[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 20th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20289 97 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
243/07:34:14
249 0
3 1
1 1
1
N/A 1
0 -0
1 227
5
000/00:02:28
499 -0
3 -0
1 220
4
Coasting Arc #1 (Orbit 452)
---------------------------------------
Vector Time (GMT): 2013/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2442125
79 A = 6793114
50 meter
Y = -4826208
36 meter E =
0010250
Z = 4107238
15 I = 51
79846
XDOT = 6629
541392 Wp = 52
29038
YDOT = 75
754791 meter/sec RA = 153
53683 deg
ZDOT = -3840
178528 TA = 77
39494
MA = 77
28034
Ha = 226
781 n
mi
Hp = 221
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8012223
73 X = 2475960
59
Y = -15834016
92 feet Y = -4798709
71 meter
Z = 13475190
79 Z = 4119183
78
XDOT = 21750
463883 XDOT = 6646
855703
YDOT = 248
539341 feet/sec YDOT = 149
987274 meter/sec
ZDOT = -12599
010920 ZDOT = -3807
931468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15243827
41 X = -4646318
60
Y = 9009382
13 feet Y = 2746059
67 meter
Z = 13525876
95 Z = 4122687
29
XDOT = -17553
532418 XDOT = -5350
316681
YDOT = -10926
293805 feet/sec YDOT = -3330
334352 meter/sec
ZDOT = -12463
793097 ZDOT = -3798
964136
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 13231
54134410
00016717 00000-0 10270-3 0 9009
2 25544 51
6486 154
4251 0004426 331
5279 28
5629 15
50366609 4535
Satellite: ISS
Catalog Number: 25544
Epoch time: 13231
54134410 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 154
4251 deg
Eccentricity:
0004426
Arg of perigee: 331
5279 deg
Mean anomaly: 28
5629 deg
Mean motion: 15
50366609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 453
Checksum: 288
Coasting Arc #2 (Orbit 467)
---------------------------------------
Vector Time (GMT): 2013/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2510363
78 A = 6794026
69 meter
Y = 5038177
75 meter E =
0004797
Z = -3805773
63 I = 51
82958
XDOT = -6386
451973 Wp = 58
01008
YDOT = 6
203607 meter/sec RA = 148
59101 deg
ZDOT = 4227
222757 TA = 256
55623
MA = 256
60969
Ha = 226
847 n
mi
Hp = 221
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8236101
65 X = -2548028
20
Y = 16529454
55 feet Y = 5009894
52 meter
Z = -12486133
95 Z = -3818060
17
XDOT = -20952
926422 XDOT = -6406
580947
YDOT = 20
353042 feet/sec YDOT = -65
326122 meter/sec
ZDOT = 13868
841065 ZDOT = 4196
149735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15648841
69 X = 4769766
95
Y = -9739870
02 feet Y = -2968712
38 meter
Z = -12538279
98 Z = -3821667
74
XDOT = 17175
622482 XDOT = 5235
129732
YDOT = 9936
734057 feet/sec YDOT = 3028
716541 meter/sec
ZDOT = 13738
523151 ZDOT = 4187
501857
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 13232
50820779
00016717 00000-0 10270-3 0 9017
2 25544 51
6492 149
6325 0004467 334
9539 25
1395 15
50399417 4683
Satellite: ISS
Catalog Number: 25544
Epoch time: 13232
50820779 = yrday
fracday
Element set: 901
Inclination: 51
6492 deg
RA of node: 149
6325 deg
Eccentricity:
0004467
Arg of perigee: 334
9539 deg
Mean anomaly: 25
1395 deg
Mean motion: 15
50399417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 468
Checksum: 324
Coasting Arc #3 (Orbit 483)
---------------------------------------
Vector Time (GMT): 2013/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2579645
53 A = 6795129
25 meter
Y = -5256088
77 meter E =
0011514
