[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 3rd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 185 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 188)
---------------------------------------
Vector Time (GMT): 2013/214/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4439413
86 A = 6789864
05 meter
Y = 620497
18 meter E =
0009751
Z = -5108675
56 I = 51
32856
XDOT = -2827
868431 Wp = 109
78630
YDOT = -6927
123190 meter/sec RA = 237
84336 deg
ZDOT = 1615
328041 TA = 175
89949
MA = 175
89149
Ha = 225
830 n
mi
Hp = 222
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14565006
11 X = -4421206
25
Y = 2035751
91 feet Y = 570954
99 meter
Z = -16760746
59 Z = -5130197
26
XDOT = -9277
783565 XDOT = -2758
044371
YDOT = -22726
782118 feet/sec YDOT = -6958
355904 meter/sec
ZDOT = 5299
632679 ZDOT = 1601
759840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11495498
29 X = 3503827
88
Y = 9005909
18 feet Y = 2745001
12 meter
Z = -16850917
90 Z = -5136159
78
XDOT = -9256
762396 XDOT = -2821
461178
YDOT = 21631
621132 feet/sec YDOT = 6593
318121 meter/sec
ZDOT = 5243
763911 ZDOT = 1598
299240
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 13214
52302331
00016717 00000-0 10270-3 0 9007
2 25544 51
6492 238
7522 0004054 263
9224 96
1464 15
50130595 1891
Satellite: ISS
Catalog Number: 25544
Epoch time: 13214
52302331 = yrday
fracday
Element set: 900
Inclination: 51
6492 deg
RA of node: 238
7522 deg
Eccentricity:
0004054
Arg of perigee: 263
9224 deg
Mean anomaly: 96
1464 deg
Mean motion: 15
50130595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 189
Checksum: 282
Coasting Arc #2 (Orbit 204)
---------------------------------------
Vector Time (GMT): 2013/215/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4578756
01 A = 6790258
61 meter
Y = -556044
57 meter E =
0003313
Z = 4983397
89 I = 51
34576
XDOT = 3044
470666 Wp = 18
40184
YDOT = 6727
363164 meter/sec RA = 232
86472 deg
ZDOT = -2043
172879 TA = 91
58450
MA = 91
54654
Ha = 225
644 n
mi
Hp = 222
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15022165
40 X = 4560425
94
Y = -1824293
20 feet Y = -504944
82 meter
Z = 16349730
61 Z = 5005596
14
XDOT = 9988
420820 XDOT = 2978
942566
YDOT = 22071
401456 feet/sec YDOT = 6761
042101 meter/sec
ZDOT = -6703
323094 ZDOT = -2028
542109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11823444
90 X = -3603786
01
Y = -9281693
76 feet Y = -2829060
26 meter
Z = 16442734
01 Z = 5011745
32
XDOT = 7876
606861 XDOT = 2400
789771
YDOT = -21821
726483 feet/sec YDOT = -6651
262232 meter/sec
ZDOT = -6642
963388 ZDOT = -2024
775241
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 13215
55449703
00016717 00000-0 10270-3 0 9017
2 25544 51
6475 233
6409 0003944 268
1578 91
9120 15
50169353 2051
Satellite: ISS
Catalog Number: 25544
Epoch time: 13215
55449703 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 233
6409 deg
Eccentricity:
0003944
Arg of perigee: 268
1578 deg
Mean anomaly: 91
9120 deg
Mean motion: 15
50169353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 205
Checksum: 302
Coasting Arc #3 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2013/216/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4742220
22 A = 6790928
65 meter
Y = 522639
60 meter E =
0007916
Z = -4840241
48 I = 51
36738
XDOT = -3223
541147 Wp = 115
20440
YDOT = -6494
284107 meter/sec RA = 227
88817 deg
ZDOT = 2456
879848 TA = 179
05441
MA = 179
05291
Ha = 225
772 n
mi
Hp = 222
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15558465
29 X = -4724199
91
Y = 1714696
85 feet Y = 469710
10 meter
Z = -15880057
35 Z = -4863234
52
XDOT = -10575
922399 XDOT = -3162
615695
YDOT = -21306
