[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 22nd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29062 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 3337)
---------------------------------------
Vector Time (GMT): 2014/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5497390
25 A = 6797305
38 meter
Y = 3231659
71 meter E =
0008945
Z = -2344715
98 I = 51
40068
XDOT = -882
715268 Wp = 145
70083
YDOT = -5388
201715 meter/sec RA = 312
48221 deg
ZDOT = -5374
087838 TA = 60
50333
MA = 60
41415
Ha = 227
235 n
mi
Hp = 219
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18036057
25 X = -5521729
02
Y = 10602558
12 feet Y = 3170048
10 meter
Z = -7692637
75 Z = -2371480
72
XDOT = -2896
047468 XDOT = -796
292170
YDOT = -17677
827149 feet/sec YDOT = -5397
590014 meter/sec
ZDOT = -17631
521778 ZDOT = -5378
165568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20876215
98 X = -6363070
63
Y = 372602
65 feet Y = 113569
29 meter
Z = -7806090
51 Z = -2379296
39
XDOT = 6306
078265 XDOT = 1922
092655
YDOT = -15237
529485 feet/sec YDOT = -4644
398987 meter/sec
ZDOT = -17647
834560 ZDOT = -5379
059974
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
52751931
00016717 00000-0 10270-3 0 9002
2 25544 51
6502 312
9526 0003643 165
3183 194
8074 15
50568024 33388
Satellite: ISS
Catalog Number: 25544
Epoch time: 14052
52751931 = yrday
fracday
Element set: 900
Inclination: 51
6502 deg
RA of node: 312
9526 deg
Eccentricity:
0003643
Arg of perigee: 165
3183 deg
Mean anomaly: 194
8074 deg
Mean motion: 15
50568024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3338
Checksum: 294
Coasting Arc #2 (Orbit 3353)
---------------------------------------
Vector Time (GMT): 2014/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5287575
14 A = 6796186
15 meter
Y = -3212523
27 meter E =
0014004
Z = 2801791
25 I = 51
37692
XDOT = 751
319140 Wp = 94
62283
YDOT = 5687
715569 meter/sec RA = 307
50761 deg
ZDOT = 5080
501013 TA = 297
24884
MA = 297
39144
Ha = 227
132 n
mi
Hp = 219
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17347687
45 X = 5309495
22
Y = -10539774
52 feet Y = -3153271
48 meter
Z = 9192228
50 Z = 2827530
78
XDOT = 2464
957807 XDOT = 662
982752
YDOT = 18660
484150 feet/sec YDOT = 5695
623719 meter/sec
ZDOT = 16668
310409 ZDOT = 5083
935847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20223556
50 X = 6164140
02
Y = -1009370
34 feet Y = -307656
08 meter
Z = 9301349
68 Z = 2835051
38
XDOT = -6905
773080 XDOT = -2104
879635
YDOT = 16051
229500 feet/sec YDOT = 4892
414752 meter/sec
ZDOT = 16681
865822 ZDOT = 5084
632703
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 14053
55869203
00016717 00000-0 10270-3 0 9019
2 25544 51
6500 307
8394 0003514 167
1518 192
9723 15
50610248 33545
Satellite: ISS
Catalog Number: 25544
Epoch time: 14053
55869203 = yrday
fracday
Element set: 901
Inclination: 51
6500 deg
RA of node: 307
8394 deg
Eccentricity:
0003514
Arg of perigee: 167
1518 deg
Mean anomaly: 192
9723 deg
Mean motion: 15
50610248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 298
Coasting Arc #3 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2014/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5083050
08 A = 6794865
70 meter
Y = 3098899
82 meter E =
0006345
Z = -3275596
73 I = 51
35505
XDOT = -634
279928 Wp = 128
16301
YDOT = -6007
155391 meter/sec RA = 302
53086 deg
ZDOT = -4708
918996 TA = 89
95058
MA = 89
87787
Ha = 226
925 n
mi
Hp = 219
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16676673
50 X = -5101413
27
Y = 10166994
16 feet Y = 3041955
04 meter
Z = -10746708
44 Z = -3300333
97
XDOT = -2080
970894 XDOT = -544
185272
