[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 29th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
243/07:34:29
797 0
4 1
3 1
4
N/A 1
2 -0
2 227
5
000/00:02:59
594 -0
4 -0
1 220
5
Coasting Arc #1 (Orbit 592)
---------------------------------------
Vector Time (GMT): 2013/240/12:19:31
524
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4411947
05 A = 6788693
66 meter
Y = 473993
69 meter E =
0004691
Z = 5133564
22 I = 51
96776
XDOT = 1161
269503 Wp = 67
09645
YDOT = -7388
936134 meter/sec RA = 109
05547 deg
ZDOT = 1680
827007 TA = 6
74448
MA = 6
73816
Ha = 227
494 n
mi
Hp = 220
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14474891
89 X = -4441856
77
Y = 1555097
39 feet Y = 424489
43 meter
Z = 16842402
29 Z = 5112058
84
XDOT = 3809
939313 XDOT = 1235
642937
YDOT = -24241
916451 feet/sec YDOT = -7375
534183 meter/sec
ZDOT = 5514
524302 ZDOT = 1686
649202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14288644
39 X = 4355178
81
Y = 3287713
49 feet Y = 1002095
07 meter
Z = 16752101
94 Z = 5106040
67
XDOT = -11241
854191 XDOT = -3426
517158
YDOT = 20639
343111 feet/sec YDOT = 6290
871780 meter/sec
ZDOT = 5539
928443 ZDOT = 1688
570189
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 13240
56484148
00016717 00000-0 10270-3 0 9007
2 25544 51
6498 109
6979 0004780 1
4500 358
6664 15
50560323 5930
Satellite: ISS
Catalog Number: 25544
Epoch time: 13240
56484148 = yrday
fracday
Element set: 900
Inclination: 51
6498 deg
RA of node: 109
6979 deg
Eccentricity:
0004780
Arg of perigee: 1
4500 deg
Mean anomaly: 358
6664 deg
Mean motion: 15
50560323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 593
Checksum: 311
Coasting Arc #2 (Orbit 607)
---------------------------------------
Vector Time (GMT): 2013/241/12:19:31
524
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4295097
58 A = 6788037
48 meter
Y = -193207
68 meter E =
0015899
Z = -5266281
45 I = 51
97414
XDOT = -1006
659308 Wp = 64
29905
YDOT = 7505
652074 meter/sec RA = 104
11517 deg
ZDOT = -1092
247492 TA = 195
23601
MA = 195
28395
Ha = 227
342 n
mi
Hp = 220
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14091527
51 X = 4322520
82
Y = -633883
47 feet Y = -145024
00 meter
Z = -17277826
27 Z = -5245349
80
XDOT = -3302
688017 XDOT = -1085
208532
YDOT = 24624
842761 feet/sec YDOT = 7493
955744 meter/sec
ZDOT = -3583
489146 ZDOT = -1097
328729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13695535
52 X = -4174399
23
Y = -3799168
82 feet Y = -1157986
66 meter
Z = -17189963
92 Z = -5239501
00
XDOT = 10477
866602 XDOT = 3193
653740
YDOT = -21394
655876 feet/sec YDOT = -6521
091111 meter/sec
ZDOT = -3605
812549 ZDOT = -1099
051665
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 13241
53157959
00016717 00000-0 10270-3 0 9013
2 25544 51
6488 104
9040 0004839 3
0054 357
1125 15
50605030 6081
Satellite: ISS
Catalog Number: 25544
Epoch time: 13241
53157959 = yrday
fracday
Element set: 901
Inclination: 51
6488 deg
RA of node: 104
9040 deg
Eccentricity:
0004839
Arg of perigee: 3
0054 deg
Mean anomaly: 357
1125 deg
Mean motion: 15
50605030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 608
Checksum: 278
Coasting Arc #3 (Orbit 623)
---------------------------------------
Vector Time (GMT): 2013/242/12:19:31
524
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4198925
36 A = 6787725
19 meter
Y = -131168
89 meter E =
0004931
