[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 5th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8342 03 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 378 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 470)
---------------------------------------
Vector Time (GMT): 2014/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3081213
67 A = 6789948
82 meter
Y = 2917529
11 meter E =
0002443
Z = 5300006
43 I = 51
35442
XDOT = -5091
051410 Wp = 21
21210
YDOT = 5723
602537 meter/sec RA = 310
52387 deg
ZDOT = -188
711818 TA = 70
60810
MA = 70
58170
Ha = 227
278 n
mi
Hp = 222
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10108968
72 X = 3022614
24
Y = 9571945
89 feet Y = 2951657
51 meter
Z = 17388472
55 Z = 5314832
36
XDOT = -16702
924573 XDOT = -5153
758940
YDOT = 18778
223548 feet/sec YDOT = 5666
320517 meter/sec
ZDOT = -619
133262 ZDOT = -213
595889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13840144
28 X = 4218475
98
Y = 312844
06 feet Y = 95354
87 meter
Z = 17450642
09 Z = 5318955
71
XDOT = 378
745850 XDOT = 115
441735
YDOT = 24117
238304 feet/sec YDOT = 7350
934235 meter/sec
ZDOT = -725
349597 ZDOT = -221
086557
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 14125
54800262
00016717 00000-0 10270-3 0 9007
2 25544 51
6444 310
9241 0002395 319
9114 40
1859 15
49815755 4712
Satellite: ISS
Catalog Number: 25544
Epoch time: 14125
54800262 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 310
9241 deg
Eccentricity:
0002395
Arg of perigee: 319
9114 deg
Mean anomaly: 40
1859 deg
Mean motion: 15
49815755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 471
Checksum: 293
Coasting Arc #2 (Orbit 485)
---------------------------------------
Vector Time (GMT): 2014/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3099819
06 A = 6789894
20 meter
Y = -2940466
14 meter E =
0013293
Z = -5288544
04 I = 51
33484
XDOT = 4770
270297 Wp = 86
32951
YDOT = -5960
295329 meter/sec RA = 305
54806 deg
ZDOT = 519
895040 TA = 188
65103
MA = 188
67396
Ha = 227
350 n
mi
Hp = 221
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10170010
04 X = -3041017
46
Y = -9647198
61 feet Y = -2974801
52 meter
Z = -17350866
28 Z = -5303459
83
XDOT = 15650
493101 XDOT = 4834
039627
YDOT = -19554
774700 feet/sec YDOT = -5906
594549 meter/sec
ZDOT = 1705
692390 ZDOT = 543
223411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13939708
16 X = -4248823
05
Y = -87232
60 feet Y = -26588
50 meter
Z = -17413415
31 Z = -5307608
99
XDOT = -2097
424221 XDOT = -639
294903
YDOT = -23935
547422 feet/sec YDOT = -7295
554854 meter/sec
ZDOT = 1805
364332 ZDOT = 550
275048
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 14126
51519209
00016717 00000-0 10270-3 0 9014
2 25544 51
6440 306
1328 0002327 323
8734 36
2259 15
49866357 4868
Satellite: ISS
Catalog Number: 25544
Epoch time: 14126
51519209 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 306
1328 deg
Eccentricity:
0002327
Arg of perigee: 323
8734 deg
Mean anomaly: 36
2259 deg
Mean motion: 15
49866357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 486
Checksum: 306
Coasting Arc #3 (Orbit 501)
---------------------------------------
Vector Time (GMT): 2014/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3116155
99 A = 6790132
08 meter
Y = 2980297
34 meter E =
0004082
Z = 5244313
92 I = 51
31783
XDOT = -4450
885007 Wp = 24
43068
YDOT = 6177
596114 meter/sec RA = 300
57125 deg
ZDOT = -862
081157 TA = 73
87815
MA = 73
83322
Ha = 227
378 n
mi
Hp = 221
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10223608
90 X = 3057122
62
Y = 9777878
41 feet Y = 3014814
16 meter
Z = 17205754
33 Z = 5259308
48
XDOT = -14602