Z = 3443675
45 I = 51
85901
XDOT = 6125
141327 Wp = 68
36380
YDOT = -20
238678 meter/sec RA = 143
64836 deg
ZDOT = -4602
717429 TA = 71
50069
MA = 71
37560
Ha = 226
936 n
mi
Hp = 220
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8463403
98 X = 2621500
42
Y = -17244385
74 feet Y = -5227007
30 meter
Z = 11298147
81 Z = 3456308
89
XDOT = 20095
608027 XDOT = 6147
270735
YDOT = -66
399863 feet/sec YDOT = 48
379981 meter/sec
ZDOT = -15100
778966 ZDOT = -4572
908865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16047073
16 X = -4891147
90
Y = 10501177
45 feet Y = 3200758
89 meter
Z = 11351779
83 Z = 3460022
49
XDOT = -16602
196747 XDOT = -5060
349569
YDOT = -9123
146762 feet/sec YDOT = -2780
735133 meter/sec
ZDOT = -14975
752210 ZDOT = -4564
609274
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 13233
53951628
00016717 00000-0 10270-3 0 9020
2 25544 51
6492 144
5210 0004456 338
7340 21
3625 15
50403433 4846
Satellite: ISS
Catalog Number: 25544
Epoch time: 13233
53951628 = yrday
fracday
Element set: 902
Inclination: 51
6492 deg
RA of node: 144
5210 deg
Eccentricity:
0004456
Arg of perigee: 338
7340 deg
Mean anomaly: 21
3625 deg
Mean motion: 15
50403433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 484
Checksum: 280
Coasting Arc #4 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2013/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2582261
63 A = 6796020
12 meter
Y = 5479828
42 meter E =
0006259
Z = -3076258
66 I = 51
88714
XDOT = -5862
436444 Wp = 28
24911
YDOT =
405756 meter/sec RA = 138
70731 deg
ZDOT = 4931
211529 TA = 296
61787
MA = 296
68197
Ha = 226
972 n
mi
Hp = 220
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8471986
98 X = -2628402
94
Y = 17978439
70 feet Y = 5450693
71 meter
Z = -10092712
13 Z = -3088915
36
XDOT = -19233
715368 XDOT = -5885
959408
YDOT = 1
331219 feet/sec YDOT = -65
282875 meter/sec
ZDOT = 16178
515514 ZDOT = 4902
675633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16243511
72 X = 4951022
37
Y = -11404344
36 feet Y = -3476044
16 meter
Z = -10146474
87 Z = -3092645
54
XDOT = 15936
812286 XDOT = 4857
540385
YDOT = 8439
130509 feet/sec YDOT = 2572
246979 meter/sec
ZDOT = 16058
821319 ZDOT = 4894
728738
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 13234
50635444
00016717 00000-0 10270-3 0 9034
2 25544 51
6497 139
7282 0004515 341
7925 18
3064 15
50444083 4990
Satellite: ISS
Catalog Number: 25544
Epoch time: 13234
50635444 = yrday
fracday
Element set: 903
Inclination: 51
6497 deg
RA of node: 139
7282 deg
Eccentricity:
0004515
Arg of perigee: 341
7925 deg
Mean anomaly: 18
3064 deg
Mean motion: 15
50444083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 308
Coasting Arc #5 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2013/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2584741
85 A = 6797088
48 meter
Y = -5697880
71 meter E =
0012196
Z = 2647537
29 I = 51
91260
XDOT = 5592
557042 Wp = 83
36892
YDOT = 93
890253 meter/sec RA = 133
76902 deg
ZDOT = -5235
791593 TA = 66
95319
MA = 66
82464
Ha = 227
082 n
mi
Hp = 220
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8480124
18 X = 2635403
81
Y = -18693834
36 feet Y = -5668693
01 meter
Z = 8686145
96 Z = 2660217
12
XDOT = 18348
284260 XDOT = 5616
525287
YDOT = 308
038887 feet/sec YDOT = 156
563362 meter/sec
ZDOT = -17177
793940 ZDOT = -5208
565529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16405214
