[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 10th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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
256/03:28:22
693 1
2 1
3 1
3
N/A 0
4 -0
1 228
0
000/00:02:45
386 -0
1 0
0 219
9
Coasting Arc #1 (Orbit 778)
---------------------------------------
Vector Time (GMT): 2013/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -662270
96 A = 6790780
05 meter
Y = 4886533
75 meter E =
0009984
Z = 4660762
87 I = 51
91060
XDOT = -6075
183052 Wp = 96
06077
YDOT = -3636
505135 meter/sec RA = 49
91737 deg
ZDOT = 2942
975395 TA = 324
71900
MA = 324
78504
Ha = 227
857 n
mi
Hp = 219
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2172805
00 X = -739504
89
Y = 16031934
87 feet Y = 4878696
44 meter
Z = 15291216
76 Z = 4657357
52
XDOT = -19931
702927 XDOT = -6048
363594
YDOT = -11930
791125 feet/sec YDOT = -3704
291442 meter/sec
ZDOT = 9655
431085 ZDOT = 2913
528040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5583115
01 X = 1701733
46
Y = -15199721
72 feet Y = -4632875
18 meter
Z = 15276210
72 Z = 4656189
03
XDOT = 15932
827867 XDOT = 4856
325934
YDOT = 15453
980568 feet/sec YDOT = 4710
373277 meter/sec
ZDOT = 9532
384918 ZDOT = 2905
470923
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
55353740
00016717 00000-0 10270-3 0 9002
2 25544 51
6465 50
2681 0003502 46
5385 313
6056 15
50481873 7791
Satellite: ISS
Catalog Number: 25544
Epoch time: 13252
55353740 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 50
2681 deg
Eccentricity:
0003502
Arg of perigee: 46
5385 deg
Mean anomaly: 313
6056 deg
Mean motion: 15
50481873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 779
Checksum: 297
Coasting Arc #2 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2013/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 773099
21 A = 6789873
58 meter
Y = -4656176
43 meter E =
0015387
Z = -4895576
42 I = 51
88840
XDOT = 6298
287229 Wp = 67
44827
YDOT = 3599
405154 meter/sec RA = 44
97610 deg
ZDOT = -2429
133751 TA = 178
75254
MA = 178
74870
Ha = 227
916 n
mi
Hp = 219
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2536414
72 X = 848889
67
Y = -15276169
38 feet Y = -4647107
77 meter
Z = -16061602
42 Z = -4891636
28
XDOT = 20663
672010 XDOT = 6269
369938
YDOT = 11809
072027 feet/sec YDOT = 3669
674718 meter/sec
ZDOT = -7969
598922 ZDOT = -2398
607575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5536373
13 X = -1687486
53
Y = 14480895
26 feet Y = 4413776
88 meter
Z = -16044378
08 Z = -4890326
44
XDOT = -16986
945053 XDOT = -5177
620852
YDOT = -15181
917607 feet/sec YDOT = -4627
448487 meter/sec
ZDOT = -7842
029058 ZDOT = -2390
250457
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
52034759
00016717 00000-0 10270-3 0 9017
2 25544 51
6478 45
4763 0003702 51
5896 308
5586 15
50487024 7949
Satellite: ISS
Catalog Number: 25544
Epoch time: 13253
52034759 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 45
4763 deg
Eccentricity:
0003702
Arg of perigee: 51
5896 deg
Mean anomaly: 308
5586 deg
Mean motion: 15
50487024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 320
Coasting Arc #3 (Orbit 809)
---------------------------------------
Vector Time (GMT): 2013/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -911982
63 A = 6789078
65 meter
Y = 4424312
48 meter E =
0007532
Z = 5061902
60 I = 51
86329
XDOT = -6532
841884 Wp = 97