706387 feet/sec YDOT = -6529
991260 meter/sec
ZDOT = 8060
629423 ZDOT = 2441
368117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12292217
85 X = 3746668
00
Y = 9530923
45 feet Y = 2905025
47 meter
Z = -15976392
81 Z = -4869604
53
XDOT = -6506
769186 XDOT = -1983
263248
YDOT = 21797
017553 feet/sec YDOT = 6643
730950 meter/sec
ZDOT = 7996
533459 ZDOT = 2437
343398
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 13216
52149717
00016717 00000-0 10270-3 0 9028
2 25544 51
6478 228
8497 0004046 272
8634 87
2053 15
50149700 2200
Satellite: ISS
Catalog Number: 25544
Epoch time: 13216
52149717 = yrday
fracday
Element set: 902
Inclination: 51
6478 deg
RA of node: 228
8497 deg
Eccentricity:
0004046
Arg of perigee: 272
8634 deg
Mean anomaly: 87
2053 deg
Mean motion: 15
50149700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 220
Checksum: 302
Coasting Arc #4 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2013/217/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4917337
30 A = 6791527
99 meter
Y = -505562
45 meter E =
0005172
Z = 4656229
35 I = 51
38977
XDOT = 3365
232279 Wp = 38
99579
YDOT = 6256
698662 meter/sec RA = 222
91232 deg
ZDOT = -2868
922656 TA = 79
66637
MA = 79
60808
Ha = 225
630 n
mi
Hp = 222
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16132996
38 X = 4900006
91
Y = -1658669
47 feet Y = -450670
75 meter
Z = 15276343
03 Z = 4680074
73
XDOT = 11040
788318 XDOT = 3308
954561
YDOT = 20527
226583 feet/sec YDOT = 6294
016264 meter/sec
ZDOT = -9412
475904 ZDOT = -2852
711453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12838109
60 X = -3913055
81
Y = -9754238
13 feet Y = -2973091
78 meter
Z = 15376254
20 Z = 4686682
28
XDOT = 5220
730265 XDOT = 1591
278585
YDOT = -21632
288851 feet/sec YDOT = -6593
521642 meter/sec
ZDOT = -9345
402607 ZDOT = -2848
478715
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 13217
55295613
00016717 00000-0 10270-3 0 9030
2 25544 51
6464 223
7379 0004024 277
2766 82
7927 15
50190893 2365
Satellite: ISS
Catalog Number: 25544
Epoch time: 13217
55295613 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 223
7379 deg
Eccentricity:
0004024
Arg of perigee: 277
2766 deg
Mean anomaly: 82
7927 deg
Mean motion: 15
50190893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 319
Coasting Arc #5 (Orbit 250)
---------------------------------------
Vector Time (GMT): 2013/218/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5103791
45 A = 6792374
08 meter
Y = 529268
80 meter E =
0005460
Z = -4456194
06 I = 51
41552
XDOT = -3466
511040 Wp = 117
15966
YDOT = -5998
807509 meter/sec RA = 217
93927 deg
ZDOT = 3258
442483 TA = 185
82387
MA = 185
83022
Ha = 225
803 n
mi
Hp = 222
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16744722
62 X = -5087684
01
Y = 1736446
19 feet Y = 472285
13 meter
Z = -14620059
25 Z = -4480948
16
XDOT = -11373
067718 XDOT = -3415
001724
YDOT = -19681
126998 feet/sec YDOT = -6037
284293 meter/sec
ZDOT = 10690
428094 ZDOT = 3241
727830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13512810
84 X = 4118704
74
Y = 9887422
87 feet Y = 3013686
49 meter
Z = -14723787
75 Z = -4487810
51
XDOT = -4001
905536 XDOT = -1219
780807
YDOT = 21282
612098 feet/sec YDOT = 6486
940168 meter/sec
ZDOT = 10621
196236 ZDOT = 3237
340613
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 13218
51994245
00016717 00000-0 10270-3 0 9045
2 25544 51
6464 218
9464 0004057 281
9355 78
1340 15
50168939 2519
Satellite: ISS
Catalog Number: 25544
Epoch time: 13218
51994245 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 218
9464 deg
Eccentricity:
0004057
Arg of perigee: 281
9355 deg
Mean anomaly: 78
1340 deg
Mean motion: 15
