[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 5th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 233)
---------------------------------------
Vector Time (GMT): 2013/217/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3975537
88 A = 6800156
02 meter
Y = -5330972
03 meter E =
0010731
Z = 1390818
33 I = 51
41524
XDOT = 4639
475169 Wp = 47
80681
YDOT = -1946
209596 meter/sec RA = 223
68094 deg
ZDOT = 5780
140723 TA = 327
37517
MA = 327
44142
Ha = 225
804 n
mi
Hp = 222
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13043103
29 X = -3922386
40
Y = -17490065
73 feet Y = -5375131
89 meter
Z = 4563052
27 Z = 1371634
81
XDOT = 15221
375227 XDOT = 4632
815516
YDOT = -6385
202088 feet/sec YDOT = -1894
365520 meter/sec
ZDOT = 18963
716284 ZDOT = 5802
662156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18828162
30 X = -5738823
87
Y = 11056476
40 feet Y = 3370014
01 meter
Z = 4483416
45 Z = 1366545
33
XDOT = -3867
757328 XDOT = -1178
892434
YDOT = -14343
887525 feet/sec YDOT = -4372
016918 meter/sec
ZDOT = 19058
268561 ZDOT = 5808
960257
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
42403311
00016717 00000-0 10270-3 0 9009
2 25544 51
6471 224
3782 0004067 275
7725 84
2962 15
50142256 2347
Satellite: ISS
Catalog Number: 25544
Epoch time: 13217
42403311 = yrday
fracday
Element set: 900
Inclination: 51
6471 deg
RA of node: 224
3782 deg
Eccentricity:
0004067
Arg of perigee: 275
7725 deg
Mean anomaly: 84
2962 deg
Mean motion: 15
50142256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 234
Checksum: 280
Coasting Arc #2 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2013/218/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4104109
61 A = 6799476
33 meter
Y = 5114268
47 meter E =
0005263
Z = -1786011
19 I = 51
43673
XDOT = -4820
482233 Wp = 173
23788
YDOT = 1900
541019 meter/sec RA = 218
71241 deg
ZDOT = -5641
671224 TA = 26
40073
MA = 26
37393
Ha = 225
777 n
mi
Hp = 222
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13464926
53 X = 4055291
49
Y = 16779096
02 feet Y = 5159890
30 meter
Z = -5859616
76 Z = -1766192
67
XDOT = -15815
230424 XDOT = -4813
971102
YDOT = 6235
370797 feet/sec YDOT = 1846
671873 meter/sec
ZDOT = -18509
420025 ZDOT = -5665
072334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17967425
44 X = 5476471
28
Y = -11873167
70 feet Y = -3618941
51 meter
Z = -5777277
05 Z = -1760914
04
XDOT = 3872
942067 XDOT = 1180
472742
YDOT = 14903
967483 feet/sec YDOT = 4542
729289 meter/sec
ZDOT = -18607
656137 ZDOT = -5671
613591
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
39102222
00016717 00000-0 10270-3 0 9014
2 25544 51
6474 219
5863 0004041 279
1361 80
9332 15
50195209 2498
Satellite: ISS
Catalog Number: 25544
Epoch time: 13218
39102222 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 219
5863 deg
Eccentricity:
0004041
Arg of perigee: 279
1361 deg
Mean anomaly: 80
9332 deg
Mean motion: 15
50195209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 286
Coasting Arc #3 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2013/219/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4207202
93 A = 6798941
19 meter
Y = -4877334
19 meter E =
0010869
Z = 2157274
01 I = 51
45867
XDOT = 5014
393131 Wp = 58
44437
YDOT = -1896
632936 meter/sec RA = 213
74486 deg
ZDOT = 5476
376643 TA = 325
51134
MA = 325
58182
Ha = 225
933 n
mi
Hp = 222
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13803159
21 X = -4162830
06
Y = -16001752
59 feet Y = -4924133
70 meter
Z = 7077670
62 Z = 2136943
97
XDOT = 16451
421035 XDOT = 5008
626811
YDOT = -6222
549003 feet/sec YDOT = -1840
591081 meter/sec
ZDOT = 17967
114972 ZDOT = 5500
