[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 7th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24218 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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 3121)
---------------------------------------
Vector Time (GMT): 2014/038/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1938645
56 A = 6792108
70 meter
Y = 4636920
38 meter E =
0012283
Z = 4561264
02 I = 51
77423
XDOT = -7004
088986 Wp = 111
83437
YDOT = -145
439965 meter/sec RA = 21
68080 deg
ZDOT = 3113
571461 TA = 306
97897
MA = 307
09135
Ha = 228
549 n
mi
Hp = 219
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6360385
69 X = 1864493
52
Y = 15212993
36 feet Y = 4658185
05 meter
Z = 14964776
98 Z = 4570501
35
XDOT = -22979
294573 XDOT = -7017
066622
YDOT = -477
165238 feet/sec YDOT = -223
836655 meter/sec
ZDOT = 10215
129465 ZDOT = 3079
515501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -776340
98 X = -236628
73
Y = 16436013
66 feet Y = 5009696
96 meter
Z = 15002965
47 Z = 4572903
88
XDOT = -19467
709325 XDOT = -5933
757802
YDOT = -10146
228130 feet/sec YDOT = -3092
570334 meter/sec
ZDOT = 10071
396229 ZDOT = 3069
761571
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 14038
60428872
00016717 00000-0 10270-3 0 9000
2 25544 51
6478 21
9511 0003678 109
5628 250
5920 15
50140778 31226
Satellite: ISS
Catalog Number: 25544
Epoch time: 14038
60428872 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 21
9511 deg
Eccentricity:
0003678
Arg of perigee: 109
5628 deg
Mean anomaly: 250
5920 deg
Mean motion: 15
50140778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3122
Checksum: 300
Coasting Arc #2 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2014/039/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1866096
95 A = 6791377
21 meter
Y = -4482044
80 meter E =
0014244
Z = -4762053
80 I = 51
74283
XDOT = 7149
929880 Wp = 80
57636
YDOT = -90
988703 meter/sec RA = 16
73155 deg
ZDOT = -2720
872377 TA = 162
51805
MA = 162
46896
Ha = 228
614 n
mi
Hp = 219
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6122365
33 X = -1792706
85
Y = -14704871
39 feet Y = -4502502
42 meter
Z = -15623536
09 Z = -4770940
57
XDOT = 23457
775196 XDOT = 7163
632864
YDOT = -298
519366 feet/sec YDOT = -10
957044 meter/sec
ZDOT = -8926
746643 ZDOT = -2686
106263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 507021
79 X = 154540
24
Y = -15884282
04 feet Y = -4841529
17 meter
Z = -15660267
96 Z = -4773249
68
XDOT = 20426
548194 XDOT = 6226
011890
YDOT = 9293
057024 feet/sec YDOT = 2832
523781 meter/sec
ZDOT = -8779
977568 ZDOT = -2676
137163
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 14039
57131462
00016717 00000-0 10270-3 0 9014
2 25544 51
6481 17
1589 0003772 110
9785 249
1770 15
50134685 31370
Satellite: ISS
Catalog Number: 25544
Epoch time: 14039
57131462 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 17
1589 deg
Eccentricity:
0003772
Arg of perigee: 110
9785 deg
Mean anomaly: 249
1770 deg
Mean motion: 15
50134685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 308
Coasting Arc #3 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2014/040/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1785675
93 A = 6790541
38 meter
Y = 4331534
57 meter E =
0010242
Z = 4909440
80 I = 51
71122
XDOT = -7295
081259 Wp = 119
31402
YDOT = 357
159509 meter/sec RA = 11
78155 deg
ZDOT = 2329
707436 TA = 307
86135
MA = 307
95397
Ha = 228
401 n
mi
Hp = 219
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5858516
82 X = 1713258
96
Y = 14211071
42 feet Y = 4351098
31 meter
Z = 16107089
23 Z = 4917939
24
XDOT = -23933
993631 XDOT = -7309
849680
YDOT = 1171