50168939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 251
Checksum: 318
Coasting Arc #6 (Orbit 266)
---------------------------------------
Vector Time (GMT): 2013/219/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5295674
58 A = 6793125
29 meter
Y = -568868
03 meter E =
0006888
Z = 4214141
21 I = 51
44264
XDOT = 3522
867791 Wp = 55
58581
YDOT = 5746
173262 meter/sec RA = 212
96741 deg
ZDOT = -3643
229846 TA = 71
90254
MA = 71
82752
Ha = 225
724 n
mi
Hp = 222
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17374260
43 X = 5281171
46
Y = -1866364
94 feet Y = -509729
54 meter
Z = 13825922
62 Z = 4239831
37
XDOT = 11557
965192 XDOT = 3476
048463
YDOT = 18852
274482 feet/sec YDOT = 5785
306424 meter/sec
ZDOT = -11952
853825 ZDOT = -3626
230135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14244119
81 X = -4341607
72
Y = -9973196
21 feet Y = -3039830
21 meter
Z = 13933584
89 Z = 4246956
67
XDOT = 2921
261737 XDOT = 890
400577
YDOT = -20809
938060 feet/sec YDOT = -6342
869121 meter/sec
ZDOT = -11882
380126 ZDOT = -3621
749463
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 13219
55138636
00016717 00000-0 10270-3 0 9055
2 25544 51
6458 213
8344 0004135 286
2829 73
7866 15
50212307 2674
Satellite: ISS
Catalog Number: 25544
Epoch time: 13219
55138636 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 213
8344 deg
Eccentricity:
0004135
Arg of perigee: 286
2829 deg
Mean anomaly: 73
7866 deg
Mean motion: 15
50212307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 267
Checksum: 313
Coasting Arc #7 (Orbit 281)
---------------------------------------
Vector Time (GMT): 2013/220/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5484209
46 A = 6794072
35 meter
Y = 654656
05 meter E =
0002793
Z = -3959387
41 I = 51
47204
XDOT = -3540
474690 Wp = 102
42679
YDOT = -5488
029055 meter/sec RA = 207
99858 deg
ZDOT = 3998
365478 TA = 209
43469
MA = 209
45042
Ha = 225
909 n
mi
Hp = 222
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17992813
18 X = -5471889
09
Y = 2147821
70 feet Y = 593396
97 meter
Z = -12990116
17 Z = -3985998
79
XDOT = -11615
730609 XDOT = -3498
265833
YDOT = -18005
344670 feet/sec YDOT = -5527
384818 meter/sec
ZDOT = 13117
996975 ZDOT = 3981
269104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15071769
90 X = 4593875
47
Y = 9913927
11 feet Y = 3021764
98 meter
Z = -13101655
77 Z = -3993384
68
XDOT = -1953
171433 XDOT = -595
326653
YDOT = 20203
809244 feet/sec YDOT = 6158
121057 meter/sec
ZDOT = 13047
071957 ZDOT = 3976
747533
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 13220
51835862
00016717 00000-0 10270-3 0 9069
2 25544 51
6459 209
0426 0004086 290
9897 69
0817 15
50191381 2824
Satellite: ISS
Catalog Number: 25544
Epoch time: 13220
51835862 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 209
0426 deg
Eccentricity:
0004086
Arg of perigee: 290
9897 deg
Mean anomaly: 69
0817 deg
Mean motion: 15
50191381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 282
Checksum: 317
Coasting Arc #8 (Orbit 297)
---------------------------------------
Vector Time (GMT): 2013/221/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5671293
81 A = 6794908
24 meter
Y = -753540
28 meter E =
0008355
Z = 3661650
58 I = 51
50281
XDOT = 3508
725541 Wp = 70
68341
YDOT = 5245
970575 meter/sec RA = 203
03172 deg
ZDOT = -4344
029997 TA = 65
78291
MA = 65
69561
Ha = 225
906 n
mi
Hp = 222
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18606606
99 X = 5661511
53
Y = -2472245
01 feet Y = -690174
87 meter
Z = 12013289
29 Z = 3689177
04
XDOT = 11511
566736 XDOT = 3470
904968
YDOT = 17211
189549 feet/sec YDOT = 5284
995772 meter/sec
ZDOT = -14252
066918 ZDOT = -4327