721594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17011768
30 X = -5185186
98
Y = 12584609
90 feet Y = 3835789
10 meter
Z = 6993142
71 Z = 2131509
90
XDOT = -4037
696356 XDOT = -1230
689849
YDOT = -15526
439585 feet/sec YDOT = -4732
458785 meter/sec
ZDOT = 18069
309229 ZDOT = 5507
525453
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
42247038
00016717 00000-0 10270-3 0 9025
2 25544 51
6468 214
4747 0003953 285
1746 74
8967 15
50171604 2658
Satellite: ISS
Catalog Number: 25544
Epoch time: 13219
42247038 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 214
4747 deg
Eccentricity:
0003953
Arg of perigee: 285
1746 deg
Mean anomaly: 74
8967 deg
Mean motion: 15
50171604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 317
Coasting Arc #4 (Orbit 279)
---------------------------------------
Vector Time (GMT): 2013/220/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4263319
13 A = 6798040
35 meter
Y = 4645734
55 meter E =
0002208
Z = -2537273
82 I = 51
48350
XDOT = -5220
055228 Wp = 174
17651
YDOT = 1915
319503 meter/sec RA = 208
77877 deg
ZDOT = -5266
745115 TA = 34
32027
MA = 34
30601
Ha = 225
886 n
mi
Hp = 222
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13987267
48 X = 4223377
81
Y = 15241911
25 feet Y = 4693186
32 meter
Z = -8324389
17 Z = -2516660
47
XDOT = -17126
165447 XDOT = -5215
500847
YDOT = 6283
856637 feet/sec YDOT = 1856
970930 meter/sec
ZDOT = -17279
347491 ZDOT = -5292
092155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16045531
09 X = 4890677
88
Y = -13111859
19 feet Y = -3996494
68 meter
Z = -8238631
29 Z = -2511134
82
XDOT = 4307
994479 XDOT = 1313
076717
YDOT = 16190
615996 feet/sec YDOT = 4934
899756 meter/sec
ZDOT = -17385
746981 ZDOT = -5299
175680
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
38944241
00016717 00000-0 10270-3 0 9033
2 25544 51
6481 209
6827 0003991 288
1142 71
9574 15
50224169 2807
Satellite: ISS
Catalog Number: 25544
Epoch time: 13220
38944241 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 209
6827 deg
Eccentricity:
0003991
Arg of perigee: 288
1142 deg
Mean anomaly: 71
9574 deg
Mean motion: 15
50224169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 280
Checksum: 304
Coasting Arc #5 (Orbit 295)
---------------------------------------
Vector Time (GMT): 2013/221/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4288245
68 A = 6797299
50 meter
Y = -4403667
27 meter E =
0010267
Z = 2888863
78 I = 51
50737
XDOT = 5430
208444 Wp = 69
27096
YDOT = -1978
670475 meter/sec RA = 203
81384 deg
ZDOT = 5033
470839 TA = 323
64798
MA = 323
71767
Ha = 226
097 n
mi
Hp = 222
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14069047
52 X = -4252717
30
Y = -14447727
27 feet Y = -4451422
42 meter
Z = 9477899
54 Z = 2868118
63
XDOT = 17815
644501 XDOT = 5427
479942
YDOT = -6491
701032 feet/sec YDOT = -1917
961558 meter/sec
ZDOT = 16514
011939 ZDOT = 5059
843299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15027781
76 X = -4580467
88
Y = 13508150
03 feet Y = 4117284
13 meter
Z = 9391547
22 Z = 2862543
59
XDOT = -4755
500881 XDOT = -1449
476669
YDOT = -16874
046620 feet/sec YDOT = -5143
209410 meter/sec
ZDOT = 16624
720453 ZDOT = 5067
214794
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
42087230
00016717 00000-0 10270-3 0 9046
2 25544 51
6472 204
5711 0003896 294
1735 65
9008 15
50205713 2968
Satellite: ISS
Catalog Number: 25544
Epoch time: 13221
42087230 = yrday
fracday
Element set: 904
Inclination: 51
6472 deg
RA of node: 204
5711 deg
Eccentricity:
0003896
Arg of perigee: 294
1735 deg
Mean anomaly: 65
9008 deg
Mean motion: 15
50205713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 288
