[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 30th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13282 67 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 126)
---------------------------------------
Vector Time (GMT): 2013/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1212462
41 A = 6797100
30 meter
Y = 5952549
06 meter E =
0003141
Z = -3045888
09 I = 51
30736
XDOT = -4759
218641 Wp = 169
23214
YDOT = -3472
220688 meter/sec RA = 257
83530 deg
ZDOT = -4895
095460 TA = 45
81550
MA = 45
78969
Ha = 226
152 n
mi
Hp = 222
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3977895
04 X = -1264139
02
Y = 19529360
43 feet Y = 5938701
71 meter
Z = -9993071
16 Z = -3051903
36
XDOT = -15614
234386 XDOT = -4696
258944
YDOT = -11391
800158 feet/sec YDOT = -3525
089065 meter/sec
ZDOT = -16060
024475 ZDOT = -4918
062337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18029543
10 X = 5495404
74
Y = -8463740
62 feet Y = -2579748
14 meter
Z = -10019067
27 Z = -3053811
70
XDOT = -552
111995 XDOT = -168
283736
YDOT = 17933
447175 feet/sec YDOT = 5466
114699 meter/sec
ZDOT = -16155
650997 ZDOT = -4924
242424
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 13210
52599558
00016717 00000-0 10270-3 0 9002
2 25544 51
6489 258
5531 0004070 245
5486 114
5240 15
50109882 1275
Satellite: ISS
Catalog Number: 25544
Epoch time: 13210
52599558 = yrday
fracday
Element set: 900
Inclination: 51
6489 deg
RA of node: 258
5531 deg
Eccentricity:
0004070
Arg of perigee: 245
5486 deg
Mean anomaly: 114
5240 deg
Mean motion: 15
50109882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 127
Checksum: 301
Coasting Arc #2 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2013/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1002245
85 A = 6796322
69 meter
Y = -5829048
05 meter E =
0008898
Z = 3341304
96 I = 51
31135
XDOT = 4975
818891 Wp = 97
23818
YDOT = 3522
513479 meter/sec RA = 252
85777 deg
ZDOT = 4640
873833 TA = 301
82291
MA = 301
90952
Ha = 226
108 n
mi
Hp = 222
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3288208
18 X = 1051122
03
Y = -19124173
38 feet Y = -5817567
19 meter
Z = 10962286
62 Z = 3346292
16
XDOT = 16324
865127 XDOT = 4913
515642
YDOT = 11556
802751 feet/sec YDOT = 3577
807639 meter/sec
ZDOT = 15225
964020 ZDOT = 4664
894566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17136417
22 X = -5223179
97
Y = 9078210
68 feet Y = 2767038
62 meter
Z = 10983958
51 Z = 3347910
55
XDOT = -38
716727 XDOT = -11
800858
YDOT = -18663
040138 feet/sec YDOT = -5688
494634 meter/sec
ZDOT = 15326
003055 ZDOT = 4671
365731
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 13211
55749838
00016717 00000-0 10270-3 0 9015
2 25544 51
6482 253
4423 0003942 249
9997 110
0730 15
50105128 1436
Satellite: ISS
Catalog Number: 25544
Epoch time: 13211
55749838 = yrday
fracday
Element set: 901
Inclination: 51
6482 deg
RA of node: 253
4423 deg
Eccentricity:
0003942
Arg of perigee: 249
9997 deg
Mean anomaly: 110
0730 deg
Mean motion: 15
50105128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 143
Checksum: 295
Coasting Arc #3 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2013/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -838306
29 A = 6795350
56 meter
Y = 5677279
53 meter E =
0001629
Z = -3640214
97 I = 51
31946
XDOT = -5204
180416 Wp = 98
29386
YDOT = -3556
058230 meter/sec RA = 247
88044 deg
ZDOT = -4349
463774 TA = 125
03265
MA = 125
01736
Ha = 225
963 n
mi
Hp = 222
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2750348
73 X = -884045
55
Y = 18626245
18 feet Y = 5667649
54 meter
Z = -11942962
51 Z = -3644398
10
XDOT = -17074
082730 XDOT = -5142
900698
