[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 9th 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
196/11:13:24
000 0
0 0
0 0
0
N/A 0
0 0
0 225
4
000/00:00:00
000 0
0 0
0 221
4
198/01:00:40
385 2
4 4
1 4
1
N/A -3
3 -0
4 225
3
000/00:01:20
771 0
1 0
1 223
6
Coasting Arc #1 (Orbit 1449)
---------------------------------------
Vector Time (GMT): 2014/188/14:44:08
601
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6485291
12 A = 6799220
89 meter
Y = 1401233
01 meter E =
0013347
Z = 1449161
39 I = 51
65426
XDOT = -2267
965981 Wp = 134
24393
YDOT = -4490
147000 meter/sec RA = 357
75716 deg
ZDOT = -5784
042003 TA = 29
96830
MA = 29
89197
Ha = 226
255 n
mi
Hp = 221
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21277201
84 X = -6507517
60
Y = 4597221
16 feet Y = 1328585
90 meter
Z = 4754466
49 Z = 1417602
85
XDOT = -7440
833272 XDOT = -2189
490511
YDOT = -14731
453413 feet/sec YDOT = -4515
069513 meter/sec
ZDOT = -18976
515758 ZDOT = -5794
869305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20192104
80 X = 6154553
54
Y = 8209166
27 feet Y = 2502153
88 meter
Z = 4620303
59 Z = 1408268
53
XDOT = -1655
956308 XDOT = -504
735483
YDOT = 14824
387596 feet/sec YDOT = 4518
473339 meter/sec
ZDOT = -19021
578098 ZDOT = -5797
777004
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 14188
64898743
00016717 00000-0 10270-3 0 9008
2 25544 51
6470 358
1384 0003661 224
3489 135
7369 15
50445978 14507
Satellite: ISS
Catalog Number: 25544
Epoch time: 14188
64898743 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 358
1384 deg
Eccentricity:
0003661
Arg of perigee: 224
3489 deg
Mean anomaly: 135
7369 deg
Mean motion: 15
50445978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1450
Checksum: 339
Coasting Arc #2 (Orbit 1464)
---------------------------------------
Vector Time (GMT): 2014/189/14:44:08
601
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6532270
49 A = 6799611
31 meter
Y = -1603127
68 meter E =
0006465
Z = -975003
02 I = 51
62574
XDOT = 1973
133000 Wp = 32
76421
YDOT = 4463
369931 meter/sec RA = 352
80248 deg
ZDOT = 5904
351663 TA = 316
69187
MA = 316
74267
Ha = 226
076 n
mi
Hp = 221
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21431333
62 X = 6554447
79
Y = -5259605
24 feet Y = -1529955
51 meter
Z = -3198828
80 Z = -943216
45
XDOT = 6473
533465 XDOT = 1894
394466
YDOT = 14643
602135 feet/sec YDOT = 4484
993839 meter/sec
ZDOT = 19371
232490 ZDOT = 5913
746140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20814697
99 X = -6344319
95
Y = -7386497
01 feet Y = -2251404
29 meter
Z = -3063661
74 Z = -933804
10
XDOT = 2197
447584 XDOT = 669
782024
YDOT = -14209
331359 feet/sec YDOT = -4331
004198 meter/sec
ZDOT = 19410
218369 ZDOT = 5916
234559
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 14189
61579913
00016717 00000-0 10270-3 0 9012
2 25544 51
6480 353
3457 0003536 229
6471 130
4371 15
50470405 14650
Satellite: ISS
Catalog Number: 25544
Epoch time: 14189
61579913 = yrday
fracday
Element set: 901
Inclination: 51
6480 deg
RA of node: 353
3457 deg
Eccentricity:
0003536
Arg of perigee: 229
6471 deg
Mean anomaly: 130
4371 deg
Mean motion: 15
50470405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1465
Checksum: 306
Coasting Arc #3 (Orbit 1480)
---------------------------------------
Vector Time (GMT): 2014/190/14:44:08
601
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6538270
27 A = 6799834
32 meter
Y = 1781923