Coasting Arc #6 (Orbit 310)
---------------------------------------
Vector Time (GMT): 2013/222/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4268086
84 A = 6796264
37 meter
Y = 4179571
53 meter E =
0001372
Z = -3242905
03 I = 51
53415
XDOT = -5635
803970 Wp = 43
39186
YDOT = 2066
761421 meter/sec RA = 198
85063 deg
ZDOT = -4753
963281 TA = 174
14942
MA = 174
14782
Ha = 226
028 n
mi
Hp = 222
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14002909
57 X = 4236785
70
Y = 13712505
02 feet Y = 4227124
85 meter
Z = -10639452
20 Z = -3222247
49
XDOT = -18490
170506 XDOT = -5635
402911
YDOT = 6780
713322 feet/sec YDOT = 2003
740363 meter/sec
ZDOT = -15596
992393 ZDOT = -4781
340255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14056653
21 X = 4284467
90
Y = -13723988
16 feet Y = -4183071
59 meter
Z = -10553428
97 Z = -3216685
15
XDOT = 5320
130680 XDOT = 1621
575831
YDOT = 17530
625402 feet/sec YDOT = 5343
334622 meter/sec
ZDOT = -15711
926317 ZDOT = -4788
995142
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
38782696
00016717 00000-0 10270-3 0 9051
2 25544 51
6485 199
7794 0003988 296
5125 63
5617 15
50249442 3114
Satellite: ISS
Catalog Number: 25544
Epoch time: 13222
38782696 = yrday
fracday
Element set: 905
Inclination: 51
6485 deg
RA of node: 199
7794 deg
Eccentricity:
0003988
Arg of perigee: 296
5125 deg
Mean anomaly: 63
5617 deg
Mean motion: 15
50249442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 311
Checksum: 339
Coasting Arc #7 (Orbit 326)
---------------------------------------
Vector Time (GMT): 2013/223/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213866
45 A = 6795364
77 meter
Y = -3956201
84 meter E =
0008930
Z = 3564220
09 I = 51
55936
XDOT = 5837
379555 Wp = 79
94107
YDOT = -2198
082639 meter/sec RA = 193
88836 deg
ZDOT = 4453
533266 TA = 322
13570
MA = 322
19848
Ha = 226
250 n
mi
Hp = 222
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13825021
17 X = -4186628
01
Y = -12979664
85 feet Y = -4003171
55 meter
Z = 11693635
47 Z = 3543816
00
XDOT = 19151
507727 XDOT = 5839
891286
YDOT = -7211
557216 feet/sec YDOT = -2132
791161 meter/sec
ZDOT = 14611
329613 ZDOT = 4481
896647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13084296
96 X = -3988093
71
Y = 13797996
88 feet Y = 4205629
45 meter
Z = 11608637
96 Z = 3538312
85
XDOT = -6058
801587 XDOT = -1846
722724
YDOT = -18160
760235 feet/sec YDOT = -5535
399720 meter/sec
ZDOT = 14730
419933 ZDOT = 4489
831996
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
41923782
00016717 00000-0 10270-3 0 9060
2 25544 51
6475 194
6677 0003937 302
2865 57
7904 15
50242155 3272
Satellite: ISS
Catalog Number: 25544
Epoch time: 13223
41923782 = yrday
fracday
Element set: 906
Inclination: 51
6475 deg
RA of node: 194
6677 deg
Eccentricity:
0003937
Arg of perigee: 302
2865 deg
Mean anomaly: 57
7904 deg
Mean motion: 15
50242155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 327
Checksum: 316
Coasting Arc #8 (Orbit 341)
---------------------------------------
Vector Time (GMT): 2013/224/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4121128
99 A = 6794294
20 meter
Y = 3762773
13 meter E =
0004738
Z = -3881134
56 I = 51
58669
XDOT = -6017
198844 Wp = 35
67211
YDOT = 2352
008992 meter/sec RA = 188
92795 deg
ZDOT = -4107
774254 TA = 191
10505
MA = 191
11552
Ha = 226
192 n
mi
Hp = 222
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13520764
39 X = 4097599
93
Y = 12345056
19 feet Y = 3808726
54 meter
Z = -12733381
09 Z = -3861171
86
XDOT = -19741
466025 XDOT = -6023
097972
YDOT = 7716
564935 feet/sec YDOT = 2284
687766 meter/sec
ZDOT = -13476
949651 ZDOT = -4137