783166 feet/sec YDOT = 275
498710 meter/sec
ZDOT = 7643
397101 ZDOT = 2294
233715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -285274
16 X = -86951
56
Y = 15331760
98 feet Y = 4673120
75 meter
Z = 16142206
09 Z = 4920144
42
XDOT = -21397
575135 XDOT = -6521
980901
YDOT = -8317
367970 feet/sec YDOT = -2535
133757 meter/sec
ZDOT = 7493
597277 ZDOT = 2284
048450
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 14040
60278749
00016717 00000-0 10270-3 0 9021
2 25544 51
6485 12
0489 0003643 116
5529 243
5996 15
50199103 31534
Satellite: ISS
Catalog Number: 25544
Epoch time: 14040
60278749 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 12
0489 deg
Eccentricity:
0003643
Arg of perigee: 116
5529 deg
Mean anomaly: 243
5996 deg
Mean motion: 15
50199103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 309
Coasting Arc #4 (Orbit 3167)
---------------------------------------
Vector Time (GMT): 2014/041/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1651394
59 A = 6789965
51 meter
Y = -4228399
97 meter E =
0016026
Z = -5063720
08 I = 51
67885
XDOT = 7385
906148 Wp = 84
61019
YDOT = -622
368377 meter/sec RA = 6
82682 deg
ZDOT = -1892
712767 TA = 167
02783
MA = 166
98655
Ha = 228
458 n
mi
Hp = 219
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5417961
24 X = -1579391
52
Y = -13872703
31 feet Y = -4246464
44 meter
Z = -16613254
87 Z = -5071567
18
XDOT = 24231
975550 XDOT = 7401
510677
YDOT = -2041
891002 feet/sec YDOT = -539
687243 meter/sec
ZDOT = -6209
687555 ZDOT = -1856
795898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 305045
60 X = 92977
90
Y = -14853823
09 feet Y = -4527445
28 meter
Z = -16645639
82 Z = -5073591
02
XDOT = 22168
036210 XDOT = 6756
817437
YDOT = 7230
417657 feet/sec YDOT = 2203
831302 meter/sec
ZDOT = -6057
973717 ZDOT = -1846
470389
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 14041
56977808
00016717 00000-0 10270-3 0 9030
2 25544 51
6487 7
2564 0003703 118
1337 242
0188 15
50193294 31686
Satellite: ISS
Catalog Number: 25544
Epoch time: 14041
56977808 = yrday
fracday
Element set: 903
Inclination: 51
6487 deg
RA of node: 7
2564 deg
Eccentricity:
0003703
Arg of perigee: 118
1337 deg
Mean anomaly: 242
0188 deg
Mean motion: 15
50193294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3168
Checksum: 310
Coasting Arc #5 (Orbit 3183)
---------------------------------------
Vector Time (GMT): 2014/042/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1511678
03 A = 6789297
03 meter
Y = 4136332
62 meter E =
0008098
Z = 5162370
96 I = 51
64694
XDOT = -7472
202044 Wp = 123
87298
YDOT = 907
598008 meter/sec RA = 1
87131 deg
ZDOT = 1454
794569 TA = 312
08912
MA = 312
15796
Ha = 228
247 n
mi
Hp = 219
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4959573
57 X = 1440235
71
Y = 13570645
08 feet Y = 4152837
88 meter
Z = 16936912
59 Z = 5169540
65
XDOT = -24515
098571 XDOT = -7488
862425
YDOT = 2977
683754 feet/sec YDOT = 823
945959 meter/sec
ZDOT = 4772
948062 ZDOT = 1418
455998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -369921
34 X = -112752
03
Y = 14409071
65 feet Y = 4391885
04 meter
Z = 16966455
09 Z = 5171375
51
XDOT = -22915
041061 XDOT = -6984
504515
YDOT = -6050
916307 feet/sec YDOT = -1844
319291 meter/sec
ZDOT = 4619
408232 ZDOT = 1407
995629
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 14042
60121303
00016717 00000-0 10270-3 0 9048
2 25544 51
6492 2
1460 0003609 123
7773 236
3721 15
50257043 31842
Satellite: ISS
Catalog Number: 25544
Epoch time: 14042
60121303 = yrday
fracday
Element set: 904
Inclination: 51
6492 deg
RA of node: 2
1460 deg
Eccentricity:
0003609
Arg of perigee: 123
7773 deg
Mean anomaly: 236
3721 deg
Mean motion: 15