Z = 5328541
45 I = 51
97998
XDOT = 845
840488 Wp = 39
63038
YDOT = -7603
656882 meter/sec RA = 99
17569 deg
ZDOT = 482
803795 TA = 45
80436
MA = 45
76386
Ha = 227
562 n
mi
Hp = 219
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13776001
85 X = -4223030
88
Y = -430344
14 feet Y = -178258
54 meter
Z = 17482091
36 Z = 5308085
11
XDOT = 2775
067219 XDOT = 928
458071
YDOT = -24946
380848 feet/sec YDOT = -7593
736200 meter/sec
ZDOT = 1584
001952 ZDOT = 487
113695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13145906
17 X = 4006872
20
Y = 4488004
35 feet Y = 1367943
73 meter
Z = 17396261
37 Z = 5302380
46
XDOT = -9642
857015 XDOT = -2939
142818
YDOT = 22075
242302 feet/sec YDOT = 6728
533854 meter/sec
ZDOT = 1603
113102 ZDOT = 488
628873
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 13242
56275679
00016717 00000-0 10270-3 0 9028
2 25544 51
6492 99
7913 0004806 7
0899 353
0319 15
50596038 6246
Satellite: ISS
Catalog Number: 25544
Epoch time: 13242
56275679 = yrday
fracday
Element set: 902
Inclination: 51
6492 deg
RA of node: 99
7913 deg
Eccentricity:
0004806
Arg of perigee: 7
0899 deg
Mean anomaly: 353
0319 deg
Mean motion: 15
50596038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 624
Checksum: 328
Coasting Arc #4 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2013/243/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149297
54 A = 6789486
71 meter
Y = -1799611
89 meter E =
0014627
Z = -5076784
29 I = 51
98741
XDOT = 835
883877 Wp = 59
17100
YDOT = 7358
517977 meter/sec RA = 95
22381 deg
ZDOT = -1922
086630 TA = 192
21788
MA = 192
25339
Ha = 227
481 n
mi
Hp = 220
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13613180
92 X = 4193774
17
Y = -5904238
49 feet Y = -1752963
33 meter
Z = -16656116
42 Z = -5056519
51
XDOT = 2742
401172 XDOT = 762
874063
YDOT = 24142
119346 feet/sec YDOT = 7367
457064 meter/sec
ZDOT = -6306
058499 ZDOT = -1918
203654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6575156
34 X = -2004107
65
Y = -13408207
66 feet Y = -4086821
69 meter
Z = -16570824
60 Z = -5050787
34
XDOT = 22997
229887 XDOT = 7009
555670
YDOT = -3489
930482 feet/sec YDOT = -1063
730811 meter/sec
ZDOT = -6290
760386 ZDOT = -1917
423766
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 13243
33613366
00016717 00000-0 10270-3 0 9034
2 25544 51
6494 95
9564 0004312
3617 359
7536 15
50389031 6364
Satellite: ISS
Catalog Number: 25544
Epoch time: 13243
33613366 = yrday
fracday
Element set: 903
Inclination: 51
6494 deg
RA of node: 95
9564 deg
Eccentricity:
0004312
Arg of perigee:
3617 deg
Mean anomaly: 359
7536 deg
Mean motion: 15
50389031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 302
Coasting Arc #5 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2013/244/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4070949
33 A = 6788821
19 meter
Y = 1567849
23 meter E =
0004173
Z = 5198028
75 I = 51
98712
XDOT = -1067
823795 Wp = 65
93569
YDOT = -7458
069837 meter/sec RA = 90
28765 deg
ZDOT = 1414
004780 TA = 10
52872
MA = 10
51998
Ha = 227
598 n
mi
Hp = 220
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13356132
97 X = -4113429
09
Y = 5143862
29 feet Y = 1522088
03 meter
Z = 17053900
08 Z = 5178149
44
XDOT = -3503
358907 XDOT = -991
215426
YDOT = -24468
733062 feet/sec YDOT = -7469
582507 meter/sec
ZDOT = 4639
123294 ZDOT = 1409
003910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6029225
