[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 15th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 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
There are no maneuvers
Coasting Arc #1 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2014/134/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166889
72 A = 6788904
46 meter
Y = -957180
21 meter E =
0002750
Z = 5271459
55 I = 51
26947
XDOT = 1031
756133 Wp = 53
81880
YDOT = 7573
769840 meter/sec RA = 265
61740 deg
ZDOT = 561
054022 TA = 30
80475
MA = 30
78862
Ha = 227
160 n
mi
Hp = 220
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13670898
05 X = 4151675
79
Y = -3140355
03 feet Y = -910668
68 meter
Z = 17294814
79 Z = 5291665
18
XDOT = 3385
026684 XDOT = 944
262356
YDOT = 24848
326246 feet/sec YDOT = 7584
818368 meter/sec
ZDOT = 1840
728419 ZDOT = 565
854088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3981453
17 X = 1213546
93
Y = -13339246
37 feet Y = -4065802
29 meter
Z = 17380403
87 Z = 5297547
10
XDOT = 22290
991629 XDOT = 6794
294248
YDOT = 9070
614185 feet/sec YDOT = 2764
723204 meter/sec
ZDOT = 1859
764808 ZDOT = 566
856314
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
57433323
00016717 00000-0 10270-3 0 9000
2 25544 51
6475 266
2106 0002776 351
9186 8
1919 15
50202667 6118
Satellite: ISS
Catalog Number: 25544
Epoch time: 14134
57433323 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 266
2106 deg
Eccentricity:
0002776
Arg of perigee: 351
9186 deg
Mean anomaly: 8
1919 deg
Mean motion: 15
50202667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 292
Coasting Arc #2 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2014/135/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4176851
30 A = 6788743
69 meter
Y = 808584
85 meter E =
0015021
Z = -5303133
58 I = 51
27272
XDOT = -1325
623756 Wp = 78
18025
YDOT = -7534
870017 meter/sec RA = 260
63459 deg
ZDOT = -102
006259 TA = 190
82437
MA = 190
85673
Ha = 227
364 n
mi
Hp = 220
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13703580
39 X = -4159821
19
Y = 2652837
42 feet Y = 761972
19 meter
Z = -17398732
22 Z = -5323383
15
XDOT = -4349
159304 XDOT = -1240
773083
YDOT = -24720
702155 feet/sec YDOT = -7549
219559 meter/sec
ZDOT = -334
666204 ZDOT = -108
240485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4194553
24 X = -1278499
83
Y = 13199998
49 feet Y = 4023359
54 meter
Z = -17484487
63 Z = -5329271
83
XDOT = -22813
623536 XDOT = -6953
592454
YDOT = -7738
008124 feet/sec YDOT = -2358
544876 meter/sec
ZDOT = -359
779209 ZDOT = -109
660703
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
54131423
00016717 00000-0 10270-3 0 9015
2 25544 51
6478 261
4200 0002874 357
2771 2
8364 15
50227070 6267
Satellite: ISS
Catalog Number: 25544
Epoch time: 14135
54131423 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 261
4200 deg
Eccentricity:
0002874
Arg of perigee: 357
2771 deg
Mean anomaly: 2
8364 deg
Mean motion: 15
50227070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 626
Checksum: 276
Coasting Arc #3 (Orbit 641)
---------------------------------------
Vector Time (GMT): 2014/136/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4211579
00 A = 6788624
34 meter
Y = -632465
99 meter E =
0004462
Z = 5284633
50 I = 51
27926
XDOT = 1602
553733 Wp = 33
77252
YDOT = 7485
426723 meter/sec RA = 255
65009 deg
ZDOT = -377
496707 TA = 59
86902
MA = 59
82480
Ha = 227
210 n
mi
Hp = 220
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13817516
42 X = 4192666
87
Y = -2075019
64 feet Y = -585475
57 meter
Z = 17338036
42 Z = 5305047
13
XDOT = 5257
722221 XDOT = 1520
564677
YDOT = 24558
486625 feet/sec YDOT = 7502
