
1329 15
50104197 23945
Satellite: ISS
Catalog Number: 25544
Epoch time: 13356
66910010 = yrday
fracday
Element set: 914
Inclination: 51
6494 deg
RA of node: 254
4468 deg
Eccentricity:
0004619
Arg of perigee: 304
9388 deg
Mean anomaly: 55
1329 deg
Mean motion: 15
50104197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 312
Coasting Arc #16 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2013/357/15:06:27
142
Vector Time (MET): N/A
Weight (LBS) : 901284
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4352407
92 A = 6796696
36 meter
Y = -4122109
29 meter E =
0003550
Z = -3199951
44 I = 51
31842
XDOT = 1884
632561 Wp = 14
99681
YDOT = -5689
251270 meter/sec RA = 248
74457 deg
ZDOT = 4769
948222 TA = 307
90049
MA = 307
93258
Ha = 226
442 n
mi
Hp = 222
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14279553
53 X = -4290445
70
Y = -13523980
60 feet Y = -4170434
10 meter
Z = -10498528
34 Z = -3220944
57
XDOT = 6183
177692 XDOT = 1924
940007
YDOT = -18665
522540 feet/sec YDOT = -5667
950940 meter/sec
ZDOT = 15649
436423 ZDOT = 4779
201194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1551038
99 X = -472756
68
Y = -19558863
26 feet Y = -5961541
52 meter
Z = -10586214
81 Z = -3226678
27
XDOT = 15565
860706 XDOT = 4744
474343
YDOT = -9718
158254 feet/sec YDOT = -2962
094636 meter/sec
ZDOT = 15689
250441 ZDOT = 4782
083534
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 13357
63615743
00016717 00000-0 10270-3 0 9157
2 25544 51
6478 249
6544 0004514 306
8013 53
2723 15
50091083 24091
Satellite: ISS
Catalog Number: 25544
Epoch time: 13357
63615743 = yrday
fracday
Element set: 915
Inclination: 51
6478 deg
RA of node: 249
6544 deg
Eccentricity:
0004514
Arg of perigee: 306
8013 deg
Mean anomaly: 53
2723 deg
Mean motion: 15
50091083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 302
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