38477
YDOT = -3532
285710 meter/sec RA = 40
03078 deg
ZDOT = 1906
997106 TA = 334
16274
MA = 334
20034
Ha = 227
918 n
mi
Hp = 219
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2992069
01 X = -985977
96
Y = 14515460
90 feet Y = 4413700
70 meter
Z = 16607291
99 Z = 5057292
23
XDOT = -21433
208280 XDOT = -6502
121278
YDOT = -11588
863878 feet/sec YDOT = -3605
168206 meter/sec
ZDOT = 6256
552185 ZDOT = 1875
335831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5604306
29 X = 1708192
56
Y = -13744345
58 feet Y = -4189276
53 meter
Z = 16587282
63 Z = 5055803
74
XDOT = 18091
867708 XDOT = 5514
401277
YDOT = 14781
361787 feet/sec YDOT = 4505
359073 meter/sec
ZDOT = 6124
216097 ZDOT = 1866
661066
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
55160367
00016717 00000-0 10270-3 0 9027
2 25544 51
6476 40
3629 0003567 53
5874 306
5606 15
50501138 8102
Satellite: ISS
Catalog Number: 25544
Epoch time: 13254
55160367 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 40
3629 deg
Eccentricity:
0003567
Arg of perigee: 53
5874 deg
Mean anomaly: 306
5606 deg
Mean motion: 15
50501138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 810
Checksum: 293
Coasting Arc #4 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2013/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927652
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1102242
27 A = 6788490
40 meter
Y = -4229138
01 meter E =
0017457
Z = -5209989
87 I = 51
83810
XDOT = 6709
909611 Wp = 75
01545
YDOT = 3414
983222 meter/sec RA = 35
08548 deg
ZDOT = -1351
889027 TA = 181
99149
MA = 181
99845
Ha = 227
942 n
mi
Hp = 219
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3616280
43 X = 1174760
27
Y = -13875124
72 feet Y = -4216406
84 meter
Z = -17093142
63 Z = -5204458
91
XDOT = 22014
139143 XDOT = 6677
790947
YDOT = 11204
013195 feet/sec YDOT = 3489
838035 meter/sec
ZDOT = -4435
331454 ZDOT = -1319
371019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5884326
17 X = -1793542
62
Y = 13106716
04 feet Y = 3994927
05 meter
Z = -17069293
93 Z = -5202720
79
XDOT = -19020
427691 XDOT = -5797
426360
YDOT = -14141
142165 feet/sec YDOT = -4310
220132 meter/sec
ZDOT = -4299
387424 ZDOT = -1310
453287
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
51840089
00016717 00000-0 10270-3 0 9031
2 25544 51
6486 35
5713 0003720 57
9558 302
1953 15
50507778 8250
Satellite: ISS
Catalog Number: 25544
Epoch time: 13255
51840089 = yrday
fracday
Element set: 903
Inclination: 51
6486 deg
RA of node: 35
5713 deg
Eccentricity:
0003720
Arg of perigee: 57
9558 deg
Mean anomaly: 302
1953 deg
Mean motion: 15
50507778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 315
Coasting Arc #5 (Orbit 834)
---------------------------------------
Vector Time (GMT): 2013/256/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1534344
88 A = 6788713
21 meter
Y = -3962275
97 meter E =
0017129
Z = -5309431
67 I = 51
82218
XDOT = 6740
914181 Wp = 77
81848
YDOT = 3547
963948 meter/sec RA = 31
89158 deg
ZDOT = -698
109061 TA = 185
50531
MA = 185
52417
Ha = 227
979 n
mi
Hp = 219
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5033939
90 X = 1604329
65
Y = -12999593
08 feet Y = -3944726
91 meter
Z = -17419395
24 Z = -5301807
78
XDOT = 22115
860175 XDOT = 6704
130293
YDOT = 11640
301666 feet/sec YDOT = 3623
139424 meter/sec
ZDOT = -2290
384057 ZDOT = -665