889111 meter/sec
ZDOT = -1238
506258 ZDOT = -369
910139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4531665
58 X = 1381251
67
Y = -13103017
12 feet Y = -3993799
62 meter
Z = 17424463
34 Z = 5310976
43
XDOT = 23238
386144 XDOT = 7083
060097
YDOT = 6414
533932 feet/sec YDOT = 1955
149942 meter/sec
ZDOT = -1207
657983 ZDOT = -368
094153
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
57273473
00016717 00000-0 10270-3 0 9022
2 25544 51
6483 256
3082 0002976 359
7038
4111 15
50277763 6426
Satellite: ISS
Catalog Number: 25544
Epoch time: 14136
57273473 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 256
3082 deg
Eccentricity:
0002976
Arg of perigee: 359
7038 deg
Mean anomaly:
4111 deg
Mean motion: 15
50277763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 642
Checksum: 302
Coasting Arc #4 (Orbit 656)
---------------------------------------
Vector Time (GMT): 2014/137/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4293491
97 A = 6788746
64 meter
Y = 472244
48 meter E =
0014689
Z = -5249920
57 I = 51
28834
XDOT = -1857
083534 Wp = 84
64387
YDOT = -7372
986318 meter/sec RA = 250
66753 deg
ZDOT = 858
969972 TA = 193
60796
MA = 193
64760
Ha = 227
389 n
mi
Hp = 220
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14086259
75 X = -4272950
87
Y = 1549358
52 feet Y = 424347
20 meter
Z = -17224148
84 Z = -5270728
08
XDOT = -6092
793748 XDOT = -1778
671759
YDOT = -24189
587657 feet/sec YDOT = -7393
315067 meter/sec
ZDOT = 2818
142952 ZDOT = 850
138229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4896275
21 X = -1492384
68
Y = 13183624
13 feet Y = 4018368
63 meter
Z = -17312223
22 Z = -5276765
64
XDOT = -23394
814665 XDOT = -7130
739510
YDOT = -5050
102201 feet/sec YDOT = -1539
271151 meter/sec
ZDOT = 2781
998787 ZDOT = 847
953230
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
53966970
00016717 00000-0 10270-3 0 9031
2 25544 51
6481 251
5173 0003065 4
5366 355
5812 15
50305424 6575
Satellite: ISS
Catalog Number: 25544
Epoch time: 14137
53966970 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 251
5173 deg
Eccentricity:
0003065
Arg of perigee: 4
5366 deg
Mean anomaly: 355
5812 deg
Mean motion: 15
50305424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 657
Checksum: 300
Coasting Arc #5 (Orbit 672)
---------------------------------------
Vector Time (GMT): 2014/138/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4402735
97 A = 6788971
55 meter
Y = -290294
70 meter E =
0006889
Z = 5157308
19 I = 51
30063
XDOT = 2079
707353 Wp = 35
31151
YDOT = 7250
261988 meter/sec RA = 245
68377 deg
ZDOT = -1360
884136 TA = 67
87565
MA = 67
80254
Ha = 227
267 n
mi
Hp = 220
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14444671
83 X = 4380602
14
Y = -952410
44 feet Y = -241184
67 meter
Z = 16920302
47 Z = 5178642
46
XDOT = 6823
186855 XDOT = 2005
089502
YDOT = 23786
948779 feet/sec YDOT = 7273
101511 meter/sec
ZDOT = -4464
842966 ZDOT = -1350
961769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5362905
03 X = 1634613
45
Y = -13331599
91 feet Y = -4063471
65 meter
Z = 17010583
73 Z = 5184825
92
XDOT = 23431
820256 XDOT = 7142
018814
YDOT = 3754
212590 feet/sec YDOT = 1144
283997 meter/sec
ZDOT = -4424
051786 ZDOT = -1348
450984
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
57104160
00016717 00000-0 10270-3 0 9042
2 25544 51
6480 246
4052 0003175 7
1119 353
0076 15
50350716 6737
Satellite: ISS
Catalog Number: 25544
Epoch time: 14138
57104160 = yrday
fracday
Element set: 904
Inclination: 51
6480 deg
RA of node: 246
4052 deg
Eccentricity:
0003175
Arg of perigee: 7
1119 deg
Mean anomaly: 353
0076 deg
Mean motion: 15
