[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 26th 2014
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) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
239/08:38:29
116 -0
0 1
4 1
4
N/A 1
4 -0
2 228
6
000/00:02:58
233 -0
2 -0
0 220
2
Coasting Arc #1 (Orbit 2207)
---------------------------------------
Vector Time (GMT): 2014/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1164271
35 A = 6793313
72 meter
Y = 5232824
73 meter E =
0010742
Z = -4181648
53 I = 51
96669
XDOT = -5200
787555 Wp = 87
87654
YDOT = 4162
264367 meter/sec RA = 115
05803 deg
ZDOT = 3769
282130 TA = 220
78325
MA = 220
86370
Ha = 228
599 n
mi
Hp = 219
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3819787
89 X = 1125982
95
Y = 17168060
13 feet Y = 5245629
95 meter
Z = -13719319
33 Z = -4176086
16
XDOT = -17062
951295 XDOT = -5265
254089
YDOT = 13655
722989 feet/sec YDOT = 4103
745640 meter/sec
ZDOT = 12366
411188 ZDOT = 3743
860939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4359232
38 X = 1328694
03
Y = -17057447
28 feet Y = -5199109
93 meter
Z = -13696473
14 Z = -4174685
01
XDOT = 20240
195574 XDOT = 6169
211611
YDOT = -4646
690302 feet/sec YDOT = -1416
311204 meter/sec
ZDOT = 12257
587372 ZDOT = 3736
112631
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 14237
50923859
00016717 00000-0 10270-3 0 9005
2 25544 51
6467 115
9893 0004582 48
8732 311
2813 15
50239461 22085
Satellite: ISS
Catalog Number: 25544
Epoch time: 14237
50923859 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 115
9893 deg
Eccentricity:
0004582
Arg of perigee: 48
8732 deg
Mean anomaly: 311
2813 deg
Mean motion: 15
50239461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2208
Checksum: 314
Coasting Arc #2 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2014/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1244868
41 A = 6794152
17 meter
Y = -5427483
61 meter E =
0015440
Z = 3883673
77 I = 51
98223
XDOT = 4961
002475 Wp = 72
92613
YDOT = -4117
621414 meter/sec RA = 110
12385 deg
ZDOT = -4146
239396 TA = 60
51133
MA = 60
35741
Ha = 228
574 n
mi
Hp = 219
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4084213
95 X = -1202949
91
Y = -17806704
77 feet Y = -5441169
81 meter
Z = 12741711
84 Z = 3877728
76
XDOT = 16276
254838 XDOT = 5026
818786
YDOT = -13509
256606 feet/sec YDOT = -4061
776653 meter/sec
ZDOT = -13603
147624 ZDOT = -4121
979634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4115071
90 X = -1254273
92
Y = 17817068
44 feet Y = 5430642
46 meter
Z = 12717272
28 Z = 3876224
59
XDOT = -19343
557692 XDOT = -5895
916385
YDOT = 5209
944957 feet/sec YDOT = 1587
991223 meter/sec
ZDOT = -13499
264856 ZDOT = -4114
575928
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 14238
54064915
00016717 00000-0 10270-3 0 9010
2 25544 51
6465 110
8775 0004643 51
4187 308
7379 15
50294879 22248
Satellite: ISS
Catalog Number: 25544
Epoch time: 14238
54064915 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 110
8775 deg
Eccentricity:
0004643
Arg of perigee: 51
4187 deg
Mean anomaly: 308
7379 deg
Mean motion: 15
50294879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 322
Coasting Arc #3 (Orbit 2236)
---------------------------------------
Vector Time (GMT): 2014/239/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4246381
42 A = 6789541
39 meter
Y = 244725
04 meter E =
0017672
Z = -5307420
04 I = 51
97158
XDOT = -1458
805419 Wp = 77
26826
YDOT = 7463
147753 meter/sec RA = 105
90701 deg
ZDOT = -821
563256 TA = 184
88572
MA = 184
90299
Ha = 228
616 n
mi
Hp = 220
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13931697
57 X = 4269110
72
Y = 802903
66 feet Y = 292337
38 meter
Z = -17412795
40 Z = -5286736
75
XDOT = -4786
107019 XDOT = -1538
160785
YDOT = 24485
392889 feet/sec YDOT = 7446
390665 meter/sec
ZDOT = -2695
417507 ZDOT = -828
843333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2781241