451851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5312856
74 X = -1619358
73
Y = -12932052
57 feet Y = -3941689
62 meter
Z = -17386801
64 Z = -5299497
14
XDOT = 23072
160831 XDOT = 7032
394621
YDOT = -6575
743719 feet/sec YDOT = -2004
286686 meter/sec
ZDOT = -2153
878186 ZDOT = -656
502071
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 13256
16292916
00016717 00000-0 10270-3 0 9044
2 25544 51
6505 32
3795 0003116 45
0211 315
1191 15
50285440 8358
Satellite: ISS
Catalog Number: 25544
Epoch time: 13256
16292916 = yrday
fracday
Element set: 904
Inclination: 51
6505 deg
RA of node: 32
3795 deg
Eccentricity:
0003116
Arg of perigee: 45
0211 deg
Mean anomaly: 315
1191 deg
Mean motion: 15
50285440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 835
Checksum: 276
Coasting Arc #6 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2013/257/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1691358
99 A = 6788485
86 meter
Y = 3845061
53 meter E =
0004937
Z = 5328729
76 I = 51
79488
XDOT = -6904
598318 Wp = 68
88972
YDOT = -3324
867733 meter/sec RA = 26
94379 deg
ZDOT = 209
164168 TA = 19
12979
MA = 19
11126
Ha = 227
995 n
mi
Hp = 219
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5549078
06 X = -1760115
01
Y = 12615031
28 feet Y = 3825763
55 meter
Z = 17482709
20 Z = 5320346
11
XDOT = -22652
881620 XDOT = -6867
921810
YDOT = -10908
358705 feet/sec YDOT = -3401
874254 meter/sec
ZDOT = 686
234148 ZDOT = 175
711685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4897900
78 X = 1492880
16
Y = 12930241
63 feet Y = 3941137
65 meter
Z = 17446943
05 Z = 5317828
24
XDOT = -22805
733749 XDOT = -6951
187647
YDOT = 7908
473333 feet/sec YDOT = 2410
502672 meter/sec
ZDOT = 546
359561 ZDOT = 166
530394
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 13257
19432089
00016717 00000-0 10270-3 0 9056
2 25544 51
6503 27
2680 0003023 46
7112 313
4290 15
50311722 8519
Satellite: ISS
Catalog Number: 25544
Epoch time: 13257
19432089 = yrday
fracday
Element set: 905
Inclination: 51
6503 deg
RA of node: 27
2680 deg
Eccentricity:
0003023
Arg of perigee: 46
7112 deg
Mean anomaly: 313
4290 deg
Mean motion: 15
50311722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 269
Coasting Arc #7 (Orbit 865)
---------------------------------------
Vector Time (GMT): 2013/258/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1868466
35 A = 6788542
88 meter
Y = -3778949
09 meter E =
0017207
Z = -5335726
71 I = 51
76763
XDOT = 7001
997501 Wp = 84
95720
YDOT = 3067
481900 meter/sec RA = 21
99382 deg
ZDOT = 281
719484 TA = 187
71679
MA = 187
74330
Ha = 227
989 n
mi
Hp = 219
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6130138
95 X = 1936503
84
Y = -12398126
94 feet Y = -3757674
69 meter
Z = -17505665
06 Z = -5326484
40
XDOT = 22972
432747 XDOT = 6965
807335
YDOT = 10063
916995 feet/sec YDOT = 3145
580353 meter/sec
ZDOT = 924
276522 ZDOT = 315
646157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4559295
14 X = -1389673
16
Y = -13110356
90 feet Y = -3996036
78 meter
Z = -17466305
68 Z = -5323729
97
XDOT = 22256
206168 XDOT = 6783
691640
YDOT = -9150
415125 feet/sec YDOT = -2789
046530 meter/sec
ZDOT = 1066
177733 ZDOT = 324
970973
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 13258
16124589
00016717 00000-0 10270-3 0 9068
2 25544 51
6509 22
4757 0003126 49
4039 310
7384 15
50306421 8669
Satellite: ISS
Catalog Number: 25544