50257043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3184
Checksum: 264
Coasting Arc #6 (Orbit 3198)
---------------------------------------
Vector Time (GMT): 2014/043/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1332788
51 A = 6788954
46 meter
Y = -4100243
12 meter E =
0017278
Z = -5259139
62 I = 51
61501
XDOT = 7493
666028 Wp = 90
61586
YDOT = -1182
135131 meter/sec RA = 356
91126 deg
ZDOT = -980
403435 TA = 169
99078
MA = 169
95633
Ha = 228
303 n
mi
Hp = 219
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4372665
71 X = -1261293
03
Y = -13452241
20 feet Y = -4114747
70 meter
Z = -17254395
09 Z = -5265440
12
XDOT = 24585
518466 XDOT = 7511
090355
YDOT = -3878
396100 feet/sec YDOT = -1098
238784 meter/sec
ZDOT = -3216
546702 ZDOT = -943
958772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 634001
99 X = 193243
81
Y = -14099192
06 feet Y = -4297433
74 meter
Z = -17280277
00 Z = -5267028
43
XDOT = 23406
038297 XDOT = 7134
160473
YDOT = 4794
045994 feet/sec YDOT = 1461
225219 meter/sec
ZDOT = -3062
516538 ZDOT = -933
455041
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 14043
56816786
00016717 00000-0 10270-3 0 9051
2 25544 51
6495 357
3534 0003671 125
4501 234
6992 15
50252265 31997
Satellite: ISS
Catalog Number: 25544
Epoch time: 14043
56816786 = yrday
fracday
Element set: 905
Inclination: 51
6495 deg
RA of node: 357
3534 deg
Eccentricity:
0003671
Arg of perigee: 125
4501 deg
Mean anomaly: 234
6992 deg
Mean motion: 15
50252265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3199
Checksum: 322
Coasting Arc #7 (Orbit 3214)
---------------------------------------
Vector Time (GMT): 2014/044/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1152936
35 A = 6788537
75 meter
Y = 4079925
62 meter E =
0006178
Z = 5297471
52 I = 51
58374
XDOT = -7508
524393 Wp = 121
32246
YDOT = 1464
490056 meter/sec RA = 351
95045 deg
ZDOT = 502
672702 TA = 323
85635
MA = 323
89809
Ha = 228
089 n
mi
Hp = 219
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3782599
57 X = 1081495
24
Y = 13385582
76 feet Y = 4092419
38 meter
Z = 17380155
92 Z = 5302898
41
XDOT = -24634
266382 XDOT = -7526
784364
YDOT = 4804
757402 feet/sec YDOT = 1380
422866 meter/sec
ZDOT = 1649
188654 ZDOT = 466
153812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -927544
62 X = -282715
60
Y = 13850969
05 feet Y = 4221775
36 meter
Z = 17402356
81 Z = 5304238
36
XDOT = -23844
836153 XDOT = -7267
906060
YDOT = -3489
588488 feet/sec YDOT = -1063
626571 meter/sec
ZDOT = 1494
803330 ZDOT = 455
616055
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 14044
59956444
00016717 00000-0 10270-3 0 9062
2 25544 51
6498 352
2428 0003581 131
0422 229
1039 15
50314656 32154
Satellite: ISS
Catalog Number: 25544
Epoch time: 14044
59956444 = yrday
fracday
Element set: 906
Inclination: 51
6498 deg
RA of node: 352
2428 deg
Eccentricity:
0003581
Arg of perigee: 131
0422 deg
Mean anomaly: 229
1039 deg
Mean motion: 15
50314656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3215
Checksum: 300
Coasting Arc #8 (Orbit 3229)
---------------------------------------
Vector Time (GMT): 2014/045/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -951675
49 A = 6788494
38 meter
Y = -4119890
14 meter E =
0017716
Z = -5326006
02 I = 51
55353
XDOT = 7452
616057 Wp = 97
90880
YDOT = -1723
341602 meter/sec RA = 346
98558 deg
ZDOT = -
974243 TA = 172
09586
MA = 172
06791
Ha = 228
139 n
mi
Hp = 219
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3122294
92 X = -879663
82
Y = -13516699
93 feet Y = -4130130
17 meter
Z = -17473773
03 Z = -5330453
78
XDOT = 24450
840081 XDOT = 7471
337689
YDOT = -5654
007879 feet/sec YDOT = -1639
897001 meter/sec