50350716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 673
Checksum: 273
Coasting Arc #6 (Orbit 687)
---------------------------------------
Vector Time (GMT): 2014/139/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4552819
35 A = 6789400
56 meter
Y = 143273
10 meter E =
0013388
Z = -5046250
17 I = 51
31544
XDOT = -2268
522540 Wp = 89
91265
YDOT = -7070
389767 meter/sec RA = 240
70237 deg
ZDOT = 1850
255101 TA = 198
10729
MA = 198
15501
Ha = 227
419 n
mi
Hp = 220
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14937071
37 X = -4529569
90
Y = 470056
10 feet Y = 92490
90 meter
Z = -16555938
86 Z = -5068310
75
XDOT = -7442
659252 XDOT = -2198
279226
YDOT = -23196
816820 feet/sec YDOT = -7095
365219 meter/sec
ZDOT = 6070
390751 ZDOT = 1839
405001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5777785
13 X = -1761068
91
Y = 13669488
88 feet Y = 4166460
21 meter
Z = -16649277
41 Z = -5074699
75
XDOT = -23201
984446 XDOT = -7071
964859
YDOT = -2484
875578 feet/sec YDOT = -757
390076 meter/sec
ZDOT = 6025
630439 ZDOT = 1836
612158
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
53793130
00016717 00000-0 10270-3 0 9051
2 25544 51
6475 241
6139 0003249 11
8225 348
3002 15
50381435 6880
Satellite: ISS
Catalog Number: 25544
Epoch time: 14139
53793130 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 241
6139 deg
Eccentricity:
0003249
Arg of perigee: 11
8225 deg
Mean anomaly: 348
3002 deg
Mean motion: 15
50381435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 688
Checksum: 295
Coasting Arc #7 (Orbit 703)
---------------------------------------
Vector Time (GMT): 2014/140/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4728600
60 A = 6789982
37 meter
Y = 18997
72 meter E =
0009431
Z = 4869531
71 I = 51
33370
XDOT = 2409
408607 Wp = 44
43468
YDOT = 6883
530197 meter/sec RA = 235
72025 deg
ZDOT = -2357
140448 TA = 68
81181
MA = 68
71107
Ha = 227
317 n
mi
Hp = 220
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15513781
50 X = 4704382
01
Y = 62328
46 feet Y = 71740
29 meter
Z = 15976153
90 Z = 4892443
85
XDOT = 7904
883882 XDOT = 2343
706614
YDOT = 22583
760488 feet/sec YDOT = 6910
106514 meter/sec
ZDOT = -7733
400419 ZDOT = -2345
595056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6262698
78 X = 1908870
59
Y = -14083805
75 feet Y = -4292743
99 meter
Z = 16073077
32 Z = 4899073
97
XDOT = 22847
109489 XDOT = 6963
798972
YDOT = 1353
342493 feet/sec YDOT = 412
498792 meter/sec
ZDOT = -7685
652997 ZDOT = -2342
587034
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 14140
56925558
00016717 00000-0 10270-3 0 9068
2 25544 51
6474 236
5011 0003362 13
7019 346
4223 15
50422262 7046
Satellite: ISS
Catalog Number: 25544
Epoch time: 14140
56925558 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 236
5011 deg
Eccentricity:
0003362
Arg of perigee: 13
7019 deg
Mean anomaly: 346
4223 deg
Mean motion: 15
50422262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 704
Checksum: 278
Coasting Arc #8 (Orbit 718)
---------------------------------------
Vector Time (GMT): 2014/141/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4933205
06 A = 6790704
82 meter
Y = -129257
08 meter E =
0011238
Z = -4674749
78 I = 51
35396
XDOT = -2507
845442 Wp = 91
85910
YDOT = -6651
903599 meter/sec RA = 230
74114 deg
ZDOT = 2835
996925 TA = 206
43427
MA = 206
49164
Ha = 227
450 n
mi
Hp = 219
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16185055
97 X = -4908684
48
Y = -424071
77 feet Y = -184286
07 meter
Z = -15337105
57 Z = -4698655
16
XDOT = -8227
839376 XDOT = -2447
052390
YDOT = -21823
830705 feet/sec YDOT = -6679
608126 meter/sec
ZDOT = 9304
451854 ZDOT = 2823