Epoch time: 13258
16124589 = yrday
fracday
Element set: 906
Inclination: 51
6509 deg
RA of node: 22
4757 deg
Eccentricity:
0003126
Arg of perigee: 49
4039 deg
Mean anomaly: 310
7384 deg
Mean motion: 15
50306421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 866
Checksum: 301
Coasting Arc #8 (Orbit 881)
---------------------------------------
Vector Time (GMT): 2013/259/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2066384
10 A = 6788629
51 meter
Y = 3723882
55 meter E =
0006316
Z = 5282515
32 I = 51
73951
XDOT = -7086
774302 Wp = 55
50418
YDOT = -2817
318256 meter/sec RA = 17
04198 deg
ZDOT = -781
951169 TA = 41
98393
MA = 41
93554
Ha = 228
011 n
mi
Hp = 219
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6779475
39 X = -2133532
60
Y = 12217462
44 feet Y = 3700399
99 meter
Z = 17331087
00 Z = 5272313
64
XDOT = -23250
571858 XDOT = -7050
945253
YDOT = -9243
170130 feet/sec YDOT = -2896
366811 meter/sec
ZDOT = -2565
456592 ZDOT = -816
290470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4209101
74 X = 1282934
21
Y = 13379563
80 feet Y = 4078091
05 meter
Z = 17287712
02 Z = 5269294
62
XDOT = -21654
300785 XDOT = -6600
230879
YDOT = 10330
392578 feet/sec YDOT = 3148
703658 meter/sec
ZDOT = -2709
123513 ZDOT = -825
740847
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 13259
19262372
00016717 00000-0 10270-3 0 9076
2 25544 51
6510 17
3641 0003063 51
1693 308
9730 15
50337204 8827
Satellite: ISS
Catalog Number: 25544
Epoch time: 13259
19262372 = yrday
fracday
Element set: 907
Inclination: 51
6510 deg
RA of node: 17
3641 deg
Eccentricity:
0003063
Arg of perigee: 51
1693 deg
Mean anomaly: 308
9730 deg
Mean motion: 15
50337204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 882
Checksum: 287
Coasting Arc #9 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2013/260/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2266122
96 A = 6789017
86 meter
Y = -3726485
62 meter E =
0016259
Z = -5216913
32 I = 51
71116
XDOT = 7101
634972 Wp = 91
59579
YDOT = 2545
725075 meter/sec RA = 12
08816 deg
ZDOT = 1269
359901 TA = 190
59134
MA = 190
62563
Ha = 227
990 n
mi
Hp = 219
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7434786
62 X = 2332967
08
Y = -12226002
69 feet Y = -3700771
26 meter
Z = -17115857
35 Z = -5205741
99
XDOT = 23299
327336 XDOT = 7066
474146
YDOT = 8352
116389 feet/sec YDOT = 2624
943624 meter/sec
ZDOT = 4164
566604 ZDOT = 1303
773030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4006136
48 X = -1221070
40
Y = -13795789
15 feet Y = -4204956
53 meter
Z = -17068416
41 Z = -5202453
32
XDOT = 20803
080596 XDOT = 6340
778966
YDOT = -11359
479965 feet/sec YDOT = -3462
369493 meter/sec
ZDOT = 4308
578300 ZDOT = 1313
254666
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 13260
15953566
00016717 00000-0 10270-3 0 9087
2 25544 51
6512 12
5717 0003116 53
6133 306
5305 15
50326590 8979
Satellite: ISS
Catalog Number: 25544
Epoch time: 13260
15953566 = yrday
fracday
Element set: 908
Inclination: 51
6512 deg
RA of node: 12
5717 deg
Eccentricity:
0003116
Arg of perigee: 53
6133 deg
Mean anomaly: 306
5305 deg
Mean motion: 15
50326590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 290
Coasting Arc #10 (Orbit 912)
---------------------------------------
Vector Time (GMT): 2013/261/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2481358
17 A = 6789421
53 meter