18 X = 1837707
83
Y = 13089694
85 feet Y = 3989738
99 meter
Z = 16970251
85 Z = 5172532
76
XDOT = -23224
720104 XDOT = -7078
894688
YDOT = 4712
221643 feet/sec YDOT = 1436
285157 meter/sec
ZDOT = 4619
153786 ZDOT = 1407
918074
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 13244
36745321
00016717 00000-0 10270-3 0 9046
2 25544 51
6491 90
8446 0004272 2
0040 358
1128 15
50418486 6523
Satellite: ISS
Catalog Number: 25544
Epoch time: 13244
36745321 = yrday
fracday
Element set: 904
Inclination: 51
6491 deg
RA of node: 90
8446 deg
Eccentricity:
0004272
Arg of perigee: 2
0040 deg
Mean anomaly: 358
1128 deg
Mean motion: 15
50418486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 283
Coasting Arc #6 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2013/245/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4046297
81 A = 6788414
31 meter
Y = -1336433
19 meter E =
0016040
Z = -5297889
35 I = 51
98559
XDOT = 1305
147351 Wp = 67
67975
YDOT = 7486
217881 meter/sec RA = 85
35066 deg
ZDOT = -887
871075 TA = 193
82792
MA = 193
87190
Ha = 227
580 n
mi
Hp = 220
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13275255
30 X = 4086676
73
Y = -4384623
32 feet Y = -1290959
50 meter
Z = -17381526
73 Z = -5278134
90
XDOT = 4281
979499 XDOT = 1225
650802
YDOT = 24561
082288 feet/sec YDOT = 7500
368318 meter/sec
ZDOT = -2912
962843 ZDOT = -881
724459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5490342
36 X = -1673456
35
Y = -12969011
17 feet Y = -3952954
61 meter
Z = -17298430
17 Z = -5272561
52
XDOT = 23169
230749 XDOT = 7061
981532
YDOT = -5939
604632 feet/sec YDOT = -1810
391492 meter/sec
ZDOT = -2888
194359 ZDOT = -880
321641
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 13245
33430572
00016717 00000-0 10270-3 0 9054
2 25544 51
6497 86
0520 0004400 6
5802 353
5406 15
50426778 6674
Satellite: ISS
Catalog Number: 25544
Epoch time: 13245
33430572 = yrday
fracday
Element set: 905
Inclination: 51
6497 deg
RA of node: 86
0520 deg
Eccentricity:
0004400
Arg of perigee: 6
5802 deg
Mean anomaly: 353
5406 deg
Mean motion: 15
50426778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 667
Checksum: 292
Coasting Arc #7 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2013/246/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4050592
25 A = 6788080
56 meter
Y = 1073765
91 meter E =
0004801
Z = 5337362
82 I = 51
98103
XDOT = -1539
749516 Wp = 40
00890
YDOT = -7501
345235 meter/sec RA = 80
41301 deg
ZDOT = 343
985319 TA = 46
74571
MA = 46
70565
Ha = 227
687 n
mi
Hp = 220
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13289344
65 X = -4088225
41
Y = 3522854
03 feet Y = 1028259
65 meter
Z = 17511032
86 Z = 5317594
17
XDOT = -5051
671640 XDOT = -1457
424360
YDOT = -24610
712713 feet/sec YDOT = -7518
103356 meter/sec
ZDOT = 1128
560757 ZDOT = 336
706048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4856742
59 X = 1480335
14
Y = 12974337
77 feet Y = 3954578
15 meter
Z = 17427910
50 Z = 5312027
12
XDOT = -23029
264941 XDOT = -7019
319954
YDOT = 7159
429391 feet/sec YDOT = 2182
194078 meter/sec
ZDOT = 1099
046175 ZDOT = 334
989274
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 13246
36560075
00016717 00000-0 10270-3 0 9061
2 25544 51
6493 80
9397 0004384 8
1954 351
9268 15
50460251 6832
Satellite: ISS
Catalog Number: 25544
Epoch time: 13246
36560075 = yrday
fracday