69 meter E =
0012476
Z = 460970
86 I = 51
59577
XDOT = -1652
025407 Wp = 146
17287
YDOT = -4496
173610 meter/sec RA = 347
84601 deg
ZDOT = -5983
534792 TA = 28
85896
MA = 28
79001
Ha = 225
911 n
mi
Hp = 221
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21451017
95 X = -6559949
45
Y = 5846206
32 feet Y = 1708687
27 meter
Z = 1512371
57 Z = 429156
49
XDOT = -5420
030864 XDOT = -1572
559352
YDOT = -14751
225753 feet/sec YDOT = -4514
202510 meter/sec
ZDOT = -19631
019660 ZDOT = -5991
367662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21259987
35 X = 6480044
14
Y = 6536683
53 feet Y = 1992381
14 meter
Z = 1377052
49 Z = 419725
60
XDOT = -2937
613350 XDOT = -895
384549
YDOT = 13748
285817 feet/sec YDOT = 4190
477517 meter/sec
ZDOT = -19663
372976 ZDOT = -5993
396083
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 14190
64705015
00016717 00000-0 10270-3 0 9022
2 25544 51
6478 348
2332 0003583 233
8348 126
2472 15
50496833 14810
Satellite: ISS
Catalog Number: 25544
Epoch time: 14190
64705015 = yrday
fracday
Element set: 902
Inclination: 51
6478 deg
RA of node: 348
2332 deg
Eccentricity:
0003583
Arg of perigee: 233
8348 deg
Mean anomaly: 126
2472 deg
Mean motion: 15
50496833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1481
Checksum: 306
Coasting Arc #4 (Orbit 1496)
---------------------------------------
Vector Time (GMT): 2014/191/14:44:08
601
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6503731
07 A = 6799850
14 meter
Y = -1968478
57 meter E =
0008923
Z = 40868
17 I = 51
56659
XDOT = 1340
875537 Wp = 40
81788
YDOT = 4570
041399 meter/sec RA = 342
88710 deg
ZDOT = 6001
298885 TA = 319
62202
MA = 319
68823
Ha = 225
795 n
mi
Hp = 221
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21337700
37 X = 6525061
16
Y = -6458263
04 feet Y = -1895630
41 meter
Z = 134081
93 Z = 72513
72
XDOT = 4399
197957 XDOT = 1260
520440
YDOT = 14993
574145 feet/sec YDOT = 4584
585795 meter/sec
ZDOT = 19689
300805 ZDOT = 6007
618099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21581972
76 X = -6578185
30
Y = -5583084
93 feet Y = -1701724
29 meter
Z = 268721
52 Z = 81906
32
XDOT = 3741
710033 XDOT = 1140
473218
YDOT = -13457
055182 feet/sec YDOT = -4101
710420 meter/sec
ZDOT = 19715
219171 ZDOT = 6009
198803
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 14191
67828567
00016717 00000-0 10270-3 0 9035
2 25544 51
6486 343
1204 0003441 239
9284 120
1526 15
50515069 14973
Satellite: ISS
Catalog Number: 25544
Epoch time: 14191
67828567 = yrday
fracday
Element set: 903
Inclination: 51
6486 deg
RA of node: 343
1204 deg
Eccentricity:
0003441
Arg of perigee: 239
9284 deg
Mean anomaly: 120
1526 deg
Mean motion: 15
50515069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1497
Checksum: 312
Coasting Arc #5 (Orbit 1511)
---------------------------------------
Vector Time (GMT): 2014/192/14:44:08
601
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6429959
76 A = 6799612
03 meter
Y = 2115763
16 meter E =
0010444
Z = -573566
88 I = 51
53653
XDOT = -1018
708381 Wp = 157
75593
YDOT = -4701
006518 meter/sec RA = 337
92675 deg
ZDOT = -5965
874700 TA = 28
43423
MA = 28
37729
Ha = 225
611 n
mi
Hp = 221
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21095668
49 X = -6450354
64
Y = 6941480
18 feet Y = 2043745
26 meter
Z = -1881781
09 Z = -604851
60
XDOT = -3342
219097 XDOT = -937
084983
YDOT = -15423
249731 feet/sec YDOT = -4711
941162 meter/sec
ZDOT = -19573