Y = 3741754
94 meter E =
0008514
Z = 5088242
77 I = 51
68296
XDOT = -7097
965365 Wp = 54
94093
YDOT = -2295
235895 meter/sec RA = 7
13288 deg
ZDOT = -1766
703198 TA = 52
17866
MA = 52
10162
Ha = 228
012 n
mi
Hp = 219
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8140938
88 X = -2547732
07
Y = 12276098
88 feet Y = 3713636
37 meter
Z = 16693709
88 Z = 5076026
90
XDOT = -23287
287942 XDOT = -7063
189866
YDOT = -7530
301492 feet/sec YDOT = -2374
415649 meter/sec
ZDOT = -5796
270336 ZDOT = -1801
099544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3817526
94 X = 1163582
21
Y = 14287459
26 feet Y = 4354817
58 meter
Z = 16641887
97 Z = 5072447
45
XDOT = -19930
335941 XDOT = -6074
766395
YDOT = 12270
748686 feet/sec YDOT = 3740
124199 meter/sec
ZDOT = -5940
240740 ZDOT = -1810
585378
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 13261
19089959
00016717 00000-0 10270-3 0 9099
2 25544 51
6516 7
4603 0003078 55
4102 304
7338 15
50361497 9133
Satellite: ISS
Catalog Number: 25544
Epoch time: 13261
19089959 = yrday
fracday
Element set: 909
Inclination: 51
6516 deg
RA of node: 7
4603 deg
Eccentricity:
0003078
Arg of perigee: 55
4102 deg
Mean anomaly: 304
7338 deg
Mean motion: 15
50361497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 913
Checksum: 306
Coasting Arc #11 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2013/262/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2678975
65 A = 6790109
37 meter
Y = -3816129
49 meter E =
0014401
Z = -4949160
67 I = 51
65397
XDOT = 7027
458292 Wp = 96
89490
YDOT = 2037
615039 meter/sec RA = 2
17545 deg
ZDOT = 2236
735855 TA = 194
96910
MA = 195
01177
Ha = 227
991 n
mi
Hp = 219
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8789290
18 X = 2745491
03
Y = -12520109
86 feet Y = -3785800
27 meter
Z = -16237403
78 Z = -4935984
35
XDOT = 23055
965526 XDOT = 6993
285474
YDOT = 6685
088712 feet/sec YDOT = 2116
009789 meter/sec
ZDOT = 7338
372228 ZDOT = 2270
791323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3832737
39 X = -1168218
36
Y = -14870298
22 feet Y = -4532466
90 meter
Z = -16181545
33 Z = -4932135
02
XDOT = 18867
727487 XDOT = 5750
883338
YDOT = -12989
627807 feet/sec YDOT = -3959
238556 meter/sec
ZDOT = 7480
940728 ZDOT = 2280
190734
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 13262
15779857
00016717 00000-0 10270-3 0 9101
2 25544 51
6512 2
6678 0003097 58
3806 301
7647 15
50345852 9285
Satellite: ISS
Catalog Number: 25544
Epoch time: 13262
15779857 = yrday
fracday
Element set: 910
Inclination: 51
6512 deg
RA of node: 2
6678 deg
Eccentricity:
0003097
Arg of perigee: 58
3806 deg
Mean anomaly: 301
7647 deg
Mean motion: 15
50345852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 320
Coasting Arc #12 (Orbit 943)
---------------------------------------
Vector Time (GMT): 2013/263/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2885853
89 A = 6790797
23 meter
Y = 3901475
98 meter E =
0010872
Z = 4744281
60 I = 51
62610
XDOT = -6935
297784 Wp = 61
55329
YDOT = -1815
756489 meter/sec RA = 357
21696 deg
ZDOT = -2715
609940 TA = 55
35988
MA = 55
25743
Ha = 227
999 n
mi
Hp = 219
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9468024
59 X = -2952313
12
Y = 12800118
04 feet Y = 3868833
60 meter
Z = 15565228
34 Z = 4730100
34
XDOT = -22753
601654 XDOT = -6901
286383
YDOT = -5957
206328 feet/sec YDOT = -1893
121612 meter/sec
