[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 28th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
301/09:00:02
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 221
3
Coasting Arc #1 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2013/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926909
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3473570
33 A = 6794078
31 meter
Y = 3690133
65 meter E =
0010877
Z = -4535914
50 I = 51
62541
XDOT = -6575
196602 Wp = 71
52545
YDOT = 2315
440680 meter/sec RA = 181
59774 deg
ZDOT = -3154
402100 TA = 166
76234
MA = 166
73377
Ha = 228
693 n
mi
Hp = 221
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11396228
11 X = 3454082
87
Y = 12106737
69 feet Y = 3728868
18 meter
Z = -14881609
26 Z = -4519087
43
XDOT = -21572
167331 XDOT = -6585
276207
YDOT = 7596
590159 feet/sec YDOT = 2241
856163 meter/sec
ZDOT = -10349
088256 ZDOT = -3186
368896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16243071
73 X = -4950888
26
Y = -3833271
71 feet Y = -1168381
22 meter
Z = -14811416
38 Z = -4514519
71
XDOT = 13551
760181 XDOT = 4130
576503
YDOT = -16952
773924 feet/sec YDOT = -5167
205492 meter/sec
ZDOT = -10483
622385 ZDOT = -3195
408103
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 13298
52191742
00016717 00000-0 10270-3 0 9001
2 25544 51
6494 182
5658 0001335 81
8440 278
2862 15
49556457 14925
Satellite: ISS
Catalog Number: 25544
Epoch time: 13298
52191742 = yrday
fracday
Element set: 900
Inclination: 51
6494 deg
RA of node: 182
5658 deg
Eccentricity:
0001335
Arg of perigee: 81
8440 deg
Mean anomaly: 278
2862 deg
Mean motion: 15
49556457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 330
Coasting Arc #2 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2013/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926909
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3575398
79 A = 6793702
39 meter
Y = -3454393
73 meter E =
0009761
Z = 4623898
50 I = 51
65501
XDOT = 6509
220997 Wp = 110
52261
YDOT = -2740
621024 meter/sec RA = 176
64636 deg
ZDOT = 2977
324515 TA = 309
74530
MA = 309
83126
Ha = 228
809 n
mi
Hp = 221
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11730311
00 X = -3558967
24
Y = -11333312
75 feet Y = -3494284
01 meter
Z = 15170270
67 Z = 4606569
36
XDOT = 21355
711932 XDOT = 6524
920191
YDOT = -8991
538792 feet/sec YDOT = -2667
742850 meter/sec
ZDOT = 9768
125049 ZDOT = 3008
984453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16149585
67 X = 4922393
71
Y = 2724822
80 feet Y = 830525
99 meter
Z = 15097930
64 Z = 4601849
26
XDOT = -12358
325572 XDOT = -3766
817634
YDOT = 18228
876420 feet/sec YDOT = 5556
161533 meter/sec
ZDOT = 9901
440316 ZDOT = 3017
959008
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 13299
55378817
00016717 00000-0 10270-3 0 9016
2 25544 51
6494 177
4572 0001438 85
6062 274
5253 15
49559387 15085
Satellite: ISS
Catalog Number: 25544
Epoch time: 13299
55378817 = yrday
fracday
Element set: 901
Inclination: 51
6494 deg
RA of node: 177
4572 deg
Eccentricity:
0001438
Arg of perigee: 85
6062 deg
Mean anomaly: 274
5253 deg
Mean motion: 15
49559387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1508
Checksum: 345
Coasting Arc #3 (Orbit 1522)
---------------------------------------
Vector Time (GMT): 2013/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926909
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3642348