077212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15925545
03 X = -4854106
12
Y = -9793315
39 feet Y = -2985002
53 meter
Z = 12128682
04 Z = 3696822
29
XDOT = 1168
592366 XDOT = 356
186953
YDOT = -19507
442421 feet/sec YDOT = -5945
868450 meter/sec
ZDOT = -14181
701473 ZDOT = -4322
582609
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 13221
54978722
00016717 00000-0 10270-3 0 9077
2 25544 51
6459 203
9308 0004228 295
0665 65
0047 15
50233857 2986
Satellite: ISS
Catalog Number: 25544
Epoch time: 13221
54978722 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 203
9308 deg
Eccentricity:
0004228
Arg of perigee: 295
0665 deg
Mean anomaly: 65
0047 deg
Mean motion: 15
50233857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 298
Checksum: 317
Coasting Arc #9 (Orbit 312)
---------------------------------------
Vector Time (GMT): 2013/222/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5840002
98 A = 6795862
73 meter
Y = 899104
57 meter E =
0002464
Z = -3355817
92 I = 51
53484
XDOT = -3444
473312 Wp = 29
75494
YDOT = -5013
348753 meter/sec RA = 198
06787 deg
ZDOT = 4654
653194 TA = 291
14163
MA = 291
16796
Ha = 226
057 n
mi
Hp = 222
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19160114
77 X = -5833321
47
Y = 2949818
13 feet Y = 833835
19 meter
Z = -11009901
32 Z = -3384171
58
XDOT = -11300
765458 XDOT = -3410
767720
YDOT = -16447
994597 feet/sec YDOT = -5051
678410 meter/sec
ZDOT = 15271
171896 ZDOT = 4638
002509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16826890
73 X = 5128836
29
Y = 9488690
08 feet Y = 2892152
74 meter
Z = -11128785
26 Z = -3392053
75
XDOT = -523
677081 XDOT = -159
616774
YDOT = 18744
768746 feet/sec YDOT = 5713
405514 meter/sec
ZDOT = 15202
033786 ZDOT = 4633
579898
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 13222
51674479
00016717 00000-0 10270-3 0 9088
2 25544 51
6463 199
1390 0004153 299
6344 60
4393 15
50218556 3139
Satellite: ISS
Catalog Number: 25544
Epoch time: 13222
51674479 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 199
1390 deg
Eccentricity:
0004153
Arg of perigee: 299
6344 deg
Mean anomaly: 60
4393 deg
Mean motion: 15
50218556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 313
Checksum: 311
Coasting Arc #10 (Orbit 328)
---------------------------------------
Vector Time (GMT): 2013/223/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6000442
37 A = 6796704
80 meter
Y = -1052489
20 meter E =
0009437
Z = 3006585
99 I = 51
56781
XDOT = 3330
309586 Wp = 84
80352
YDOT = 4807
701311 meter/sec RA = 193
10649 deg
ZDOT = -4949
274611 TA = 60
79651
MA = 60
70214
Ha = 226
126 n
mi
Hp = 222
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19686490
72 X = 5997160
51
Y = -3453048
54 feet Y = -985406
69 meter
Z = 9864127
26 Z = 3035727
41
XDOT = 10926
212552 XDOT = 3300
343335
YDOT = 15773
298264 feet/sec YDOT = 4844
775221 meter/sec
ZDOT = -16237
777595 ZDOT = -4933
169360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17716871
49 X = -5400102
43
Y = -9119647
11 feet Y = -2779668
44 meter
Z = 9986339
12 Z = 3043836
16
XDOT = 92
276078 XDOT = 28
125749
YDOT = -17937
554361 feet/sec YDOT = -5467
366569 meter/sec
ZDOT = -16170
891803 ZDOT = -4928
887821
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 13223
54815769
00016717 00000-0 10270-3 0 9092
2 25544 51
6466 194
0275 0004293 303
4541 56
6199 15
50254997 3293
Satellite: ISS
Catalog Number: 25544
Epoch time: 13223
54815769 = yrday
fracday
Element set: 909
Inclination: 51
6466 deg
RA of node: 194
0275 deg
Eccentricity:
0004293
Arg of perigee: 303
4541 deg
Mean anomaly: 56
6199 deg
Mean motion: 15
50254997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 329
Checksum: 329
Coasting Arc #11 (Orbit 343)