YDOT = -11666
857709 feet/sec YDOT = -3613
911767 meter/sec
ZDOT = -14269
894271 ZDOT = -4374
596348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16249461
84 X = 4952835
97
Y = -9487856
54 feet Y = -2891898
67 meter
Z = -11961243
65 Z = -3645787
06
XDOT = 734
773983 XDOT = 223
959110
YDOT = 19372
442052 feet/sec YDOT = 5904
720337 meter/sec
ZDOT = -14374
593162 ZDOT = -4381
375996
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 13212
52452423
00016717 00000-0 10270-3 0 9025
2 25544 51
6493 248
6510 0003952 254
2131 105
8584 15
50137007 1587
Satellite: ISS
Catalog Number: 25544
Epoch time: 13212
52452423 = yrday
fracday
Element set: 902
Inclination: 51
6493 deg
RA of node: 248
6510 deg
Eccentricity:
0003952
Arg of perigee: 254
2131 deg
Mean anomaly: 105
8584 deg
Mean motion: 15
50137007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 158
Checksum: 276
Coasting Arc #4 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2013/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 690689
29 A = 6794526
23 meter
Y = -5513432
84 meter E =
0007701
Z = 3906035
09 I = 51
32764
XDOT = 5452
931721 Wp = 109
38480
YDOT = 3553
688499 meter/sec RA = 242
90306 deg
ZDOT = 4042
817092 TA = 298
05790
MA = 298
13576
Ha = 225
951 n
mi
Hp = 222
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2266040
99 X = 733316
13
Y = -18088690
43 feet Y = -5505471
04 meter
Z = 12815075
77 Z = 3909493
53
XDOT = 17890
195936 XDOT = 5393
149651
YDOT = 11659
083002 feet/sec YDOT = 3614
332101 meter/sec
ZDOT = 13263
835605 ZDOT = 4069
161664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15357552
48 X = -4680982
00
Y = 9802597
12 feet Y = 2987831
60 meter
Z = 12830296
25 Z = 3910674
30
XDOT = -1593
720037 XDOT = -485
765867
YDOT = -20039
967364 feet/sec YDOT = -6108
182053 meter/sec
ZDOT = 13373
621023 ZDOT = 4076
279688
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 13213
55601120
00016717 00000-0 10270-3 0 9030
2 25544 51
6478 243
5400 0003811 258
8722 101
2000 15
50129432 1746
Satellite: ISS
Catalog Number: 25544
Epoch time: 13213
55601120 = yrday
fracday
Element set: 903
Inclination: 51
6478 deg
RA of node: 243
5400 deg
Eccentricity:
0003811
Arg of perigee: 258
8722 deg
Mean anomaly: 101
2000 deg
Mean motion: 15
50129432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 174
Checksum: 250
Coasting Arc #5 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2013/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -593202
86 A = 6793550
65 meter
Y = 5334388
10 meter E =
0004001
Z = -4169102
05 I = 51
34035
XDOT = -5701
947812 Wp = 58
71572
YDOT = -3525
136755 meter/sec RA = 237
92643 deg
ZDOT = -3699
730202 TA = 173
05926
MA = 173
05372
Ha = 225
838 n
mi
Hp = 222
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1946203
61 X = -632556
98
Y = 17501273
28 feet Y = 5327534
76 meter
Z = -13678156
32 Z = -4172078
96
XDOT = -18707
177862 XDOT = -5644
133158
YDOT = -11565
409301 feet/sec YDOT = -3588
576035 meter/sec
ZDOT = -12138
222446 ZDOT = -3727
289162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14528574
74 X = 4428309
58
Y = -9931878
00 feet Y = -3027236
41 meter
Z = -13691331
22 Z = -4173117
76
XDOT = 2553
623119 XDOT = 778
344327
YDOT = 20623
975196 feet/sec YDOT = 6286
187640 meter/sec
ZDOT = -12253
110440 ZDOT = -3734
748062
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
52302160
00016717 00000-0 10270-3 0 9041
2 25544 51
6487 238
7489 0003903 262
9041 97
1666 15
50159136 1892
Satellite: ISS
Catalog Number: 25544
Epoch time: 13214
52302160 = yrday
fracday
Element set: 904
Inclination: 51
6487 deg
RA of node: 238
7489 deg
Eccentricity:
0003903
Arg of perigee: 262
9041 deg