641100 XDOT = -4515
445736
YDOT = 20267
703787 feet/sec YDOT = 6127
462474 meter/sec
ZDOT = -2828
350251 ZDOT = -883
859977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14069537
55 X = 4288395
04
Y = -97402
24 feet Y = -29688
20 meter
Z = 17268633
22 Z = 5263479
40
XDOT = 3765
162491 XDOT = 1147
621527
YDOT = 23657
050939 feet/sec YDOT = 7210
669126 meter/sec
ZDOT = -2921
498914 ZDOT = -890
472869
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 14127
54685432
00016717 00000-0 10270-3 0 9021
2 25544 51
6437 301
0225 0002332 328
4737 31
6274 15
49837820 5022
Satellite: ISS
Catalog Number: 25544
Epoch time: 14127
54685432 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 301
0225 deg
Eccentricity:
0002332
Arg of perigee: 328
4737 deg
Mean anomaly: 31
6274 deg
Mean motion: 15
49837820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 287
Coasting Arc #4 (Orbit 516)
---------------------------------------
Vector Time (GMT): 2014/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3168391
28 A = 6790216
17 meter
Y = -3025748
86 meter E =
0012831
Z = -5198995
83 I = 51
30401
XDOT = 4102
758543 Wp = 90
98384
YDOT = -6347
502022 meter/sec RA = 295
59339 deg
ZDOT = 1196
201669 TA = 190
55679
MA = 190
58375
Ha = 227
438 n
mi
Hp = 221
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10394984
50 X = -3109065
88
Y = -9926997
58 feet Y = -3060848
23 meter
Z = -17057072
95 Z = -5214243
44
XDOT = 13460
493908 XDOT = 4167
622000
YDOT = -20825
137869 feet/sec YDOT = -6301
259649 meter/sec
ZDOT = 3924
546158 ZDOT = 1216
290145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14292925
43 X = -4356483
67
Y = 357445
06 feet Y = 108949
26 meter
Z = -17121017
40 Z = -5218486
10
XDOT = -5373
729282 XDOT = -1637
912685
YDOT = -23145
155316 feet/sec YDOT = -7054
643340 meter/sec
ZDOT = 4010
567323 ZDOT = 1222
420920
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 14128
51402814
00016717 00000-0 10270-3 0 9031
2 25544 51
6441 296
2316 0002277 332
5426 27
5604 15
49890783 5176
Satellite: ISS
Catalog Number: 25544
Epoch time: 14128
51402814 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 296
2316 deg
Eccentricity:
0002277
Arg of perigee: 332
5426 deg
Mean anomaly: 27
5604 deg
Mean motion: 15
49890783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 517
Checksum: 301
Coasting Arc #5 (Orbit 532)
---------------------------------------
Vector Time (GMT): 2014/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3220715
58 A = 6790611
55 meter
Y = 3087173
73 meter E =
0005797
Z = 5117901
68 I = 51
29186
XDOT = -3763
848980 Wp = 32
18517
YDOT = 6493
963065 meter/sec RA = 290
61399 deg
ZDOT = -1542
994999 TA = 72
80048
MA = 72
73702
Ha = 227
478 n
mi
Hp = 221
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10566652
17 X = 3161093
30
Y = 10128522
73 feet Y = 3122856
58 meter
Z = 16791016
02 Z = 5133402
77
XDOT = -12348
585892 XDOT = -3828
690741
YDOT = 21305
653099 feet/sec YDOT = 6451
510702 meter/sec
ZDOT = -5062
319552 ZDOT = -1561
437117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14550116
12 X = 4434875
39
Y = -589806
97 feet Y = -179773
16 meter
Z = 16856024
98 Z = 5137716
42
XDOT = 6891
646260 XDOT = 2100
573780
YDOT = 22550
894930 feet/sec YDOT = 6873
512775 meter/sec
ZDOT = -5141
395287 ZDOT = -1567
097283
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 14129
54567364
00016717 00000-0 10270-3 0 9048
2 25544 51
6435 291
1208 0002285 337
5735 22
5315 15
49862856 5332
Satellite: ISS
Catalog Number: 25544
Epoch time: 14129
54567364 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 291
1208 deg
Eccentricity:
0002285
Arg of perigee: 337
5735 deg
Mean anomaly: 22
