[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 29th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7857 65 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 1290)
---------------------------------------
Vector Time (GMT): 2014/178/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5316472
42 A = 6793627
83 meter
Y = 1169481
01 meter E =
0008654
Z = -4074398
74 I = 51
91661
XDOT = 1588
589552 Wp = 131
01709
YDOT = 6386
790682 meter/sec RA = 48
31718 deg
ZDOT = 3905
964046 TA = 179
40511
MA = 179
40408
Ha = 227
377 n
mi
Hp = 220
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17442494
81 X = 5322791
88
Y = 3836879
96 feet Y = 1228969
15 meter
Z = -13367449
95 Z = -4048556
70
XDOT = 5211
907980 XDOT = 1498
079131
YDOT = 20954
037669 feet/sec YDOT = 6404
048670 meter/sec
ZDOT = 12814
842669 ZDOT = 3913
462233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13100445
00 X = 3993015
63
Y = -12257844
68 feet Y = -3736191
06 meter
Z = -13258000
44 Z = -4041038
53
XDOT = 19274
507538 XDOT = 5874
869898
YDOT = 6705
469045 feet/sec YDOT = 2043
826965 meter/sec
ZDOT = 12845
450674 ZDOT = 3915
293365
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 14178
40010235
00016717 00000-0 10270-3 0 9003
2 25544 51
6478 48
9389 0003534 183
6525 176
4601 15
50291390 12912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14178
40010235 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 48
9389 deg
Eccentricity:
0003534
Arg of perigee: 183
6525 deg
Mean anomaly: 176
4601 deg
Mean motion: 15
50291390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1291
Checksum: 299
Coasting Arc #2 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2014/179/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5527978
96 A = 6794643
67 meter
Y = -1162547
38 meter E =
0011396
Z = 3764264
64 I = 51
89818
XDOT = -1625
317252 Wp = 101
38841
YDOT = -6150
973268 meter/sec RA = 43
37890 deg
ZDOT = -4277
741442 TA = 33
80723
MA = 33
73462
Ha = 227
440 n
mi
Hp = 220
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18136413
90 X = -5532853
66
Y = -3814131
83 feet Y = -1224392
57 meter
Z = 12349949
62 Z = 3737398
73
XDOT = -5332
405683 XDOT = -1535
635158
YDOT = -20180
358490 feet/sec YDOT = -6168
646582 meter/sec
ZDOT = -14034
584784 ZDOT = -4285
419953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13248973
03 X = -4038286
98
Y = 13066737
85 feet Y = 3982741
70 meter
Z = 12236153
06 Z = 3729579
45
XDOT = -18762
179159 XDOT = -5718
712208
YDOT = -5824
793797 feet/sec YDOT = -1775
397149 meter/sec
ZDOT = -14065
997861 ZDOT = -4287
316148
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 14179
43148564
00016717 00000-0 10270-3 0 9015
2 25544 51
6474 43
8275 0003507 187
2918 172
8182 15
50286551 13077
Satellite: ISS
Catalog Number: 25544
Epoch time: 14179
43148564 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 43
8275 deg
Eccentricity:
0003507
Arg of perigee: 187
2918 deg
Mean anomaly: 172
8182 deg
Mean motion: 15
50286551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1307
Checksum: 316
Coasting Arc #3 (Orbit 1321)
---------------------------------------
Vector Time (GMT): 2014/180/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5753273
13 A = 6795529
65 meter
Y = 1111705
49 meter E =
0005290
Z = -3448354
87 I = 51
87885
XDOT = 1619
019778 Wp = 128