Mean anomaly: 97
1666 deg
Mean motion: 15
50159136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 189
Checksum: 307
Coasting Arc #6 (Orbit 204)
---------------------------------------
Vector Time (GMT): 2013/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 517967
02 A = 6792732
02 meter
Y = -5149469
96 meter E =
0006045
Z = 4397073
73 I = 51
35303
XDOT = 5962
580862 Wp = 123
22533
YDOT = 3460
531637 meter/sec RA = 232
94951 deg
ZDOT = 3343
697896 TA = 292
77289
MA = 292
83675
Ha = 225
840 n
mi
Hp = 222
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1699366
87 X = 554151
59
Y = -16894586
49 feet Y = -5143475
68 meter
Z = 14426094
91 Z = 4399677
49
XDOT = 19562
273170 XDOT = 5907
198791
YDOT = 11353
450253 feet/sec YDOT = 3526
899122 meter/sec
ZDOT = 10970
137454 ZDOT = 3372
528783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13734204
92 X = -4186185
66
Y = 9967558
73 feet Y = 3038111
90 meter
Z = 14437676
50 Z = 4400603
80
XDOT = -3652
964642 XDOT = -1113
423623
YDOT = -21128
739089 feet/sec YDOT = -6440
039674 meter/sec
ZDOT = 11090
375850 ZDOT = 3380
346559
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
55449236
00016717 00000-0 10270-3 0 9052
2 25544 51
6470 233
6375 0003798 267
9528 92
1188 15
50154595 2056
Satellite: ISS
Catalog Number: 25544
Epoch time: 13215
55449236 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 233
6375 deg
Eccentricity:
0003798
Arg of perigee: 267
9528 deg
Mean anomaly: 92
1188 deg
Mean motion: 15
50154595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 205
Checksum: 322
Coasting Arc #7 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2013/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -492401
02 A = 6791846
22 meter
Y = 4963917
03 meter E =
0006735
Z = -4616096
84 I = 51
36982
XDOT = -6210
055400 Wp = 58
06912
YDOT = -3363
802532 meter/sec RA = 227
97390 deg
ZDOT = -2954
525781 TA = 182
32395
MA = 182
32709
Ha = 225
786 n
mi
Hp = 222
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1615488
91 X = -525448
71
Y = 16285817
03 feet Y = 4958226
15 meter
Z = -15144674
67 Z = -4618568
84
XDOT = -20374
197506 XDOT = -6157
627075
YDOT = -11036
097546 feet/sec YDOT = -3432
954003 meter/sec
ZDOT = -9693
326054 ZDOT = -2984
565925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13051557
50 X = 3978114
73
Y = -9857039
69 feet Y = -3004425
70 meter
Z = -15155673
10 Z = -4619449
16
XDOT = 4828
275754 XDOT = 1471
658450
YDOT = 21491
259650 feet/sec YDOT = 6550
535941 meter/sec
ZDOT = -9818
658277 ZDOT = -2992
727043
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
52148737
00016717 00000-0 10270-3 0 9063
2 25544 51
6473 228
8462 0003903 271
6907 88
3797 15
50177601 2206
Satellite: ISS
Catalog Number: 25544
Epoch time: 13216
52148737 = yrday
fracday
Element set: 906
Inclination: 51
6473 deg
RA of node: 228
8462 deg
Eccentricity:
0003903
Arg of perigee: 271
6907 deg
Mean anomaly: 88
3797 deg
Mean motion: 15
50177601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 220
Checksum: 313
Coasting Arc #8 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2013/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 493088
46 A = 6791100
99 meter
Y = -4779638
38 meter E =
0004066
Z = 4798075
70 I = 51
38735
XDOT = 6459
382886 Wp = 140
16512
YDOT = 3234
336222 meter/sec RA = 222
99809 deg
ZDOT = 2553
823620 TA = 284
56267
MA = 284
60776
Ha = 225
787 n
mi
Hp = 222
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1617744
30 X = 523191
50
Y = -15681228
27 feet Y = -4773956
22 meter
Z = 15741718
17 Z = 4800543
96
XDOT = 21192
201070 XDOT = 6410
330235
YDOT = 10611
339310 feet/sec YDOT = 3306
294763 meter/sec
ZDOT = 8378