961525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6614200
55 X = -2016008
33
Y = 14672298
56 feet Y = 4472116
60 meter
Z = -15438221
63 Z = -4705569
95
XDOT = -22259
573220 XDOT = -6784
717918
YDOT = -315
933456 feet/sec YDOT = -96
296517 meter/sec
ZDOT = 9254
580206 ZDOT = 2820
796047
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 14141
53610142
00016717 00000-0 10270-3 0 9077
2 25544 51
6467 231
7092 0003427 18
9106 341
2172 15
50453318 7198
Satellite: ISS
Catalog Number: 25544
Epoch time: 14141
53610142 = yrday
fracday
Element set: 907
Inclination: 51
6467 deg
RA of node: 231
7092 deg
Eccentricity:
0003427
Arg of perigee: 18
9106 deg
Mean anomaly: 341
2172 deg
Mean motion: 15
50453318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 719
Checksum: 279
Coasting Arc #9 (Orbit 734)
---------------------------------------
Vector Time (GMT): 2014/142/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5157248
83 A = 6791592
80 meter
Y = 249231
30 meter E =
0011824
Z = 4407262
65 I = 51
37803
XDOT = 2542
876641 Wp = 56
63908
YDOT = 6420
062051 meter/sec RA = 225
76218 deg
ZDOT = -3325
795958 TA = 67
16154
MA = 67
03671
Ha = 227
365 n
mi
Hp = 219
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16920107
72 X = 5132669
33
Y = 817687
99 feet Y = 306765
42 meter
Z = 14459523
12 Z = 4432256
35
XDOT = 8342
771131 XDOT = 2487
052836
YDOT = 21063
195704 feet/sec YDOT = 6448
186090 meter/sec
ZDOT = -10911
404063 ZDOT = -3313
578344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7000919
65 X = 2133880
31
Y = -15325716
51 feet Y = -4671278
39 meter
Z = 14565232
75 Z = 4439482
94
XDOT = 21562
018689 XDOT = 6572
103296
YDOT = -511
875685 feet/sec YDOT = -156
019709 meter/sec
ZDOT = -10860
713016 ZDOT = -3310
345327
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 14142
56737948
00016717 00000-0 10270-3 0 9086
2 25544 51
6470 226
5961 0003543 19
7246 340
4041 15
50492840 7359
Satellite: ISS
Catalog Number: 25544
Epoch time: 14142
56737948 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 226
5961 deg
Eccentricity:
0003543
Arg of perigee: 19
7246 deg
Mean anomaly: 340
4041 deg
Mean motion: 15
50492840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 735
Checksum: 309
Coasting Arc #10 (Orbit 749)
---------------------------------------
Vector Time (GMT): 2014/143/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5393328
76 A = 6792543
44 meter
Y = -304309
33 meter E =
0008819
Z = -4125197
74 I = 51
40299
XDOT = -2531
960965 Wp = 85
75017
YDOT = -6161
531090 meter/sec RA = 220
78659 deg
ZDOT = 3772
474486 TA = 223
30308
MA = 223
37243
Ha = 227
486 n
mi
Hp = 219
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17694648
16 X = -5369485
93
Y = -998390
18 feet Y = -364487
57 meter
Z = -13534113
32 Z = -4151340
18
XDOT = -8306
958545 XDOT = -2481
198831
YDOT = -20214
997013 feet/sec YDOT = -6189
561379 meter/sec
ZDOT = 12376
884798 ZDOT = 3760
297561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7181976
20 X = -2189066
34
Y = 16109358
28 feet Y = 4910132
40 meter
Z = -13644682
98 Z = -4158899
37
XDOT = -20698
906768 XDOT = -6309
026783
YDOT = 1191
271821 feet/sec YDOT = 363
099651 meter/sec
ZDOT = 12326
316314 ZDOT = 3757
061212
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 14143
53418311
00016717 00000-0 10270-3 0 9095
2 25544 51
6462 221
8037 0003606 25
8558 334
2773 15
50520653 7500
Satellite: ISS
Catalog Number: 25544
Epoch time: 14143
53418311 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 221
8037 deg
Eccentricity:
0003606
Arg of perigee: 25
8558 deg
Mean anomaly: 334
2773 deg
Mean motion: 15
50520653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 750
