[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 12th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 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
There are no maneuvers
Coasting Arc #1 (Orbit 343)
---------------------------------------
Vector Time (GMT): 2013/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1300668
71 A = 6788798
88 meter
Y = 4057029
61 meter E =
0011303
Z = -5295140
73 I = 51
57056
XDOT = -7463
179085 Wp = 83
94328
YDOT = -1579
437316 meter/sec RA = 188
21970 deg
ZDOT = 625
397656 TA = 192
03019
MA = 192
05721
Ha = 226
251 n
mi
Hp = 221
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4267285
78 X = -1320216
41
Y = 13310464
59 feet Y = 4042375
27 meter
Z = -17372508
96 Z = -5301506
81
XDOT = -24485
495686 XDOT = -7448
000787
YDOT = -5181
880959 feet/sec YDOT = -1662
810431 meter/sec
ZDOT = 2051
829579 ZDOT = 589
179316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11703787
16 X = 3567314
33
Y = -7579904
87 feet Y = -2310355
00 meter
Z = -17399674
46 Z = -5303420
78
XDOT = 14980
488789 XDOT = 4566
052983
YDOT = 18786
029245 feet/sec YDOT = 5725
981714 meter/sec
ZDOT = 1900
276985 ZDOT = 579
204425
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
51513450
00016717 00000-0 10270-3 0 9003
2 25544 51
6462 189
2429 0004175 305
5829 54
4932 15
50243720 3447
Satellite: ISS
Catalog Number: 25544
Epoch time: 13224
51513450 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 189
2429 deg
Eccentricity:
0004175
Arg of perigee: 305
5829 deg
Mean anomaly: 54
4932 deg
Mean motion: 15
50243720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 344
Checksum: 284
Coasting Arc #2 (Orbit 359)
---------------------------------------
Vector Time (GMT): 2013/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1492703
45 A = 6789012
09 meter
Y = -4065755
18 meter E =
0004730
Z = 5228865
86 I = 51
60227
XDOT = 7467
211916 Wp = 358
90928
YDOT = 1306
874688 meter/sec RA = 183
25768 deg
ZDOT = -1110
911974 TA = 101
77898
MA = 101
72592
Ha = 226
283 n
mi
Hp = 221
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4897321
02 X = 1512656
35
Y = -13339091
81 feet Y = -4048951
21 meter
Z = 17155071
71 Z = 5236165
75
XDOT = 24498
726758 XDOT = 7457
439665
YDOT = 4287
646615 feet/sec YDOT = 1390
323132 meter/sec
ZDOT = -3644
724325 ZDOT = -1074
660824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12082122
54 X = -3682630
95
Y = 7407429
22 feet Y = 2257784
43 meter
Z = 17186154
78 Z = 5238339
98
XDOT = -15906
182166 XDOT = -4848
204324
YDOT = -17805
115023 feet/sec YDOT = -5426
999059 meter/sec
ZDOT = -3492
986252 ZDOT = -1064
662210
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
54653623
00016717 00000-0 10270-3 0 9015
2 25544 51
6464 184
1319 0004243 309
6670 50
4106 15
50259867 3602
Satellite: ISS
Catalog Number: 25544
Epoch time: 13225
54653623 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 184
1319 deg
Eccentricity:
0004243
Arg of perigee: 309
6670 deg
Mean anomaly: 50
4106 deg
Mean motion: 15
50259867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 360
Checksum: 291
Coasting Arc #3 (Orbit 374)
---------------------------------------
Vector Time (GMT): 2013/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1669794
01 A = 6789382
64 meter
Y = 4120387
74 meter E =
0010204
Z = -5140079
31 I = 51
63442
XDOT = -7417
372240 Wp = 89
37697
YDOT = -1033
760786 meter/sec RA = 178
29723 deg
ZDOT = 1583
740473 TA = 195
90729
MA = 195
93936
Ha = 226
416 n
mi
Hp = 221
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5478326
81 X = -1690775
97
Y = 13518332