079726 ZDOT = -5970
625780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21700645
38 X = 6614356
71
Y = 4666322
79 feet Y = 1422295
19 meter
Z = -2014918
82 Z = -614147
26
XDOT = -4677
958780 XDOT = -1425
841836
YDOT = 13354
455229 feet/sec YDOT = 4070
437954 meter/sec
ZDOT = -19592
323322 ZDOT = -5971
740148
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 14192
64505435
00016717 00000-0 10270-3 0 9040
2 25544 51
6485 338
3277 0003506 243
4610 116
6181 15
50543160 15121
Satellite: ISS
Catalog Number: 25544
Epoch time: 14192
64505435 = yrday
fracday
Element set: 904
Inclination: 51
6485 deg
RA of node: 338
3277 deg
Eccentricity:
0003506
Arg of perigee: 243
4610 deg
Mean anomaly: 116
6181 deg
Mean motion: 15
50543160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1512
Checksum: 285
Coasting Arc #6 (Orbit 1527)
---------------------------------------
Vector Time (GMT): 2014/193/14:44:08
601
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6316259
39 A = 6799176
61 meter
Y = -2255057
88 meter E =
0010343
Z = 1084599
47 I = 51
50753
XDOT = 725
388564 Wp = 52
91577
YDOT = 4870
988222 meter/sec RA = 332
96342 deg
ZDOT = 5870
568430 TA = 318
85332
MA = 318
93127
Ha = 225
536 n
mi
Hp = 221
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20722635
79 X = 6335737
98
Y = -7398483
86 feet Y = -2184316
63 meter
Z = 3558397
21 Z = 1115329
49
XDOT = 2379
883739 XDOT = 642
349296
YDOT = 15980
932486 feet/sec YDOT = 4878
634957 meter/sec
ZDOT = 19260
395113 ZDOT = 5873
891117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21667533
56 X = -6604264
23
Y = -3706093
16 feet Y = -1129617
20 meter
Z = 3689207
42 Z = 1124470
42
XDOT = 5600
729048 XDOT = 1707
102214
YDOT = -13455
890532 feet/sec YDOT = -4101
355434 meter/sec
ZDOT = 19273
551666 ZDOT = 5874
578548
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 14193
67625954
00016717 00000-0 10270-3 0 9054
2 25544 51
6493 333
2148 0003384 249
6753 110
4034 15
50564630 15282
Satellite: ISS
Catalog Number: 25544
Epoch time: 14193
67625954 = yrday
fracday
Element set: 905
Inclination: 51
6493 deg
RA of node: 333
2148 deg
Eccentricity:
0003384
Arg of perigee: 249
6753 deg
Mean anomaly: 110
4034 deg
Mean motion: 15
50564630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1528
Checksum: 310
Coasting Arc #7 (Orbit 1542)
---------------------------------------
Vector Time (GMT): 2014/194/14:44:08
601
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6170651
27 A = 6798492
35 meter
Y = 2340220
74 meter E =
0007300
Z = -1614766
59 I = 51
47776
XDOT = -438
030849 Wp = 167
72070
YDOT = -5088
064875 meter/sec RA = 327
99876 deg
ZDOT = -5711
802672 TA = 29
96419
MA = 29
92243
Ha = 225
380 n
mi
Hp = 221
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20244918
88 X = -6188517
68
Y = 7677889
57 feet Y = 2271116
81 meter
Z = -5297790
64 Z = -1644785
31
XDOT = -1437
109085 XDOT = -353
356841
YDOT = -16693
126229 feet/sec YDOT = -5092
489201 meter/sec
ZDOT = -18739
510078 ZDOT = -5713
725373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21430960
72 X = 6532156
83
Y = 2854845
87 feet Y = 870157
02 meter
Z = -5425595
99 Z = -1653721
66
XDOT = -6568
391313 XDOT = -2002
045672
YDOT = 13751
751391 feet/sec YDOT = 4191
533824 meter/sec
ZDOT = -18746
693247 ZDOT = -5713
992102
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 14194
64300031
00016717 00000-0 10270-3 0 9069
2 25544 51
6489 328
4223 0003446 253
3693 106