YDOT = -19708
515062 feet/sec YDOT = -6013
744830 meter/sec
ZDOT = -15449
209306 ZDOT = -4711
781038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19427198
90 X = -5921410
23
Y = 1340931
65 feet Y = 408715
97 meter
Z = -10851580
37 Z = -3307561
70
XDOT = 7445
472518 XDOT = 2269
380023
YDOT = -16979
666133 feet/sec YDOT = -5175
402237 meter/sec
ZDOT = -15460
302010 ZDOT = -4712
300053
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 14054
52539361
00016717 00000-0 10270-3 0 9027
2 25544 51
6503 303
0459 0003540 175
0317 185
0870 15
50641058 33697
Satellite: ISS
Catalog Number: 25544
Epoch time: 14054
52539361 = yrday
fracday
Element set: 902
Inclination: 51
6503 deg
RA of node: 303
0459 deg
Eccentricity:
0003540
Arg of perigee: 175
0317 deg
Mean anomaly: 185
0870 deg
Mean motion: 15
50641058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 288
Coasting Arc #4 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2014/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4872487
33 A = 6793549
29 meter
Y = -2961712
33 meter E =
0012700
Z = 3686831
95 I = 51
33500
XDOT = 579
192935 Wp = 110
63817
YDOT = 6320
363962 meter/sec RA = 297
55131 deg
ZDOT = 4295
388500 TA = 293
42032
MA = 293
55382
Ha = 226
820 n
mi
Hp = 219
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15985850
83 X = 4887334
56
Y = -9716903
97 feet Y = -2907141
85 meter
Z = 12095905
34 Z = 3710537
66
XDOT = 1900
239287 XDOT = 487
608862
YDOT = 20736
102239 feet/sec YDOT = 6326
329020 meter/sec
ZDOT = 14092
481955 ZDOT = 4297
979312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18574542
94 X = 5661520
69
Y = -1584526
48 feet Y = -482963
67 meter
Z = 12196401
36 Z = 3717463
13
XDOT = -7758
845361 XDOT = -2364
896066
YDOT = 18007
793126 feet/sec YDOT = 5488
775345 meter/sec
ZDOT = 14102
388221 ZDOT = 4298
407930
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 14055
55652062
00016717 00000-0 10270-3 0 9036
2 25544 51
6502 297
9325 0003410 176
3470 183
7706 15
50676313 33852
Satellite: ISS
Catalog Number: 25544
Epoch time: 14055
55652062 = yrday
fracday
Element set: 903
Inclination: 51
6502 deg
RA of node: 297
9325 deg
Eccentricity:
0003410
Arg of perigee: 176
3470 deg
Mean anomaly: 183
7706 deg
Mean motion: 15
50676313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 302
Coasting Arc #5 (Orbit 3399)
---------------------------------------
Vector Time (GMT): 2014/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4685350
98 A = 6792084
07 meter
Y = 2730651
75 meter E =
0006863
Z = -4094660
27 I = 51
31668
XDOT = -543
473003 Wp = 97
97590
YDOT = -6624
212144 meter/sec RA = 292
56953 deg
ZDOT = -3802
116201 TA = 132
55162
MA = 132
49367
Ha = 226
604 n
mi
Hp = 219
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15371886
42 X = -4695647
36
Y = 8958831
21 feet Y = 2678199
34 meter
Z = -13433924
77 Z = -4117445
77
XDOT = -1783
047911 XDOT = -450
890083
YDOT = -21732
979475 feet/sec YDOT = -6629
772174 meter/sec
ZDOT = -12474
134518 ZDOT = -3804
530995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17656070
46 X = -5381570
28
Y = 1488170
71 feet Y = 453594
43 meter
Z = -13530499
14 Z = -4124096
14
XDOT = 7944
133302 XDOT = 2421
371831
YDOT = -19056
466966 feet/sec YDOT = -5808
411131 meter/sec
ZDOT = -12483
261071 ZDOT = -3804
897975
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 14056
52317879
00016717 00000-0 10270-3 0 9049
2 25544 51
6498 293
1388 0003430 184
8012 175
3107 15
50718439 34007
Satellite: ISS
Catalog Number: 25544
Epoch time: 14056
52317879 = yrday
fracday
Element set: 904
Inclination: 51
6498 deg
RA of node: 293
1388 deg
Eccentricity:
0003430