019481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12213210
20 X = 3722586
47
Y = -13717156
11 feet Y = -4180989
18 meter
Z = -12650201
61 Z = -3855781
45
XDOT = 6903
243537 XDOT = 2104
108630
YDOT = 18692
042116 feet/sec YDOT = 5697
334437 meter/sec
ZDOT = -13599
763335 ZDOT = -4145
207864
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
38617484
00016717 00000-0 10270-3 0 9077
2 25544 51
6480 189
8761 0004026 304
6170 55
4601 15
50272750 3423
Satellite: ISS
Catalog Number: 25544
Epoch time: 13224
38617484 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 189
8761 deg
Eccentricity:
0004026
Arg of perigee: 304
6170 deg
Mean anomaly: 55
4601 deg
Mean motion: 15
50272750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 342
Checksum: 294
Coasting Arc #9 (Orbit 357)
---------------------------------------
Vector Time (GMT): 2013/225/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3994359
60 A = 6793319
89 meter
Y = -3581624
25 meter E =
0006986
Z = 4161205
87 I = 51
61282
XDOT = 6185
547089 Wp = 89
71904
YDOT = -2543
351610 meter/sec RA = 183
96822 deg
ZDOT = 3743
015421 TA = 321
71600
MA = 321
76558
Ha = 226
395 n
mi
Hp = 221
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13104854
35 X = -3974226
16
Y = -11750735
74 feet Y = -3626179
09 meter
Z = 13652250
22 Z = 4141850
66
XDOT = 20293
789662 XDOT = 6195
345193
YDOT = -8344
329429 feet/sec YDOT = -2474
126071 meter/sec
ZDOT = 12280
234322 ZDOT = 3773
087961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11392255
65 X = -3472359
52
Y = 13499239
95 feet Y = 4114568
34 meter
Z = 13571586
72 Z = 4136619
63
XDOT = -7897
432402 XDOT = -2407
137396
YDOT = -19155
779113 feet/sec YDOT = -5838
681474 meter/sec
ZDOT = 12406
550343 ZDOT = 3781
516545
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
41756590
00016717 00000-0 10270-3 0 9085
2 25544 51
6468 184
7643 0004055 309
6425 50
4367 15
50277466 3582
Satellite: ISS
Catalog Number: 25544
Epoch time: 13225
41756590 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 184
7643 deg
Eccentricity:
0004055
Arg of perigee: 309
6425 deg
Mean anomaly: 50
4367 deg
Mean motion: 15
50277466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 358
Checksum: 321
Coasting Arc #10 (Orbit 372)
---------------------------------------
Vector Time (GMT): 2013/226/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3840383
97 A = 6792313
78 meter
Y = 3440200
19 meter E =
0008002
Z = -4429881
50 I = 51
64016
XDOT = -6315
887180 Wp = 42
80629
YDOT = 2750
660484 meter/sec RA = 179
01018 deg
ZDOT = -3337
098030 TA = 193
40479
MA = 193
42606
Ha = 226
376 n
mi
Hp = 221
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12599684
93 X = 3823148
55
Y = 11286746
03 feet Y = 3483049
45 meter
Z = -14533731
95 Z = -4411267
18
XDOT = -20721
414632 XDOT = -6329
965600
YDOT = 9024
476653 feet/sec YDOT = 2679
953532 meter/sec
ZDOT = -10948
484351 ZDOT = -3367
814099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10716726
60 X = 3266458
27
Y = -13173595
21 feet Y = -4015311
82 meter
Z = -14456148
21 Z = -4406233
98
XDOT = 8962
416068 XDOT = 2731
744418
YDOT = 19454
846558 feet/sec YDOT = 5929
837231 meter/sec
ZDOT = -11077
537771 ZDOT = -3376
433513
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
38448483
00016717 00000-0 10270-3 0 9092
2 25544 51
6466 179
9723 0004088 312
7219 47
3587 15
50296035 3736
Satellite: ISS
Catalog Number: 25544
Epoch time: 13226
38448483 = yrday
fracday
Element set: 909
Inclination: 51
6466 deg
RA of node: 179
9723 deg
Eccentricity:
0004088
Arg of perigee: 312
7219 deg
Mean anomaly: 47
3587 deg
Mean motion: 15
50296035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 373