Element set: 906
Inclination: 51
6493 deg
RA of node: 80
9397 deg
Eccentricity:
0004384
Arg of perigee: 8
1954 deg
Mean anomaly: 351
9268 deg
Mean motion: 15
50460251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 317
Coasting Arc #8 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2013/247/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4108255
65 A = 6788061
32 meter
Y = -832293
87 meter E =
0016248
Z = -5352683
21 I = 51
97532
XDOT = 1765
003959 Wp = 75
74668
YDOT = 7441
898218 meter/sec RA = 75
47471 deg
ZDOT = 201
914105 TA = 196
14724
MA = 196
19908
Ha = 227
664 n
mi
Hp = 220
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13478529
04 X = 4143258
80
Y = -2730622
92 feet Y = -786157
58 meter
Z = -17561296
62 Z = -5332640
80
XDOT = 5790
695405 XDOT = 1680
675013
YDOT = 24415
676567 feet/sec YDOT = 7461
164123 meter/sec
ZDOT = 662
447850 ZDOT = 210
282644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4314836
37 X = -1315162
13
Y = -13170452
49 feet Y = -4014353
92 meter
Z = -17477057
94 Z = -5327007
26
XDOT = 22602
815032 XDOT = 6889
338022
YDOT = -8310
075848 feet/sec YDOT = -2532
911118 meter/sec
ZDOT = 696
536216 ZDOT = 212
304239
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 13247
33242999
00016717 00000-0 10270-3 0 9072
2 25544 51
6498 76
1468 0004492 12
0677 348
0581 15
50463976 6987
Satellite: ISS
Catalog Number: 25544
Epoch time: 13247
33242999 = yrday
fracday
Element set: 907
Inclination: 51
6498 deg
RA of node: 76
1468 deg
Eccentricity:
0004492
Arg of perigee: 12
0677 deg
Mean anomaly: 348
0581 deg
Mean motion: 15
50463976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 698
Checksum: 343
Coasting Arc #9 (Orbit 713)
---------------------------------------
Vector Time (GMT): 2013/248/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4197925
60 A = 6788119
16 meter
Y = 566876
91 meter E =
0007055
Z = 5301534
01 I = 51
96719
XDOT = -1969
277447 Wp = 33
15601
YDOT = -7368
369800 meter/sec RA = 70
53556 deg
ZDOT = -765
231599 TA = 64
16184
MA = 64
08909
Ha = 227
758 n
mi
Hp = 219
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13772721
78 X = -4229705
74
Y = 1859832
39 feet Y = 519755
97 meter
Z = 17393484
27 Z = 5281063
78
XDOT = -6460
884011 XDOT = -1883
019105
YDOT = -24174
441600 feet/sec YDOT = -7389
909302 meter/sec
ZDOT = -2510
602359 ZDOT = -774
587713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3717473
04 X = 1133085
78
Y = 13502273
87 feet Y = 4115493
08 meter
Z = 17307487
73 Z = 5275322
26
XDOT = -22098
986181 XDOT = -6735
770988
YDOT = 9377
812989 feet/sec YDOT = 2858
357399 meter/sec
ZDOT = -2548
838340 ZDOT = -776
885926
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 13248
36369995
00016717 00000-0 10270-3 0 9083
2 25544 51
6497 71
0342 0004504 13
9221 346
2053 15
50503781 7142
Satellite: ISS
Catalog Number: 25544
Epoch time: 13248
36369995 = yrday
fracday
Element set: 908
Inclination: 51
6497 deg
RA of node: 71
0342 deg
Eccentricity:
0004504
Arg of perigee: 13
9221 deg
Mean anomaly: 346
2053 deg
Mean motion: 15
50503781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 714
Checksum: 299
Coasting Arc #10 (Orbit 728)
---------------------------------------
Vector Time (GMT): 2013/249/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4334455
97 A = 6788516
56 meter
Y = -343630
99 meter E =
0015194
Z = -5225897
83 I = 51
95749