Arg of perigee: 184
8012 deg
Mean anomaly: 175
3107 deg
Mean motion: 15
50718439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3400
Checksum: 310
Coasting Arc #6 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2014/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4508244
84 A = 6790796
18 meter
Y = -2475055
69 meter E =
0010507
Z = 4431060
52 I = 51
30128
XDOT = 562
396467 Wp = 128
50054
YDOT = 6906
602338 meter/sec RA = 287
58535 deg
ZDOT = 3273
913718 TA = 288
25620
MA = 288
37051
Ha = 226
498 n
mi
Hp = 220
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14790829
53 X = 4514062
22
Y = -8120261
45 feet Y = -2424608
74 meter
Z = 14537600
15 Z = 4452974
77
XDOT = 1845
132765 XDOT = 469
220227
YDOT = 22659
456491 feet/sec YDOT = 6912
370688 meter/sec
ZDOT = 10741
186740 ZDOT = 3276
418858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16744477
46 X = 5103716
73
Y = -1273327
17 feet Y = -388110
12 meter
Z = 14630455
05 Z = 4459362
70
XDOT = -7896
142587 XDOT = -2406
744260
YDOT = 20127
520354 feet/sec YDOT = 6134
868204 meter/sec
ZDOT = 10750
664327 ZDOT = 3276
802487
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 14057
55426018
00016717 00000-0 10270-3 0 9050
2 25544 51
6495 288
0252 0003321 186
1123 173
9988 15
50740158 34165
Satellite: ISS
Catalog Number: 25544
Epoch time: 14057
55426018 = yrday
fracday
Element set: 905
Inclination: 51
6495 deg
RA of node: 288
0252 deg
Eccentricity:
0003321
Arg of perigee: 186
1123 deg
Mean anomaly: 173
9988 deg
Mean motion: 15
50740158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 309
Coasting Arc #7 (Orbit 3430)
---------------------------------------
Vector Time (GMT): 2014/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4372720
03 A = 6789438
01 meter
Y = 2135503
46 meter E =
0009749
Z = -4743119
81 I = 51
28757
XDOT = -597
161835 Wp = 87
99369
YDOT = -7148
832051 meter/sec RA = 282
59848 deg
ZDOT = -2672
549356 TA = 155
45227
MA = 155
40583
Ha = 226
294 n
mi
Hp = 219
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14346194
31 X = -4373234
71
Y = 7006244
94 feet Y = 2086601
55 meter
Z = -15561416
69 Z = -4764362
82
XDOT = -1959
192372 XDOT = -504
195528
YDOT = -23454
173395 feet/sec YDOT = -7154
990357 meter/sec
ZDOT = -8768
206550 ZDOT = -2675
223704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15861070
02 X = -4834454
14
Y = 720504
18 feet Y = 219609
68 meter
Z = -15651382
70 Z = -4770541
45
XDOT = 7689
445070 XDOT = 2343
742857
YDOT = -21101
782192 feet/sec YDOT = -6431
823212 meter/sec
ZDOT = -8778
376853 ZDOT = -2675
649265
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 14058
52087482
00016717 00000-0 10270-3 0 9067
2 25544 51
6483 283
2307 0003350 194
1249 165
9809 15
50796281 34318
Satellite: ISS
Catalog Number: 25544
Epoch time: 14058
52087482 = yrday
fracday
Element set: 906
Inclination: 51
6483 deg
RA of node: 283
2307 deg
Eccentricity:
0003350
Arg of perigee: 194
1249 deg
Mean anomaly: 165
9809 deg
Mean motion: 15
50796281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3431
Checksum: 319
Coasting Arc #8 (Orbit 3446)
---------------------------------------
Vector Time (GMT): 2014/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4261616
57 A = 6788433
45 meter
Y = -1776335
53 meter E =
0007675
Z = 4974997
42 I = 51
27817
XDOT = 670
673284 Wp = 147
36394
YDOT = 7355
894128 meter/sec RA = 277
61012 deg
ZDOT = 2044
106901 TA = 282
60308
MA = 282
68890
Ha = 226
170 n
mi
Hp = 220
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13981681
65 X = 4256996
82
Y = -5827872
47 feet Y = -1728704
62 meter
Z = 16322170
03 Z = 4995688
29
XDOT = 2200
371666 XDOT = 578
438784