Checksum: 289
Coasting Arc #11 (Orbit 765)
---------------------------------------
Vector Time (GMT): 2014/144/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5638274
40 A = 6793621
51 meter
Y = 366395
28 meter E =
0013864
Z = 3764815
09 I = 51
43168
XDOT = 2444
731437 Wp = 70
25735
YDOT = 5912
907607 meter/sec RA = 215
81226 deg
ZDOT = -4219
439363 TA = 64
57266
MA = 64
42924
Ha = 227
430 n
mi
Hp = 219
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18498275
58 X = 5615469
69
Y = 1202084
24 feet Y = 429318
43 meter
Z = 12351755
55 Z = 3792150
08
XDOT = 8020
772432 XDOT = 2398
927260
YDOT = 19399
303174 feet/sec YDOT = 5939
990217 meter/sec
ZDOT = -13843
304997 ZDOT = -4207
674054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7370021
84 X = 2246382
66
Y = -16924671
78 feet Y = -5158639
96 meter
Z = 12467370
78 Z = 3800054
61
XDOT = 19763
314790 XDOT = 6023
858348
YDOT = -1596
792159 feet/sec YDOT = -486
702250 meter/sec
ZDOT = -13794
432837 ZDOT = -4204
543129
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 14144
56541640
00016717 00000-0 10270-3 0 9103
2 25544 51
6468 216
6906 0003735 26
1526 333
9813 15
50561400 7668
Satellite: ISS
Catalog Number: 25544
Epoch time: 14144
56541640 = yrday
fracday
Element set: 910
Inclination: 51
6468 deg
RA of node: 216
6906 deg
Eccentricity:
0003735
Arg of perigee: 26
1526 deg
Mean anomaly: 333
9813 deg
Mean motion: 15
50561400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 766
Checksum: 295
Coasting Arc #12 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2014/145/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5875522
97 A = 6794676
57 meter
Y = -356893
90 meter E =
0007627
Z = -3396719
14 I = 51
46031
XDOT = -2314
903260 Wp = 66
15719
YDOT = -5659
280439 meter/sec RA = 210
84114 deg
ZDOT = 4610
100475 TA = 254
12610
MA = 254
21018
Ha = 227
530 n
mi
Hp = 219
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19276650
18 X = -5854594
96
Y = -1170911
76 feet Y = -422480
58 meter
Z = -11144091
68 Z = -3425211
30
XDOT = -7594
826968 XDOT = -2273
842633
YDOT = -18567
193041 feet/sec YDOT = -5684
937837 meter/sec
ZDOT = 15125
001560 ZDOT = 4598
954234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7301588
72 X = -2225524
24
Y = 17802985
37 feet Y = 5426349
94 meter
Z = -11264615
83 Z = -3433454
91
XDOT = -18755
419565 XDOT = -5716
651884
YDOT = 1825
560155 feet/sec YDOT = 556
430735 meter/sec
ZDOT = 15078
704862 ZDOT = 4595
989242
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 14145
53217905
00016717 00000-0 10270-3 0 9116
2 25544 51
6459 211
8977 0003794 32
7784 327
3602 15
50583526 7810
Satellite: ISS
Catalog Number: 25544
Epoch time: 14145
53217905 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 211
8977 deg
Eccentricity:
0003794
Arg of perigee: 32
7784 deg
Mean anomaly: 327
3602 deg
Mean motion: 15
50583526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 320
Coasting Arc #13 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2014/146/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6107757
16 A = 6795773
58 meter
Y = 356084
04 meter E =
0015306
Z = 2946964
70 I = 51
49173
XDOT = 2100
822164 Wp = 84
28658
YDOT = 5428
079002 meter/sec RA = 205
87217 deg
ZDOT = -4986
098679 TA = 62
03251
MA = 61
87769
Ha = 227
524 n
mi
Hp = 219
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20038573
36 X = 6089005
73
Y = 1168254
71 feet Y = 424279
84 meter
Z = 9668519
34 Z = 2976590
35
XDOT = 6892
461168 XDOT = 2064
189321
YDOT = 17808
658143 feet/sec YDOT = 5451
367276 meter/sec
ZDOT = -16358
591468 ZDOT = -4975
981584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7227657