86543
YDOT = 5897
293193 meter/sec RA = 38
43874 deg
ZDOT = 4603
925278 TA = 190
99223
MA = 191
00379
Ha = 227
146 n
mi
Hp = 220
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18875568
02 X = 5757165
01
Y = 3647327
71 feet Y = 1176064
48 meter
Z = -11313500
23 Z = -3420396
98
XDOT = 5311
744677 XDOT = 1530
590420
YDOT = 19348
074780 feet/sec YDOT = 5914
903101 meter/sec
ZDOT = 15104
741726 ZDOT = 4611
576118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13276363
77 X = 4046635
68
Y = -13999791
01 feet Y = -4267136
30 meter
Z = -11195060
14 Z = -3412254
33
XDOT = 18092
103546 XDOT = 5514
473161
YDOT = 5057
541878 feet/sec YDOT = 1541
538764 meter/sec
ZDOT = 15136
082183 ZDOT = 4613
477849
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 14180
39839955
00016717 00000-0 10270-3 0 9024
2 25544 51
6481 39
0346 0003454 192
6654 167
4411 15
50314491 13226
Satellite: ISS
Catalog Number: 25544
Epoch time: 14180
39839955 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 39
0346 deg
Eccentricity:
0003454
Arg of perigee: 192
6654 deg
Mean anomaly: 167
4411 deg
Mean motion: 15
50314491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1322
Checksum: 304
Coasting Arc #4 (Orbit 1337)
---------------------------------------
Vector Time (GMT): 2014/181/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5958811
50 A = 6796554
26 meter
Y = -1040701
86 meter E =
0012947
Z = 3082719
82 I = 51
85693
XDOT = -1562
003068 Wp = 111
02717
YDOT = -5667
658263 meter/sec RA = 33
49838 deg
ZDOT = -4920
546558 TA = 33
70924
MA = 33
62697
Ha = 227
203 n
mi
Hp = 220
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19549906
48 X = -5961705
95
Y = -3414376
17 feet Y = -1107353
64 meter
Z = 10113910
16 Z = 3053765
93
XDOT = -5124
681983 XDOT = -1474
607770
YDOT = -18594
679342 feet/sec YDOT = -5684
636387 meter/sec
ZDOT = -16143
525453 ZDOT = -4927
922816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13184673
17 X = -4018688
38
Y = 14916020
78 feet Y = 4546403
13 meter
Z = 9991231
38 Z = 3045327
33
XDOT = -17383
070339 XDOT = -5298
359839
YDOT = -4504
712605 feet/sec YDOT = -1373
036402 meter/sec
ZDOT = -16173
741825 ZDOT = -4929
756508
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 14181
42976886
00016717 00000-0 10270-3 0 9035
2 25544 51
6478 33
9229 0003433 195
7126 164
3919 15
50303948 13381
Satellite: ISS
Catalog Number: 25544
Epoch time: 14181
42976886 = yrday
fracday
Element set: 903
Inclination: 51
6478 deg
RA of node: 33
9229 deg
Eccentricity:
0003433
Arg of perigee: 195
7126 deg
Mean anomaly: 164
3919 deg
Mean motion: 15
50303948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1338
Checksum: 330
Coasting Arc #5 (Orbit 1352)
---------------------------------------
Vector Time (GMT): 2014/182/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6163451
80 A = 6797354
92 meter
Y = 923839
12 meter E =
0002759
Z = -2716151
36 I = 51
83405
XDOT = 1467
973999 Wp = 95
67301
YDOT = 5438
731869 meter/sec RA = 28
55604 deg
ZDOT = 5185
237606 TA = 233
78593
MA = 233
81144
Ha = 226
897 n
mi
Hp = 221
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20221298
54 X = 6165857
18
Y = 3030968
23 feet Y = 992776
51 meter
Z = -8911257
74 Z = -2686204
58
XDOT = 4816
187661 XDOT = 1381
859819
YDOT = 17843
608493 feet/sec YDOT = 5454
665708 meter/sec