YDOT = 24133
510918 feet/sec YDOT = 7362
878563 meter/sec
ZDOT = 6706
387472 ZDOT = 2047
139941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15052665
46 X = 4588052
43
Y = -47104
34 feet Y = -14357
40 meter
Z = 16409747
03 Z = 5001690
89
XDOT = -7282
697509 XDOT = -2219
766201
YDOT = 22013
458038 feet/sec YDOT = 6709
702010 meter/sec
ZDOT = 6718
056487 ZDOT = 2047
663617
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 14059
55190997
00016717 00000-0 10270-3 0 9078
2 25544 51
6480 278
1167 0003285 196
1035 164
0012 15
50805226 34477
Satellite: ISS
Catalog Number: 25544
Epoch time: 14059
55190997 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 278
1167 deg
Eccentricity:
0003285
Arg of perigee: 196
1035 deg
Mean anomaly: 164
0012 deg
Mean motion: 15
50805226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3447
Checksum: 309
Coasting Arc #9 (Orbit 3461)
---------------------------------------
Vector Time (GMT): 2014/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206678
20 A = 6787466
99 meter
Y = 1352615
88 meter E =
0012401
Z = -5162756
98 I = 51
27072
XDOT = -747
487919 Wp = 92
55288
YDOT = -7495
514885 meter/sec RA = 272
61883 deg
ZDOT = -1358
104822 TA = 164
31953
MA = 164
28108
Ha = 226
009 n
mi
Hp = 220
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13801437
65 X = -4196412
25
Y = 4437716
14 feet Y = 1305630
79 meter
Z = -16938179
06 Z = -5183167
30
XDOT = -2452
388187 XDOT = -657
018719
YDOT = -24591
584270 feet/sec YDOT = -7503
368122 meter/sec
ZDOT = -4455
724483 ZDOT = -1361
515158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14366529
33 X = -4378918
14
Y = -918693
87 feet Y = -280017
89 meter
Z = -17024504
46 Z = -5189068
96
XDOT = 6734
883965 XDOT = 2052
792633
YDOT = -22708
983659 feet/sec YDOT = -6921
698219 meter/sec
ZDOT = -4468
980304 ZDOT = -1362
145197
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 14060
51848087
00016717 00000-0 10270-3 0 9087
2 25544 51
6463 273
3210 0003316 202
6776 157
4229 15
50871357 34625
Satellite: ISS
Catalog Number: 25544
Epoch time: 14060
51848087 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 273
3210 deg
Eccentricity:
0003316
Arg of perigee: 202
6776 deg
Mean anomaly: 157
4229 deg
Mean motion: 15
50871357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3462
Checksum: 306
Coasting Arc #10 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2014/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4185870
83 A = 6786979
60 meter
Y = -919717
93 meter E =
0004462
Z = 5261985
15 I = 51
26878
XDOT = 839
676301 Wp = 163
61771
YDOT = 7589
876325 meter/sec RA = 267
62760 deg
ZDOT = 654
300296 TA = 280
07421
MA = 280
12455
Ha = 225
838 n
mi
Hp = 220
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13733172
02 X = 4170283
54
Y = -3017447
27 feet Y = -872995
21 meter
Z = 17263730
80 Z = 5282281
51
XDOT = 2754
843508 XDOT = 751
563856
YDOT = 24901
169044 feet/sec YDOT = 7598
773555 meter/sec
ZDOT = 2146
654513 ZDOT = 658
164125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13814179
26 X = 4210561
84
Y = 1975961
33 feet Y = 602273
01 meter
Z = 17349508
10 Z = 5288130
07
XDOT = -6060
523471 XDOT = -1847
247554
YDOT = 23263
929487 feet/sec YDOT = 7090
845708 meter/sec
ZDOT = 2161
823454 ZDOT = 658
923789
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 14061
54946877
00016717 00000-0 10270-3 0 9098
2 25544 51
6464 268
2065 0003306 205
9005 154
1981 15
50875175 34785
Satellite: ISS
Catalog Number: 25544
Epoch time: 14061
54946877 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 268
2065 deg
Eccentricity:
0003306
Arg of perigee: 205
9005 deg
Mean anomaly: 154
1981 deg