5315 deg
Mean motion: 15
49862856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 533
Checksum: 314
Coasting Arc #6 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2014/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3313129
81 A = 6790841
14 meter
Y = -3142647
85 meter E =
0011869
Z = -5036757
72 I = 51
28408
XDOT = 3405
675631 Wp = 94
72748
YDOT = -6591
370085 meter/sec RA = 285
63485 deg
ZDOT = 1875
294830 TA = 193
56121
MA = 193
59313
Ha = 227
517 n
mi
Hp = 221
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10869848
46 X = -3253274
44
Y = -10310524
45 feet Y = -3179362
84 meter
Z = -16524795
69 Z = -5052707
23
XDOT = 11173
476481 XDOT = 3470
018986
YDOT = -21625
229938 feet/sec YDOT = -6552
925825 meter/sec
ZDOT = 6152
542093 ZDOT = 1891
995818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14878149
65 X = -4534860
01
Y = 941138
58 feet Y = 286859
04 meter
Z = -16591694
11 Z = -5057148
37
XDOT = -8306
509240 XDOT = -2531
824016
YDOT = -21750
709515 feet/sec YDOT = -6629
616260 meter/sec
ZDOT = 6224
264397 ZDOT = 1897
155788
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 14130
51283151
00016717 00000-0 10270-3 0 9057
2 25544 51
6445 286
3302 0002293 340
8077 19
2986 15
49914832 5484
Satellite: ISS
Catalog Number: 25544
Epoch time: 14130
51283151 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 286
3302 deg
Eccentricity:
0002293
Arg of perigee: 340
8077 deg
Mean anomaly: 19
2986 deg
Mean motion: 15
49914832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 305
Coasting Arc #7 (Orbit 563)
---------------------------------------
Vector Time (GMT): 2014/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3407032
43 A = 6791382
26 meter
Y = 3212195
30 meter E =
0007533
Z = 4916689
67 I = 51
27769
XDOT = -3065
472209 Wp = 41
11267
YDOT = 6662
646243 meter/sec RA = 280
65383 deg
ZDOT = -2221
122390 TA = 70
73711
MA = 70
65564
Ha = 227
564 n
mi
Hp = 221
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11177927
91 X = 3346975
57
Y = 10538698
50 feet Y = 3249959
21 meter
Z = 16130871
61 Z = 4933094
93
XDOT = -10057
323521 XDOT = -3128
957894
YDOT = 21859
075599 feet/sec YDOT = 6628
011159 meter/sec
ZDOT = -7287
146949 ZDOT = -2236
168612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15236581
13 X = 4644109
93
Y = -1277481
87 feet Y = -389376
47 meter
Z = 16199688
05 Z = 4937664
92
XDOT = 9594
441784 XDOT = 2924
385856
YDOT = 20892
835131 feet/sec YDOT = 6368
136148 meter/sec
ZDOT = -7351
878277 ZDOT = -2240
852499
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 14131
54446022
00016717 00000-0 10270-3 0 9060
2 25544 51
6440 281
2189 0002296 346
1540 13
9547 15
49890664 5641
Satellite: ISS
Catalog Number: 25544
Epoch time: 14131
54446022 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 281
2189 deg
Eccentricity:
0002296
Arg of perigee: 346
1540 deg
Mean anomaly: 13
9547 deg
Mean motion: 15
49890664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 564
Checksum: 305
Coasting Arc #8 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2014/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3542168
44 A = 6791757
48 meter
Y = -3263295
58 meter E =
0010447
Z = -4798265
77 I = 51
27583
XDOT = 2716
081371 Wp = 96
73430
YDOT = -6686
745557 meter/sec RA = 275
67421 deg
ZDOT = 2546
183182 TA = 198
48834
MA = 198
52633
Ha = 227
589 n
mi
Hp = 221
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11621287
55 X = -3482105
33
Y = -10706350
34 feet Y = -3302570
55 meter
Z = -15742341
77 Z = -4815327
60
XDOT = 8911
028121 XDOT = 2778
283402
YDOT = -21938
141590 feet/sec YDOT = -6656
024798 meter/sec
ZDOT = 8353
619362 ZDOT = 2559