ZDOT = -3
196334 ZDOT = 35
274253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1357935
06 X = 413898
61
Y = -13783115
21 feet Y = -4201093
52 meter
Z = -17491837
93 Z = -5331512
20
XDOT = 23988
361842 XDOT = 7311
652689
YDOT = 2162
991131 feet/sec YDOT = 659
279697 meter/sec
ZDOT = 150
083453 ZDOT = 45
745437
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 14045
56648312
00016717 00000-0 10270-3 0 9073
2 25544 51
6504 347
4503 0003653 132
8324 227
3135 15
50311623 32307
Satellite: ISS
Catalog Number: 25544
Epoch time: 14045
56648312 = yrday
fracday
Element set: 907
Inclination: 51
6504 deg
RA of node: 347
4503 deg
Eccentricity:
0003653
Arg of perigee: 132
8324 deg
Mean anomaly: 227
3135 deg
Mean motion: 15
50311623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3230
Checksum: 274
Coasting Arc #9 (Orbit 3245)
---------------------------------------
Vector Time (GMT): 2014/046/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 755329
21 A = 6788398
66 meter
Y = 4177382
28 meter E =
0005211
Z = 5292858
85 I = 51
52385
XDOT = -7390
403997 Wp = 106
86652
YDOT = 1975
822018 meter/sec RA = 342
01980 deg
ZDOT = -505
818532 TA = 347
96160
MA = 347
97405
Ha = 227
921 n
mi
Hp = 219
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2478114
22 X = 682850
21
Y = 13705322
44 feet Y = 4185424
11 meter
Z = 17365022
48 Z = 5296351
61
XDOT = -24246
732275 XDOT = -7409
491764
YDOT = 6482
355703 feet/sec YDOT = 1893
071016 meter/sec
ZDOT = -1659
509619 ZDOT = -541
765829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1791131
24 X = -545936
80
Y = 13794250
96 feet Y = 4204487
69 meter
Z = 17379050
85 Z = 5297134
70
XDOT = -24062
860247 XDOT = -7334
359803
YDOT = -846
550029 feet/sec YDOT = -258
028449 meter/sec
ZDOT = -1811
550941 ZDOT = -552
160727
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 14046
59784113
00016717 00000-0 10270-3 0 9088
2 25544 51
6503 342
3395 0003550 138
2874 221
8548 15
50372721 32465
Satellite: ISS
Catalog Number: 25544
Epoch time: 14046
59784113 = yrday
fracday
Element set: 908
Inclination: 51
6503 deg
RA of node: 342
3395 deg
Eccentricity:
0003550
Arg of perigee: 138
2874 deg
Mean anomaly: 221
8548 deg
Mean motion: 15
50372721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3246
Checksum: 307
Coasting Arc #10 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2014/047/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -556947
58 A = 6788696
84 meter
Y = -4294100
73 meter E =
0017101
Z = -5243450
64 I = 51
49627
XDOT = 7257
652160 Wp = 105
95237
YDOT = -2190
723489 meter/sec RA = 337
05069 deg
ZDOT = 1021
380499 TA = 173
88192
MA = 173
86101
Ha = 227
951 n
mi
Hp = 219
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1827255
84 X = -483418
08
Y = -14088257
00 feet Y = -4299918
32 meter
Z = -17202922
03 Z = -5245977
09
XDOT = 23811
194750 XDOT = 7276
648475
YDOT = -7187
413022 feet/sec YDOT = -2109
457451 meter/sec
ZDOT = 3350
985889 ZDOT = 1056
682848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2284516
01 X = 696320
48
Y = -14009173
06 feet Y = -4269995
95 meter
Z = -17212856
61 Z = -5246478
69
XDOT = 23828
854016 XDOT = 7263
034704
YDOT = -422
260227 feet/sec YDOT = -128
704917 meter/sec
ZDOT = 3500
330489 ZDOT = 1066
900733
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 14047
56472333
00016717 00000-0 10270-3 0 9095
2 25544 51
6510 337
5471 0003612 140
5318 219
6096 15
50371270 32610
Satellite: ISS
Catalog Number: 25544
Epoch time: 14047
56472333 = yrday
fracday
Element set: 909
Inclination: 51
6510 deg
RA of node: 337
5471 deg
Eccentricity:
0003612
Arg of perigee: 140
5318 deg
Mean anomaly: 219
6096 deg
Mean motion: 15