76 A = 6793183
41 meter
Y = 3250136
37 meter E =
0011921
Z = -4735571
26 I = 51
68397
XDOT = -6402
088871 Wp = 72
63964
YDOT = 3144
863771 meter/sec RA = 171
69651 deg
ZDOT = -2768
046388 TA = 169
91383
MA = 169
88989
Ha = 228
578 n
mi
Hp = 221
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11949963
12 X = 3628738
76
Y = 10663177
06 feet Y = 3290791
05 meter
Z = -15536651
12 Z = -4717910
05
XDOT = -21004
228579 XDOT = -6423
332995
YDOT = 10317
794524 feet/sec YDOT = 3073
152594 meter/sec
ZDOT = -9081
517022 ZDOT = -2799
199391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15989220
36 X = -4873514
37
Y = -1771043
67 feet Y = -539814
11 meter
Z = -15462882
27 Z = -4713086
52
XDOT = 11044
094796 XDOT = 3366
240094
YDOT = -19337
511199 feet/sec YDOT = -5894
073413 meter/sec
ZDOT = -9212
769048 ZDOT = -2808
052006
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 13300
52115065
00016717 00000-0 10270-3 0 9021
2 25544 51
6491 172
6678 0001201 85
5753 274
5534 15
49599475 15231
Satellite: ISS
Catalog Number: 25544
Epoch time: 13300
52115065 = yrday
fracday
Element set: 902
Inclination: 51
6491 deg
RA of node: 172
6678 deg
Eccentricity:
0001201
Arg of perigee: 85
5753 deg
Mean anomaly: 274
5534 deg
Mean motion: 15
49599475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1523
Checksum: 306
Coasting Arc #4 (Orbit 1536)
---------------------------------------
Vector Time (GMT): 2013/301/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1255921
61 A = 6790462
77 meter
Y = -4024139
67 meter E =
0003822
Z = 5320271
43 I = 51
70132
XDOT = 7416
157277 Wp = 101
99737
YDOT = -1910
866808 meter/sec RA = 167
34995 deg
ZDOT = 304
383865 TA = 345
09634
MA = 345
10760
Ha = 228
560 n
mi
Hp = 221
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4120477
73 X = -1236674
28
Y = -13202557
97 feet Y = -4038076
20 meter
Z = 17454958
75 Z = 5314217
21
XDOT = 24331
224661 XDOT = 7435
495184
YDOT = -6269
248059 feet/sec YDOT = -1827
826473 meter/sec
ZDOT = 998
634728 ZDOT = 340
458528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2126464
69 X = 648146
44
Y = 13697931
79 feet Y = 4175129
61 meter
Z = 17430039
34 Z = 5312675
99
XDOT = -24004
335153 XDOT = -7316
521355
YDOT = 2258
556230 feet/sec YDOT = 688
407939 meter/sec
ZDOT = 1150
415741 ZDOT = 350
646718
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 13301
42401124
00016717 00000-0 10270-3 0 9036
2 25544 51
6484 168
1978 0001257 93
0796 267
0499 15
49647233 15376
Satellite: ISS
Catalog Number: 25544
Epoch time: 13301
42401124 = yrday
fracday
Element set: 903
Inclination: 51
6484 deg
RA of node: 168
1978 deg
Eccentricity:
0001257
Arg of perigee: 93
0796 deg
Mean anomaly: 267
0499 deg
Mean motion: 15
49647233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1537
Checksum: 316
Coasting Arc #5 (Orbit 1551)
---------------------------------------
Vector Time (GMT): 2013/302/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1337998
55 A = 6790438
53 meter
Y = 3994641
22 meter E =
0016205
Z = -5339683
42 I = 51
73177
XDOT = -7276
619084 Wp = 89
94285
YDOT = 2357
450310 meter/sec RA = 162
40270 deg
ZDOT = -59
871347 TA = 179
48677
MA = 179
48511
Ha = 228
558 n
mi
Hp = 221
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4389759
03 X = 1319169
32
Y = 13105778
27 feet Y = 4009497
86 meter
Z = -17518646
38 Z = -5333229
49
XDOT = -23873
422193 XDOT = -7302
148950
YDOT = 7734