49 feet Y = 4101597
77 meter
Z = -16863777
25 Z = -5148241
91
XDOT = -24335
210761 XDOT = -7412
954574
YDOT = -3391
603627 feet/sec YDOT = -1116
681852 meter/sec
ZDOT = 5195
998926 ZDOT = 1547
718421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12523496
18 X = 3817161
64
Y = -7399156
87 feet Y = -2255263
01 meter
Z = -16898487
57 Z = -5150659
01
XDOT = 16652
672618 XDOT = 5075
734614
YDOT = 16684
426207 feet/sec YDOT = 5085
413108 meter/sec
ZDOT = 5045
170539 ZDOT = 1537
767980
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
51346641
00016717 00000-0 10270-3 0 9023
2 25544 51
6465 179
3396 0004302 313
1840 46
8950 15
50273107 3754
Satellite: ISS
Catalog Number: 25544
Epoch time: 13226
51346641 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 179
3396 deg
Eccentricity:
0004302
Arg of perigee: 313
1840 deg
Mean anomaly: 46
8950 deg
Mean motion: 15
50273107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 375
Checksum: 291
Coasting Arc #4 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2013/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1861076
58 A = 6789903
07 meter
Y = -4198610
08 meter E =
0006750
Z = 5001321
61 I = 51
66744
XDOT = 7336
677445 Wp = 17
90004
YDOT = 785
837525 meter/sec RA = 173
33970 deg
ZDOT = -2063
375546 TA = 92
21799
MA = 92
14070
Ha = 226
463 n
mi
Hp = 221
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6105894
29 X = 1883593
13
Y = -13774967
45 feet Y = -4177672
56 meter
Z = 16408535
45 Z = 5010417
09
XDOT = 24070
464060 XDOT = 7337
368013
YDOT = 2578
207102 feet/sec YDOT = 867
884808 meter/sec
ZDOT = -6769
604810 ZDOT = -2027
733167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13053001
96 X = -3978555
00
Y = 7441867
93 feet Y = 2268281
34 meter
Z = 16447171
51 Z = 5013097
88
XDOT = -17232
291210 XDOT = -5252
402361
YDOT = -15543
132016 feet/sec YDOT = -4737
546638 meter/sec
ZDOT = -6620
318012 ZDOT = -2017
872930
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
54485053
00016717 00000-0 10270-3 0 9039
2 25544 51
6469 174
2284 0004313 317
2275 42
8540 15
50289094 3918
Satellite: ISS
Catalog Number: 25544
Epoch time: 13227
54485053 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 174
2284 deg
Eccentricity:
0004313
Arg of perigee: 317
2275 deg
Mean anomaly: 42
8540 deg
Mean motion: 15
50289094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 301
Coasting Arc #5 (Orbit 405)
---------------------------------------
Vector Time (GMT): 2013/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2019376
43 A = 6790533
39 meter
Y = 4319277
90 meter E =
0008335
Z = -4842306
46 I = 51
70017
XDOT = -7208
335794 Wp = 91
50880
YDOT = -549
538017 meter/sec RA = 168
38379 deg
ZDOT = 2519
435073 TA = 203
26558
MA = 203
30332
Ha = 226
583 n
mi
Hp = 221
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6625250
75 X = -2044003
09
Y = 14170859
25 feet Y = 4296558
40 meter
Z = -15886832
21 Z = -4852175
99
XDOT = -23649
395651 XDOT = -7213
893604
YDOT = -1802
946250 feet/sec YDOT = -630
177344 meter/sec
ZDOT = 8265
863099 ZDOT = 2484
404481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13578500
02 X = 4138726
81
Y = -7681040
97 feet Y = -2341181
29 meter
Z = -15928734
53 Z = -4855078
28
XDOT = 17615
140002 XDOT = 5369
094673
YDOT = 14326
813154 feet/sec YDOT = 4366
812649 meter/sec
ZDOT = 8119
090770 ZDOT = 2474
698867
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
51176408
00016717 00000-0 10270-3 0 9049
2 25544 51
6469 169
4358 0004390 320
5822 39
5009 15
50304289 4060
Satellite: ISS
Catalog Number: 25544
Epoch time: 13228
51176408 = yrday