82 X = -5000309
48
Y = 12300475
66 feet Y = 3749184
98 meter
Z = 8740040
39 Z = 2663964
31
XDOT = -15115
259489 XDOT = -4607
131092
YDOT = -7983
760980 feet/sec YDOT = -2433
450347 meter/sec
ZDOT = -17063
599148 ZDOT = -5200
985020
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 13235
53763610
00016717 00000-0 10270-3 0 9046
2 25544 51
6492 134
6162 0004486 345
7063 14
3960 15
50437161 5159
Satellite: ISS
Catalog Number: 25544
Epoch time: 13235
53763610 = yrday
fracday
Element set: 904
Inclination: 51
6492 deg
RA of node: 134
6162 deg
Eccentricity:
0004486
Arg of perigee: 345
7063 deg
Mean anomaly: 14
3960 deg
Mean motion: 15
50437161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 289
Coasting Arc #6 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2013/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2519292
90 A = 6797820
01 meter
Y = 5904611
18 meter E =
0009437
Z = -2221925
54 I = 51
93655
XDOT = -5341
693204 Wp = 20
04118
YDOT = -219
265147 meter/sec RA = 128
83202 deg
ZDOT = 5489
416849 TA = 315
41253
MA = 315
48840
Ha = 227
093 n
mi
Hp = 220
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8265396
66 X = -2574338
87
Y = 19372083
93 feet Y = 5876130
90 meter
Z = -7289781
94 Z = -2234298
11
XDOT = -17525
240170 XDOT = -5365
510254
YDOT = -719
373841 feet/sec YDOT = -279
132094 meter/sec
ZDOT = 18009
897797 ZDOT = 5463
409725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16326379
89 X = 4976280
59
Y = -13276802
24 feet Y = -4046769
32 meter
Z = -7342423
34 Z = -2237970
64
XDOT = 14284
356354 XDOT = 4353
871817
YDOT = 7693
669023 feet/sec YDOT = 2345
030318 meter/sec
ZDOT = 17900
826023 ZDOT = 5456
171772
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 13236
50444842
00016717 00000-0 10270-3 0 9058
2 25544 51
6497 129
8231 0004604 348
0536 12
0505 15
50486087 5308
Satellite: ISS
Catalog Number: 25544
Epoch time: 13236
50444842 = yrday
fracday
Element set: 905
Inclination: 51
6497 deg
RA of node: 129
8231 deg
Eccentricity:
0004604
Arg of perigee: 348
0536 deg
Mean anomaly: 12
0505 deg
Mean motion: 15
50486087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 290
Coasting Arc #7 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2013/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2456342
79 A = 6798694
45 meter
Y = -6092838
57 meter E =
0012064
Z = 1737007
42 I = 51
95740
XDOT = 5096
308508 Wp = 96
92473
YDOT = 418
981756 meter/sec RA = 123
89754 deg
ZDOT = -5704
645057 TA = 64
13497
MA = 64
01062
Ha = 227
209 n
mi
Hp = 220
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8058867
41 X = 2515853
80
Y = -19989627
85 feet Y = -6065037
33 meter
Z = 5698843
25 Z = 1749085
02
XDOT = 16720
172269 XDOT = 5118
956099
YDOT = 1374
612060 feet/sec YDOT = 476
098162 meter/sec
ZDOT = -18716
027090 ZDOT = -5679
832774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16199697
59 X = -4937667
83
Y = 14195471
89 feet Y = 4326779
83 meter
Z = 5750283
10 Z = 1752686
29
XDOT = -13357
457871 XDOT = -4071
353159
YDOT = -7661
218994 feet/sec YDOT = -2335
139549 meter/sec
ZDOT = -18611
987278 ZDOT = -5672
933722
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 13237
53570333
00016717 00000-0 10270-3 0 9068
2 25544 51
6493 124
7108 0004524 352
1153 7
9926 15
50468383 5469
Satellite: ISS
Catalog Number: 25544
Epoch time: 13237
53570333 = yrday
fracday