ZDOT = 17011
934404 ZDOT = 5192
160099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12934351
64 X = 3942390
38
Y = -15907105
54 feet Y = -4848485
77 meter
Z = -8784346
24 Z = -2677468
73
XDOT = 16595
896411 XDOT = 5058
429226
YDOT = 4092
153099 feet/sec YDOT = 1247
288265 meter/sec
ZDOT = 17040
266626 ZDOT = 5193
873268
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 14182
39666917
00016717 00000-0 10270-3 0 9044
2 25544 51
6484 29
1299 0003377 202
6711 157
4291 15
50334037 13533
Satellite: ISS
Catalog Number: 25544
Epoch time: 14182
39666917 = yrday
fracday
Element set: 904
Inclination: 51
6484 deg
RA of node: 29
1299 deg
Eccentricity:
0003377
Arg of perigee: 202
6711 deg
Mean anomaly: 157
4291 deg
Mean motion: 15
50334037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1353
Checksum: 311
Coasting Arc #6 (Orbit 1368)
---------------------------------------
Vector Time (GMT): 2014/183/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6338426
24 A = 6798263
43 meter
Y = -793891
18 meter E =
0013844
Z = 2302793
71 I = 51
80913
XDOT = -1323
429057 Wp = 121
69355
YDOT = -5243
535824 meter/sec RA = 23
61342 deg
ZDOT = -5433
539309 TA = 32
74464
MA = 32
65891
Ha = 226
943 n
mi
Hp = 221
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20795361
67 X = -6340263
80
Y = -2604629
84 feet Y = -864782
00 meter
Z = 7555097
49 Z = 2271998
30
XDOT = -4341
958850 XDOT = -1238
302156
YDOT = -17203
201523 feet/sec YDOT = -5257
858835 meter/sec
ZDOT = -17826
572537 ZDOT = -5439
761951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12567932
28 X = -3830705
76
Y = 16829544
84 feet Y = 5129645
27 meter
Z = 7424564
66 Z = 2263007
31
XDOT = -15819
029860 XDOT = -4821
640301
YDOT = -3912
780046 feet/sec YDOT = -1192
615358 meter/sec
ZDOT = -17851
969979 ZDOT = -5441
280450
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 14183
42802464
00016717 00000-0 10270-3 0 9059
2 25544 51
6483 24
0182 0003378 204
8710 155
2278 15
50319983 13692
Satellite: ISS
Catalog Number: 25544
Epoch time: 14183
42802464 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 24
0182 deg
Eccentricity:
0003378
Arg of perigee: 204
8710 deg
Mean anomaly: 155
2278 deg
Mean motion: 15
50319983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1369
Checksum: 305
Coasting Arc #7 (Orbit 1383)
---------------------------------------
Vector Time (GMT): 2014/184/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6498828
86 A = 6798874
98 meter
Y = 621332
65 meter E =
0003897
Z = -1894279
35 I = 51
78279
XDOT = 1152
834531 Wp = 43
62507
YDOT = 5065
787984 meter/sec RA = 18
66841 deg
ZDOT = 5626
363443 TA = 295
60096
MA = 295
64123
Ha = 226
645 n
mi
Hp = 221
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21321616
99 X = 6500599
70
Y = 2038492
95 feet Y = 694016
78 meter
Z = -6214827
28 Z = -1862704
85
XDOT = 3782
265522 XDOT = 1068
771196
YDOT = 16620
039319 feet/sec YDOT = 5078
209282 meter/sec
ZDOT = 18459
197648 ZDOT = 5631
759900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12028072
48 X = 3666156
49
Y = -17769025
35 feet Y = -5415998
93 meter
Z = -6080961
52 Z = -1853477
07
XDOT = 15049
123897 XDOT = 4586
972964
YDOT = 3873
360642 feet/sec YDOT = 1180
600324 meter/sec
ZDOT = 18481
120878 ZDOT = 5633
045644
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 14184
39491161
