[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 16th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16684 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
202/21:41:30
000 0
0 0
0 0
0
N/A 0
0 0
0 225
3
000/00:00:00
000 0
0 0
0 222
9
205/03:28:03
000 0
0 0
0 0
0
N/A 0
0 0
0 225
7
000/00:00:00
000 0
0 0
0 222
8
Coasting Arc #1 (Orbit 1590)
---------------------------------------
Vector Time (GMT): 2014/197/16:24:19
926
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5222794
44 A = 6793123
18 meter
Y = -582923
82 meter E =
0005451
Z = 4303907
12 I = 51
37869
XDOT = -2167
809508 Wp = 137
91870
YDOT = 6460
711803 meter/sec RA = 312
76646 deg
ZDOT = 3499
130016 TA = 276
27270
MA = 276
33480
Ha = 225
400 n
mi
Hp = 223
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17135152
35 X = 5208017
96
Y = -1912479
73 feet Y = -524601
98 meter
Z = 14120430
19 Z = 4329242
44
XDOT = -7112
235918 XDOT = -2256
890953
YDOT = 21196
561035 feet/sec YDOT = 6435
971723 meter/sec
ZDOT = 11480
085355 ZDOT = 3488
383171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17056309
89 X = -5198763
25
Y = 1817516
69 feet Y = 553979
09 meter
Z = 14228018
12 Z = 4336699
92
XDOT = 7433
175550 XDOT = 2265
631908
YDOT = -19913
997972 feet/sec YDOT = -6069
786582 meter/sec
ZDOT = 11433
291160 ZDOT = 3484
867146
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 14197
73827363
00016717 00000-0 10270-3 0 9008
2 25544 51
6466 313
1010 0005669 259
3506 100
7006 15
50102751 15912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14197
73827363 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 313
1010 deg
Eccentricity:
0005669
Arg of perigee: 259
3506 deg
Mean anomaly: 100
7006 deg
Mean motion: 15
50102751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1591
Checksum: 284
Coasting Arc #2 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2014/198/16:24:19
926
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5039896
82 A = 6792312
50 meter
Y = 604614
35 meter E =
0004557
Z = -4517878
34 I = 51
35592
XDOT = 2011
319292 Wp = 52
41468
YDOT = -6688
548403 meter/sec RA = 307
79130 deg
ZDOT = -3138
283430 TA = 185
93097
MA = 185
93637
Ha = 225
311 n
mi
Hp = 222
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16535094
55 X = -5024337
01
Y = 1983642
89 feet Y = 548342
18 meter
Z = -14822435
50 Z = -4542323
37
XDOT = 6598
816576 XDOT = 2101
207293
YDOT = -21944
056439 feet/sec YDOT = -6665
553805 meter/sec
ZDOT = -10296
205478 ZDOT = -3128
294792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16417271
49 X = 5003984
35
Y = -2174660
42 feet Y = -662836
50 meter
Z = -14926246
47 Z = -4549519
92
XDOT = -6564
634910 XDOT = -2000
900721
YDOT = 20824
290670 feet/sec YDOT = 6347
243796 meter/sec
ZDOT = -10252
595570 ZDOT = -3124
991130
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 14198
70531027
00016717 00000-0 10270-3 0 9016
2 25544 51
6470 308
3094 0005603 263
5757 96
4756 15
50109217 16062
Satellite: ISS
Catalog Number: 25544
Epoch time: 14198
70531027 = yrday
fracday
Element set: 901
Inclination: 51
6470 deg
RA of node: 308
3094 deg
Eccentricity:
0005603
Arg of perigee: 263
5757 deg
Mean anomaly: 96
4756 deg
Mean motion: 15
50109217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 302
Coasting Arc #3 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2014/199/16:24:19
926
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4863189
02 A = 6791488
80 meter
Y = -597418
68 meter E =
0003985
Z = 4703268
81 I = 51
33416
XDOT = -1825
869569 Wp = 158
65257
YDOT = 6908
592465 meter/sec RA = 302