417027 feet/sec YDOT = 2275
935773 meter/sec
ZDOT = -196
428303 ZDOT = -95
283293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2642244
35 X = -805356
08
Y = -13600785
33 feet Y = -4145519
37 meter
Z = -17492042
84 Z = -5331574
66
XDOT = 23720
479819 XDOT = 7230
002249
YDOT = -4164
465917 feet/sec YDOT = -1269
329212 meter/sec
ZDOT = -345
496466 ZDOT = -105
307323
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 13302
39134915
00016717 00000-0 10270-3 0 9045
2 25544 51
6491 163
4083 0001373 93
1142 267
0166 15
49647745 15520
Satellite: ISS
Catalog Number: 25544
Epoch time: 13302
39134915 = yrday
fracday
Element set: 904
Inclination: 51
6491 deg
RA of node: 163
4083 deg
Eccentricity:
0001373
Arg of perigee: 93
1142 deg
Mean anomaly: 267
0166 deg
Mean motion: 15
49647745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1552
Checksum: 299
Coasting Arc #6 (Orbit 1567)
---------------------------------------
Vector Time (GMT): 2013/303/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1408997
70 A = 6790288
90 meter
Y = -3961699
46 meter E =
0003613
Z = 5328644
97 I = 51
76055
XDOT = 7133
451675 Wp = 87
90740
YDOT = -2796
540801 meter/sec RA = 157
45770 deg
ZDOT = -192
685022 TA = 3
92825
MA = 3
92542
Ha = 228
468 n
mi
Hp = 221
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4622695
88 X = -1390478
00
Y = -12997701
63 feet Y = -3977351
74 meter
Z = 17482431
01 Z = 5321845
40
XDOT = 23403
712846 XDOT = 7165
129062
YDOT = -9175
002629 feet/sec YDOT = -2716
592903 meter/sec
ZDOT = -632
168708 ZDOT = -157
953495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3119904
89 X = 950947
01
Y = 13474274
82 feet Y = 4106958
97 meter
Z = 17454371
10 Z = 5320092
31
XDOT = -23364
737402 XDOT = -7121
571960
YDOT = 6040
437090 feet/sec YDOT = 1841
125225 meter/sec
ZDOT = -485
889581 ZDOT = -148
099144
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 13303
42315796
00016717 00000-0 10270-3 0 9059
2 25544 51
6488 158
2997 0001194 96
8430 263
2856 15
49695137 15682
Satellite: ISS
Catalog Number: 25544
Epoch time: 13303
42315796 = yrday
fracday
Element set: 905
Inclination: 51
6488 deg
RA of node: 158
2997 deg
Eccentricity:
0001194
Arg of perigee: 96
8430 deg
Mean anomaly: 263
2856 deg
Mean motion: 15
49695137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1568
Checksum: 345
Coasting Arc #7 (Orbit 1582)
---------------------------------------
Vector Time (GMT): 2013/304/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1481701
18 A = 6790342
67 meter
Y = 3957885
60 meter E =
0016001
Z = -5328801
50 I = 51
78916
XDOT = -6931
198649 Wp = 93
83912
YDOT = 3204
224091 meter/sec RA = 152
51398 deg
ZDOT = 452
763354 TA = 180
48026
MA = 180
48180
Ha = 228
430 n
mi
Hp = 221
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4861224
35 X = 1463219
58
Y = 12985188
98 feet Y = 3974351
11 meter
Z = -17482944
56 Z = -5321648
62
XDOT = -22740
153048 XDOT = -6968
713294
YDOT = 10512
546230 feet/sec YDOT = 3126
505299 meter/sec
ZDOT = 1485
444076 ZDOT = 419
000039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3589752
30 X = -1094156
50
Y = -13431025
63 feet Y = -4093776
61 meter
Z = -17453401
23 Z = -5319796
70
XDOT = 22741
207758 XDOT = 6931
520125
YDOT = -7822
977586 feet/sec YDOT = -2384
443568 meter/sec
ZDOT = 1343
166982 ZDOT = 409
397296
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 13304
39046599
00016717 00000-0 10270-3 0 9069
2 25544 51