fracday
Element set: 904
Inclination: 51
6469 deg
RA of node: 169
4358 deg
Eccentricity:
0004390
Arg of perigee: 320
5822 deg
Mean anomaly: 39
5009 deg
Mean motion: 15
50304289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 406
Checksum: 303
Coasting Arc #6 (Orbit 421)
---------------------------------------
Vector Time (GMT): 2013/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2185913
95 A = 6791327
86 meter
Y = -4460773
54 meter E =
0008622
Z = 4630058
95 I = 51
73355
XDOT = 7050
331337 Wp = 35
42699
YDOT = 353
485076 meter/sec RA = 163
43113 deg
ZDOT = -2978
356889 TA = 84
29911
MA = 84
20081
Ha = 226
644 n
mi
Hp = 221
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7171633
69 X = 2213141
60
Y = -14635083
80 feet Y = -4436177
14 meter
Z = 15190482
13 Z = 4640743
79
XDOT = 23131
008324 XDOT = 7060
322424
YDOT = 1159
727941 feet/sec YDOT = 432
382284 meter/sec
ZDOT = -9771
512102 ZDOT = -2944
083262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14161519
16 X = -4316431
04
Y = 7980584
30 feet Y = 2432482
09 meter
Z = 15235826
34 Z = 4643879
87
XDOT = -17803
074775 XDOT = -5426
377191
YDOT = -13150
620951 feet/sec YDOT = -4008
309266 meter/sec
ZDOT = -9627
867841 ZDOT = -2934
574118
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
54313037
00016717 00000-0 10270-3 0 9055
2 25544 51
6476 164
3245 0004373 324
5705 35
5155 15
50317316 4223
Satellite: ISS
Catalog Number: 25544
Epoch time: 13229
54313037 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 164
3245 deg
Eccentricity:
0004373
Arg of perigee: 324
5705 deg
Mean anomaly: 35
5155 deg
Mean motion: 15
50317316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 422
Checksum: 282
Coasting Arc #7 (Orbit 436)
---------------------------------------
Vector Time (GMT): 2013/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957463
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2303427
32 A = 6792148
13 meter
Y = 4636263
40 meter E =
0006138
Z = -4401841
39 I = 51
76610
XDOT = -6856
519088 Wp = 84
86820
YDOT = -179
180730 meter/sec RA = 158
48024 deg
ZDOT = 3403
830369 TA = 219
57664
MA = 219
62147
Ha = 226
749 n
mi
Hp = 221
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7557176
25 X = -2333717
30
Y = 15210837
94 feet Y = 4610335
70 meter
Z = -14441736
85 Z = -4413104
55
XDOT = -22495
141364 XDOT = -6870
540423
YDOT = -587
863288 feet/sec YDOT = -255
933097 meter/sec
ZDOT = 11167
422471 ZDOT = 3370
488609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14666709
85 X = 4470413
16
Y = -8484416
17 feet Y = -2586050
05 meter
Z = -14489533
17 Z = -4416409
71
XDOT = 17804
618507 XDOT = 5426
847721
YDOT = 11971
228107 feet/sec YDOT = 3648
830327 meter/sec
ZDOT = 11027
644041 ZDOT = 3361
225904
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
51002739
00016717 00000-0 10270-3 0 9069
2 25544 51
6480 159
5319 0004438 328
0219 32
0662 15
50336756 4377
Satellite: ISS
Catalog Number: 25544
Epoch time: 13230
51002739 = yrday
fracday
Element set: 906
Inclination: 51
6480 deg
RA of node: 159
5319 deg
Eccentricity:
0004438
Arg of perigee: 328
0219 deg
Mean anomaly: 32
0662 deg
Mean motion: 15
50336756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 437
Checksum: 290
Coasting Arc #8 (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 = 2423953
86 A = 6793147
02 meter
Y = -4826611
31 meter E =
0010263
Z = 4117579
91 I = 51
79832
XDOT = 6637
844080 Wp = 52
04877
YDOT = 58
759038 meter/sec RA = 153
53279 deg
ZDOT = -3826
057788 TA = 77
46264
MA = 77
34786
Ha = 226
828 n
mi
Hp = 221
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7952604