81426 deg
ZDOT = 2761
113343 TA = 263
83371
MA = 263
87911
Ha = 225
132 n
mi
Hp = 222
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15955344
55 X = 4846661
26
Y = -1960035
05 feet Y = -543128
02 meter
Z = 15430671
96 Z = 4726853
14
XDOT = -5990
385724 XDOT = -1916
399822
YDOT = 22665
985778 feet/sec YDOT = 6887
668091 meter/sec
ZDOT = 9058
770809 ZDOT = 2752
024057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15794799
21 X = -4814254
80
Y = 2416218
09 feet Y = 736463
27 meter
Z = 15530827
49 Z = 4733796
22
XDOT = 5565
701833 XDOT = 1696
425919
YDOT = -21680
325460 feet/sec YDOT = -6608
163200 meter/sec
ZDOT = 9018
944005 ZDOT = 2748
974133
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 14199
73680062
00016717 00000-0 10270-3 0 9025
2 25544 51
6460 303
1981 0005497 268
5726 91
4795 15
50141235 16223
Satellite: ISS
Catalog Number: 25544
Epoch time: 14199
73680062 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 303
1981 deg
Eccentricity:
0005497
Arg of perigee: 268
5726 deg
Mean anomaly: 91
4795 deg
Mean motion: 15
50141235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 312
Coasting Arc #4 (Orbit 1636)
---------------------------------------
Vector Time (GMT): 2014/200/16:24:19
926
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4702800
42 A = 6790776
91 meter
Y = 547526
21 meter E =
0007015
Z = -4874670
00 I = 51
31681
XDOT = 1616
856704 Wp = 57
50153
YDOT = -7102
756625 meter/sec RA = 297
83527 deg
ZDOT = -2356
429522 TA = 189
27063
MA = 189
28359
Ha = 225
237 n
mi
Hp = 222
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15429135
24 X = -4684894
03
Y = 1796345
84 feet Y = 495036
90 meter
Z = -15993011
81 Z = -4897471
87
XDOT = 5304
647979 XDOT = 1707
607890
YDOT = -23303
007299 feet/sec YDOT = -7084
168325 meter/sec
ZDOT = -7731
067986 ZDOT = -2348
355128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15229273
83 X = 4641882
66
Y = -2499568
39 feet Y = -761868
44 meter
Z = -16089837
66 Z = -4904182
52
XDOT = -4455
551964 XDOT = -1358
052239
YDOT = 22415
129034 feet/sec YDOT = 6832
131329 meter/sec
ZDOT = -7695
518235 ZDOT = -2345
593958
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 14200
70381061
00016717 00000-0 10270-3 0 9033
2 25544 51
6471 298
4063 0005543 272
6429 87
4087 15
50152102 16370
Satellite: ISS
Catalog Number: 25544
Epoch time: 14200
70381061 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 298
4063 deg
Eccentricity:
0005543
Arg of perigee: 272
6429 deg
Mean anomaly: 87
4087 deg
Mean motion: 15
50152102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1637
Checksum: 287
Coasting Arc #5 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2014/201/16:24:19
926
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4556294
54 A = 6790100
86 meter
Y = -467660
71 meter E =
0002560
Z = 5013959
47 I = 51
29981
XDOT = -1385
671021 Wp = 194
07601
YDOT = 7281
363347 meter/sec RA = 292
85440 deg
ZDOT = 1936
106729 TA = 237
01659
MA = 237
04119
Ha = 225
169 n
mi
Hp = 222
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14948472
90 X = 4536829
35
Y = -1534319
91 feet Y = -416818
51 meter
Z = 16449998
26 Z = 5036045
85
XDOT = -4546
164767 XDOT = -1476
394830
YDOT = 23888
987359 feet/sec YDOT = 7265
360469 meter/sec
ZDOT = 6352
056199 ZDOT = 1929
155567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14718044
89 X = -4486060
08
Y = 2469026
50 feet Y = 752559
28 meter
Z = 16543774
81 Z = 5042542
56
XDOT = 3245
354504 XDOT = 989
184053
YDOT = -23058
582615 feet/sec YDOT = -7028
255981 meter/sec
ZDOT = 6321
245884 ZDOT = 1926