Element set: 906
Inclination: 51
6493 deg
RA of node: 124
7108 deg
Eccentricity:
0004524
Arg of perigee: 352
1153 deg
Mean anomaly: 7
9926 deg
Mean motion: 15
50468383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 301
Coasting Arc #8 (Orbit 560)
---------------------------------------
Vector Time (GMT): 2013/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2330691
22 A = 6799125
74 meter
Y = 6253174
87 meter E =
0012750
Z = -1264728
24 I = 51
97607
XDOT = -4889
017973 Wp = 23
24329
YDOT = -641
834532 meter/sec RA = 118
96383 deg
ZDOT = 5867
754766 TA = 323
08417
MA = 323
17186
Ha = 227
211 n
mi
Hp = 220
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7646624
72 X = -2394298
67
Y = 20515665
59 feet Y = 6226755
89 meter
Z = -4149370
87 Z = -1276205
32
XDOT = -16040
085214 XDOT = -4909
981344
YDOT = -2105
756340 feet/sec YDOT = -696
623537 meter/sec
ZDOT = 19251
163931 ZDOT = 5843
953555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15820962
86 X = 4822229
48
Y = -15121239
40 feet Y = -4608953
77 meter
Z = -4198325
43 Z = -1279649
59
XDOT = 12511
693421 XDOT = 3813
564155
YDOT = 7801
739712 feet/sec YDOT = 2377
970264 meter/sec
ZDOT = 19151
388815 ZDOT = 5837
343311
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 13238
50249005
00016717 00000-0 10270-3 0 9076
2 25544 51
6496 119
9173 0004709 353
9680 6
1414 15
50527018 5610
Satellite: ISS
Catalog Number: 25544
Epoch time: 13238
50249005 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 119
9173 deg
Eccentricity:
0004709
Arg of perigee: 353
9680 deg
Mean anomaly: 6
1414 deg
Mean motion: 15
50527018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 561
Checksum: 300
Coasting Arc #9 (Orbit 576)
---------------------------------------
Vector Time (GMT): 2013/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2214500
25 A = 6799655
11 meter
Y = -6382917
89 meter E =
0010955
Z = 738215
64 I = 51
99151
XDOT = 4699
422676 Wp = 108
20766
YDOT = 931
125436 meter/sec RA = 114
03246 deg
ZDOT = -5977
110958 TA = 63
86856
MA = 63
75589
Ha = 227
310 n
mi
Hp = 220
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7265420
76 X = 2282124
81
Y = -20941331
66 feet Y = -6357775
80 meter
Z = 2421967
32 Z = 749137
95
XDOT = 15418
053399 XDOT = 4717
696426
YDOT = 3054
873477 feet/sec YDOT = 983
779296 meter/sec
ZDOT = -19609
944089 ZDOT = -5954
237332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15402055
21 X = -4694546
43
Y = 15933430
93 feet Y = 4856509
75 meter
Z = 2468625
23 Z = 752436
97
XDOT = -11642
392218 XDOT = -3548
601148
YDOT = -8196
157091 feet/sec YDOT = -2498
188681 meter/sec
ZDOT = -19514
092873 ZDOT = -5947
895508
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 13239
53371829
00016717 00000-0 10270-3 0 9081
2 25544 51
6495 114
8049 0004575 357
8503 2
2628 15
50500570 5778
Satellite: ISS
Catalog Number: 25544
Epoch time: 13239
53371829 = yrday
fracday
Element set: 908
Inclination: 51
6495 deg
RA of node: 114
8049 deg
Eccentricity:
0004575
Arg of perigee: 357
8503 deg
Mean anomaly: 2
2628 deg
Mean motion: 15
50500570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 577
Checksum: 313
Coasting Arc #10 (Orbit 591)
---------------------------------------
Vector Time (GMT): 2013/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2046936
36 A = 6799670
24 meter
Y = 6470874
91 meter E =
0015392
Z = -234591
77 I = 52
00381