53 X = 2457744
28
Y = -15835338
94 feet Y = -4799316
12 meter
Z = 13509120
45 Z = 4129437
15
XDOT = 21777
703673 XDOT = 6655
279231
YDOT = 192
778995 feet/sec YDOT = 133
085043 meter/sec
ZDOT = -12552
683032 ZDOT = -3793
770101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15194261
87 X = -4631211
02
Y = 9042915
15 feet Y = 2756280
54 meter
Z = 13559436
03 Z = 4132916
10
XDOT = -17603
955069 XDOT = -5365
685505
YDOT = -10897
656105 feet/sec YDOT = -3321
605581 meter/sec
ZDOT = -12417
292749 ZDOT = -3784
790830
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
54137595
00016717 00000-0 10270-3 0 9073
2 25544 51
6486 154
4206 0004424 331
9256 28
1656 15
50343311 4533
Satellite: ISS
Catalog Number: 25544
Epoch time: 13231
54137595 = yrday
fracday
Element set: 907
Inclination: 51
6486 deg
RA of node: 154
4206 deg
Eccentricity:
0004424
Arg of perigee: 331
9256 deg
Mean anomaly: 28
1656 deg
Mean motion: 15
50343311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 453
Checksum: 290
Coasting Arc #9 (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 = -2483277
04 A = 6794057
92 meter
Y = 5038345
43 meter E =
0004853
Z = -3823477
17 I = 51
82937
XDOT = -6399
660573 Wp = 58
98956
YDOT = 33
411692 meter/sec RA = 148
58714 deg
ZDOT = 4206
877757 TA = 255
30629
MA = 255
36008
Ha = 226
909 n
mi
Hp = 221
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8147234
39 X = -2520859
34
Y = 16530004
69 feet Y = 5010365
56 meter
Z = -12544216
44 Z = -3835631
93
XDOT = -20996
261723 XDOT = -6419
993983
YDOT = 109
618412 feet/sec YDOT = -38
266888 meter/sec
ZDOT = 13802
092377 ZDOT = 4175
740073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15573322
31 X = 4746748
64
Y = -9787392
74 feet Y = -2983197
31 meter
Z = -12595809
81 Z = -3839202
83
XDOT = 17255
699505 XDOT = 5259
537209
YDOT = 9889
041469 feet/sec YDOT = 3014
179840 meter/sec
ZDOT = 13671
499935 ZDOT = 4167
073180
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
50825638
00016717 00000-0 10270-3 0 9083
2 25544 51
6492 149
6281 0004471 335
4537 24
6401 15
50369415 4680
Satellite: ISS
Catalog Number: 25544
Epoch time: 13232
50825638 = yrday
fracday
Element set: 908
Inclination: 51
6492 deg
RA of node: 149
6281 deg
Eccentricity:
0004471
Arg of perigee: 335
4537 deg
Mean anomaly: 24
6401 deg
Mean motion: 15
50369415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 468
Checksum: 307
Coasting Arc #10 (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 = 2542287
62 A = 6795156
30 meter
Y = -5256101
70 meter E =
0011544
Z = 3471428
35 I = 51
85871
XDOT = 6144
761780 Wp = 67
73076
YDOT = -61
021479 meter/sec RA = 143
64469 deg
ZDOT = -4576
056056 TA = 71
74346
MA = 71
61786
Ha = 227
012 n
mi
Hp = 221
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8340838
66 X = 2584010
61
Y = -17244428
16 feet Y = -5227438
73 meter
Z = 11389200
63 Z = 3483879
99
XDOT = 20159
979593 XDOT = 6167
216261
YDOT = -200
201702 feet/sec YDOT = 7
818409 meter/sec
ZDOT = -15013
307271 ZDOT = -4546
151388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15941379
12 X = -4858932
36
Y = 10564338
39 feet Y = 3220010
34 meter
Z = 11442070
16 Z = 3487542
98
XDOT = -16720
989949 XDOT = -5096
557736
YDOT = -9048
709308 feet/sec YDOT = -2758
046597 meter/sec
ZDOT = -14887
872424 ZDOT = -4537
823515
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
53958726
00016717 00000-0 10270-3 0 9093
2 25544 51
6492 144
5167 0004465 339
3528 20
7442 15
50366585 4848
Satellite: ISS
Catalog Number: 25544
Epoch time: 13233
53958726 = yrday
fracday
Element set: 909