528896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15629901
92 X = -4763994
11
Y = 1768450
46 feet Y = 539023
70 meter
Z = -15813928
52 Z = -4820085
41
XDOT = -10746
606658 XDOT = -3275
565709
YDOT = -19870
864004 feet/sec YDOT = -6056
639348 meter/sec
ZDOT = 8411
160500 ZDOT = 2563
721721
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 14132
51160217
00016717 00000-0 10270-3 0 9078
2 25544 51
6452 276
4286 0002379 348
0564 12
0530 15
49937402 5797
Satellite: ISS
Catalog Number: 25544
Epoch time: 14132
51160217 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 276
4286 deg
Eccentricity:
0002379
Arg of perigee: 348
0564 deg
Mean anomaly: 12
0530 deg
Mean motion: 15
49937402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 299
Coasting Arc #9 (Orbit 594)
---------------------------------------
Vector Time (GMT): 2014/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3678830
76 A = 6792420
63 meter
Y = 3326072
49 meter E =
0009228
Z = 4637782
77 I = 51
27575
XDOT = -2394
036381 Wp = 50
48838
YDOT = 6683
607899 meter/sec RA = 270
69297 deg
ZDOT = -2884
627920 TA = 68
40965
MA = 68
31135
Ha = 227
640 n
mi
Hp = 221
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12069654
72 X = 3618835
06
Y = 10912311
30 feet Y = 3366875
98 meter
Z = 15215822
73 Z = 4655508
77
XDOT = -7854
450068 XDOT = -2454
583146
YDOT = 21927
847439 feet/sec YDOT = 6656
497773 meter/sec
ZDOT = -9464
002362 ZDOT = -2896
405005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16043948
48 X = 4890195
50
Y = -2253338
75 feet Y = -686817
65 meter
Z = 15290210
79 Z = 4660456
25
XDOT = 11741
789963 XDOT = 3578
897581
YDOT = 18825
090717 feet/sec YDOT = 5737
887651 meter/sec
ZDOT = -9514
908202 ZDOT = -2900
144020
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 14133
54321418
00016717 00000-0 10270-3 0 9085
2 25544 51
6453 271
3174 0002365 353
7986 6
3135 15
49920257 5959
Satellite: ISS
Catalog Number: 25544
Epoch time: 14133
54321418 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 271
3174 deg
Eccentricity:
0002365
Arg of perigee: 353
7986 deg
Mean anomaly: 6
3135 deg
Mean motion: 15
49920257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 595
Checksum: 308
Coasting Arc #10 (Orbit 609)
---------------------------------------
Vector Time (GMT): 2014/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3854643
50 A = 6792928
05 meter
Y = -3357792
82 meter E =
0008728
Z = -4481370
77 I = 51
27940
XDOT = 2072
344682 Wp = 95
46298
YDOT = -6638
935186 meter/sec RA = 265
71372 deg
ZDOT = 3196
469573 TA = 206
87547
MA = 206
92070
Ha = 227
660 n
mi
Hp = 221
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12646468
16 X = -3795039
84
Y = -11016380
64 feet Y = -3400564
45 meter
Z = -14702660
00 Z = -4499951
89
XDOT = 6799
031109 XDOT = 2130
900956
YDOT = -21781
283419 feet/sec YDOT = -6615
433634 meter/sec
ZDOT = 10487
104898 ZDOT = 3206
678900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16446464
73 X = -5012882
45
Y = 2916812
50 feet Y = 889044
45 meter
Z = -14780663
49 Z = -4505146
23
XDOT = -12584
581486 XDOT = -3835
780437
YDOT = -17667
350869 feet/sec YDOT = -5385
008545 meter/sec
ZDOT = 10531
373306 ZDOT = 3209
962584
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 14134
51034052
00016717 00000-0 10270-3 0 9099
2 25544 51
6463 266
5272 0002510 354
5325 5
5798 15
49958680 6108
Satellite: ISS
Catalog Number: 25544
Epoch time: 14134
51034052 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 266
5272 deg
Eccentricity:
0002510
Arg of perigee: 354
5325 deg
Mean anomaly: 5
5798 deg
Mean motion: 15
49958680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 610
Checksum: 301