---------------------------------------
Vector Time (GMT): 2013/224/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6128736
21 A = 6797566
58 meter
Y = 1248101
95 meter E =
0005400
Z = -2654835
28 I = 51
60094
XDOT = -3193
972455 Wp = 7
58867
YDOT = -4625
019656 meter/sec RA = 188
14794 deg
ZDOT = 5205
452781 TA = 322
50648
MA = 322
54413
Ha = 226
221 n
mi
Hp = 221
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20107402
28 X = -6129340
86
Y = 4094822
67 feet Y = 1179563
09 meter
Z = -8710089
52 Z = -2684609
47
XDOT = -10478
912254 XDOT = -3167
303634
YDOT = -15173
949004 feet/sec YDOT = -4660
587434 meter/sec
ZDOT = 17078
257154 ZDOT = 5190
001732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18595767
49 X = 5667989
93
Y = 8548759
94 feet Y = 2605662
03 meter
Z = -8834986
90 Z = -2692904
01
XDOT = 194
626989 XDOT = 59
322306
YDOT = 17138
847808 feet/sec YDOT = 5223
920812 meter/sec
ZDOT = 17014
083933 ZDOT = 5185
892783
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 13224
51509974
00016717 00000-0 10270-3 0 9100
2 25544 51
6468 189
2359 0004260 307
5543 52
5220 15
50249123 3447
Satellite: ISS
Catalog Number: 25544
Epoch time: 13224
51509974 = yrday
fracday
Element set: 910
Inclination: 51
6468 deg
RA of node: 189
2359 deg
Eccentricity:
0004260
Arg of perigee: 307
5543 deg
Mean anomaly: 52
5220 deg
Mean motion: 15
50249123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 344
Checksum: 291
Coasting Arc #12 (Orbit 359)
---------------------------------------
Vector Time (GMT): 2013/225/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6242863
25 A = 6798324
16 meter
Y = -1443852
96 meter E =
0009977
Z = 2260247
69 I = 51
63472
XDOT = 3011
509797 Wp = 98
01338
YDOT = 4478
951528 meter/sec RA = 183
19193 deg
ZDOT = -5437
465681 TA = 56
88251
MA = 56
78679
Ha = 226
345 n
mi
Hp = 221
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20481834
83 X = 6247565
12
Y = -4737050
39 feet Y = -1374014
99 meter
Z = 7415510
80 Z = 2290586
28
XDOT = 9880
281487 XDOT = 2987
614996
YDOT = 14694
722862 feet/sec YDOT = 4512
494480 meter/sec
ZDOT = -17839
454335 ZDOT = -5422
894180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19423072
03 X = -5920152
36
Y = -7923717
46 feet Y = -2415149
08 meter
Z = 7542809
76 Z = 2299048
42
XDOT = -258
773763 XDOT = -78
874243
YDOT = -16349
016961 feet/sec YDOT = -4983
180370 meter/sec
ZDOT = -17778
943425 ZDOT = -5419
021956
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 13225
54649633
00016717 00000-0 10270-3 0 9112
2 25544 51
6473 184
1244 0004343 311
3089 48
7688 15
50275411 3602
Satellite: ISS
Catalog Number: 25544
Epoch time: 13225
54649633 = yrday
fracday
Element set: 911
Inclination: 51
6473 deg
RA of node: 184
1244 deg
Eccentricity:
0004343
Arg of perigee: 311
3089 deg
Mean anomaly: 48
7688 deg
Mean motion: 15
50275411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 360
Checksum: 298
Coasting Arc #13 (Orbit 374)
---------------------------------------
Vector Time (GMT): 2013/226/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6313746
56 A = 6799000
83 meter
Y = 1673024
36 meter E =
0008622
Z = -1869483
29 I = 51
66751
XDOT = -2820
416313 Wp = 9
44361
YDOT = -4366
548447 meter/sec RA = 178
23847 deg
ZDOT = 5629
610793 TA = 330
02062
MA = 330
06996
Ha = 226
402 n
mi
Hp = 221
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20714391
60 X = -6322904
03
Y = 5488925
07 feet Y = 1602368
86 meter
Z = -6133475
37 Z = -1900177
01
XDOT = -9253
334360 XDOT = -2798
726006
YDOT = -14325
946348 feet/sec YDOT = -4397
966895 meter/sec
ZDOT = 18469
851683 ZDOT = 5615
962174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20178569