7080 15
50585143 15439
Satellite: ISS
Catalog Number: 25544
Epoch time: 14194
64300031 = yrday
fracday
Element set: 906
Inclination: 51
6489 deg
RA of node: 328
4223 deg
Eccentricity:
0003446
Arg of perigee: 253
3693 deg
Mean anomaly: 106
7080 deg
Mean motion: 15
50585143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1543
Checksum: 292
Coasting Arc #8 (Orbit 1558)
---------------------------------------
Vector Time (GMT): 2014/195/14:44:08
601
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5991670
14 A = 6797602
39 meter
Y = -2402300
91 meter E =
0010541
Z = 2113248
02 I = 51
44967
XDOT = 194
426556 Wp = 67
16892
YDOT = 5336
161640 meter/sec RA = 323
03060 deg
ZDOT = 5496
859218 TA = 316
27296
MA = 316
35641
Ha = 225
299 n
mi
Hp = 221
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19657710
44 X = 6007822
64
Y = -7881564
66 feet Y = -2335208
04 meter
Z = 6933228
40 Z = 2142393
17
XDOT = 637
882402 XDOT = 108
040491
YDOT = 17507
091994 feet/sec YDOT = 5337
852411 meter/sec
ZDOT = 18034
315020 ZDOT = 5497
594281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21040128
17 X = -6413031
07
Y = -2030110
29 feet Y = -618777
62 meter
Z = 7057333
51 Z = 2151075
25
XDOT = 7444
289017 XDOT = 2269
019292
YDOT = -14251
348182 feet/sec YDOT = -4343
810926 meter/sec
ZDOT = 18036
421483 ZDOT = 5497
501268
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 14195
67417507
00016717 00000-0 10270-3 0 9071
2 25544 51
6493 323
3094 0003383 259
3495 100
7275 15
50617859 15597
Satellite: ISS
Catalog Number: 25544
Epoch time: 14195
67417507 = yrday
fracday
Element set: 907
Inclination: 51
6493 deg
RA of node: 323
3094 deg
Eccentricity:
0003383
Arg of perigee: 259
3495 deg
Mean anomaly: 100
7275 deg
Mean motion: 15
50617859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1559
Checksum: 332
Coasting Arc #9 (Orbit 1571)
---------------------------------------
Vector Time (GMT): 2014/196/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 679248
57 A = 6789380
46 meter
Y = 4628309
49 meter E =
0003854
Z = 4919560
62 I = 51
39877
XDOT = -6522
036955 Wp = 39
97101
YDOT = 3342
086324 meter/sec RA = 318
74548 deg
ZDOT = -2239
846289 TA = 72
01294
MA = 71
97094
Ha = 225
399 n
mi
Hp = 221
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2228505
82 X = 603546
07
Y = 15184742
42 feet Y = 4635481
72 meter
Z = 16140290
75 Z = 4922676
65
XDOT = -21397
759040 XDOT = -6548
043946
YDOT = 10964
850145 feet/sec YDOT = 3269
007425 meter/sec
ZDOT = -7348
577065 ZDOT = -2271
591816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14522600
91 X = 4426488
76
Y = -4923202
44 feet Y = -1500592
10 meter
Z = 16152639
62 Z = 4923324
55
XDOT = 14396
478130 XDOT = 4388
046534
YDOT = 17871
414889 feet/sec YDOT = 5447
207258 meter/sec
ZDOT = -7483
884473 ZDOT = -2281
087987
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 14196
51199618
00016717 00000-0 10270-3 0 9086
2 25544 51
6471 319
1524 0003168 260
5879 99
4914 15
50594621 15725
Satellite: ISS
Catalog Number: 25544
Epoch time: 14196
51199618 = yrday
fracday
Element set: 908
Inclination: 51
6471 deg
RA of node: 319
1524 deg
Eccentricity:
0003168
Arg of perigee: 260
5879 deg
Mean anomaly: 99
4914 deg
Mean motion: 15
50594621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1572
Checksum: 335
Coasting Arc #10 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2014/197/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -500311