XDOT = -4563
262032 Wp = 31
25773
YDOT = -1231
556280 meter/sec RA = 109
10103 deg
ZDOT = 6035
791970 TA = 326
22987
MA = 326
32782
Ha = 227
312 n
mi
Hp = 220
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6715670
47 X = -2118003
39
Y = 21229904
55 feet Y = 6447587
40 meter
Z = -769658
05 Z = -244708
37
XDOT = -14971
332126 XDOT = -4578
471424
YDOT = -4040
538977 feet/sec YDOT = -1282
670417 meter/sec
ZDOT = 19802
467093 ZDOT = 6013
587279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14749827
23 X = 4495747
34
Y = -16678823
17 feet Y = -5083705
30 meter
Z = -812960
63 Z = -247790
40
XDOT = 10939
229912 XDOT = 3334
277277
YDOT = 8742
079039 feet/sec YDOT = 2664
585691 meter/sec
ZDOT = 19709
457141 ZDOT = 6007
442537
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
50047994
00016717 00000-0 10270-3 0 9094
2 25544 51
6494 110
0112 0004781 359
7502
3645 15
50569565 5929
Satellite: ISS
Catalog Number: 25544
Epoch time: 13240
50047994 = yrday
fracday
Element set: 909
Inclination: 51
6494 deg
RA of node: 110
0112 deg
Eccentricity:
0004781
Arg of perigee: 359
7502 deg
Mean anomaly:
3645 deg
Mean motion: 15
50569565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 592
Checksum: 297
Coasting Arc #11 (Orbit 607)
---------------------------------------
Vector Time (GMT): 2013/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1899864
43 A = 6799736
15 meter
Y = -6519009
33 meter E =
0008887
Z = -315035
90 I = 52
01280
XDOT = 4454
061405 Wp = 114
88502
YDOT = 1582
685829 meter/sec RA = 104
17158 deg
ZDOT = -6026
173014 TA = 68
48611
MA = 68
39139
Ha = 227
388 n
mi
Hp = 220
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6233151
03 X = 1974150
57
Y = -21387825
90 feet Y = -6497348
50 meter
Z = -1033582
34 Z = -305625
97
XDOT = 14613
062351 XDOT = 4465
305715
YDOT = 5192
538809 feet/sec YDOT = 1632
556659 meter/sec
ZDOT = -19770
908837 ZDOT = -6004
508493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14088429
56 X = -4294153
33
Y = 17259467
42 feet Y = 5260685
67 meter
Z = -993225
90 Z = -302735
25
XDOT = -10284
522809 XDOT = -3134
722552
YDOT = -9500
669540 feet/sec YDOT = -2895
804076 meter/sec
ZDOT = -19680
207801 ZDOT = -5998
527338
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
53168136
00016717 00000-0 10270-3 0 9102
2 25544 51
6493 104
8988 0004653 3
1175 357
0004 15
50540380 6087
Satellite: ISS
Catalog Number: 25544
Epoch time: 13241
53168136 = yrday
fracday
Element set: 910
Inclination: 51
6493 deg
RA of node: 104
8988 deg
Eccentricity:
0004653
Arg of perigee: 3
1175 deg
Mean anomaly: 357
0004 deg
Mean motion: 15
50540380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 608
Checksum: 283
Coasting Arc #12 (Orbit 623)
---------------------------------------
Vector Time (GMT): 2013/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1717662
03 A = 6799286
10 meter
Y = 6515941
80 meter E =
0016910
Z = 831212
40 I = 52
01809
XDOT = -4407
912256 Wp = 41
66220
YDOT = -1930
750182 meter/sec RA = 99
24099 deg
ZDOT = 5969
383590 TA = 327
27317
MA = 327
37782
Ha = 227
389 n
mi
Hp = 219
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5635374
11 X = -1794434
82
Y = 21377761
81 feet Y = 6496304
58 meter
Z = 2727074
81 Z = 822681
55
XDOT = -14461
654382 XDOT = -4414
991934
YDOT = -6334
482226 feet/sec YDOT = -1980
081640 meter/sec
ZDOT = 19584
591831 ZDOT = 5947