17 X = 6150427
88
Y = 7102303
10 feet Y = 2164781
98 meter
Z = -6262305
88 Z = -1908750
83
XDOT = 197
187684 XDOT = 60
102806
YDOT = 15641
239494 feet/sec YDOT = 4767
449798 meter/sec
ZDOT = 18413
189341 ZDOT = 5612
340111
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 13226
51342222
00016717 00000-0 10270-3 0 9125
2 25544 51
6470 179
3326 0004378 314
8971 45
1824 15
50279473 3753
Satellite: ISS
Catalog Number: 25544
Epoch time: 13226
51342222 = yrday
fracday
Element set: 912
Inclination: 51
6470 deg
RA of node: 179
3326 deg
Eccentricity:
0004378
Arg of perigee: 314
8971 deg
Mean anomaly: 45
1824 deg
Mean motion: 15
50279473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 375
Checksum: 302
Coasting Arc #14 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2013/227/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6366471
92 A = 6799571
55 meter
Y = -1892574
93 meter E =
0009837
Z = 1437762
92 I = 51
70100
XDOT = 2591
292526 Wp = 110
12465
YDOT = 4297
697350 meter/sec RA = 173
28745 deg
ZDOT = -5788
260132 TA = 54
23548
MA = 54
14405
Ha = 226
548 n
mi
Hp = 221
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20887375
06 X = 6380177
72
Y = -6209235
34 feet Y = -1821304
41 meter
Z = 4717069
94 Z = 1468723
71
XDOT = 8501
615900 XDOT = 2571
159761
YDOT = 14100
056923 feet/sec YDOT = 4326
562388 meter/sec
ZDOT = -18990
354763 ZDOT = -5775
720753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20844950
51 X = -6353540
92
Y = -6251543
39 feet Y = -1905470
42 meter
Z = 4847064
33 Z = 1477385
21
XDOT = 72
274899 XDOT = 22
029389
YDOT = -14996
119993 feet/sec YDOT = -4570
817374 meter/sec
ZDOT = -18938
327471 ZDOT = -5772
402213
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 13227
54480187
00016717 00000-0 10270-3 0 9133
2 25544 51
6478 174
2209 0004386 318
7075 41
3744 15
50296172 3914
Satellite: ISS
Catalog Number: 25544
Epoch time: 13227
54480187 = yrday
fracday
Element set: 913
Inclination: 51
6478 deg
RA of node: 174
2209 deg
Eccentricity:
0004386
Arg of perigee: 318
7075 deg
Mean anomaly: 41
3744 deg
Mean motion: 15
50296172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 311
Coasting Arc #15 (Orbit 405)
---------------------------------------
Vector Time (GMT): 2013/228/12:13:54
725
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6368688
05 A = 6799990
25 meter
Y = 2133455
94 meter E =
0011478
Z = -1016876
66 I = 51
73256
XDOT = -2369
050432 Wp = 16
65967
YDOT = -4269
261685 meter/sec RA = 168
33869 deg
ZDOT = 5907
468528 TA = 332
34898
MA = 332
40998
Ha = 226
604 n
mi
Hp = 221
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20894645
83 X = -6387131
83
Y = 6999527
35 feet Y = 2062134
14 meter
Z = -3336209
51 Z = -1047859
58
XDOT = -7772
475171 XDOT = -2349
831121
YDOT = -14006
764059 feet/sec YDOT = -4295
646621 meter/sec
ZDOT = 19381
458424 ZDOT = 5896
006573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21384975
92 X = 6518140
66
Y = 5232318
48 feet Y = 1594810
67 meter
Z = -3466345
31 Z = -1056542
05
XDOT = -426
912936 XDOT = -130
123063
YDOT = 14496
328933 feet/sec YDOT = 4418
481059 meter/sec
ZDOT = 19333
937874 ZDOT = 5892
984264
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 13228
51171142
00016717 00000-0 10270-3 0 9140
2 25544 51
6475 169
4289 0004476 322
1041 37
9794 15
50306472 4065
Satellite: ISS
Catalog Number: 25544
Epoch time: 13228
51171142 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node: 169
4289 deg
Eccentricity:
0004476
Arg of perigee: 322
1041 deg
Mean anomaly: 37
9794 deg
Mean motion: 15
50306472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 406
Checksum: 299
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