6492 153
5101 0001248 96
5341 263
5951 15
49698154 15838
Satellite: ISS
Catalog Number: 25544
Epoch time: 13304
39046599 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 153
5101 deg
Eccentricity:
0001248
Arg of perigee: 96
5341 deg
Mean anomaly: 263
5951 deg
Mean motion: 15
49698154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1583
Checksum: 321
Coasting Arc #8 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2013/305/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1544595
33 A = 6790296
09 meter
Y = -3953972
12 meter E =
0003971
Z = 5296685
76 I = 51
81599
XDOT = 6727
713340 Wp = 73
36751
YDOT = -3599
766373 meter/sec RA = 147
57206 deg
ZDOT = -723
760500 TA = 23
54153
MA = 23
52336
Ha = 228
363 n
mi
Hp = 221
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5067569
98 X = -1525996
89
Y = -12972349
48 feet Y = -3971140
36 meter
Z = 17377577
96 Z = 5289227
55
XDOT = 22072
550327 XDOT = 6770
982623
YDOT = -11810
257130 feet/sec YDOT = -3524
290925 meter/sec
ZDOT = -2374
542323 ZDOT = -690
971623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4026276
52 X = 1227209
08
Y = 13372417
35 feet Y = 4075912
81 meter
Z = 17346754
27 Z = 5287290
70
XDOT = -22056
378246 XDOT = -6722
784089
YDOT = 9548
483709 feet/sec YDOT = 2910
377835 meter/sec
ZDOT = -2236
293639 ZDOT = -681
622301
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 13305
42224325
00016717 00000-0 10270-3 0 9070
2 25544 51
6488 148
4011 0001100 99
5068 260
6207 15
49742925 15997
Satellite: ISS
Catalog Number: 25544
Epoch time: 13305
42224325 = yrday
fracday
Element set: 907
Inclination: 51
6488 deg
RA of node: 148
4011 deg
Eccentricity:
0001100
Arg of perigee: 99
5068 deg
Mean anomaly: 260
6207 deg
Mean motion: 15
49742925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 301
Coasting Arc #9 (Orbit 1613)
---------------------------------------
Vector Time (GMT): 2013/306/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1619161
43 A = 6790446
86 meter
Y = 3977380
43 meter E =
0015457
Z = -5273662
95 I = 51
84176
XDOT = -6471
075142 Wp = 97
85349
YDOT = 3955
983121 meter/sec RA = 142
63122 deg
ZDOT = 997
239619 TA = 181
68703
MA = 181
69225
Ha = 228
294 n
mi
Hp = 221
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5312209
43 X = 1600183
93
Y = 13049148
41 feet Y = 3995380
50 meter
Z = -17302043
79 Z = -5265843
31
XDOT = -21230
561491 XDOT = -6519
675331
YDOT = 12978
947248 feet/sec YDOT = 3883
347760 meter/sec
ZDOT = 3271
783527 ZDOT = 965
684506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4493901
93 X = -1369741
31
Y = -13394870
84 feet Y = -4082756
63 meter
Z = -17269708
84 Z = -5263807
25
XDOT = 21129
433009 XDOT = 6440
251181
YDOT = -11133
496460 feet/sec YDOT = -3393
489721 meter/sec
ZDOT = 3138
655658 ZDOT = 956
662244
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 13306
38952121
00016717 00000-0 10270-3 0 9089
2 25544 51
6486 143
6109 0001091 99
1165 261
0109 15
49747065 16147
Satellite: ISS
Catalog Number: 25544
Epoch time: 13306
38952121 = yrday
fracday
Element set: 908
Inclination: 51
6486 deg
RA of node: 143
6109 deg
Eccentricity:
0001091
Arg of perigee: 99
1165 deg
Mean anomaly: 261
0109 deg
Mean motion: 15
49747065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1614
Checksum: 300
Coasting Arc #10 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2013/307/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1685559