76 X = -847722
49
Y = -13786138
84 feet Y = -4202015
12 meter
Z = -17324819
35 Z = -5280604
94
XDOT = 23889
349812 XDOT = 7281
473823
YDOT = -1385
647014 feet/sec YDOT = -422
345210 meter/sec
ZDOT = -2727
584271 ZDOT = -831
367686
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 14239
37866192
00016717 00000-0 10270-3 0 9020
2 25544 51
6453 106
7229 0003662 50
8918 309
2558 15
50032525 22375
Satellite: ISS
Catalog Number: 25544
Epoch time: 14239
37866192 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 106
7229 deg
Eccentricity:
0003662
Arg of perigee: 50
8918 deg
Mean anomaly: 309
2558 deg
Mean motion: 15
50032525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2237
Checksum: 309
Coasting Arc #4 (Orbit 2252)
---------------------------------------
Vector Time (GMT): 2014/240/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4184079
84 A = 6789216
83 meter
Y = -323822
02 meter E =
0005469
Z = 5332196
82 I = 51
97831
XDOT = 1128
308368 Wp = 76
78479
YDOT = -7570
954167 meter/sec RA = 100
97301 deg
ZDOT = 426
432595 TA = 9
17130
MA = 9
16132
Ha = 228
654 n
mi
Hp = 219
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13727296
08 X = -4206049
74
Y = -1062408
22 feet Y = -370733
41 meter
Z = 17494084
06 Z = 5311817
96
XDOT = 3701
799107 XDOT = 1210
813204
YDOT = -24839
088476 feet/sec YDOT = -7557
875339 meter/sec
ZDOT = 1399
057069 ZDOT = 432
114889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2713073
89 X = 826944
92
Y = 13609977
47 feet Y = 4148321
13 meter
Z = 17407414
78 Z = 5305780
02
XDOT = -23921
421022 XDOT = -7291
249127
YDOT = 2950
285553 feet/sec YDOT = 899
247037 meter/sec
ZDOT = 1424
453003 ZDOT = 434
173275
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 14240
41021298
00016717 00000-0 10270-3 0 9038
2 25544 51
6449 101
6121 0003506 52
9040 307
2431 15
50080358 22534
Satellite: ISS
Catalog Number: 25544
Epoch time: 14240
41021298 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 101
6121 deg
Eccentricity:
0003506
Arg of perigee: 52
9040 deg
Mean anomaly: 307
2431 deg
Mean motion: 15
50080358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2253
Checksum: 256
Coasting Arc #5 (Orbit 2267)
---------------------------------------
Vector Time (GMT): 2014/241/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4168305
99 A = 6789174
14 meter
Y = 414552
94 meter E =
0017982
Z = -5358278
98 I = 51
98380
XDOT = -787
475786 Wp = 83
42341
YDOT = 7607
964909 meter/sec RA = 96
03860 deg
ZDOT = -22
052242 TA = 186
35548
MA = 186
37832
Ha = 228
578 n
mi
Hp = 220
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13675544
57 X = 4189389
27
Y = 1360081
81 feet Y = 461282
98 meter
Z = -17579655
45 Z = -5337978
85
XDOT = -2583
581976 XDOT = -872
384153
YDOT = 24960
514792 feet/sec YDOT = 7598
684093 meter/sec
ZDOT = -72
349875 ZDOT = -26
084668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2646919
33 X = -806781
01
Y = -13597487
75 feet Y = -4144514
27 meter
Z = -17493335
09 Z = -5331968
54
XDOT = 23663
058965 XDOT = 7212
500372
YDOT = -4481
352470 feet/sec YDOT = -1365
916233 meter/sec
ZDOT = -90
743725 ZDOT = -27
658687
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 14241
37728034
00016717 00000-0 10270-3 0 9047
2 25544 51
6455 96
8202 0003633 56
3021 303
8475 15
50079657 22680
Satellite: ISS
Catalog Number: 25544
Epoch time: 14241
37728034 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 96
8202 deg
Eccentricity:
0003633
Arg of perigee: 56
3021 deg
Mean anomaly: 303
8475 deg
Mean motion: 15
50079657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2268
Checksum: 301
Coasting Arc #6 (Orbit 2283)
---------------------------------------
Vector Time (GMT): 2014/242/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4160409
96 A = 6789065
80 meter
Y = -526762
13 meter E =
0006074
Z = 5334436
29 I = 51
98618
XDOT = 456
647919 Wp = 64
24737
YDOT = -7642