Inclination: 51
6492 deg
RA of node: 144
5167 deg
Eccentricity:
0004465
Arg of perigee: 339
3528 deg
Mean anomaly: 20
7442 deg
Mean motion: 15
50366585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 484
Checksum: 325
Coasting Arc #11 (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 = -2533176
95 A = 6796041
28 meter
Y = 5479859
97 meter E =
0006196
Z = -3117108
81 I = 51
88675
XDOT = -5889
341324 Wp = 29
61430
YDOT = 58
557462 meter/sec RA = 138
70383 deg
ZDOT = 4898
423567 TA = 294
71631
MA = 294
78079
Ha = 227
063 n
mi
Hp = 220
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8310948
00 X = -2579123
82
Y = 17978543
22 feet Y = 5451275
24 meter
Z = -10226734
93 Z = -3129526
59
XDOT = -19321
985972 XDOT = -5913
353281
YDOT = 192
117656 feet/sec YDOT = -7
434773 meter/sec
ZDOT = 16070
943462 ZDOT = 4869
755779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16103178
81 X = 4908248
90
Y = -11485015
63 feet Y = -3500632
76 meter
Z = -10279495
53 Z = -3133190
24
XDOT = 16101
885711 XDOT = 4907
854765
YDOT = 8327
526514 feet/sec YDOT = 2538
230082 meter/sec
ZDOT = 15950
688888 ZDOT = 4861
769973
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
50645066
00016717 00000-0 10270-3 0 9103
2 25544 51
6497 139
7242 0004528 342
5080 17
5915 15
50400430 4995
Satellite: ISS
Catalog Number: 25544
Epoch time: 13234
50645066 = yrday
fracday
Element set: 910
Inclination: 51
6497 deg
RA of node: 139
7242 deg
Eccentricity:
0004528
Arg of perigee: 342
5080 deg
Mean anomaly: 17
5915 deg
Mean motion: 15
50400430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 292
Coasting Arc #12 (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 = 2523271
43 A = 6797106
53 meter
Y = -5698756
90 meter E =
0012271
Z = 2704473
70 I = 51
91212
XDOT = 5627
929176 Wp = 82
25451
YDOT = 14
502141 meter/sec RA = 133
76574 deg
ZDOT = -5198
506417 TA = 67
36297
MA = 67
23323
Ha = 227
186 n
mi
Hp = 220
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8278449
58 X = 2573671
17
Y = -18696708
98 feet Y = -5670258
06 meter
Z = 8872945
23 Z = 2716854
28
XDOT = 18464
334568 XDOT = 5652
601408
YDOT = 47
579203 feet/sec YDOT = 77
574743 meter/sec
ZDOT = -17055
467249 ZDOT = -5171
106805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16228981
11 X = -4946593
44
Y = 12400924
36 feet Y = 3779801
74 meter
Z = 8925584
49 Z = 2720518
15
XDOT = -15334
658899 XDOT = -4674
004032
YDOT = -7824
211506 feet/sec YDOT = -2384
819667 meter/sec
ZDOT = -16940
534626 ZDOT = -5163
474954
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
53776376
00016717 00000-0 10270-3 0 9117
2 25544 51
6492 134
6124 0004507 346
5457 13
5572 15
50387030 5156
Satellite: ISS
Catalog Number: 25544
Epoch time: 13235
53776376 = yrday
fracday
Element set: 911
Inclination: 51
6492 deg
RA of node: 134
6124 deg
Eccentricity:
0004507
Arg of perigee: 346
5457 deg
Mean anomaly: 13
5572 deg
Mean motion: 15
50387030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 297
Coasting Arc #13 (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 = -2444284
14 A = 6797841
90 meter
Y = 5907225
46 meter E =
0009238
Z = -2298169
91 I = 51
93601
XDOT = -5385
606499 Wp = 20
64286
YDOT = -114
332965 meter/sec RA = 128
82893 deg
ZDOT = 5449
197403 TA = 313
91040
MA = 313
98663
Ha = 227
212 n
mi
Hp = 220
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8019304
94 X = -2498994
55
Y = 19380660
97 feet Y = 5879585
85 meter
Z = -7539927
54 Z = -2310177
29
XDOT = -17669
312661 XDOT = -5410
398286
YDOT = -375
108154 feet/sec YDOT = -174
696432 meter/sec
ZDOT = 17877
944235 ZDOT = 5422