XDOT = 2149
788191 Wp = 82
52965
YDOT = 7225
201578 meter/sec RA = 65
59585 deg
ZDOT = 1313
164743 TA = 200
02681
MA = 200
08650
Ha = 227
737 n
mi
Hp = 219
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14220656
06 X = 4363362
26
Y = -1127398
27 feet Y = -294999
38 meter
Z = -17145334
07 Z = -5204771
28
XDOT = 7053
110864 XDOT = 2062
455659
YDOT = 23704
729587 feet/sec YDOT = 7248
753734 meter/sec
ZDOT = 4308
283276 ZDOT = 1323
395147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3293080
09 X = -1003730
81
Y = -13988853
82 feet Y = -4263802
64 meter
Z = -17056616
27 Z = -5198856
64
XDOT = 21341
681921 XDOT = 6504
944650
YDOT = -10307
333824 feet/sec YDOT = -3141
675350 meter/sec
ZDOT = 4350
199389 ZDOT = 1325
940774
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 13249
33050541
00016717 00000-0 10270-3 0 9096
2 25544 51
6499 66
2409 0004577 17
1695 342
9610 15
50501002 7297
Satellite: ISS
Catalog Number: 25544
Epoch time: 13249
33050541 = yrday
fracday
Element set: 909
Inclination: 51
6499 deg
RA of node: 66
2409 deg
Eccentricity:
0004577
Arg of perigee: 17
1695 deg
Mean anomaly: 342
9610 deg
Mean motion: 15
50501002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 729
Checksum: 297
Coasting Arc #11 (Orbit 744)
---------------------------------------
Vector Time (GMT): 2013/250/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4501484
18 A = 6788979
93 meter
Y = 104032
48 meter E =
0009735
Z = 5077782
84 I = 51
94624
XDOT = -2290
147968 Wp = 39
13166
YDOT = -7070
326601 meter/sec RA = 60
65554 deg
ZDOT = -1876
064790 TA = 69
02936
MA = 68
92522
Ha = 227
814 n
mi
Hp = 219
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14768648
90 X = -4526979
41
Y = 341313
90 feet Y = 53552
09 meter
Z = 16659392
52 Z = 5055853
12
XDOT = -7513
608818 XDOT = -2201
802410
YDOT = -23196
609583 feet/sec YDOT = -7095
442753 meter/sec
ZDOT = -6155
068210 ZDOT = -1886
974652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2850482
28 X = 868827
00
Y = 14600096
40 feet Y = 4450109
38 meter
Z = 16567340
78 Z = 5049725
47
XDOT = -20535
824803 XDOT = -6259
319400
YDOT = 11079
434006 feet/sec YDOT = 3377
011485 meter/sec
ZDOT = -6199
846618 ZDOT = -1889
713249
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 13250
36174975
00016717 00000-0 10270-3 0 9101
2 25544 51
6502 61
1282 0004618 19
2741 340
8583 15
50547253 7458
Satellite: ISS
Catalog Number: 25544
Epoch time: 13250
36174975 = yrday
fracday
Element set: 910
Inclination: 51
6502 deg
RA of node: 61
1282 deg
Eccentricity:
0004618
Arg of perigee: 19
2741 deg
Mean anomaly: 340
8583 deg
Mean motion: 15
50547253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 745
Checksum: 293
Coasting Arc #12 (Orbit 759)
---------------------------------------
Vector Time (GMT): 2013/251/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4702879
28 A = 6789760
39 meter
Y = 74741
17 meter E =
0013067
Z = -4907693
04 I = 51
93265
XDOT = 2395
377932 Wp = 86
38315
YDOT = 6858
732665 meter/sec RA = 55
71452 deg
ZDOT = 2406
187282 TA = 207
12058
MA = 207
18890
Ha = 227
804 n
mi
Hp = 219
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15429393
96 X = 4725534
29
Y = 245213
81 feet Y = 127457
86 meter
Z = -16101355
13 Z = -4884791
80
XDOT = 7858
851482 XDOT = 2306
815410
YDOT = 22502
403756 feet/sec YDOT = 6885
024399 meter/sec
ZDOT = 7894
315229 ZDOT = 2417