00016717 00000-0 10270-3 0 9065
2 25544 51
6485 19
2251 0003327 212
9544 147
1400 15
50352041 13842
Satellite: ISS
Catalog Number: 25544
Epoch time: 14184
39491161 = yrday
fracday
Element set: 906
Inclination: 51
6485 deg
RA of node: 19
2251 deg
Eccentricity:
0003327
Arg of perigee: 212
9544 deg
Mean anomaly: 147
1400 deg
Mean motion: 15
50352041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1384
Checksum: 281
Coasting Arc #8 (Orbit 1399)
---------------------------------------
Vector Time (GMT): 2014/185/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6621344
79 A = 6799547
88 meter
Y = -445931
63 meter E =
0013911
Z = 1443276
94 I = 51
75514
XDOT = -936
720608 Wp = 132
87271
YDOT = -4930
177775 meter/sec RA = 13
72309 deg
ZDOT = -5794
560691 TA = 31
42797
MA = 31
34493
Ha = 226
660 n
mi
Hp = 221
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21723572
14 X = -6622877
11
Y = -1463030
30 feet Y = -519984
44 meter
Z = 4735160
57 Z = 1411107
78
XDOT = -3073
230342 XDOT = -853
372640
YDOT = -16175
123935 feet/sec YDOT = -4940
186363 meter/sec
ZDOT = -19011
025889 ZDOT = -5798
909021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11393328
30 X = -3472686
47
Y = 18588152
26 feet Y = 5665668
81 meter
Z = 4598744
99 Z = 1401697
47
XDOT = -14343
914080 XDOT = -4372
025011
YDOT = -4062
351641 feet/sec YDOT = -1238
204780 meter/sec
ZDOT = -19028
525025 ZDOT = -5799
894428
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 14185
42625315
00016717 00000-0 10270-3 0 9071
2 25544 51
6485 14
1135 0003357 214
7139 145
3793 15
50336738 14009
Satellite: ISS
Catalog Number: 25544
Epoch time: 14185
42625315 = yrday
fracday
Element set: 907
Inclination: 51
6485 deg
RA of node: 14
1135 deg
Eccentricity:
0003357
Arg of perigee: 214
7139 deg
Mean anomaly: 145
3793 deg
Mean motion: 15
50336738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1400
Checksum: 294
Coasting Arc #9 (Orbit 1414)
---------------------------------------
Vector Time (GMT): 2014/186/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6718243
22 A = 6799878
08 meter
Y = 235801
43 meter E =
0006519
Z = -1003544
26 I = 51
72563
XDOT = 709
220151 Wp = 36
52509
YDOT = 4825
039141 meter/sec RA = 8
77470 deg
ZDOT = 5906
489136 TA = 312
63452
MA = 312
68947
Ha = 226
403 n
mi
Hp = 221
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22041480
37 X = 6719982
00
Y = 773626
74 feet Y = 310938
94 meter
Z = -3292468
04 Z = -970903
80
XDOT = 2326
837766 XDOT = 626
520983
YDOT = 15830
180909 feet/sec YDOT = 4832
507285 meter/sec
ZDOT = 19378
245198 ZDOT = 5909
733890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10594617
33 X = 3229239
36
Y = -19366774
24 feet Y = -5902992
79 meter
Z = -3154019
65 Z = -961345
19
XDOT = 13724
689083 XDOT = 4183
285233
YDOT = 4364
001751 feet/sec YDOT = 1330
147734 meter/sec
ZDOT = 19391
079220 ZDOT = 5910
400946
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 14186
39312704
00016717 00000-0 10270-3 0 9084
2 25544 51
6479 9
3202 0003323 222
6428 137
4465 15
50371382 14153
Satellite: ISS
Catalog Number: 25544
Epoch time: 14186
39312704 = yrday
fracday
Element set: 908
Inclination: 51
6479 deg
RA of node: 9
3202 deg
Eccentricity:
0003323
Arg of perigee: 222
6428 deg
Mean anomaly: 137
4465 deg
Mean motion: 15
50371382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1415