Coasting Arc #11 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2014/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030439
67 A = 6793681
16 meter
Y = 3398871
22 meter E =
0010829
Z = 4279785
19 I = 51
28539
XDOT = -1787
617558 Wp = 60
14672
YDOT = 6567
745684 meter/sec RA = 260
73369 deg
ZDOT = -3520
407338 TA = 65
97908
MA = 65
86577
Ha = 227
719 n
mi
Hp = 221
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13223227
27 X = 3971342
91
Y = 11151152
30 feet Y = 3443611
47 meter
Z = 14041290
00 Z = 4299221
59
XDOT = -5864
887002 XDOT = -1843
825351
YDOT = 21547
722060 feet/sec YDOT = 6547
441352 meter/sec
ZDOT = -11549
892842 ZDOT = -3529
227614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16855592
09 X = 5137584
47
Y = -3576615
52 feet Y = -1090152
41 meter
Z = 14122910
40 Z = 4304663
09
XDOT = 13249
345812 XDOT = 4038
400604
YDOT = 16527
244316 feet/sec YDOT = 5037
504067 meter/sec
ZDOT = -11588
274907 ZDOT = -3532
106192
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 14135
54193595
00016717 00000-0 10270-3 0 9103
2 25544 51
6466 261
4165 0002477 1
0109 359
1046 15
49950335 6262
Satellite: ISS
Catalog Number: 25544
Epoch time: 14135
54193595 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 261
4165 deg
Eccentricity:
0002477
Arg of perigee: 1
0109 deg
Mean anomaly: 359
1046 deg
Mean motion: 15
49950335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 626
Checksum: 299
Coasting Arc #12 (Orbit 640)
---------------------------------------
Vector Time (GMT): 2014/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4240110
47 A = 6794290
79 meter
Y = -3397182
40 meter E =
0007060
Z = -4085552
62 I = 51
29412
XDOT = 1511
091838 Wp = 88
03652
YDOT = -6464
127801 meter/sec RA = 255
75548 deg
ZDOT = 3812
710248 TA = 221
59553
MA = 221
64926
Ha = 227
738 n
mi
Hp = 221
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13911123
58 X = -4181960
62
Y = -11145611
53 feet Y = -3444272
57 meter
Z = -13404044
04 Z = -4106009
87
XDOT = 4957
650386 XDOT = 1564
741630
YDOT = -21207
768375 feet/sec YDOT = -6446
930134 meter/sec
ZDOT = 12508
891891 ZDOT = 3820
180844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17200582
26 X = -5242737
47
Y = 4424083
41 feet Y = 1348460
62 meter
Z = -13489991
42 Z = -4111749
38
XDOT = -13764
137821 XDOT = -4195
309208
YDOT = -15331
649317 feet/sec YDOT = -4673
086712 meter/sec
ZDOT = 12541
547386 ZDOT = 3822
663643
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 14136
50904695
00016717 00000-0 10270-3 0 9112
2 25544 51
6471 256
6264 0002657
8972 359
2183 15
49979630 6418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14136
50904695 = yrday
fracday
Element set: 911
Inclination: 51
6471 deg
RA of node: 256
6264 deg
Eccentricity:
0002657
Arg of perigee:
8972 deg
Mean anomaly: 359
2183 deg
Mean motion: 15
49979630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 641
Checksum: 324
Coasting Arc #13 (Orbit 656)
---------------------------------------
Vector Time (GMT): 2014/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4446631
92 A = 6795093
79 meter
Y = 3403089
00 meter E =
0012277
Z = 3843074
65 I = 51
30535
XDOT = -1280
790450 Wp = 69
93911
YDOT = 6336
790670 meter/sec RA = 250
77750 deg
ZDOT = -4114
482684 TA = 63
58975
MA = 63
46380
Ha = 227
813 n
mi
Hp = 220
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14588687
41 X = 4389578
67
Y = 11164990
17 feet Y = 3452494
76 meter
Z = 12608512
62 Z = 3864537
75
XDOT = -4202
068407 XDOT = -1331
567601
YDOT = 20789
995636 feet/sec YDOT = 6322
184493 meter/sec
ZDOT = -13498
958937 ZDOT = -4120
827452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17536051