715746
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 14201
73527385
00016717 00000-0 10270-3 0 9049
2 25544 51
6458 293
2946 0005421 277
8065 82
2470 15
50179641 16530
Satellite: ISS
Catalog Number: 25544
Epoch time: 14201
73527385 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 293
2946 deg
Eccentricity:
0005421
Arg of perigee: 277
8065 deg
Mean anomaly: 82
2470 deg
Mean motion: 15
50179641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 313
Coasting Arc #6 (Orbit 1667)
---------------------------------------
Vector Time (GMT): 2014/202/16:24:19
926
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4438161
69 A = 6789576
45 meter
Y = 356396
80 meter E =
0008853
Z = -5133633
44 I = 51
28789
XDOT = 1134
714321 Wp = 64
46705
YDOT = -7421
900597 meter/sec RA = 287
87279 deg
ZDOT = -1494
529186 TA = 191
03436
MA = 191
05379
Ha = 225
386 n
mi
Hp = 222
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14560897
92 X = -4416879
80
Y = 1169280
83 feet Y = 306885
85 meter
Z = -16842629
39 Z = -5155141
51
XDOT = 3722
816014 XDOT = 1224
883262
YDOT = -24350
067577 feet/sec YDOT = -7408
707198 meter/sec
ZDOT = -4903
310978 ZDOT = -1488
798577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14313981
72 X = 4362901
63
Y = -2326568
60 feet Y = -709138
11 meter
Z = -16933934
47 Z = -5161463
23
XDOT = -1952
598455 XDOT = -595
152009
YDOT = 23529
713013 feet/sec YDOT = 7171
856527 meter/sec
ZDOT = -4877
660811 ZDOT = -1486
711015
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 14202
70225816
00016717 00000-0 10270-3 0 9052
2 25544 51
6468 288
5031 0005547 281
6429 78
4099 15
50190215 16689
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
70225816 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 288
5031 deg
Eccentricity:
0005547
Arg of perigee: 281
6429 deg
Mean anomaly: 78
4099 deg
Mean motion: 15
50190215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1668
Checksum: 315
Coasting Arc #7 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2014/202/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4274312
24 A = 6794611
48 meter
Y = -3684072
40 meter E =
0005793
Z = 3779781
17 I = 51
30197
XDOT = 1635
292081 Wp = 90
43030
YDOT = 6202
808295 meter/sec RA = 286
78925 deg
ZDOT = 4190
866517 TA = 315
05520
MA = 315
10208
Ha = 225
277 n
mi
Hp = 222
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14023334
13 X = 4296829
90
Y = -12086851
71 feet Y = -3636148
72 meter
Z = 12400856
85 Z = 3800599
37
XDOT = 5365
131498 XDOT = 1545
451611
YDOT = 20350
420915 feet/sec YDOT = 6220
592486 meter/sec
ZDOT = 13749
562063 ZDOT = 4198
592803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10594140
04 X = 3229093
88
Y = 15109445
16 feet Y = 4605358
89 meter
Z = 12489835
81 Z = 3806901
96
XDOT = -19683
406120 XDOT = -5999
502186
YDOT = 2394
161044 feet/sec YDOT = 729
740286 meter/sec
ZDOT = 13781
220280 ZDOT = 4200
515941
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 14202
96011888
00016717 00000-0 10270-3 0 9063
2 25544 51
6459 287
2251 0005735 284
0606 75
9907 15
50215380 16728
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
96011888 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 287
2251 deg
Eccentricity:
0005735
Arg of perigee: 284
0606 deg
Mean anomaly: 75
9907 deg
Mean motion: 15
50215380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1672
Checksum: 315
Coasting Arc #8 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2014/203/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4080938
53 A = 6793623
71 meter
Y = 3609699
82 meter E =