Checksum: 332
Coasting Arc #11 (Orbit 388)
---------------------------------------
Vector Time (GMT): 2013/227/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3655195
77 A = 6791375
81 meter
Y = -3321814
36 meter E =
0004671
Z = 4657530
37 I = 51
66705
XDOT = 6429
296390 Wp = 96
00828
YDOT = -2985
668321 meter/sec RA = 174
05299 deg
ZDOT = 2913
253031 TA = 324
99084
MA = 325
02154
Ha = 226
548 n
mi
Hp = 221
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11992112
11 X = -3640403
74
Y = -10898341
07 feet Y = -3362606
46 meter
Z = 15280611
47 Z = 4639809
73
XDOT = 21093
492092 XDOT = 6448
053236
YDOT = -9795
499741 feet/sec YDOT = -2913
667042 meter/sec
ZDOT = 9557
916767 ZDOT = 2944
531278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10137668
93 X = -3089961
49
Y = 12730439
68 feet Y = 3880238
01 meter
Z = 15206750
21 Z = 4635017
46
XDOT = -10134
320762 XDOT = -3088
940968
YDOT = -19656
216271 feet/sec YDOT = -5991
214719 meter/sec
ZDOT = 9689
372984 ZDOT = 2953
320886
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
41585556
00016717 00000-0 10270-3 0 9102
2 25544 51
6458 174
8602 0004198 316
7813 43
3008 15
50310012 3896
Satellite: ISS
Catalog Number: 25544
Epoch time: 13227
41585556 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 174
8602 deg
Eccentricity:
0004198
Arg of perigee: 316
7813 deg
Mean anomaly: 43
3008 deg
Mean motion: 15
50310012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 389
Checksum: 292
Coasting Arc #12 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2013/228/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3458233
06 A = 6790529
92 meter
Y = 3249265
45 meter E =
0010799
Z = -4867314
28 I = 51
69461
XDOT = -6491
467847 Wp = 51
56400
YDOT = 3225
916712 meter/sec RA = 169
09720 deg
ZDOT = -2455
825024 TA = 194
28473
MA = 194
31529
Ha = 226
568 n
mi
Hp = 221
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11345908
99 X = 3445285
90
Y = 10660319
71 feet Y = 3287865
35 meter
Z = -15968878
86 Z = -4850546
01
XDOT = -21297
466689 XDOT = -6515
128676
YDOT = 10583
716248 feet/sec YDOT = 3153
192783 meter/sec
ZDOT = -8057
168715 ZDOT = -2487
417053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9730112
55 X = 2965738
30
Y = -12244351
33 feet Y = -3732078
29 meter
Z = -15898991
46 Z = -4846012
60
XDOT = 11321
572450 XDOT = 3450
815283
YDOT = 19643
516012 feet/sec YDOT = 5987
343680 meter/sec
ZDOT = -8189
989227 ZDOT = -2496
308716
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
38275591
00016717 00000-0 10270-3 0 9115
2 25544 51
6456 170
0677 0004173 320
7626 39
3221 15
50321248 4047
Satellite: ISS
Catalog Number: 25544
Epoch time: 13228
38275591 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 170
0677 deg
Eccentricity:
0004173
Arg of perigee: 320
7626 deg
Mean anomaly: 39
3221 deg
Mean motion: 15
50321248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 404
Checksum: 286
Coasting Arc #13 (Orbit 419)
---------------------------------------
Vector Time (GMT): 2013/229/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3235372
35 A = 6789749
53 meter
Y = -3208594
97 meter E =
0002415
Z = 5031544
55 I = 51
72208
XDOT = 6533
911367 Wp = 85
43440
YDOT = -3481
017793 meter/sec RA = 164
14286 deg
ZDOT = 1980
958339 TA = 345
33755
MA = 345
34456
Ha = 226
710 n
mi
Hp = 221
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10614738
66 X = -3223694
20
Y = -10526886
38 feet Y = -3244709
79 meter
Z = 16507692
08 Z = 5015855
91
XDOT = 21436
717083 XDOT = 6562
728434
YDOT = -11420
662050 feet/sec YDOT = -3407
790383 meter/sec
ZDOT = 6499
207150 ZDOT = 2012
768931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9454655