20 X = 2202989
91
Y = -18660946
20 feet Y = -5687856
40 meter
Z = 9793853
49 Z = 2985166
54
XDOT = 17732
803839 XDOT = 5404
958610
YDOT = -1735
852256 feet/sec YDOT = -529
087768 meter/sec
ZDOT = -16316
610560 ZDOT = -4973
302899
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 14146
56336883
00016717 00000-0 10270-3 0 9128
2 25544 51
6462 206
7845 0003941 33
6653 326
4748 15
50624918 7979
Satellite: ISS
Catalog Number: 25544
Epoch time: 14146
56336883 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 206
7845 deg
Eccentricity:
0003941
Arg of perigee: 33
6653 deg
Mean anomaly: 326
4748 deg
Mean motion: 15
50624918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 331
Coasting Arc #14 (Orbit 811)
---------------------------------------
Vector Time (GMT): 2014/147/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6312190
18 A = 6796753
95 meter
Y = -284505
89 meter E =
0009172
Z = -2499613
90 I = 51
52298
XDOT = -1854
864974 Wp = 46
19928
YDOT = -5214
225022 meter/sec RA = 200
90606 deg
ZDOT = 5295
886503 TA = 285
77349
MA = 285
87462
Ha = 227
581 n
mi
Hp = 219
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20709285
38 X = -6296397
10
Y = -933418
26 feet Y = -355004
32 meter
Z = -8200833
02 Z = -2530239
84
XDOT = -6085
515005 XDOT = -1822
146629
YDOT = -17107
037475 feet/sec YDOT = -5234
784847 meter/sec
ZDOT = 17374
955718 ZDOT = 5286
954678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6877641
34 X = -2096305
08
Y = 19501319
58 feet Y = 5944002
21 meter
Z = -8330427
19 Z = -2539114
21
XDOT = -16744
388200 XDOT = -5103
689523
YDOT = 1475
605459 feet/sec YDOT = 449
764544 meter/sec
ZDOT = 17337
955079 ZDOT = 5284
608708
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 14147
53009103
00016717 00000-0 10270-3 0 9139
2 25544 51
6456 201
9911 0003983 39
6029 320
5412 15
50642898 8120
Satellite: ISS
Catalog Number: 25544
Epoch time: 14147
53009103 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 201
9911 deg
Eccentricity:
0003983
Arg of perigee: 39
6029 deg
Mean anomaly: 320
5412 deg
Mean motion: 15
50642898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 812
Checksum: 293
Coasting Arc #15 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2014/148/12:35:59
401
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6496143
60 A = 6797666
33 meter
Y = 228609
43 meter E =
0015819
Z = 1970735
27 I = 51
55536
XDOT = 1524
190348 Wp = 97
84278
YDOT = 5035
759928 meter/sec RA = 195
94242 deg
ZDOT = -5572
048069 TA = 60
41378
MA = 60
25624
Ha = 227
628 n
mi
Hp = 218
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21312807
08 X = 6483531
08
Y = 750030
92 feet Y = 301182
75 meter
Z = 6465666
90 Z = 2002262
50
XDOT = 5000
624500 XDOT = 1494
833688
YDOT = 16521
522073 feet/sec YDOT = 5052
640842 meter/sec
ZDOT = -18280
997602 ZDOT = -5564
714433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6532436
16 X = 1991086
54
Y = -20257893
91 feet Y = -6174606
06 meter
Z = 6599102
41 Z = 2011406
42
XDOT = 15811
667840 XDOT = 4819
396358
YDOT = -884
588131 feet/sec YDOT = -269
622462 meter/sec
ZDOT = -18250
731547 ZDOT = -5562
822976
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 14148
56123827
00016717 00000-0 10270-3 0 9144
2 25544 51
6453 196
8775 0004125 41
9351 318
2115 15
50680397 8287
Satellite: ISS
Catalog Number: 25544
Epoch time: 14148
56123827 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 196
8775 deg
Eccentricity:
0004125
Arg of perigee: 41
9351 deg
Mean anomaly: 318
2115 deg
Mean motion: 15
50680397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 315
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