0004507
Z = -4062656
54 I = 51
29109
XDOT = -1811
224666 Wp = 19
49985
YDOT = -6372
222981 meter/sec RA = 281
80903 deg
ZDOT = -3839
460006 TA = 210
50110
MA = 210
52732
Ha = 225
627 n
mi
Hp = 222
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13388905
95 X = -4101264
86
Y = 11842847
18 feet Y = 3563950
87 meter
Z = -13328925
64 Z = -4082529
97
XDOT = -5942
338144 XDOT = -1721
183746
YDOT = -20906
243376 feet/sec YDOT = -6391
973455 meter/sec
ZDOT = -12596
653564 ZDOT = -3848
040478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10663879
02 X = -3250350
33
Y = -14266238
11 feet Y = -4348349
38 meter
Z = -13413881
80 Z = -4088551
17
XDOT = 20290
885121 XDOT = 6184
661785
YDOT = -3281
057134 feet/sec YDOT = -1000
066214 meter/sec
ZDOT = -12631
915517 ZDOT = -3850
207850
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 14203
92708858
00016717 00000-0 10270-3 0 9071
2 25544 51
6462 282
4330 0005738 289
5307 70
5223 15
50235157 16870
Satellite: ISS
Catalog Number: 25544
Epoch time: 14203
92708858 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 282
4330 deg
Eccentricity:
0005738
Arg of perigee: 289
5307 deg
Mean anomaly: 70
5223 deg
Mean motion: 15
50235157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1687
Checksum: 315
Coasting Arc #9 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2014/204/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3904267
83 A = 6792662
16 meter
Y = -3498055
18 meter E =
0003928
Z = 4316938
75 I = 51
28250
XDOT = 2015
650435 Wp = 101
82769
YDOT = 6530
174525 meter/sec RA = 276
82816 deg
ZDOT = 3465
016389 TA = 312
73485
MA = 312
76790
Ha = 225
593 n
mi
Hp = 222
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12809277
66 X = 3922123
71
Y = -11476558
98 feet Y = -3454295
70 meter
Z = 14163184
86 Z = 4335947
90
XDOT = 6613
026360 XDOT = 1925
647029
YDOT = 21424
457103 feet/sec YDOT = 6552
211267 meter/sec
ZDOT = 11368
164005 ZDOT = 3474
589991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10582036
10 X = 3225404
60
Y = 13472226
29 feet Y = 4106334
57 meter
Z = 14244452
82 Z = 4341709
22
XDOT = -20838
934512 XDOT = -6351
707239
YDOT = 4294
869099 feet/sec YDOT = 1309
076101 meter/sec
ZDOT = 11407
624044 ZDOT = 3477
043809
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 14204
95850887
00016717 00000-0 10270-3 0 9086
2 25544 51
6462 277
3219 0005763 292
6936 67
3606 15
50252237 17036
Satellite: ISS
Catalog Number: 25544
Epoch time: 14204
95850887 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 277
3219 deg
Eccentricity:
0005763
Arg of perigee: 292
6936 deg
Mean anomaly: 67
3606 deg
Mean motion: 15
50252237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1703
Checksum: 326
Coasting Arc #10 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2014/205/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2304942
87 A = 6795378
69 meter
Y = -5341221
49 meter E =
0001915
Z = -3510066
76 I = 51
28901
XDOT = 4066
445171 Wp = 349
29979
YDOT = -4697
956445 meter/sec RA = 275
57800 deg
ZDOT = 4479
970945 TA = 329
24206
MA = 329
25328
Ha = 225
665 n
mi
Hp = 222
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7562148
52 X = -2227994
28
Y = -17523692
54 feet Y = -5366566
28 meter
Z = -11515967
07 Z = -3521077
27
XDOT = 13341
355547 XDOT = 4096
914640
YDOT = -15413
242930 feet/sec YDOT = -4652
312881 meter/sec
ZDOT = 14698
067404 ZDOT = 4499
798445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5287867
85 X = -1611742
12
Y = -18309780
95 feet Y = -5580821
23 meter
Z = -11561737
03 Z = -3524017
45
XDOT = 13700
602084 XDOT = 4175