62 X = -2881779
03
Y = 11672687
90 feet Y = 3557835
27 meter
Z = 16442316
02 Z = 5011617
92
XDOT = -12559
009371 XDOT = -3827
986056
YDOT = -19518
823634 feet/sec YDOT = -5949
337443 meter/sec
ZDOT = 6632
995025 ZDOT = 2021
736884
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 13229
41410621
00016717 00000-0 10270-3 0 9126
2 25544 51
6454 164
9557 0004330 324
0220 36
0639 15
50340717 4203
Satellite: ISS
Catalog Number: 25544
Epoch time: 13229
41410621 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 164
9557 deg
Eccentricity:
0004330
Arg of perigee: 324
0220 deg
Mean anomaly: 36
0639 deg
Mean motion: 15
50340717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 263
Coasting Arc #14 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2013/230/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3018969
85 A = 6789152
14 meter
Y = 3214985
54 meter E =
0012809
Z = -5172649
88 I = 51
74986
XDOT = -6516
916368 Wp = 60
53089
YDOT = 3727
770047 meter/sec RA = 159
18974 deg
ZDOT = -1483
223863 TA = 195
16189
MA = 195
20032
Ha = 226
751 n
mi
Hp = 221
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9904756
74 X = 3007921
66
Y = 10547852
81 feet Y = 3248683
85 meter
Z = -16970636
09 Z = -5158011
07
XDOT = -21380
959214 XDOT = -6550
911793
YDOT = 12230
216691 feet/sec YDOT = 3654
703696 meter/sec
ZDOT = -4866
220023 ZDOT = -1514
964385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9352857
67 X = 2850751
02
Y = -11133354
42 feet Y = -3393446
43 meter
Z = -16909653
06 Z = -5154062
25
XDOT = 13743
364289 XDOT = 4188
977435
YDOT = 19156
114314 feet/sec YDOT = 5838
783643 meter/sec
ZDOT = -4999
762825 ZDOT = -1523
927709
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 13230
38098762
00016717 00000-0 10270-3 0 9133
2 25544 51
6458 160
1630 0004290 328
3668 31
7224 15
50349664 4353
Satellite: ISS
Catalog Number: 25544
Epoch time: 13230
38098762 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 160
1630 deg
Eccentricity:
0004290
Arg of perigee: 328
3668 deg
Mean anomaly: 31
7224 deg
Mean motion: 15
50349664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 300
Coasting Arc #15 (Orbit 450)
---------------------------------------
Vector Time (GMT): 2013/231/08:41:36
139
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2783822
24 A = 6788642
51 meter
Y = -3259201
48 meter E =
0002167
Z = 5263284
83 I = 51
77719
XDOT = 6480
561916 Wp = 25
69424
YDOT = -3974
279144 meter/sec RA = 154
23869 deg
ZDOT = 968
405454 TA = 55
05975
MA = 55
03940
Ha = 226
872 n
mi
Hp = 221
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9133275
07 X = -2772737
30
Y = -10692918
23 feet Y = -3290269
90 meter
Z = 17267994
86 Z = 5249788
53
XDOT = 21261
686077 XDOT = 6519
817375
YDOT = -13038
973571 feet/sec YDOT = -3901
589892 meter/sec
ZDOT = 3177
183247 ZDOT = 999
982150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9403553
55 X = -2866203
12
Y = 10548269
58 feet Y = 3215112
57 meter
Z = 17211799
73 Z = 5246156
56
XDOT = -14913
078479 XDOT = -4545
506320
YDOT = -18686
384410 feet/sec YDOT = -5695
609968 meter/sec
ZDOT = 3310
085165 ZDOT = 1008
913958
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
41231763
00016717 00000-0 10270-3 0 9149
2 25544 51
6462 155
0513 0004441 331
3485 28
7421 15
50371425 4513
Satellite: ISS
Catalog Number: 25544
Epoch time: 13231
41231763 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 155
0513 deg
Eccentricity:
0004441
Arg of perigee: 331
3485 deg
Mean anomaly: 28
7421 deg
Mean motion: 15
50371425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 451
Checksum: 266
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