72 A = 6790520
57 meter
Y = -4003141
24 meter E =
0004863
Z = 5216277
65 I = 51
86622
XDOT = 6216
751200 Wp = 64
36232
YDOT = -4295
017701 meter/sec RA = 137
69215 deg
ZDOT = -1284
306916 TA = 37
95496
MA = 37
92069
Ha = 228
251 n
mi
Hp = 221
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5530051
58 X = -1666010
49
Y = -13133665
50 feet Y = -4021880
76 meter
Z = 17113771
82 Z = 5208136
73
XDOT = 20396
165354 XDOT = 6270
555995
YDOT = -14091
265424 feet/sec YDOT = -4225
197238 meter/sec
ZDOT = -4213
605367 ZDOT = -1253
974723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4935554
65 X = 1504357
06
Y = 13411430
59 feet Y = 4087804
04 meter
Z = 17080095
31 Z = 5206013
05
XDOT = -20159
138573 XDOT = -6144
505437
YDOT = 12634
415646 feet/sec YDOT = 3850
969889 meter/sec
ZDOT = -4085
552095 ZDOT = -1245
276279
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 13307
42126667
00016717 00000-0 10270-3 0 9094
2 25544 51
6484 138
5015 0000983 101
4417 258
6844 15
49789522 16300
Satellite: ISS
Catalog Number: 25544
Epoch time: 13307
42126667 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 138
5015 deg
Eccentricity:
0000983
Arg of perigee: 101
4417 deg
Mean anomaly: 258
6844 deg
Mean motion: 15
49789522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 318
Coasting Arc #11 (Orbit 1644)
---------------------------------------
Vector Time (GMT): 2013/308/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1773205
84 A = 6790781
10 meter
Y = 4051588
11 meter E =
0014565
Z = -5166168
79 I = 51
88869
XDOT = -5917
304769 Wp = 101
90482
YDOT = 4588
355224 meter/sec RA = 132
75372 deg
ZDOT = 1568
232119 TA = 183
19216
MA = 183
20146
Ha = 228
163 n
mi
Hp = 221
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5817604
45 X = 1752864
90
Y = 13292611
92 feet Y = 4071303
45 meter
Z = -16949372
66 Z = -5157603
90
XDOT = -19413
729558 XDOT = -5975
791254
YDOT = 15053
658871 feet/sec YDOT = 4521
857156 meter/sec
ZDOT = 5145
118501 ZDOT = 1539
343406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5446210
87 X = -1660005
07
Y = -13493597
63 feet Y = -4112848
56 meter
Z = -16913926
13 Z = -5155364
68
XDOT = 18984
744122 XDOT = 5786
550008
YDOT = -13955
453645 feet/sec YDOT = -4253
622271 meter/sec
ZDOT = 5023
070381 ZDOT = 1531
031852
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 13308
38851445
00016717 00000-0 10270-3 0 9101
2 25544 51
6479 133
7107 0000940 101
3848 258
7408 15
49794365 16457
Satellite: ISS
Catalog Number: 25544
Epoch time: 13308
38851445 = yrday
fracday
Element set: 910
Inclination: 51
6479 deg
RA of node: 133
7107 deg
Eccentricity:
0000940
Arg of perigee: 101
3848 deg
Mean anomaly: 258
7408 deg
Mean motion: 15
49794365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1645
Checksum: 322
Coasting Arc #12 (Orbit 1660)
---------------------------------------
Vector Time (GMT): 2013/309/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1854458
67 A = 6790990
14 meter
Y = -4103752
28 meter E =
0006092
Z = 5079264
35 I = 51
91035
XDOT = 5625
088556 Wp = 61
75050
YDOT = -4859
451044 meter/sec RA = 127
81746 deg
ZDOT = -1867
904181 TA = 46
31278
MA = 46
26232
Ha = 228
135 n
mi
Hp = 221
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6084181
99 X = -1833106
14
Y = -13463754
19 feet Y = -4124370
68 meter
Z = 16664253
11 Z = 5070307
13
XDOT = 18455
014949 XDOT = 5688
083957
YDOT = -15943
080853 feet/sec YDOT = -4796
195480 meter/sec