ZDOT = -8909
481431 ZDOT = -2749
218281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3878736
25 X = 1182238
81
Y = 15501894
32 feet Y = 4724977
39 meter
Z = 15505145
03 Z = 4725968
20
XDOT = -17829
179738 XDOT = -5434
333984
YDOT = 13545
434591 feet/sec YDOT = 4128
648463 meter/sec
ZDOT = -9050
196342 ZDOT = -2758
499845
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 13263
18914857
00016717 00000-0 10270-3 0 9117
2 25544 51
6514 357
5566 0003062 59
9096 300
2359 15
50383005 9449
Satellite: ISS
Catalog Number: 25544
Epoch time: 13263
18914857 = yrday
fracday
Element set: 911
Inclination: 51
6514 deg
RA of node: 357
5566 deg
Eccentricity:
0003062
Arg of perigee: 59
9096 deg
Mean anomaly: 300
2359 deg
Mean motion: 15
50383005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 944
Checksum: 310
Coasting Arc #13 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2013/264/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3056555
63 A = 6791713
93 meter
Y = -4041982
65 meter E =
0011913
Z = -4533077
96 I = 51
59704
XDOT = 6786
112930 Wp = 99
20347
YDOT = 1600
301666 meter/sec RA = 352
25594 deg
ZDOT = 3154
035498 TA = 202
50197
MA = 202
55426
Ha = 227
995 n
mi
Hp = 219
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10028069
67 X = 3123547
46
Y = -13261097
93 feet Y = -4007428
34 meter
Z = -14872303
02 Z = -4518066
10
XDOT = 22264
150033 XDOT = 6752
392057
YDOT = 5250
333550 feet/sec YDOT = 1676
000172 meter/sec
ZDOT = 10347
885491 ZDOT = 3186
919983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4163353
39 X = -1268990
11
Y = -16154648
63 feet Y = -4923936
90 meter
Z = -14808717
47 Z = -4513697
08
XDOT = 16677
296280 XDOT = 5083
239906
YDOT = -13894
200539 feet/sec YDOT = -4234
952324 meter/sec
ZDOT = 10485
585829 ZDOT = 3196
006561
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 13264
15603459
00016717 00000-0 10270-3 0 9129
2 25544 51
6502 352
7638 0003078 64
1751 295
9717 15
50364095 9598
Satellite: ISS
Catalog Number: 25544
Epoch time: 13264
15603459 = yrday
fracday
Element set: 912
Inclination: 51
6502 deg
RA of node: 352
7638 deg
Eccentricity:
0003078
Arg of perigee: 64
1751 deg
Mean anomaly: 295
9717 deg
Mean motion: 15
50364095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 321
Coasting Arc #14 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2013/265/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3230349
74 A = 6792611
95 meter
Y = 4188186
21 meter E =
0013059
Z = 4253797
79 I = 51
57016
XDOT = -6615
491365 Wp = 71
59033
YDOT = -1434
865022 meter/sec RA = 347
29419 deg
ZDOT = -3597
975701 TA = 55
27836
MA = 55
15543
Ha = 227
977 n
mi
Hp = 219
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10598260
29 X = -3297606
89
Y = 13740768
40 feet Y = 4151686
84 meter
Z = 13956029
50 Z = 4237941
00
XDOT = -21704
367994 XDOT = -6581
476520
YDOT = -4707
562407 feet/sec YDOT = -1508
653897 meter/sec
ZDOT = -11804
382221 ZDOT = -3630
030718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4481143
28 X = 1365852
47
Y = 16820254
42 feet Y = 5126813
55 meter
Z = 13888880
19 Z = 4233330
68
XDOT = -15605
710590 XDOT = -4756
620588
YDOT = 14051
284970 feet/sec YDOT = 4282
831659 meter/sec
ZDOT = -11938
619283 ZDOT = -3638
891158
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 13265
18737055
00016717 00000-0 10270-3 0 9134
2 25544 51
6503 347
6522 0003023 65