607934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2647039
96 X = -806817
78
Y = -15303756
05 feet Y = -4664584
84 meter
Z = -16005255
23 Z = -4878401
80
XDOT = 19543
015417 XDOT = 5956
711099
YDOT = -11663
737787 feet/sec YDOT = -3555
107278 meter/sec
ZDOT = 7941
254942 ZDOT = 2420
494506
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 13251
32853100
00016717 00000-0 10270-3 0 9113
2 25544 51
6500 56
3347 0004646 22
4085 337
7268 15
50538458 7601
Satellite: ISS
Catalog Number: 25544
Epoch time: 13251
32853100 = yrday
fracday
Element set: 911
Inclination: 51
6500 deg
RA of node: 56
3347 deg
Eccentricity:
0004646
Arg of perigee: 22
4085 deg
Mean anomaly: 337
7268 deg
Mean motion: 15
50538458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 760
Checksum: 288
Coasting Arc #13 (Orbit 775)
---------------------------------------
Vector Time (GMT): 2013/252/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4928432
76 A = 6790582
55 meter
Y = -263421
72 meter E =
0012292
Z = 4659638
84 I = 51
91827
XDOT = -2442
163884 Wp = 50
39854
YDOT = -6641
523129 meter/sec RA = 50
77331 deg
ZDOT = -2945
706456 TA = 68
89213
MA = 68
76077
Ha = 227
855 n
mi
Hp = 219
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16169398
80 X = -4947756
21
Y = -864244
49 feet Y = -318642
16 meter
Z = 15287529
01 Z = 4635649
92
XDOT = -8012
348702 XDOT = -2353
405886
YDOT = -21789
774046 feet/sec YDOT = -6668
336983 meter/sec
ZDOT = -9664
391260 ZDOT = -2957
354064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2452686
49 X = 747578
84
Y = 16101163
20 feet Y = 4907634
54 meter
Z = 15186895
41 Z = 4628965
72
XDOT = -18551
270795 XDOT = -5654
427338
YDOT = 12026
587848 feet/sec YDOT = 3665
703976 meter/sec
ZDOT = -9712
301715 ZDOT = -2960
309563
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 13252
35974911
00016717 00000-0 10270-3 0 9122
2 25544 51
6505 51
2222 0004712 24
5032 335
6342 15
50589271 7767
Satellite: ISS
Catalog Number: 25544
Epoch time: 13252
35974911 = yrday
fracday
Element set: 912
Inclination: 51
6505 deg
RA of node: 51
2222 deg
Eccentricity:
0004712
Arg of perigee: 24
5032 deg
Mean anomaly: 335
6342 deg
Mean motion: 15
50589271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 776
Checksum: 283
Coasting Arc #14 (Orbit 790)
---------------------------------------
Vector Time (GMT): 2013/253/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5171022
63 A = 6791649
10 meter
Y = 377396
24 meter E =
0010450
Z = -4395150
45 I = 51
90073
XDOT = 2447
893037 Wp = 83
75531
YDOT = 6387
105682 meter/sec RA = 45
83096 deg
ZDOT = 3436
576530 TA = 220
98940
MA = 221
06799
Ha = 227
866 n
mi
Hp = 219
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16965297
33 X = 5187768
77
Y = 1238176
64 feet Y = 435315
16 meter
Z = -14419784
93 Z = -4369989
28
XDOT = 8031
145133 XDOT = 2359
595019
YDOT = 20955
071136 feet/sec YDOT = 6413
986164 meter/sec
ZDOT = 11274
857381 ZDOT = 3448
253238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2537997
04 X = -773581
50
Y = -16909919
02 feet Y = -5154143
32 meter
Z = -14314251
71 Z = -4362983
92
XDOT = 17463
286493 XDOT = 5322
809723
YDOT = -12183
183545 feet/sec YDOT = -3713
434345 meter/sec
ZDOT = 11322
914746 ZDOT = 3451
224415
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 13253
32650560
00016717 00000-0 10270-3 0 9132
2 25544 51
6497 46
4285 0004691 28
1866 331
9538 15