34 A = 6790170
88 meter
Y = -4892935
30 meter E =
0007727
Z = -4688983
59 I = 51
37957
XDOT = 6295
679295 Wp = 118
76275
YDOT = -3332
460016 meter/sec RA = 313
76742 deg
ZDOT = 2805
545452 TA = 179
20970
MA = 179
20847
Ha = 225
262 n
mi
Hp = 221
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1641441
42 X = -422783
01
Y = -16052937
33 feet Y = -4898096
40 meter
Z = -15383804
41 Z = -4691225
91
XDOT = 20655
115796 XDOT = 6318
847486
YDOT = -10933
267770 feet/sec YDOT = -3261
928264 meter/sec
ZDOT = 9204
545445 ZDOT = 2836
184634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15404208
30 X = -4695202
69
Y = 4778788
44 feet Y = 1456574
72 meter
Z = -15392404
39 Z = -4691604
86
XDOT = -14545
906316 XDOT = -4433
592245
YDOT = -16818
453106 feet/sec YDOT = -5126
264507 meter/sec
ZDOT = 9335
147711 ZDOT = 2845
353022
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
47869597
00016717 00000-0 10270-3 0 9093
2 25544 51
6476 314
3597 0003303 266
3528 93
7246 15
50653173 15872
Satellite: ISS
Catalog Number: 25544
Epoch time: 14197
47869597 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 314
3597 deg
Eccentricity:
0003303
Arg of perigee: 266
3528 deg
Mean anomaly: 93
7246 deg
Mean motion: 15
50653173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 349
Coasting Arc #11 (Orbit 1595)
---------------------------------------
Vector Time (GMT): 2014/198/01:01:20
771
Vector Time (MET): N/A
Weight (LBS) : 898427
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3222885
72 A = 6789624
58 meter
Y = -2760193
91 meter E =
0008400
Z = -5307610
81 I = 51
35903
XDOT = 5001
720065 Wp = 87
05896
YDOT = -5795
788260 meter/sec RA = 310
92966 deg
ZDOT = -22
683671 TA = 182
72140
MA = 182
72597
Ha = 225
291 n
mi
Hp = 223
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10573772
04 X = -3165998
74
Y = -9055754
30 feet Y = -2795915
99 meter
Z = -17413421
30 Z = -5323128
88
XDOT = 16409
842732 XDOT = 5066
268345
YDOT = -19015
053346 feet/sec YDOT = -5739
494894 meter/sec
ZDOT = -74
421494 ZDOT = 1
770197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 382936
71 X = 116719
11
Y = -13834218
34 feet Y = -4216669
75 meter
Z = -17478739
80 Z = -5327519
89
XDOT = 24099
489298 XDOT = 7345
524338
YDOT = 630
298789 feet/sec YDOT = 192
115071 meter/sec
ZDOT = 30
393527 ZDOT = 9
263947
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
05871180
00016717 00000-0 10270-3 0 9101
2 25544 51
6481 311
4861 0006467 273
6410 86
4001 15
49922688 15961
Satellite: ISS
Catalog Number: 25544
Epoch time: 14198
05871180 = yrday
fracday
Element set: 910
Inclination: 51
6481 deg
RA of node: 311
4861 deg
Eccentricity:
0006467
Arg of perigee: 273
6410 deg
Mean anomaly: 86
4001 deg
Mean motion: 15
49922688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1596
Checksum: 316
Coasting Arc #12 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2014/199/01:01:20
771
Vector Time (MET): N/A
Weight (LBS) : 898427
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3203074
56 A = 6789530
45 meter
Y = 2799287
96 meter E =
0004374
Z = 5295314
12 I = 51
33910
XDOT = -4708
856941 Wp = 291
41222
YDOT = 6030
875639 meter/sec RA = 305
95436 deg
ZDOT = -338
458119 TA = 161
83988
MA = 161
82426
Ha = 225
303 n
mi
Hp = 223
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10508774
81 X = 3145811
54
Y = 9184015
62 feet Y = 2834786
39 meter
Z = 17373077
81 Z = 5310735
09
XDOT = -15449
005712 XDOT = -4774
301495