2172 294
9294 15
50401681 9753
Satellite: ISS
Catalog Number: 25544
Epoch time: 13265
18737055 = yrday
fracday
Element set: 913
Inclination: 51
6503 deg
RA of node: 347
6522 deg
Eccentricity:
0003023
Arg of perigee: 65
2172 deg
Mean anomaly: 294
9294 deg
Mean motion: 15
50401681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 301
Coasting Arc #15 (Orbit 989)
---------------------------------------
Vector Time (GMT): 2013/266/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3352221
70 A = 6793656
62 meter
Y = -4380737
00 meter E =
0009345
Z = -3974272
30 I = 51
54200
XDOT = 6403
525708 Wp = 95
18873
YDOT = 1286
428657 meter/sec RA = 342
32978 deg
ZDOT = 3990
540600 TA = 216
52303
MA = 216
58680
Ha = 228
003 n
mi
Hp = 219
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10998102
69 X = 3420265
08
Y = -14372496
71 feet Y = -4342870
29 meter
Z = -13038951
10 Z = -3957821
58
XDOT = 21008
942611 XDOT = 6369
279457
YDOT = 4220
566461 feet/sec YDOT = 1357
845886 meter/sec
ZDOT = 13092
324802 ZDOT = 4021
565393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5046390
66 X = -1538139
87
Y = -17431947
62 feet Y = -5313257
63 meter
Z = -12969283
48 Z = -3953037
60
XDOT = 14502
799617 XDOT = 4420
453323
YDOT = -14017
838736 feet/sec YDOT = -4272
637247 meter/sec
ZDOT = 13222
256303 ZDOT = 4030
143721
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 13266
15424364
00016717 00000-0 10270-3 0 9149
2 25544 51
6487 342
8589 0003075 71
1563 288
9921 15
50381438 9905
Satellite: ISS
Catalog Number: 25544
Epoch time: 13266
15424364 = yrday
fracday
Element set: 914
Inclination: 51
6487 deg
RA of node: 342
8589 deg
Eccentricity:
0003075
Arg of perigee: 71
1563 deg
Mean anomaly: 288
9921 deg
Mean motion: 15
50381438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 990
Checksum: 328
Coasting Arc #16 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2013/267/03:29:45
386
Vector Time (MET): N/A
Weight (LBS) : 927530
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3472267
49 A = 6794650
75 meter
Y = 4570244
47 meter E =
0014875
Z = 3625222
57 I = 51
51687
XDOT = -6173
921895 Wp = 83
21092
YDOT = -1200
494068 meter/sec RA = 337
36501 deg
ZDOT = -4382
783250 TA = 53
77422
MA = 53
63681
Ha = 227
949 n
mi
Hp = 219
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11391953
72 X = -3540725
45
Y = 14994240
39 feet Y = 4531032
92 meter
Z = 11893774
83 Z = 3608187
73
XDOT = -20255
649263 XDOT = -6138
748235
YDOT = -3938
628833 feet/sec YDOT = -1269
338510 meter/sec
ZDOT = -14379
210137 ZDOT = -4412
690386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5630031
81 X = 1716033
69
Y = 18017145
41 feet Y = 5491625
92 meter
Z = 11821630
47 Z = 3603232
97
XDOT = -13540
853806 XDOT = -4127
252240
YDOT = 13785
392061 feet/sec YDOT = 4201
787500 meter/sec
ZDOT = -14504
462151 ZDOT = -4420
960064
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 13267
18556553
00016717 00000-0 10270-3 0 9150
2 25544 51
6489 337
7469 0002984 71
7233 288
4243 15
50419208 10063
Satellite: ISS
Catalog Number: 25544
Epoch time: 13267
18556553 = yrday
fracday
Element set: 915
Inclination: 51
6489 deg
RA of node: 337
7469 deg
Eccentricity:
0002984
Arg of perigee: 71
7233 deg
Mean anomaly: 288
4243 deg
Mean motion: 15
50419208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 327
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