50576369 7910
Satellite: ISS
Catalog Number: 25544
Epoch time: 13253
32650560 = yrday
fracday
Element set: 913
Inclination: 51
6497 deg
RA of node: 46
4285 deg
Eccentricity:
0004691
Arg of perigee: 28
1866 deg
Mean anomaly: 331
9538 deg
Mean motion: 15
50576369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 791
Checksum: 326
Coasting Arc #15 (Orbit 806)
---------------------------------------
Vector Time (GMT): 2013/254/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5426899
93 A = 6792711
35 meter
Y = -497512
54 meter E =
0014418
Z = 4048406
44 I = 51
88307
XDOT = -2379
921361 Wp = 63
91989
YDOT = -6136
689549 meter/sec RA = 40
88864 deg
ZDOT = -3927
412633 TA = 66
79481
MA = 66
64303
Ha = 227
877 n
mi
Hp = 219
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17804789
79 X = -5440599
47
Y = -1632258
99 feet Y = -558275
91 meter
Z = 13282173
35 Z = 4022009
66
XDOT = -7808
140949 XDOT = -2292
044257
YDOT = -20133
495897 feet/sec YDOT = -6162
812253 meter/sec
ZDOT = -12885
212052 ZDOT = -3938
760282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2642220
03 X = 805348
67
Y = 17765749
61 feet Y = 5415000
48 meter
Z = 13171474
94 Z = 4014665
56
XDOT = -16442
247039 XDOT = -5011
596898
YDOT = 12074
818137 feet/sec YDOT = 3680
404568 meter/sec
ZDOT = -12931
914919 ZDOT = -3941
647667
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 13254
35769670
00016717 00000-0 10270-3 0 9140
2 25544 51
6501 41
3159 0004769 29
9278 330
2145 15
50630015 8075
Satellite: ISS
Catalog Number: 25544
Epoch time: 13254
35769670 = yrday
fracday
Element set: 914
Inclination: 51
6501 deg
RA of node: 41
3159 deg
Eccentricity:
0004769
Arg of perigee: 29
9278 deg
Mean anomaly: 330
2145 deg
Mean motion: 15
50630015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 807
Checksum: 299
Coasting Arc #16 (Orbit 821)
---------------------------------------
Vector Time (GMT): 2013/255/07:35:59
594
Vector Time (MET): N/A
Weight (LBS) : 957331
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5679627
01 A = 6793914
64 meter
Y = 535738
81 meter E =
0008655
Z = -3693714
90 I = 51
86168
XDOT = 2272
051008 Wp = 69
49774
YDOT = 5872
662364 meter/sec RA = 35
94464 deg
ZDOT = 4356
596486 TA = 246
79213
MA = 246
88331
Ha = 227
920 n
mi
Hp = 219
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18633946
89 X = 5691157
25
Y = 1757673
26 feet Y = 599316
28 meter
Z = -12118487
21 Z = -3666095
74
XDOT = 7454
235591 XDOT = 2185
049521
YDOT = 19267
264973 feet/sec YDOT = 5897
583660 meter/sec
ZDOT = 14293
295557 ZDOT = 4367
422298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3033959
83 X = -924750
95
Y = -18544600
79 feet Y = -5652394
32 meter
Z = -12002666
10 Z = -3658412
63
XDOT = 15425
623449 XDOT = 4701
730027
YDOT = -11779
563043 feet/sec YDOT = -3590
410815 meter/sec
ZDOT = 14337
839928 ZDOT = 4370
173610
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 13255
32442770
00016717 00000-0 10270-3 0 9158
2 25544 51
6487 36
5218 0004711 34
6395 325
5062 15
50614277 8224
Satellite: ISS
Catalog Number: 25544
Epoch time: 13255
32442770 = yrday
fracday
Element set: 915
Inclination: 51
6487 deg
RA of node: 36
5218 deg
Eccentricity:
0004711
Arg of perigee: 34
6395 deg
Mean anomaly: 325
5062 deg
Mean motion: 15
50614277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 822
Checksum: 296
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