686417 ZDOT = 2585
083048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12439654
26 X = -3791606
62
Y = 9665821
57 feet Y = 2946142
42 meter
Z = 15752669
71 Z = 4801413
73
XDOT = -6103
691199 XDOT = -1860
405077
YDOT = -21745
708503 feet/sec YDOT = -6628
091952 meter/sec
ZDOT = 8509
159480 ZDOT = 2593
591810
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
55294150
00016717 00000-0 10270-3 0 9079
2 25544 51
6460 223
7343 0003881 276
9677 83
1032 15
50179283 2361
Satellite: ISS
Catalog Number: 25544
Epoch time: 13217
55294150 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 223
7343 deg
Eccentricity:
0003881
Arg of perigee: 276
9677 deg
Mean anomaly: 83
1032 deg
Mean motion: 15
50179283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 304
Coasting Arc #9 (Orbit 250)
---------------------------------------
Vector Time (GMT): 2013/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -538130
06 A = 6790384
86 meter
Y = 4609533
94 meter E =
0009063
Z = -4965391
74 I = 51
40818
XDOT = -6681
626659 Wp = 63
33276
YDOT = -3071
074164 meter/sec RA = 218
02394 deg
ZDOT = -2125
880086 TA = 185
84894
MA = 185
85953
Ha = 225
821 n
mi
Hp = 222
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1765518
55 X = -565514
86
Y = 15123142
85 feet Y = 4603363
22 meter
Z = -16290655
30 Z = -4968072
29
XDOT = -21921
347307 XDOT = -6636
461917
YDOT = -10075
702638 feet/sec YDOT = -3145
539770 meter/sec
ZDOT = -6974
672197 ZDOT = -2158
228498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11973534
79 X = 3649533
40
Y = -9384881
08 feet Y = -2860511
75 meter
Z = -16302466
91 Z = -4968991
91
XDOT = 7411
766556 XDOT = 2259
106446
YDOT = 21812
017177 feet/sec YDOT = 6648
302836 meter/sec
ZDOT = -7109
744729 ZDOT = -2167
050193
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
51992107
00016717 00000-0 10270-3 0 9084
2 25544 51
6459 218
9426 0003925 280
6430 79
4278 15
50195562 2510
Satellite: ISS
Catalog Number: 25544
Epoch time: 13218
51992107 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 218
9426 deg
Eccentricity:
0003925
Arg of perigee: 280
6430 deg
Mean anomaly: 79
4278 deg
Mean motion: 15
50195562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 251
Checksum: 318
Coasting Arc #10 (Orbit 266)
---------------------------------------
Vector Time (GMT): 2013/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 611268
28 A = 6789790
97 meter
Y = -4448008
87 meter E =
0001971
Z = 5093511
41 I = 51
43051
XDOT = 6895
890022 Wp = 166
88796
YDOT = 2881
857560 meter/sec RA = 213
05026 deg
ZDOT = 1687
058258 TA = 266
74362
MA = 266
76617
Ha = 225
819 n
mi
Hp = 222
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2005473
37 X = 636219
07
Y = -14593204
97 feet Y = -4441033
79 meter
Z = 16710995
44 Z = 5096541
43
XDOT = 22624
311097 XDOT = 6854
956843
YDOT = 9454
913256 feet/sec YDOT = 2958
742897 meter/sec
ZDOT = 5534
968039 ZDOT = 1720
457763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11606788
22 X = -3537749
05
Y = 9045610
04 feet Y = 2757101
94 meter
Z = 16724243
76 Z = 5097549
50
XDOT = -8768
324315 XDOT = -2672
585251
YDOT = -21754
612498 feet/sec YDOT = -6630
805890 meter/sec
ZDOT = 5674
483762 ZDOT = 1729
582651
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
55135824
00016717 00000-0 10270-3 0 9095
2 25544 51
6453 213
8306 0003993 285
7785 74
2925 15
50203548 2672
Satellite: ISS
Catalog Number: 25544
Epoch time: 13219
55135824 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 213
8306 deg
Eccentricity:
0003993
Arg of perigee: 285
7785 deg
Mean anomaly: 74
2925 deg
Mean motion: 15
50203548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 267