50371270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 289
Coasting Arc #11 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2014/048/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 369743
42 A = 6788959
90 meter
Y = 4426390
13 meter E =
0005989
Z = 5129029
08 I = 51
46926
XDOT = -7121
748277 Wp = 90
25879
YDOT = 2383
885606 meter/sec RA = 332
08040 deg
ZDOT = -1542
380092 TA = 14
65185
MA = 14
63450
Ha = 227
734 n
mi
Hp = 219
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1213068
96 X = 295304
27
Y = 14522277
32 feet Y = 4430109
21 meter
Z = 16827523
24 Z = 5130643
91
XDOT = -23365
315870 XDOT = -7140
383848
YDOT = 7821
147000 feet/sec YDOT = 2304
141282 meter/sec
ZDOT = -5060
302140 ZDOT = -1577
021530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2747571
75 X = -837459
87
Y = 14304357
03 feet Y = 4359968
02 meter
Z = 16833592
39 Z = 5130878
96
XDOT = -23525
240794 XDOT = -7170
493394
YDOT = 1614
750095 feet/sec YDOT = 492
175829 meter/sec
ZDOT = -5206
878750 ZDOT = -1587
056643
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 14048
59604273
00016717 00000-0 10270-3 0 9101
2 25544 51
6507 332
4358 0003498 145
6857 214
4520 15
50431662 32774
Satellite: ISS
Catalog Number: 25544
Epoch time: 14048
59604273 = yrday
fracday
Element set: 910
Inclination: 51
6507 deg
RA of node: 332
4358 deg
Eccentricity:
0003498
Arg of perigee: 145
6857 deg
Mean anomaly: 214
4520 deg
Mean motion: 15
50431662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 309
Coasting Arc #12 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2014/049/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -199613
89 A = 6789603
81 meter
Y = -4610944
31 meter E =
0015317
Z = -4993899
25 I = 51
44490
XDOT = 6922
558040 Wp = 114
19144
YDOT = -2526
581574 meter/sec RA = 327
10758 deg
ZDOT = 2054
985121 TA = 175
90446
MA = 175
89191
Ha = 227
731 n
mi
Hp = 219
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -654901
20 X = -123779
97
Y = -15127770
05 feet Y = -4612753
08 meter
Z = -16384183
89 Z = -4994684
22
XDOT = 22711
804593 XDOT = 6940
314006
YDOT = -8289
309625 feet/sec YDOT = -2449
069585 meter/sec
ZDOT = 6742
077167 ZDOT = 2088
656931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3188439
42 X = 971836
34
Y = -14799626
03 feet Y = -4510926
01 meter
Z = -16386724
13 Z = -4994673
52
XDOT = 22932
781137 XDOT = 6989
911691
YDOT = -2686
365454 feet/sec YDOT = -818
804190 meter/sec
ZDOT = 6884
575401 ZDOT = 2098
418582
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 14049
56288831
00016717 00000-0 10270-3 0 9118
2 25544 51
6511 327
6432 0003530 148
8951 211
2409 15
50430771 32923
Satellite: ISS
Catalog Number: 25544
Epoch time: 14049
56288831 = yrday
fracday
Element set: 911
Inclination: 51
6511 deg
RA of node: 327
6432 deg
Eccentricity:
0003530
Arg of perigee: 148
8951 deg
Mean anomaly: 211
2409 deg
Mean motion: 15
50430771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3292
Checksum: 295
Coasting Arc #13 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2014/050/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 45973
04 A = 6790216
80 meter
Y = 4805005
01 meter E =
0008074
Z = 4790828
09 I = 51
42168
XDOT = -6726
492523 Wp = 85
97573
YDOT = 2632
191096 meter/sec RA = 322
13355 deg
ZDOT = -2571
124972 TA = 29
44872
MA = 29
40326
Ha = 227
521 n
mi
Hp = 219
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 150830
19 X = -31033
11
Y = 15764452
13 feet Y = 4805089
05 meter
Z = 15717939
94 Z = 4790863
87
XDOT = -22068
545023 XDOT = -6742
936761
YDOT = 8635
797560 feet/sec YDOT = 2556
878933 meter/sec
ZDOT = -8435
449382 ZDOT = -2603
841241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3566021