943515
YDOT = -13288
499066 feet/sec YDOT = -4050
334515 meter/sec
ZDOT = 14783
018802 ZDOT = 4505
864131
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 14205
15189715
00016717 00000-0 10270-3 0 9095
2 25544 51
6446 276
3615 0005919 292
7338 67
3187 15
50252266 17066
Satellite: ISS
Catalog Number: 25544
Epoch time: 14205
15189715 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 276
3615 deg
Eccentricity:
0005919
Arg of perigee: 292
7338 deg
Mean anomaly: 67
3187 deg
Mean motion: 15
50252266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 325
Coasting Arc #11 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2014/206/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2482731
45 A = 6796202
20 meter
Y = 5473119
88 meter E =
0007599
Z = 3169033
91 I = 51
29029
XDOT = -3886
329694 Wp = 75
51671
YDOT = 4542
984015 meter/sec RA = 270
59840 deg
ZDOT = -4789
782486 TA = 67
77527
MA = 67
69468
Ha = 225
881 n
mi
Hp = 222
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8145444
38 X = 2405951
37
Y = 17956430
06 feet Y = 5500453
82 meter
Z = 10397092
88 Z = 3180908
42
XDOT = -12750
425505 XDOT = -3913
574733
YDOT = 14904
803199 feet/sec YDOT = 4499
372636 meter/sec
ZDOT = -15714
509467 ZDOT = -4808
727191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6143499
20 X = 1872538
56
Y = 18708523
29 feet Y = 5702357
90 meter
Z = 10446518
99 Z = 3184098
99
XDOT = -12786
532138 XDOT = -3897
334996
YDOT = 13039
934619 feet/sec YDOT = 3974
572072 meter/sec
ZDOT = -15795
683789 ZDOT = -4814
524419
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 14206
18330063
00016717 00000-0 10270-3 0 9105
2 25544 51
6448 271
2502 0006119 297
2839 62
7688 15
50300936 17227
Satellite: ISS
Catalog Number: 25544
Epoch time: 14206
18330063 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 271
2502 deg
Eccentricity:
0006119
Arg of perigee: 297
2839 deg
Mean anomaly: 62
7688 deg
Mean motion: 15
50300936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 296
Coasting Arc #12 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2014/207/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2689990
84 A = 6797132
18 meter
Y = -5566801
59 meter E =
0005265
Z = -2816115
46 I = 51
29233
XDOT = 3737
059061 Wp = 349
69275
YDOT = -4366
810587 meter/sec RA = 265
61762 deg
ZDOT = 5066
083528 TA = 338
22139
MA = 338
24377
Ha = 225
938 n
mi
Hp = 222
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8825429
28 X = -2613862
16
Y = -18263784
75 feet Y = -5596456
94 meter
Z = -9239223
96 Z = -2828998
29
XDOT = 12260
692458 XDOT = 3761
003074
YDOT = -14326
806388 feet/sec YDOT = -4324
886865 meter/sec
ZDOT = 16621
008950 ZDOT = 5084
295125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7121868
76 X = -2170745
60
Y = -18966754
70 feet Y = -5781066
83 meter
Z = -9292927
21 Z = -2832484
21
XDOT = 11989
108273 XDOT = 3654
280202
YDOT = -12677
888507 feet/sec YDOT = -3864
220417 meter/sec
ZDOT = 16699
037088 ZDOT = 5089
866504
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 14207
15023227
00016717 00000-0 10270-3 0 9115
2 25544 51
6432 266
4567 0005846 300
2258 59
8314 15
50286448 17373
Satellite: ISS
Catalog Number: 25544
Epoch time: 14207
15023227 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 266
4567 deg
Eccentricity:
0005846
Arg of perigee: 300
2258 deg
Mean anomaly: 59
8314 deg
Mean motion: 15
50286448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 302
Coasting Arc #13 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2014/208/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2898342