Checksum: 321
Coasting Arc #11 (Orbit 281)
---------------------------------------
Vector Time (GMT): 2013/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -718685
28 A = 6789306
44 meter
Y = 4314194
34 meter E =
0010721
Z = -5202292
00 I = 51
45541
XDOT = -7070
312651 Wp = 70
21634
YDOT = -2661
822280 meter/sec RA = 208
07832 deg
ZDOT = -1229
187005 TA = 187
92649
MA = 187
94345
Ha = 225
929 n
mi
Hp = 222
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2357891
34 X = -741603
27
Y = 14154180
90 feet Y = 4306029
32 meter
Z = -17067887
15 Z = -5205838
98
XDOT = -23196
563817 XDOT = -7034
051148
YDOT = -8733
012729 feet/sec YDOT = -2740
684265 meter/sec
ZDOT = -4032
765765 ZDOT = -1263
445185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11399730
40 X = 3474637
83
Y = -8684526
41 feet Y = -2647043
65 meter
Z = -17083278
62 Z = -5206983
32
XDOT = 10101
217304 XDOT = 3078
851034
YDOT = 21483
319392 feet/sec YDOT = 6548
115751 meter/sec
ZDOT = -4175
921269 ZDOT = -1272
820803
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
51832206
00016717 00000-0 10270-3 0 9103
2 25544 51
6455 209
0386 0003968 289
6585 70
4138 15
50216279 2828
Satellite: ISS
Catalog Number: 25544
Epoch time: 13220
51832206 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 209
0386 deg
Eccentricity:
0003968
Arg of perigee: 289
6585 deg
Mean anomaly: 70
4138 deg
Mean motion: 15
50216279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 282
Checksum: 305
Coasting Arc #12 (Orbit 297)
---------------------------------------
Vector Time (GMT): 2013/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 853744
98 A = 6788939
55 meter
Y = -4195659
62 meter E =
0000904
Z = 5269282
43 I = 51
48189
XDOT = 7227
721080 Wp = 277
02219
YDOT = 2425
771003 meter/sec RA = 203
10783 deg
ZDOT = 760
680760 TA = 165
68901
MA = 165
68645
Ha = 225
932 n
mi
Hp = 222
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2801000
58 X = 875001
96
Y = -13765287
48 feet Y = -4185993
50 meter
Z = 17287672
03 Z = 5273481
54
XDOT = 23712
995669 XDOT = 7196
363277
YDOT = 7958
566283 feet/sec YDOT = 2506
420651 meter/sec
ZDOT = 2495
671784 ZDOT = 795
715582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11309834
05 X = -3447237
42
Y = 8293979
70 feet Y = 2528005
01 meter
Z = 17305776
55 Z = 5274800
69
XDOT = -11423
660079 XDOT = -3481
931592
YDOT = -21088
933781 feet/sec YDOT = -6427
907016 meter/sec
ZDOT = 2642
123910 ZDOT = 805
319368
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
54974193
00016717 00000-0 10270-3 0 9110
2 25544 51
6454 203
9269 0004090 294
3564 65
7160 15
50228973 2980
Satellite: ISS
Catalog Number: 25544
Epoch time: 13221
54974193 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 203
9269 deg
Eccentricity:
0004090
Arg of perigee: 294
3564 deg
Mean anomaly: 65
7160 deg
Mean motion: 15
50228973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 298
Checksum: 314
Coasting Arc #13 (Orbit 312)
---------------------------------------
Vector Time (GMT): 2013/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1008962
63 A = 6788731
88 meter
Y = 4115563
72 meter E =
0011501
Z = -5313710
41 I = 51
51034
XDOT = -7335
472712 Wp = 77
45856
YDOT = -2166
295510 meter/sec RA = 198
13905 deg
ZDOT = -283
058747 TA = 189
82205
MA = 189
84455
Ha = 226
075 n
mi
Hp = 222
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3310244
85 X = -1029096
52
Y = 13502505
64 feet Y = 4104168
09 meter
Z = -17433433
09 Z = -5318660
85
XDOT = -24066
511521 XDOT = -7309
328528
YDOT = -7107
268733 feet/sec YDOT = -2248
179244 meter/sec
ZDOT = -928
670429 ZDOT = -318
629790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11370334