YDOT = 19786
337398 feet/sec YDOT = 5977
852262 meter/sec
ZDOT = -1110
426900 ZDOT = -361
491549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -284620
31 X = -86752
27
Y = 13872282
19 feet Y = 4228271
61 meter
Z = 17437978
71 Z = 5315095
91
XDOT = -24066
684359 XDOT = -7335
525393
YDOT = 1031
796699 feet/sec YDOT = 314
491634 meter/sec
ZDOT = -1209
249416 ZDOT = -368
579222
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
09033540
00016717 00000-0 10270-3 0 9117
2 25544 51
6478 306
3763 0006624 277
8030 82
2368 15
49969594 16126
Satellite: ISS
Catalog Number: 25544
Epoch time: 14199
09033540 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 306
3763 deg
Eccentricity:
0006624
Arg of perigee: 277
8030 deg
Mean anomaly: 82
2368 deg
Mean motion: 15
49969594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 327
Coasting Arc #13 (Orbit 1626)
---------------------------------------
Vector Time (GMT): 2014/200/01:01:20
771
Vector Time (MET): N/A
Weight (LBS) : 898427
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3204205
15 A = 6789672
48 meter
Y = -2855781
44 meter E =
0008123
Z = -5267985
56 I = 51
32253
XDOT = 4395
893930 Wp = 90
24694
YDOT = -6228
427341 meter/sec RA = 300
97676 deg
ZDOT = 703
584849 TA = 186
50834
MA = 186
51889
Ha = 225
581 n
mi
Hp = 223
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10512484
10 X = -3146443
01
Y = -9369361
70 feet Y = -2891289
67 meter
Z = -17283417
18 Z = -5283410
88
XDOT = 14422
224181 XDOT = 4461
797152
YDOT = -20434
472902 feet/sec YDOT = -6178
901176 meter/sec
ZDOT = 2308
349243 ZDOT = 725
099064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 182456
71 X = 55612
81
Y = -14000571
21 feet Y = -4267374
11 meter
Z = -17348328
02 Z = -5287770
38
XDOT = 23841
198607 XDOT = 7266
797336
YDOT = -2660
427551 feet/sec YDOT = -810
898318 meter/sec
ZDOT = 2400
755264 ZDOT = 731
750205
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
05747174
00016717 00000-0 10270-3 0 9122
2 25544 51
6483 301
5851 0006520 282
1398 77
9022 15
49966703 16271
Satellite: ISS
Catalog Number: 25544
Epoch time: 14200
05747174 = yrday
fracday
Element set: 912
Inclination: 51
6483 deg
RA of node: 301
5851 deg
Eccentricity:
0006520
Arg of perigee: 282
1398 deg
Mean anomaly: 77
9022 deg
Mean motion: 15
49966703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1627
Checksum: 307
Coasting Arc #14 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2014/201/01:01:20
771
Vector Time (MET): N/A
Weight (LBS) : 898427
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3215810
33 A = 6789761
64 meter
Y = 2933571
27 meter E =
0005092
Z = 5214346
79 I = 51
30784
XDOT = -4078
292682 Wp = 320
67003
YDOT = 6392
648012 meter/sec RA = 295
99834 deg
ZDOT = -1078
015153 TA = 139
73786
MA = 139
70014
Ha = 225
781 n
mi
Hp = 223
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10550558
84 X = 3157438
00
Y = 9624577
66 feet Y = 2969205
80 meter
Z = 17107436
98 Z = 5229827
07
XDOT = -13380
225334 XDOT = -4144
237007
YDOT = 20973
254632 feet/sec YDOT = 6346
673273 meter/sec
ZDOT = -3536
795120 ZDOT = -1097
986547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -104168
14 X = -31750
45
Y = 14202224
87 feet Y = 4328838
14 meter
Z = 17172569
54 Z = 5234199
20
XDOT = -23470
246659 XDOT = -7153
731182
YDOT = 4221
186166 feet/sec YDOT = 1286
617543 meter/sec
ZDOT = -3622
679955 ZDOT = -1104
192850
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