591635 meter/sec RA = 91
10448 deg
ZDOT = -395
622433 TA = 29
52530
MA = 29
49101
Ha = 228
612 n
mi
Hp = 219
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13649638
97 X = -4180123
33
Y = -1728222
22 feet Y = -573396
26 meter
Z = 17501431
40 Z = 5314177
79
XDOT = 1498
188710 XDOT = 543
997005
YDOT = -25074
119537 feet/sec YDOT = -7636
996742 meter/sec
ZDOT = -1297
973860 ZDOT = -393
191242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2521572
24 X = 768575
22
Y = 13636285
52 feet Y = 4156339
83 meter
Z = 17415306
14 Z = 5308185
31
XDOT = -23358
455391 XDOT = -7119
657203
YDOT = 5974
511510 feet/sec YDOT = 1821
031108 meter/sec
ZDOT = -1286
374013 ZDOT = -392
086799
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 14242
40880122
00016717 00000-0 10270-3 0 9050
2 25544 51
6454 91
7090 0003494 58
0802 302
0688 15
50128301 22845
Satellite: ISS
Catalog Number: 25544
Epoch time: 14242
40880122 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 91
7090 deg
Eccentricity:
0003494
Arg of perigee: 58
0802 deg
Mean anomaly: 302
0688 deg
Mean motion: 15
50128301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2284
Checksum: 279
Coasting Arc #7 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2014/243/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4202109
88 A = 6789252
31 meter
Y = 635423
94 meter E =
0017534
Z = -5309666
57 I = 51
98715
XDOT = -127
044527 Wp = 89
47822
YDOT = 7604
712205 meter/sec RA = 86
17020 deg
ZDOT = 812
004661 TA = 188
25095
MA = 188
27982
Ha = 228
516 n
mi
Hp = 219
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13786449
74 X = 4220484
79
Y = 2084724
22 feet Y = 682516
97 meter
Z = -17420165
91 Z = -5289208
72
XDOT = -416
812752 XDOT = -216
017189
YDOT = 24949
843191 feet/sec YDOT = 7602
794100 meter/sec
ZDOT = 2664
057286 ZDOT = 811
170790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2461412
64 X = -750238
57
Y = -13833861
95 feet Y = -4216561
12 meter
Z = -17333209
84 Z = -5283162
36
XDOT = 22774
416813 XDOT = 6941
642245
YDOT = -7373
888727 feet/sec YDOT = -2247
561284 meter/sec
ZDOT = 2659
245869 ZDOT = 810
538141
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 14243
37583998
00016717 00000-0 10270-3 0 9069
2 25544 51
6461 86
9170 0003566 60
9910 299
1598 15
50126697 22998
Satellite: ISS
Catalog Number: 25544
Epoch time: 14243
37583998 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 86
9170 deg
Eccentricity:
0003566
Arg of perigee: 60
9910 deg
Mean anomaly: 299
1598 deg
Mean motion: 15
50126697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 351
Coasting Arc #8 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2014/244/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4254716
34 A = 6789385
41 meter
Y = -761995
65 meter E =
0007570
Z = 5230831
93 I = 51
98530
XDOT = -181
718717 Wp = 58
74296
YDOT = -7562
597664 meter/sec RA = 81
23587 deg
ZDOT = -1244
333332 TA = 43
17560
MA = 43
11627
Ha = 228
549 n
mi
Hp = 219
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13959043
12 X = -4271289
03
Y = -2499985
73 feet Y = -809666
97 meter
Z = 17161522
08 Z = 5210122
90
XDOT = -596
190015 XDOT = -91
093926
YDOT = -24811
672127 feet/sec YDOT = -7564
123128 meter/sec
ZDOT = -4082
458437 ZDOT = -1244
995488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2365143
91 X = 720895
86
Y = 14089845
45 feet Y = 4294584
89 meter
Z = 17073517
60 Z = 5204008
16
XDOT = -22155
431874 XDOT = -6752
975635
YDOT = 8688
455081 feet/sec YDOT = 2648
241109 meter/sec
ZDOT = -4084
005316 ZDOT = -1244
804820
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 14244
40733046
00016717 00000-0 10270-3 0 9076
2 25544 51
6463 81
8058 0003458 62
6396 297
5106 15
50177727 23152
Satellite: ISS
Catalog Number: 25544
Epoch time: 14244
40733046 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 81
8058 deg
Eccentricity:
0003458
Arg of perigee: 62
6396 deg
Mean anomaly: 297