Checksum: 291
Coasting Arc #10 (Orbit 1430)
---------------------------------------
Vector Time (GMT): 2014/187/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6771966
46 A = 6800212
16 meter
Y = -35595
51 meter E =
0013040
Z = 527096
98 I = 51
69560
XDOT = -445
804305 Wp = 144
16509
YDOT = -4767
686116 meter/sec RA = 3
82589 deg
ZDOT = -5984
874014 TA = 30
15983
MA = 30
08482
Ha = 226
357 n
mi
Hp = 221
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22217737
75 X = -6773625
59
Y = -116783
17 feet Y = -111333
32 meter
Z = 1729320
80 Z = 494195
67
XDOT = -1462
612548 XDOT = -363
385214
YDOT = -15642
014816 feet/sec YDOT = -4772
210086 meter/sec
ZDOT = -19635
413432 ZDOT = -5986
839853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9740256
21 X = -2968830
09
Y = 19980796
14 feet Y = 6090146
66 meter
Z = 1589733
87 Z = 484550
88
XDOT = -13221
175836 XDOT = -4029
814395
YDOT = -4863
871829 feet/sec YDOT = -1482
508133 meter/sec
ZDOT = -19642
829419 ZDOT = -5987
134407
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 14187
42445433
00016717 00000-0 10270-3 0 9096
2 25544 51
6478 4
2086 0003364 224
9301 135
1577 15
50359009 14315
Satellite: ISS
Catalog Number: 25544
Epoch time: 14187
42445433 = yrday
fracday
Element set: 909
Inclination: 51
6478 deg
RA of node: 4
2086 deg
Eccentricity:
0003364
Arg of perigee: 224
9301 deg
Mean anomaly: 135
1577 deg
Mean motion: 15
50359009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1431
Checksum: 295
Coasting Arc #11 (Orbit 1445)
---------------------------------------
Vector Time (GMT): 2014/188/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6792960
48 A = 6800207
02 meter
Y = -187949
46 meter E =
0008697
Z = -68708
16 I = 51
66378
XDOT = 187
588472 Wp = 42
66140
YDOT = 4748
765467 meter/sec RA = 358
87324 deg
ZDOT = 6008
673994 TA = 316
60007
MA = 316
66852
Ha = 226
176 n
mi
Hp = 221
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22286615
75 X = 6794891
07
Y = -616632
08 feet Y = -111975
40 meter
Z = -225420
47 Z = -35704
19
XDOT = 615
447743 XDOT = 105
284500
YDOT = 15579
939195 feet/sec YDOT = 4750
402455 meter/sec
ZDOT = 19713
497355 ZDOT = 6009
385804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8753772
80 X = 2668149
95
Y = -20505815
43 feet Y = -6250172
54 meter
Z = -85360
18 Z = -26017
78
XDOT = 12865
984425 XDOT = 3921
552053
YDOT = 5426
638452 feet/sec YDOT = 1654
039400 meter/sec
ZDOT = 19715
593909 ZDOT = 6009
313023
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
39131534
00016717 00000-0 10270-3 0 9109
2 25544 51
6467 359
4148 0003358 231
2770 128
8080 15
50392722 14464
Satellite: ISS
Catalog Number: 25544
Epoch time: 14188
39131534 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 359
4148 deg
Eccentricity:
0003358
Arg of perigee: 231
2770 deg
Mean anomaly: 128
8080 deg
Mean motion: 15
50392722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1446
Checksum: 307
Coasting Arc #12 (Orbit 1461)
---------------------------------------
Vector Time (GMT): 2014/189/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6769472
05 A = 6800128
34 meter
Y = 387374
93 meter E =
0011217
Z = -419117
66 I = 51
63210
XDOT = 93
151004 Wp = 155
01174
YDOT = -4779
086796 meter/sec RA = 353
92000 deg
ZDOT = -5990
232738 TA = 29
50137
MA = 29
43811
Ha = 226
058 n