953437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13241155
25 X = 4035904
12
Y = -17709789
74 feet Y = -5397943
91 meter
Z = 2690396
50 Z = 820032
85
XDOT = 9862
281497 XDOT = 3006
023400
YDOT = 10364
246732 feet/sec YDOT = 3159
022404 meter/sec
ZDOT = 19494
917398 ZDOT = 5942
050823
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
56286642
00016717 00000-0 10270-3 0 9110
2 25544 51
6488 99
7851 0004801 5
6911 354
4293 15
50614286 6248
Satellite: ISS
Catalog Number: 25544
Epoch time: 13242
56286642 = yrday
fracday
Element set: 911
Inclination: 51
6488 deg
RA of node: 99
7851 deg
Eccentricity:
0004801
Arg of perigee: 5
6911 deg
Mean anomaly: 354
4293 deg
Mean motion: 15
50614286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 624
Checksum: 312
Coasting Arc #13 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2013/243/07:35:28
499
Vector Time (MET): N/A
Weight (LBS) : 957353
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4110199
68 A = 6789759
54 meter
Y = -2101669
60 meter E =
0014351
Z = -4991972
25 I = 51
98793
XDOT = 1052
262726 Wp = 57
14622
YDOT = 7256
510281 meter/sec RA = 95
22218 deg
ZDOT = -2185
663299 TA = 191
57917
MA = 191
61221
Ha = 227
491 n
mi
Hp = 220
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13484907
07 X = 4157644
89
Y = -6895241
47 feet Y = -2055441
66 meter
Z = -16377861
73 Z = -4971890
19
XDOT = 3452
305531 XDOT = 981
657871
YDOT = 23807
448427 feet/sec YDOT = 7267
882490 meter/sec
ZDOT = -7170
811349 ZDOT = -2180
723341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7528498
93 X = -2294686
47
Y = -13246571
13 feet Y = -4037554
88 meter
Z = -16293295
73 Z = -4966196
54
XDOT = 22649
914801 XDOT = 6903
694031
YDOT = -4064
745343 feet/sec YDOT = -1238
934381 meter/sec
ZDOT = -7151
063435 ZDOT = -2179
644135
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
33625129
00016717 00000-0 10270-3 0 9124
2 25544 51
6488 95
9503 0004390 2
0773 358
0396 15
50417564 6367
Satellite: ISS
Catalog Number: 25544
Epoch time: 13243
33625129 = yrday
fracday
Element set: 912
Inclination: 51
6488 deg
RA of node: 95
9503 deg
Eccentricity:
0004390
Arg of perigee: 2
0773 deg
Mean anomaly: 358
0396 deg
Mean motion: 15
50417564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 305
Coasting Arc #14 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2013/244/07:35:28
499
Vector Time (MET): N/A
Weight (LBS) : 957353
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4024319
86 A = 6789007
73 meter
Y = 1862202
72 meter E =
0004673
Z = 5136597
09 I = 51
98734
XDOT = -1272
803161 Wp = 72
38014
YDOT = -7371
601412 meter/sec RA = 90
28588 deg
ZDOT = 1675
407226 TA = 1
51593
MA = 1
51452
Ha = 227
613 n
mi
Hp = 220
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13203149
15 X = -4069796
19
Y = 6109588
98 feet Y = 1816946
21 meter
Z = 16852352
67 Z = 5116937
02
XDOT = -4175
863390 XDOT = -1198
416273
YDOT = -24185
044003 feet/sec YDOT = -7385
418699 meter/sec
ZDOT = 5496
742869 ZDOT = 1669
405198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6953334
32 X = 2119376
30
Y = 12887365
90 feet Y = 3928069
12 meter
Z = 16769584
30 Z = 5111369
30
XDOT = -22924
371951 XDOT = -6987
348571
YDOT = 5248
177975 feet/sec YDOT = 1599
644647 meter/sec
ZDOT = 5472
559661 ZDOT = 1668
036185
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
36755158
00016717 00000-0 10270-3 0 9135
2 25544 51
6486 90
8383 0004340 3