Mean motion: 15
50875175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 327
Coasting Arc #11 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2014/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4228590
67 A = 6786647
55 meter
Y = 449592
62 meter E =
0013510
Z = -5300680
57 I = 51
26914
XDOT = -915
243484 Wp = 102
94938
YDOT = -7598
262607 meter/sec RA = 262
63397 deg
ZDOT = 82
871056 TA = 167
86221
MA = 167
82963
Ha = 225
742 n
mi
Hp = 220
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13873328
98 X = -4207555
07
Y = 1475041
41 feet Y = 402422
65 meter
Z = -17390684
28 Z = -5321171
24
XDOT = -3002
767337 XDOT = -830
612539
YDOT = -24928
683094 feet/sec YDOT = -7608
024235 meter/sec
ZDOT = 271
886666 ZDOT = 78
631649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13459048
38 X = -4102317
95
Y = -3237594
04 feet Y = -986818
66 meter
Z = -17477211
03 Z = -5327053
92
XDOT = 5311
543872 XDOT = 1618
958572
YDOT = -23507
087925 feet/sec YDOT = -7164
960399 meter/sec
ZDOT = 255
122960 ZDOT = 77
761478
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 14062
51599563
00016717 00000-0 10270-3 0 9104
2 25544 51
6450 263
4099 0003313 210
4836 149
6123 15
50943390 34934
Satellite: ISS
Catalog Number: 25544
Epoch time: 14062
51599563 = yrday
fracday
Element set: 910
Inclination: 51
6450 deg
RA of node: 263
4099 deg
Eccentricity:
0003313
Arg of perigee: 210
4836 deg
Mean anomaly: 149
6123 deg
Mean motion: 15
50943390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 302
Coasting Arc #12 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2014/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4307684
66 A = 6786835
56 meter
Y = 15320
77 meter E =
0001477
Z = 5243546
91 I = 51
27523
XDOT = 977
510579 Wp = 140
82395
YDOT = 7556
861275 meter/sec RA = 257
64213 deg
ZDOT = -826
122600 TA = 317
11161
MA = 317
12312
Ha = 225
506 n
mi
Hp = 220
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14132823
69 X = 4281721
87
Y = 50264
99 feet Y = 63347
60 meter
Z = 17203237
88 Z = 5264409
83
XDOT = 3207
055707 XDOT = 896
948422
YDOT = 24792
851951 feet/sec YDOT = 7567
341863 meter/sec
ZDOT = -2710
375984 ZDOT = -821
570726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13271929
95 X = 4045284
25
Y = 4534152
91 feet Y = 1382009
81 meter
Z = 17291268
27 Z = 5270378
57
XDOT = -4543
435800 XDOT = -1384
839232
YDOT = 23553
857774 feet/sec YDOT = 7179
215850 meter/sec
ZDOT = -2692
278430 ZDOT = -820
606465
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 14063
54693516
00016717 00000-0 10270-3 0 9112
2 25544 51
6454 258
2952 0003341 215
0590 145
0341 15
50950902 35094
Satellite: ISS
Catalog Number: 25544
Epoch time: 14063
54693516 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 258
2952 deg
Eccentricity:
0003341
Arg of perigee: 215
0590 deg
Mean anomaly: 145
0341 deg
Mean motion: 15
50950902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 290
Coasting Arc #13 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2014/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4447497
94 A = 6787251
64 meter
Y = -485622
94 meter E =
0012492
Z = -5115071
24 I = 51
28397
XDOT = -999
612726 Wp = 115
75513
YDOT = -7423
907643 meter/sec RA = 252
64905 deg
ZDOT = 1571
660998 TA = 169
51605
MA = 169
48998
Ha = 225
481 n
mi
Hp = 220
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14591528
69 X = -4416889
80
Y = -1593251
12 feet Y = -535187
19 meter
Z = -16781729
80 Z = -5136602
05
XDOT = -3279
569312 XDOT = -924
157217
YDOT = -24356
652371 feet/sec YDOT = -7434
663869 meter/sec
ZDOT = 5156
368103 ZDOT = 1566
989207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13319317