974578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16111504
17 X = 4910786
47
Y = -13400200
19 feet Y = -4084381
02 meter
Z = -7591037
28 Z = -2313748
16
XDOT = 14562
997637 XDOT = 4438
801680
YDOT = 7472
070022 feet/sec YDOT = 2277
486943 meter/sec
ZDOT = 17767
954470 ZDOT = 5415
672522
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
50460980
00016717 00000-0 10270-3 0 9127
2 25544 51
6497 129
8195 0004626 348
9639 11
1409 15
50428710 5306
Satellite: ISS
Catalog Number: 25544
Epoch time: 13236
50460980 = yrday
fracday
Element set: 912
Inclination: 51
6497 deg
RA of node: 129
8195 deg
Eccentricity:
0004626
Arg of perigee: 348
9639 deg
Mean anomaly: 11
1409 deg
Mean motion: 15
50428710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 307
Coasting Arc #14 (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 = 2367537
90 A = 6798730
42 meter
Y = -6099224
16 meter E =
0012244
Z = 1835311
10 I = 51
95684
XDOT = 5149
291586 Wp = 95
31370
YDOT = 284
665032 meter/sec RA = 123
89464 deg
ZDOT = -5665
168906 TA = 64
62944
MA = 64
50272
Ha = 227
341 n
mi
Hp = 220
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7767512
80 X = 2426649
39
Y = -20010577
95 feet Y = -6072418
22 meter
Z = 6021361
87 Z = 1846956
32
XDOT = 16894
001266 XDOT = 5173
245434
YDOT = 933
940395 feet/sec YDOT = 342
381235 meter/sec
ZDOT = -18586
512158 ZDOT = -5640
096055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15947562
91 X = -4860817
18
Y = 14346867
88 feet Y = 4372925
33 meter
Z = 6070988
63 Z = 1850437
34
XDOT = -13700
104442 XDOT = -4175
791834
YDOT = -7364
922450 feet/sec YDOT = -2244
828363 meter/sec
ZDOT = -18481
362195 ZDOT = -5633
119197
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
53590517
00016717 00000-0 10270-3 0 9132
2 25544 51
6492 124
7074 0004555 353
1917 6
9171 15
50405251 5469
Satellite: ISS
Catalog Number: 25544
Epoch time: 13237
53590517 = yrday
fracday
Element set: 913
Inclination: 51
6492 deg
RA of node: 124
7074 deg
Eccentricity:
0004555
Arg of perigee: 353
1917 deg
Mean anomaly: 6
9171 deg
Mean motion: 15
50405251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 295
Coasting Arc #15 (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 = -2226777
70 A = 6799194
84 meter
Y = 6265224
63 meter E =
0012473
Z = -1388038
20 I = 51
97554
XDOT = -4950
109838 Wp = 23
01918
YDOT = -473
688124 meter/sec RA = 118
96114 deg
ZDOT = 5831
985866 TA = 321
94586
MA = 322
03391
Ha = 227
356 n
mi
Hp = 220
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7305701
12 X = -2289928
62
Y = 20555198
92 feet Y = 6239970
22 meter
Z = -4553931
11 Z = -1399009
37
XDOT = -16240
517842 XDOT = -4972
775163
YDOT = -1554
094896 feet/sec YDOT = -529
169815 meter/sec
ZDOT = 19133
811896 ZDOT = 5807
883734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15529339
85 X = 4733342
79
Y = -15306871
93 feet Y = -4665534
56 meter
Z = -4600764
69 Z = -1402313
08
XDOT = 12918
884502 XDOT = 3937
675996
YDOT = 7414
117893 feet/sec YDOT = 2259
823134 meter/sec
ZDOT = 19032
752689 ZDOT = 5801
183019
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
50273404
00016717 00000-0 10270-3 0 9144
2 25544 51
6495 119
9143 0004738 355
0578 5
0525 15
50455639 5617
Satellite: ISS
Catalog Number: 25544
Epoch time: 13238
50273404 = yrday
fracday
Element set: 914
Inclination: 51
6495 deg
RA of node: 119
9143 deg
Eccentricity:
0004738
Arg of perigee: 355
0578 deg
Mean anomaly: 5
0525 deg
Mean motion: 15
50455639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 561
Checksum: 305
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