9240 356
1944 15
50445334 6521
Satellite: ISS
Catalog Number: 25544
Epoch time: 13244
36755158 = yrday
fracday
Element set: 913
Inclination: 51
6486 deg
RA of node: 90
8383 deg
Eccentricity:
0004340
Arg of perigee: 3
9240 deg
Mean anomaly: 356
1944 deg
Mean motion: 15
50445334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 300
Coasting Arc #15 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2013/245/07:35:28
499
Vector Time (MET): N/A
Weight (LBS) : 957353
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3993032
99 A = 6788487
54 meter
Y = -1619439
05 meter E =
0016060
Z = -5259356
86 I = 51
98549
XDOT = 1498
718638 Wp = 65
79069
YDOT = 7415
133551 meter/sec RA = 85
34867 deg
ZDOT = -1141
721072 TA = 193
26962
MA = 193
31191
Ha = 227
581 n
mi
Hp = 220
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13100501
94 X = 4036393
32
Y = -5313120
25 feet Y = -1574544
33 meter
Z = -17255107
82 Z = -5239853
91
XDOT = 4917
055898 XDOT = 1421
235700
YDOT = 24327
865980 feet/sec YDOT = 7431
459867 meter/sec
ZDOT = -3745
804043 ZDOT = -1134
629222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6372035
78 X = -1942196
51
Y = -12730884
39 feet Y = -3880373
56 meter
Z = -17173027
88 Z = -5234338
90
XDOT = 22916
280644 XDOT = 6984
882340
YDOT = -6439
732258 feet/sec YDOT = -1962
830392 meter/sec
ZDOT = -3717
058479 ZDOT = -1132
959424
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
33438454
00016717 00000-0 10270-3 0 9141
2 25544 51
6492 86
0455 0004476 8
2374 351
8850 15
50459615 6672
Satellite: ISS
Catalog Number: 25544
Epoch time: 13245
33438454 = yrday
fracday
Element set: 914
Inclination: 51
6492 deg
RA of node: 86
0455 deg
Eccentricity:
0004476
Arg of perigee: 8
2374 deg
Mean anomaly: 351
8850 deg
Mean motion: 15
50459615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 667
Checksum: 317
Coasting Arc #16 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2013/246/07:35:28
499
Vector Time (MET): N/A
Weight (LBS) : 957353
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3991529
05 A = 6788062
35 meter
Y = 1343736
97 meter E =
0004684
Z = 5320334
18 I = 51
98060
XDOT = -1725
102760 Wp = 46
17625
YDOT = -7445
868503 meter/sec RA = 80
41068 deg
ZDOT = 589
167031 TA = 38
24176
MA = 38
20855
Ha = 227
691 n
mi
Hp = 219
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13095567
74 X = -4032102
75
Y = 4408585
86 feet Y = 1298874
75 meter
Z = 17455164
65 Z = 5300845
29
XDOT = -5659
785958 XDOT = -1644
575192
YDOT = -24428
702439 feet/sec YDOT = -7464
709393 meter/sec
ZDOT = 1932
962699 ZDOT = 580
982972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5689598
06 X = 1734189
49
Y = 12704858
04 feet Y = 3872440
73 meter
Z = 17373179
12 Z = 5295345
00
XDOT = -22824
288497 XDOT = -6956
843134
YDOT = 7636
484611 feet/sec YDOT = 2327
600509 meter/sec
ZDOT = 1899
642833 ZDOT = 579
011136
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
36565761
00016717 00000-0 10270-3 0 9158
2 25544 51
6488 80
9330 0004449 9
9968 350
1271 15
50491604 6830
Satellite: ISS
Catalog Number: 25544
Epoch time: 13246
36565761 = yrday
fracday
Element set: 915
Inclination: 51
6488 deg
RA of node: 80
9330 deg
Eccentricity:
0004449
Arg of perigee: 9
9968 deg
Mean anomaly: 350
1271 deg
Mean motion: 15
50491604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 322
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