78 X = -1086923
44
Y = 15357233
31 feet Y = 4680884
71 meter
Z = 15717290
17 Z = 4790630
04
XDOT = -22289
432009 XDOT = -6793
818876
YDOT = 3613
696585 feet/sec YDOT = 1101
454719 meter/sec
ZDOT = -8573
924168 ZDOT = -2613
332086
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 14050
59416922
00016717 00000-0 10270-3 0 9128
2 25544 51
6508 322
5313 0003416 153
4864 206
6462 15
50490740 33086
Satellite: ISS
Catalog Number: 25544
Epoch time: 14050
59416922 = yrday
fracday
Element set: 912
Inclination: 51
6508 deg
RA of node: 322
5313 deg
Eccentricity:
0003416
Arg of perigee: 153
4864 deg
Mean anomaly: 206
6462 deg
Mean motion: 15
50490740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 288
Coasting Arc #14 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2014/051/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73904
82 A = 6791159
34 meter
Y = -5038652
26 meter E =
0012433
Z = -4565206
02 I = 51
40101
XDOT = 6481
235129 Wp = 121
65336
YDOT = -2678
324492 meter/sec RA = 317
15765 deg
ZDOT = 3060
795325 TA = 179
13391
MA = 179
13175
Ha = 227
482 n
mi
Hp = 219
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 242469
87 X = 152418
81
Y = -16531011
36 feet Y = -5037387
24 meter
Z = -14977710
04 Z = -4564655
83
XDOT = 21263
894779 XDOT = 6495
834800
YDOT = -8787
153844 feet/sec YDOT = -2605
765252 meter/sec
ZDOT = 10041
979414 ZDOT = 3092
315734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3844109
19 X = 1171684
48
Y = -16082615
69 feet Y = -4901981
26 meter
Z = -14974552
52 Z = -4564243
61
XDOT = 21411
501890 XDOT = 6526
225776
YDOT = -4357
163486 feet/sec YDOT = -1328
063430 meter/sec
ZDOT = 10175
409181 ZDOT = 3101
464718
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 14051
56097838
00016717 00000-0 10270-3 0 9138
2 25544 51
6509 317
7382 0003423 158
0121 202
1178 15
50489019 33233
Satellite: ISS
Catalog Number: 25544
Epoch time: 14051
56097838 = yrday
fracday
Element set: 913
Inclination: 51
6509 deg
RA of node: 317
7382 deg
Eccentricity:
0003423
Arg of perigee: 158
0121 deg
Mean anomaly: 202
1178 deg
Mean motion: 15
50489019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 295
Coasting Arc #15 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2014/052/13:12:36
088
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -174430
82 A = 6792053
20 meter
Y = 5271763
69 meter E =
0010557
Z = 4269697
79 I = 51
38242
XDOT = -6248
470853 Wp = 91
32379
YDOT = 2673
687962 meter/sec RA = 312
18102 deg
ZDOT = -3549
072123 TA = 35
04053
MA = 34
97112
Ha = 227
283 n
mi
Hp = 219
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -572279
60 X = -254108
58
Y = 17295812
62 feet Y = 5269367
93 meter
Z = 14008194
86 Z = 4268656
49
XDOT = -20500
232457 XDOT = -6260
664098
YDOT = 8771
942132 feet/sec YDOT = 2603
745102 meter/sec
ZDOT = -11643
937410 ZDOT = -3579
455928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4034123
63 X = -1229600
88
Y = 16832882
97 feet Y = 5130662
73 meter
Z = 14002930
36 Z = 4268093
18
XDOT = -20521
633850 XDOT = -6254
993998
YDOT = 4895
347133 feet/sec YDOT = 1492
101806 meter/sec
ZDOT = -11772
566251 ZDOT = -3588
278193
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 14052
59222113
00016717 00000-0 10270-3 0 9149
2 25544 51
6508 312
6258 0003314 161
8658 198
2612 15
50548395 33392
Satellite: ISS
Catalog Number: 25544
Epoch time: 14052
59222113 = yrday
fracday
Element set: 914
Inclination: 51
6508 deg
RA of node: 312
6258 deg
Eccentricity:
0003314
Arg of perigee: 161
8658 deg
Mean anomaly: 198
2612 deg
Mean motion: 15
50548395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3339
Checksum: 305
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