60 X = -4059728
00
Y = -5915377
61 feet Y = -1803007
10 meter
Z = -16872513
16 Z = -5142742
01
XDOT = 3804
094619 XDOT = 1159
488040
YDOT = -23241
439972 feet/sec YDOT = -7083
990903 meter/sec
ZDOT = 5137
736822 ZDOT = 1565
982183
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 14064
51341717
00016717 00000-0 10270-3 0 9124
2 25544 51
6446 253
4985 0003303 217
7818 142
3102 15
51014420 35247
Satellite: ISS
Catalog Number: 25544
Epoch time: 14064
51341717 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 253
4985 deg
Eccentricity:
0003303
Arg of perigee: 217
7818 deg
Mean anomaly: 142
3102 deg
Mean motion: 15
51014420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 275
Coasting Arc #14 (Orbit 3539)
---------------------------------------
Vector Time (GMT): 2014/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4616348
97 A = 6788140
24 meter
Y = 934981
27 meter E =
0003549
Z = 4885567
86 I = 51
29747
XDOT = 977
798302 Wp = 73
11444
YDOT = 7243
645254 meter/sec RA = 247
65899 deg
ZDOT = -2307
770192 TA = 39
59188
MA = 39
56596
Ha = 225
196 n
mi
Hp = 220
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15145501
86 X = 4581818
30
Y = 3067523
84 feet Y = 986411
67 meter
Z = 16028765
94 Z = 4907909
34
XDOT = 3207
999677 XDOT = 907
935910
YDOT = 23765
240334 feet/sec YDOT = 7254
188760 meter/sec
ZDOT = -7571
424513 ZDOT = -2303
190647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13531131
18 X = 4124288
78
Y = 7257927
16 feet Y = 2212216
20 meter
Z = 16122910
68 Z = 4914263
18
XDOT = -3173
362838 XDOT = -967
240993
YDOT = 22712
343752 feet/sec YDOT = 6922
722376 meter/sec
ZDOT = -7553
148127 ZDOT = -2302
199549
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 14065
54430707
00016717 00000-0 10270-3 0 9137
2 25544 51
6448 248
3837 0003334 223
2357 136
8533 15
51029253 35406
Satellite: ISS
Catalog Number: 25544
Epoch time: 14065
54430707 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 248
3837 deg
Eccentricity:
0003334
Arg of perigee: 223
2357 deg
Mean anomaly: 136
8533 deg
Mean motion: 15
51029253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3540
Checksum: 297
Coasting Arc #15 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2014/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4831512
09 A = 6789215
43 meter
Y = -1358182
01 meter E =
0009280
Z = -4581476
85 I = 51
31417
XDOT = -894
098102 Wp = 128
72952
YDOT = -6981
260853 meter/sec RA = 242
66920 deg
ZDOT = 3010
940872 TA = 171
53491
MA = 171
51924
Ha = 225
217 n
mi
Hp = 220
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15851417
60 X = -4793710
30
Y = -4455977
71 feet Y = -1412000
13 meter
Z = -15031092
04 Z = -4604855
56
XDOT = -2933
392722 XDOT = -830
591710
YDOT = -22904
399123 feet/sec YDOT = -6990
903872 meter/sec
ZDOT = 9878
414936 ZDOT = 3006
752387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13964007
75 X = -4256229
56
Y = -8553349
13 feet Y = -2607060
81 meter
Z = -15129560
85 Z = -4611490
15
XDOT = 2688
261181 XDOT = 819
382008
YDOT = -21841
653934 feet/sec YDOT = -6657
336119 meter/sec
ZDOT = 9861
742338 ZDOT = 3005
859065
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 14066
51074259
00016717 00000-0 10270-3 0 9142
2 25544 51
6447 243
5871 0003255 224
9644 135
1244 15
51088106 35558
Satellite: ISS
Catalog Number: 25544
Epoch time: 14066
51074259 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 243
5871 deg
Eccentricity:
0003255
Arg of perigee: 224
9644 deg
Mean anomaly: 135
1244 deg
Mean motion: 15
51088106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 304
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