90 X = 5344988
62
Y = -5262191
33 feet Y = -1603915
92 meter
Z = 12698725
22 Z = 3870571
45
XDOT = 14091
664210 XDOT = 4295
139251
YDOT = 14199
985024 feet/sec YDOT = 4328
155435 meter/sec
ZDOT = -13526
828364 ZDOT = -4122
977285
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 14137
54062590
00016717 00000-0 10270-3 0 9127
2 25544 51
6471 251
5161 0002620 8
3655 351
7539 15
49980195 6576
Satellite: ISS
Catalog Number: 25544
Epoch time: 14137
54062590 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 251
5161 deg
Eccentricity:
0002620
Arg of perigee: 8
3655 deg
Mean anomaly: 351
7539 deg
Mean motion: 15
49980195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 657
Checksum: 307
Coasting Arc #14 (Orbit 671)
---------------------------------------
Vector Time (GMT): 2014/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4678909
61 A = 6795763
74 meter
Y = -3356472
54 meter E =
0006087
Z = -3612137
63 I = 51
31899
XDOT = 1063
866312 Wp = 71
54009
YDOT = -6188
862634 meter/sec RA = 245
80081 deg
ZDOT = 4380
747516 TA = 245
56013
MA = 245
62364
Ha = 227
826 n
mi
Hp = 220
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15350753
32 X = -4623482
28
Y = -11012049
03 feet Y = -3408484
90 meter
Z = -11850845
23 Z = -3634732
95
XDOT = 3490
375040 XDOT = 1111
712070
YDOT = -20304
667436 feet/sec YDOT = -6176
698641 meter/sec
ZDOT = 14372
531219 ZDOT = 4386
031373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17754042
94 X = -5411432
29
Y = 6280411
82 feet Y = 1914269
52 meter
Z = -11945868
35 Z = -3641100
67
XDOT = -14291
173263 XDOT = -4355
949611
YDOT = -13066
867971 feet/sec YDOT = -3982
781357 meter/sec
ZDOT = 14395
883396 ZDOT = 4387
865259
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 14138
50772168
00016717 00000-0 10270-3 0 9134
2 25544 51
6472 246
7256 0002801 7
5721 352
5471 15
50000563 6729
Satellite: ISS
Catalog Number: 25544
Epoch time: 14138
50772168 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 246
7256 deg
Eccentricity:
0002801
Arg of perigee: 7
5721 deg
Mean anomaly: 352
5471 deg
Mean motion: 15
50000563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 672
Checksum: 287
Coasting Arc #15 (Orbit 687)
---------------------------------------
Vector Time (GMT): 2014/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4903463
94 A = 6796563
68 meter
Y = 3316586
39 meter E =
0013476
Z = 3330160
60 I = 51
33485
XDOT = -901
167251 Wp = 79
64843
YDOT = 6022
234108 meter/sec RA = 240
82519 deg
ZDOT = -4652
281121 TA = 61
45408
MA = 61
31850
Ha = 227
915 n
mi
Hp = 220
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16087480
11 X = 4849835
75
Y = 10881188
94 feet Y = 3371119
98 meter
Z = 10925723
75 Z = 3353851
04
XDOT = -2956
585470 XDOT = -945
842861
YDOT = 19757
985919 feet/sec YDOT = 6011
907210 meter/sec
ZDOT = -15263
389503 ZDOT = -4656
766976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17946958
07 X = 5470232
82
Y = -7275023
50 feet Y = -2217427
16 meter
Z = 11025400
56 Z = 3360542
09
XDOT = 14308
470455 XDOT = 4361
221795
YDOT = 12044
754974 feet/sec YDOT = 3671
241316 meter/sec
ZDOT = -15283
331626 ZDOT = -4658
359479
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 14139
53928434
00016717 00000-0 10270-3 0 9148
2 25544 51
6468 241
6153 0002785 15
6500 344
4736 15
50010415 6888
Satellite: ISS
Catalog Number: 25544
Epoch time: 14139
53928434 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 241
6153 deg
Eccentricity:
0002785
Arg of perigee: 15
6500 deg
Mean anomaly: 344
4736 deg
Mean motion: 15
50010415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 688
Checksum: 300
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