5106 deg
Mean motion: 15
50177727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 312
Coasting Arc #9 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2014/245/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4355873
20 A = 6789814
81 meter
Y = 868906
18 meter E =
0016306
Z = -5149821
66 I = 51
98127
XDOT = 477
223808 Wp = 95
03729
YDOT = 7451
265881 meter/sec RA = 76
30121 deg
ZDOT = 1664
009219 TA = 190
97335
MA = 191
00897
Ha = 228
441 n
mi
Hp = 219
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14290922
56 X = 4370849
30
Y = 2850742
05 feet Y = 917699
84 meter
Z = -16895740
36 Z = -5128625
13
XDOT = 1565
694909 XDOT = 385
783354
YDOT = 24446
410371 feet/sec YDOT = 7456
091319 meter/sec
ZDOT = 5459
347833 ZDOT = 1666
105016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2394885
12 X = -729960
99
Y = -14479535
35 feet Y = -4413362
37 meter
Z = -16805678
25 Z = -5122370
73
XDOT = 21291
499645 XDOT = 6489
649092
YDOT = -9854
823077 feet/sec YDOT = -3003
750074 meter/sec
ZDOT = 5467
000543 ZDOT = 1666
341765
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 14245
37434033
00016717 00000-0 10270-3 0 9088
2 25544 51
6466 77
0138 0003477 65
3190 294
8323 15
50173635 23306
Satellite: ISS
Catalog Number: 25544
Epoch time: 14245
37434033 = yrday
fracday
Element set: 908
Inclination: 51
6466 deg
RA of node: 77
0138 deg
Eccentricity:
0003477
Arg of perigee: 65
3190 deg
Mean anomaly: 294
8323 deg
Mean motion: 15
50173635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 298
Coasting Arc #10 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2014/246/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4468474
01 A = 6790198
53 meter
Y = -989601
52 meter E =
0009531
Z = 5010366
93 I = 51
97502
XDOT = -739
701522 Wp = 60
33584
YDOT = -7335
729144 meter/sec RA = 71
36633 deg
ZDOT = -2101
001821 TA = 50
06464
MA = 49
98094
Ha = 228
470 n
mi
Hp = 219
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14660347
82 X = -4481414
61
Y = -3246724
16 feet Y = -1039643
02 meter
Z = 16438211
72 Z = 4988628
42
XDOT = -2426
842265 XDOT = -647
410782
YDOT = -24067
352835 feet/sec YDOT = -7343
485030 meter/sec
ZDOT = -6893
050594 ZDOT = -2104
370680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2410081
73 X = 734592
91
Y = 14922671
21 feet Y = 4548430
18 meter
Z = 16345862
18 Z = 4982218
79
XDOT = -20417
676061 XDOT = -6223
307663
YDOT = 10889
731489 feet/sec YDOT = 3319
190158 meter/sec
ZDOT = -6906
128946 ZDOT = -2104
988103
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 14246
40579983
00016717 00000-0 10270-3 0 9098
2 25544 51
6468 71
9025 0003402 66
8535 293
2974 15
50227060 23467
Satellite: ISS
Catalog Number: 25544
Epoch time: 14246
40579983 = yrday
fracday
Element set: 909
Inclination: 51
6468 deg
RA of node: 71
9025 deg
Eccentricity:
0003402
Arg of perigee: 66
8535 deg
Mean anomaly: 293
2974 deg
Mean motion: 15
50227060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 319
Coasting Arc #11 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2014/247/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4624206
85 A = 6790857
61 meter
Y = 1075018
44 meter E =
0014373
Z = -4868753
75 I = 51
96575
XDOT = 978
019631 Wp = 99
38293
YDOT = 7159
512014 meter/sec RA = 66
43048 deg
ZDOT = 2513
757990 TA = 195
25001
MA = 195
29338
Ha = 228
363 n
mi
Hp = 219
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15171282
33 X = 4635492
73
Y = 3526963
37 feet Y = 1126792
19 meter
Z = -15973601
55 Z = -4846262
81
XDOT = 3208
725825 XDOT = 885
676694
YDOT = 23489
212645 feet/sec YDOT = 7169
932657 meter/sec
ZDOT = 8247
237500 ZDOT = 2518
284416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2602453
69 X = -793227
88
Y = -15455664
93 feet Y = -4710886
67 meter
Z = -15878062
89 Z = -4839633
57
XDOT = 19354
823487 XDOT = 5899
350199
YDOT = -11736
434430 feet/sec YDOT = -3577
265214 meter/sec