ZDOT = -6128
294557 ZDOT = -1840
424289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5939126
12 X = 1810245
64
Y = 13573919
95 feet Y = 4137330
80 meter
Z = 16627169
25 Z = 5067961
19
XDOT = -17792
986571 XDOT = -5423
302307
YDOT = 15167
742679 feet/sec YDOT = 4623
127968 meter/sec
ZDOT = -6012
107743 ZDOT = -1832
490440
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 13309
42022791
00016717 00000-0 10270-3 0 9112
2 25544 51
6482 128
6012 0000847 103
3510 256
7735 15
49834162 16612
Satellite: ISS
Catalog Number: 25544
Epoch time: 13309
42022791 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 128
6012 deg
Eccentricity:
0000847
Arg of perigee: 103
3510 deg
Mean anomaly: 256
7735 deg
Mean motion: 15
49834162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1661
Checksum: 288
Coasting Arc #13 (Orbit 1675)
---------------------------------------
Vector Time (GMT): 2013/310/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1965256
75 A = 6791364
94 meter
Y = 4171357
12 meter E =
0013321
Z = -4998263
01 I = 51
92904
XDOT = -5297
636717 Wp = 105
79177
YDOT = 5080
656328 meter/sec RA = 122
88134 deg
ZDOT = 2158
410957 TA = 185
20025
MA = 185
21410
Ha = 228
047 n
mi
Hp = 221
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6447692
75 X = 1942746
42
Y = 13685554
87 feet Y = 4193208
11 meter
Z = -16398500
69 Z = -4988770
34
XDOT = -17380
697891 XDOT = -5364
541218
YDOT = 16668
819973 feet/sec YDOT = 5021
040655 meter/sec
ZDOT = 7081
400777 ZDOT = 2132
512514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6533331
29 X = -1991359
38
Y = -13691998
84 feet Y = -4173321
25 meter
Z = -16359178
72 Z = -4986277
68
XDOT = 16445
738896 XDOT = 5012
661216
YDOT = -16172
278381 feet/sec YDOT = -4929
310450 meter/sec
ZDOT = 6971
808509 ZDOT = 2125
007234
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 13310
38744549
00016717 00000-0 10270-3 0 9122
2 25544 51
6475 123
8099 0000824 104
1996 255
9246 15
49840282 16762
Satellite: ISS
Catalog Number: 25544
Epoch time: 13310
38744549 = yrday
fracday
Element set: 912
Inclination: 51
6475 deg
RA of node: 123
8099 deg
Eccentricity:
0000824
Arg of perigee: 104
1996 deg
Mean anomaly: 255
9246 deg
Mean motion: 15
49840282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1676
Checksum: 328
Coasting Arc #14 (Orbit 1691)
---------------------------------------
Vector Time (GMT): 2013/311/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2071168
60 A = 6791718
25 meter
Y = -4242868
06 meter E =
0007499
Z = 4877660
95 I = 51
94710
XDOT = 4983
818686 Wp = 63
83190
YDOT = -5274
984807 meter/sec RA = 117
94767 deg
ZDOT = -2466
084428 TA = 50
31829
MA = 50
25218
Ha = 228
021 n
mi
Hp = 221
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6795172
56 X = -2047264
76
Y = -13920170
79 feet Y = -4265895
63 meter
Z = 16002824
65 Z = 4867657
19
XDOT = 16351
111176 XDOT = 5054
414109
YDOT = -17306
380602 feet/sec YDOT = -5218
857802 meter/sec
ZDOT = -8090
828177 ZDOT = -2441
701679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7116617
88 X = 2169145
13
Y = 13806681
77 feet Y = 4208276
60 meter
Z = 15961366
17 Z = 4865024
41
XDOT = -15115
050475 XDOT = -4607
067385
YDOT = 17048
517775 feet/sec YDOT = 5196
388218 meter/sec
ZDOT = -7987
560253 ZDOT = -2434
608365
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 13311
41912668
00016717 00000-0 10270-3 0 9137
2 25544 51
6480 118
7005 0000716 106