87 A = 6797859
51 meter
Y = 5648419
66 meter E =
0008218
Z = 2422621
30 I = 51
29846
XDOT = -3632
459672 Wp = 91
73077
YDOT = 4150
606116 meter/sec RA = 260
63888 deg
ZDOT = -5316
068195 TA = 61
08603
MA = 61
00362
Ha = 226
148 n
mi
Hp = 222
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9508998
91 X = 2823197
47
Y = 18531560
58 feet Y = 5680410
50 meter
Z = 7948232
61 Z = 2436518
54
XDOT = -11917
518608 XDOT = -3652
779517
YDOT = 13617
474134 feet/sec YDOT = 4109
872293 meter/sec
ZDOT = -17441
168618 ZDOT = -5333
762929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8117970
70 X = 2474357
47
Y = 19157579
01 feet Y = 5839230
08 meter
Z = 8006242
41 Z = 2440302
69
XDOT = -11348
344332 XDOT = -3458
975352
YDOT = 12150
464009 feet/sec YDOT = 3703
461430 meter/sec
ZDOT = -17516
961155 ZDOT = -5339
169760
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 14208
18161030
00016717 00000-0 10270-3 0 9125
2 25544 51
6432 261
3449 0006072 304
6849 55
3729 15
50337668 17532
Satellite: ISS
Catalog Number: 25544
Epoch time: 14208
18161030 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 261
3449 deg
Eccentricity:
0006072
Arg of perigee: 304
6849 deg
Mean anomaly: 55
3729 deg
Mean motion: 15
50337668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 301
Coasting Arc #14 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2014/209/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3125714
19 A = 6798653
83 meter
Y = -5681727
83 meter E =
0008538
Z = -2023842
83 I = 51
30615
XDOT = 3566
541857 Wp = 358
62519
YDOT = -3928
658688 meter/sec RA = 255
65950 deg
ZDOT = 5528
858800 TA = 338
93544
MA = 338
97058
Ha = 226
191 n
mi
Hp = 222
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10254967
80 X = -3052116
52
Y = -18640839
32 feet Y = -5716269
99 meter
Z = -6639904
30 Z = -2038848
26
XDOT = 11701
252812 XDOT = 3583
351085
YDOT = -12889
300158 feet/sec YDOT = -3888
681551 meter/sec
ZDOT = 18139
300526 ZDOT = 5546
224873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9193505
84 X = -2802180
58
Y = -19164754
62 feet Y = -5841417
21 meter
Z = -6702627
49 Z = -2042960
86
XDOT = 10867
165863 XDOT = 3312
312155
YDOT = -11574
105096 feet/sec YDOT = -3527
787233 meter/sec
ZDOT = 18213
655554 ZDOT = 5551
522213
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 14209
14851855
00016717 00000-0 10270-3 0 9134
2 25544 51
6424 256
5513 0005731 307
9248 52
1384 15
50321751 17685
Satellite: ISS
Catalog Number: 25544
Epoch time: 14209
14851855 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 256
5513 deg
Eccentricity:
0005731
Arg of perigee: 307
9248 deg
Mean anomaly: 52
1384 deg
Mean motion: 15
50321751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 303
Coasting Arc #15 (Orbit 1783)
---------------------------------------
Vector Time (GMT): 2014/210/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3343516
34 A = 6799174
11 meter
Y = 5700280
61 meter E =
0008291
Z = 1585621
65 I = 51
31666
XDOT = -3551
642565 Wp = 106
04270
YDOT = 3676
494398 meter/sec RA = 250
68212 deg
ZDOT = -5705
061729 TA = 56
56655
MA = 56
48729
Ha = 226
390 n
mi
Hp = 222
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10969541
81 X = 3271823
71
Y = 18701708
04 feet Y = 5737269
07 meter
Z = 5202170
78 Z = 1601689
67
XDOT = -11652
370619 XDOT = -3564
777188
YDOT = 12061
989494 feet/sec YDOT = 3636
704335 meter/sec
ZDOT = -18717
394125 ZDOT = -5722
346588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10242687
49 X = 3121971
15
Y = 19091042
82 feet Y = 5818949
85 meter
Z = 5269416
36 Z = 1606118