ZDOT = 8265
263514 ZDOT = 2519
252319
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 14247
37278022
00016717 00000-0 10270-3 0 9107
2 25544 51
6462 67
1100 0003388 69
8781 290
2734 15
50220451 23616
Satellite: ISS
Catalog Number: 25544
Epoch time: 14247
37278022 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 67
1100 deg
Eccentricity:
0003388
Arg of perigee: 69
8781 deg
Mean anomaly: 290
2734 deg
Mean motion: 15
50220451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 287
Coasting Arc #12 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2014/248/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4789028
96 A = 6791476
35 meter
Y = -1170232
92 meter E =
0011614
Z = 4664214
11 I = 51
95513
XDOT = -1170
571434 Wp = 66
55027
YDOT = -6981
495944 meter/sec RA = 61
49440 deg
ZDOT = -2943
229912 TA = 52
67829
MA = 52
57251
Ha = 228
378 n
mi
Hp = 219
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15712037
26 X = -4798244
22
Y = -3839346
84 feet Y = -1223838
19 meter
Z = 15302539
72 Z = 4640927
62
XDOT = -3840
457462 XDOT = -1078
118630
YDOT = -22905
170420 feet/sec YDOT = -6994
069266 meter/sec
ZDOT = -9656
266114 ZDOT = -2948
691361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2795799
97 X = 852159
83
Y = 16025278
25 feet Y = 4884504
81 meter
Z = 15203630
50 Z = 4634066
58
XDOT = -18321
004894 XDOT = -5584
242292
YDOT = 12410
643235 feet/sec YDOT = 3782
764058 meter/sec
ZDOT = -9678
296071 ZDOT = -2949
944643
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 14248
40420781
00016717 00000-0 10270-3 0 9114
2 25544 51
6463 61
9983 0003324 71
1524 288
9987 15
50275131 23775
Satellite: ISS
Catalog Number: 25544
Epoch time: 14248
40420781 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 61
9983 deg
Eccentricity:
0003324
Arg of perigee: 71
1524 deg
Mean anomaly: 288
9987 deg
Mean motion: 15
50275131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 313
Coasting Arc #13 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2014/249/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4987418
70 A = 6792321
92 meter
Y = 1216617
63 meter E =
0011932
Z = -4459015
37 I = 51
94097
XDOT = 1330
840374 Wp = 101
01038
YDOT = 6756
197041 meter/sec RA = 56
55671 deg
ZDOT = 3337
295323 TA = 202
59826
MA = 202
65085
Ha = 228
289 n
mi
Hp = 219
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16362922
24 X = 4995103
70
Y = 3991527
65 feet Y = 1272432
79 meter
Z = -14629315
51 Z = -4434768
94
XDOT = 4366
274192 XDOT = 1238
980815
YDOT = 22166
000791 feet/sec YDOT = 6770
566002 meter/sec
ZDOT = 10949
131637 ZDOT = 3343
536629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3200991
20 X = -975662
12
Y = -16626298
96 feet Y = -5067695
92 meter
Z = -14526328
78 Z = -4427625
01
XDOT = 17170
037572 XDOT = 5233
427452
YDOT = -12878
601016 feet/sec YDOT = -3925
397590 meter/sec
ZDOT = 10974
515653 ZDOT = 3345
032371
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 14249
37115785
00016717 00000-0 10270-3 0 9127
2 25544 51
6451 57
2050 0003312 75
0745 285
0772 15
50267218 23924
Satellite: ISS
Catalog Number: 25544
Epoch time: 14249
37115785 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 57
2050 deg
Eccentricity:
0003312
Arg of perigee: 75
0745 deg
Mean anomaly: 285
0772 deg
Mean motion: 15
50267218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 295
Coasting Arc #14 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2014/250/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5189459
88 A = 6793125
53 meter
Y = -1269758
70 meter E =
0013580
Z = 4186655
12 I = 51
92648
XDOT = -1433
222816 Wp = 75
52228
YDOT = -6534
198374 meter/sec RA = 51
61896 deg
ZDOT = -3744
802950 TA = 52
89243
MA = 52
76841
Ha = 228
272 n
mi
Hp = 219
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17025786
99 X = -5195212
61
Y = -4165875
01 feet Y = -1327822
34 meter
Z = 13735745
14 Z = 4161431
95
XDOT = -4702