1339 253
9891 15
49876830 16921
Satellite: ISS
Catalog Number: 25544
Epoch time: 13311
41912668 = yrday
fracday
Element set: 913
Inclination: 51
6480 deg
RA of node: 118
7005 deg
Eccentricity:
0000716
Arg of perigee: 106
1339 deg
Mean anomaly: 253
9891 deg
Mean motion: 15
49876830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1692
Checksum: 312
Coasting Arc #15 (Orbit 1706)
---------------------------------------
Vector Time (GMT): 2013/312/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2212806
45 A = 6792202
45 meter
Y = 4320500
40 meter E =
0011742
Z = -4762151
24 I = 51
96125
XDOT = -4646
040907 Wp = 109
07643
YDOT = 5417
941471 meter/sec RA = 113
01356 deg
ZDOT = 2758
439275 TA = 188
15424
MA = 188
17334
Ha = 227
950 n
mi
Hp = 221
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7259863
68 X = 2187462
77
Y = 14174870
09 feet Y = 4345103
77 meter
Z = -15623855
77 Z = -4751462
97
XDOT = -15242
916363 XDOT = -4719
680162
YDOT = 17775
398527 feet/sec YDOT = 5365
574709 meter/sec
ZDOT = 9049
997622 ZDOT = 2735
690104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7823594
35 X = -2384631
56
Y = -13921458
20 feet Y = -4243260
46 meter
Z = -15579531
60 Z = -4748641
23
XDOT = 13684
937302 XDOT = 4171
168890
YDOT = -17703
913351 feet/sec YDOT = -5396
152789 meter/sec
ZDOT = 8953
560523 ZDOT = 2729
045247
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 13312
38631378
00016717 00000-0 10270-3 0 9141
2 25544 51
6469 113
9090 0000761 108
1971 251
9263 15
49885490 17073
Satellite: ISS
Catalog Number: 25544
Epoch time: 13312
38631378 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 113
9090 deg
Eccentricity:
0000761
Arg of perigee: 108
1971 deg
Mean anomaly: 251
9263 deg
Mean motion: 15
49885490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1707
Checksum: 318
Coasting Arc #16 (Orbit 1722)
---------------------------------------
Vector Time (GMT): 2013/313/09:00:02
000
Vector Time (MET): N/A
Weight (LBS) : 893840
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2350271
87 A = 6792699
57 meter
Y = -4401102
09 meter E =
0008996
Z = 4603863
96 I = 51
97484
XDOT = 4329
784538 Wp = 69
09999
YDOT = -5530
303514 meter/sec RA = 108
08176 deg
ZDOT = -3068
434339 TA = 51
48493
MA = 51
40430
Ha = 227
923 n
mi
Hp = 221
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7710865
72 X = -2323247
69
Y = -14439311
33 feet Y = -4427233
22 meter
Z = 15104540
55 Z = 4592512
06
XDOT = 14205
329849 XDOT = 4406
209614
YDOT = -18144
040399 feet/sec YDOT = -5481
457797 meter/sec
ZDOT = -10067
041794 ZDOT = -3047
214736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8522432
80 X = 2597637
52
Y = 14026403
18 feet Y = 4275247
69 meter
Z = 15057438
69 Z = 4589507
31
XDOT = -12312
256814 XDOT = -3752
775877
YDOT = 18219
393286 feet/sec YDOT = 5553
271074 meter/sec
ZDOT = -9977
006149 ZDOT = -3040
991474
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 13313
41796209
00016717 00000-0 10270-3 0 9152
2 25544 51
6473 108
7995 0000629 110
6772 249
4446 15
49918076 17234
Satellite: ISS
Catalog Number: 25544
Epoch time: 13313
41796209 = yrday
fracday
Element set: 915
Inclination: 51
6473 deg
RA of node: 108
7995 deg
Eccentricity:
0000629
Arg of perigee: 110
6772 deg
Mean anomaly: 249
4446 deg
Mean motion: 15
49918076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1723
Checksum: 330
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