89 X = 3465678
07
Y = -7952976
84 feet Y = -2424067
34 meter
Z = -17454673
10 Z = -5320184
36
XDOT = 12661
192475 XDOT = 3859
131466
YDOT = 20480
114977 feet/sec YDOT = 6242
339045 meter/sec
ZDOT = -1077
413764 ZDOT = -328
395715
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
51668935
00016717 00000-0 10270-3 0 9123
2 25544 51
6458 199
1348 0004052 298
3670 61
7072 15
50241341 3138
Satellite: ISS
Catalog Number: 25544
Epoch time: 13222
51668935 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 199
1348 deg
Eccentricity:
0004052
Arg of perigee: 298
3670 deg
Mean anomaly: 61
7072 deg
Mean motion: 15
50241341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 313
Checksum: 295
Coasting Arc #14 (Orbit 328)
---------------------------------------
Vector Time (GMT): 2013/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1189110
31 A = 6788651
30 meter
Y = -4056060
72 meter E =
0002780
Z = 5313271
08 I = 51
53997
XDOT = 7418
715021 Wp = 337
33974
YDOT = 1903
378126 meter/sec RA = 193
17250 deg
ZDOT = -204
827718 TA = 114
63126
MA = 114
60230
Ha = 226
089 n
mi
Hp = 222
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3901280
53 X = 1208567
47
Y = -13307285
83 feet Y = -4042654
36 meter
Z = 17431991
75 Z = 5319095
03
XDOT = 24339
616209 XDOT = 7397
874644
YDOT = 6244
678890 feet/sec YDOT = 1986
222366 meter/sec
ZDOT = -672
006949 ZDOT = -168
839270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11552616
70 X = -3521237
57
Y = 7613963
32 feet Y = 2320736
02 meter
Z = 17456883
80 Z = 5320858
18
XDOT = -13827
662129 XDOT = -4214
671417
YDOT = -19766
435093 feet/sec YDOT = -6024
809416 meter/sec
ZDOT = -521
470185 ZDOT = -158
944112
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
54809139
00016717 00000-0 10270-3 0 9131
2 25544 51
6460 194
0235 0004169 302
6179 57
4569 15
50257076 3294
Satellite: ISS
Catalog Number: 25544
Epoch time: 13223
54809139 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 194
0235 deg
Eccentricity:
0004169
Arg of perigee: 302
6179 deg
Mean anomaly: 57
4569 deg
Mean motion: 15
50257076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 329
Checksum: 309
Coasting Arc #15 (Orbit 343)
---------------------------------------
Vector Time (GMT): 2013/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1372382
10 A = 6788747
40 meter
Y = 4041635
97 meter E =
0011280
Z = -5288711
99 I = 51
57088
XDOT = -7447
040748 Wp = 84
30557
YDOT = -1627
892866 meter/sec RA = 188
20759 deg
ZDOT = 690
781609 TA = 192
29614
MA = 192
32369
Ha = 226
232 n
mi
Hp = 221
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4502565
93 X = -1391783
56
Y = 13259960
53 feet Y = 4026180
51 meter
Z = -17351417
31 Z = -5295426
09
XDOT = -24432
548385 XDOT = -7431
639424
YDOT = -5340
855860 feet/sec YDOT = -1711
084264 meter/sec
ZDOT = 2266
343860 ZDOT = 654
642210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11852597
24 X = 3612671
64
Y = -7390637
13 feet Y = -2252666
20 meter
Z = -17380039
05 Z = -5297435
90
XDOT = 14853
015449 XDOT = 4527
199109
YDOT = 18864
471145 feet/sec YDOT = 5749
890805 meter/sec
ZDOT = 2115
127872 ZDOT = 644
690975
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
51502160
00016717 00000-0 10270-3 0 9144
2 25544 51
6464 189
2313 0004176 306
4435 53
6330 15
50270347 3443
Satellite: ISS
Catalog Number: 25544
Epoch time: 13224
51502160 = yrday
fracday
Element set: 914
Inclination: 51
6464 deg
RA of node: 189
2313 deg
Eccentricity:
0004176
Arg of perigee: 306
4435 deg
Mean anomaly: 53
6330 deg
Mean motion: 15
50270347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 344
Checksum: 271
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