174592 XDOT = -1341
858574
YDOT = -21437
658706 feet/sec YDOT = -6549
715133 meter/sec
ZDOT = -12286
098917 ZDOT = -3751
542669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3612187
81 X = 1100994
84
Y = 17237042
92 feet Y = 5253850
68 meter
Z = 13628612
64 Z = 4154001
13
XDOT = -16098
971427 XDOT = -4906
966491
YDOT = 13144
739348 feet/sec YDOT = 4006
516553 meter/sec
ZDOT = -12313
639415 ZDOT = -3753
197294
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 14250
40255250
00016717 00000-0 10270-3 0 9136
2 25544 51
6454 52
0928 0003228 75
9289 284
2220 15
50322155 24081
Satellite: ISS
Catalog Number: 25544
Epoch time: 14250
40255250 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 52
0928 deg
Eccentricity:
0003228
Arg of perigee: 75
9289 deg
Mean anomaly: 284
2220 deg
Mean motion: 15
50322155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2408
Checksum: 281
Coasting Arc #15 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2014/251/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5412116
67 A = 6794085
31 meter
Y = 1264000
87 meter E =
0009434
Z = -3916785
49 I = 51
90823
XDOT = 1499
516798 Wp = 96
79500
YDOT = 6282
169151 meter/sec RA = 46
67931 deg
ZDOT = 4106
738263 TA = 216
15501
MA = 216
21883
Ha = 228
219 n
mi
Hp = 219
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17756288
30 X = 5416606
36
Y = 4146984
49 feet Y = 1324547
28 meter
Z = -12850346
11 Z = -3890483
74
XDOT = 4919
674533 XDOT = 1409
207687
YDOT = 20610
791177 feet/sec YDOT = 6298
433277 meter/sec
ZDOT = 13473
550731 ZDOT = 4113
802496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4248443
08 X = -1294925
45
Y = -17812713
71 feet Y = -5429315
14 meter
Z = -12738626
74 Z = -3882733
43
XDOT = 14990
174124 XDOT = 4569
005073
YDOT = -13213
953221 feet/sec YDOT = -4027
612942 meter/sec
ZDOT = 13502
512258 ZDOT = 4115
565736
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 14251
36947142
00016717 00000-0 10270-3 0 9141
2 25544 51
6441 47
2990 0003263 81
0474 279
1046 15
50314307 24231
Satellite: ISS
Catalog Number: 25544
Epoch time: 14251
36947142 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 47
2990 deg
Eccentricity:
0003263
Arg of perigee: 81
0474 deg
Mean anomaly: 279
1046 deg
Mean motion: 15
50314307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 286
Coasting Arc #16 (Orbit 2438)
---------------------------------------
Vector Time (GMT): 2014/252/08:39:58
233
Vector Time (MET): N/A
Weight (LBS) : 928846
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5630072
61 A = 6794983
10 meter
Y = -1263928
65 meter E =
0015241
Z = 3576252
06 I = 51
89035
XDOT = -1497
834353 Wp = 86
09395
YDOT = -6041
214299 meter/sec RA = 41
73993 deg
ZDOT = -4475
702210 TA = 51
87553
MA = 51
73823
Ha = 228
158 n
mi
Hp = 219
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18471366
85 X = -5632892
81
Y = -4146747
54 feet Y = -1326903
05 meter
Z = 11733110
44 Z = 3548895
47
XDOT = -4914
154702 XDOT = -1408
427395
YDOT = -19820
256888 feet/sec YDOT = -6057
464758 meter/sec
ZDOT = -14684
062369 ZDOT = -4482
760446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4881114
56 X = 1487763
72
Y = 18365046
58 feet Y = 5597666
20 meter
Z = 11616908
96 Z = 3540833
85
XDOT = -14019
712014 XDOT = -4273
208222
YDOT = 13069
546880 feet/sec YDOT = 3983
597889 meter/sec
ZDOT = -14713
034853 ZDOT = -4484
533023
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 14252
40083224
00016717 00000-0 10270-3 0 9150
2 25544 51
6447 42
1866 0003139 81
4806 278
6700 15
50369890 24393
Satellite: ISS
Catalog Number: 25544
Epoch time: 14252
40083224 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 42
1866 deg
Eccentricity:
0003139
Arg of perigee: 81
4806 deg
Mean anomaly: 278
6700 deg
Mean motion: 15
50369890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2439
Checksum: 307
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