11
XDOT = -10577
247808 XDOT = -3223
945132
YDOT = 10881
882756 feet/sec YDOT = 3316
797864 meter/sec
ZDOT = -18791
357656 ZDOT = -5727
605814
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 14210
17987155
00016717 00000-0 10270-3 0 9143
2 25544 51
6420 251
4389 0005959 312
3830 47
6816 15
50374732 17849
Satellite: ISS
Catalog Number: 25544
Epoch time: 14210
17987155 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 251
4389 deg
Eccentricity:
0005959
Arg of perigee: 312
3830 deg
Mean anomaly: 47
6816 deg
Mean motion: 15
50374732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1784
Checksum: 316
Coasting Arc #16 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2014/211/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3566931
39 A = 6799725
08 meter
Y = -5665050
62 meter E =
0011442
Z = -1149872
22 I = 51
32988
XDOT = 3579
064887 Wp = 9
19722
YDOT = -3435
481154 meter/sec RA = 245
70496 deg
ZDOT = 5842
315285 TA = 338
28030
MA = 338
32879
Ha = 226
427 n
mi
Hp = 221
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11702530
80 X = -3497732
78
Y = -18586124
07 feet Y = -5704551
42 meter
Z = -3772546
64 Z = -1167031
55
XDOT = 11742
338869 XDOT = 3588
835625
YDOT = -11271
263629 feet/sec YDOT = -3395
403168 meter/sec
ZDOT = 19167
701065 ZDOT = 5859
725274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11313644
57 X = -3448398
87
Y = -18810822
24 feet Y = -5733538
62 meter
Z = -3844444
87 Z = -1171786
80
XDOT = 10467
564135 XDOT = 3190
513548
YDOT = -10215
644291 feet/sec YDOT = -3113
728380 meter/sec
ZDOT = 19242
152137 ZDOT = 5865
007971
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 14211
14675631
00016717 00000-0 10270-3 0 9155
2 25544 51
6424 246
6455 0005612 315
8493 44
2210 15
50360287 17999
Satellite: ISS
Catalog Number: 25544
Epoch time: 14211
14675631 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 246
6455 deg
Eccentricity:
0005612
Arg of perigee: 315
8493 deg
Mean anomaly: 44
2210 deg
Mean motion: 15
50360287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 298
Coasting Arc #17 (Orbit 1814)
---------------------------------------
Vector Time (GMT): 2014/212/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3768898
76 A = 6799950
78 meter
Y = 5615579
91 meter E =
0007619
Z = 677655
52 I = 51
34428
XDOT = -3658
696812 Wp = 117
99818
YDOT = 3177
145147 meter/sec RA = 240
72950 deg
ZDOT = -5932
080648 TA = 54
66680
MA = 54
59559
Ha = 226
613 n
mi
Hp = 221
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12365153
42 X = 3702532
16
Y = 18423818
61 feet Y = 5657355
09 meter
Z = 2223279
25 Z = 695802
83
XDOT = -12003
598465 XDOT = -3665
136734
YDOT = 10423
704550 feet/sec YDOT = 3136
195232 meter/sec
ZDOT = -19462
206850 ZDOT = -5949
869465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12308268
28 X = 3751560
17
Y = 18452544
70 feet Y = 5624335
62 meter
Z = 2299392
94 Z = 700854
97
XDOT = -10559
463139 XDOT = -3218
524365
YDOT = 9496
952346 feet/sec YDOT = 2894
671075 meter/sec
ZDOT = -19538
221239 ZDOT = -5955
249834
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 14212
17808459
00016717 00000-0 10270-3 0 9166
2 25544 51
6419 241
5326 0005823 320
3200 39
7524 15
50409831 18150
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
17808459 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 241
5326 deg
Eccentricity:
0005823
Arg of perigee: 320
3200 deg
Mean anomaly: 39
7524 deg
Mean motion: 15
50409831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1815
Checksum: 290
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