08906797
00016717 00000-0 10270-3 0 9135
2 25544 51
6481 296
4748 0006678 286
3005 73
7410 15
50013653 16433
Satellite: ISS
Catalog Number: 25544
Epoch time: 14201
08906797 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 296
4748 deg
Eccentricity:
0006678
Arg of perigee: 286
3005 deg
Mean anomaly: 73
7410 deg
Mean motion: 15
50013653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 312
Coasting Arc #15 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2014/202/01:01:20
771
Vector Time (MET): N/A
Weight (LBS) : 898427
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3256701
73 A = 6790088
82 meter
Y = -3016552
66 meter E =
0007252
Z = -5144431
39 I = 51
29663
XDOT = 3748
381437 Wp = 92
57771
YDOT = -6516
728019 meter/sec RA = 291
01861 deg
ZDOT = 1449
760295 TA = 191
45635
MA = 191
47287
Ha = 225
974 n
mi
Hp = 223
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10684716
96 X = -3197738
08
Y = -9896826
33 feet Y = -3052641
10 meter
Z = -16878055
74 Z = -5160108
91
XDOT = 12297
839359 XDOT = 3813
931970
YDOT = -21380
341269 feet/sec YDOT = -6474
444806 meter/sec
ZDOT = 4756
431413 ZDOT = 1468
127979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -34690
50 X = -10573
67
Y = -14487176
90 feet Y = -4415691
52 meter
Z = -16944014
15 Z = -5164535
51
XDOT = 22923
204466 XDOT = 6986
992721
YDOT = -5704
892399 feet/sec YDOT = -1738
851203 meter/sec
ZDOT = 4835
530119 ZDOT = 1473
869580
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
05617885
00016717 00000-0 10270-3 0 9141
2 25544 51
6486 291
6836 0006633 290
4672 69
5767 15
50009167 16589
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
05617885 = yrday
fracday
Element set: 914
Inclination: 51
6486 deg
RA of node: 291
6836 deg
Eccentricity:
0006633
Arg of perigee: 290
4672 deg
Mean anomaly: 69
5767 deg
Mean motion: 15
50009167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 334
Coasting Arc #16 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2014/203/01:01:20
771
Vector Time (MET): N/A
Weight (LBS) : 898427
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3310428
38 A = 6790368
07 meter
Y = 3119448
27 meter E =
0006144
Z = 5044801
50 I = 51
28774
XDOT = -3424
157257 Wp = 344
88792
YDOT = 6602
081334 meter/sec RA = 286
03838 deg
ZDOT = -1830
121442 TA = 122
97360
MA = 122
91452
Ha = 226
191 n
mi
Hp = 223
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10860985
49 X = 3250794
15
Y = 10234410
34 feet Y = 3156133
73 meter
Z = 16551186
01 Z = 5060738
38
XDOT = -11234
111736 XDOT = -3488
838687
YDOT = 21660
371831 feet/sec YDOT = 6563
428712 meter/sec
ZDOT = -6004
335438 ZDOT = -1846
911886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 166330
99 X = 50697
68
Y = 14847646
86 feet Y = 4525562
76 meter
Z = 16618232
03 Z = 5065237
12
XDOT = -22248
478255 XDOT = -6781
336172
YDOT = 7070
092576 feet/sec YDOT = 2154
964217 meter/sec
ZDOT = -6076
752939 ZDOT = -1852
194296
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
08774852
00016717 00000-0 10270-3 0 9154
2 25544 51
6486 286
5732 0006775 294
6671 65
3774 15
50057495 16746
Satellite: ISS
Catalog Number: 25544
Epoch time: 14203
08774852 = yrday
fracday
Element set: 915
Inclination: 51
6486 deg
RA of node: 286
5732 deg
Eccentricity:
0006775
Arg of perigee: 294
6671 deg
Mean anomaly: 65
3774 deg
Mean motion: 15
50057495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 344
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