mi
Hp = 221
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22209553
98 X = -6771264
70
Y = 1270915
14 feet Y = 311664
37 meter
Z = -1375057
95 Z = -452007
16
XDOT = 305
613529 XDOT = 175
683577
YDOT = -15679
418621 feet/sec YDOT = -4777
582988 meter/sec
ZDOT = -19652
994547 ZDOT = -5989
580289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7765814
93 X = -2367020
39
Y = 20836703
14 feet Y = 6351027
12 meter
Z = -1514667
73 Z = -461670
72
XDOT = -12664
828588 XDOT = -3860
239754
YDOT = -6133
677265 feet/sec YDOT = -1869
544830 meter/sec
ZDOT = -19649
295136 ZDOT = -5989
105157
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
42262808
00016717 00000-0 10270-3 0 9114
2 25544 51
6464 354
3028 0003364 234
9017 125
1819 15
50390148 14621
Satellite: ISS
Catalog Number: 25544
Epoch time: 14189
42262808 = yrday
fracday
Element set: 911
Inclination: 51
6464 deg
RA of node: 354
3028 deg
Eccentricity:
0003364
Arg of perigee: 234
9017 deg
Mean anomaly: 125
1819 deg
Mean motion: 15
50390148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1462
Checksum: 299
Coasting Arc #13 (Orbit 1477)
---------------------------------------
Vector Time (GMT): 2014/190/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6710867
92 A = 6799784
52 meter
Y = -596808
34 meter E =
0010062
Z = 881953
03 I = 51
59932
XDOT = -352
195847 Wp = 53
22707
YDOT = 4850
123516 meter/sec RA = 348
96243 deg
ZDOT = 5920
918441 TA = 316
30645
MA = 316
38606
Ha = 225
967 n
mi
Hp = 221
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22017283
21 X = 6712758
56
Y = -1958032
61 feet Y = -521752
64 meter
Z = 2893546
67 Z = 914557
96
XDOT = -1155
498185 XDOT = -435
166744
YDOT = 15912
478726 feet/sec YDOT = 4845
720355 meter/sec
ZDOT = 19425
585437 ZDOT = 5919
006619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6694643
30 X = 2040527
28
Y = -21046521
33 feet Y = -6414979
70 meter
Z = 3031988
56 Z = 924150
11
XDOT = 12649
777460 XDOT = 3855
652170
YDOT = 6839
405049 feet/sec YDOT = 2084
650659 meter/sec
ZDOT = 19416
528212 ZDOT = 5918
157799
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
45393253
00016717 00000-0 10270-3 0 9129
2 25544 51
6454 349
1889 0003391 239
1046 120
9771 15
50415505 14788
Satellite: ISS
Catalog Number: 25544
Epoch time: 14190
45393253 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 349
1889 deg
Eccentricity:
0003391
Arg of perigee: 239
1046 deg
Mean anomaly: 120
9771 deg
Mean motion: 15
50415505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1478
Checksum: 311
Coasting Arc #14 (Orbit 1492)
---------------------------------------
Vector Time (GMT): 2014/191/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6611177
78 A = 6799274
30 meter
Y = 767965
92 meter E =
0008539
Z = -1365560
42 I = 51
56724
XDOT = 618
054403 Wp = 164
24691
YDOT = -4966
530767 meter/sec RA = 344
00410 deg
ZDOT = -5801
880565 TA = 30
62017
MA = 30
57036
Ha = 225
815 n
mi
Hp = 221
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21690215
80 X = -6612640
57
Y = 2519573
23 feet Y = 694027
49 meter
Z = -4480185
12 Z = -1397679
88
XDOT = 2027
737542 XDOT = 701
728871
YDOT = -16294
392281 feet/sec YDOT = -4959
150623 meter/sec
ZDOT = -19035
041224 ZDOT = -5798
675615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5685310
71 X = -1732882
70
Y = 21053503
42 feet Y = 6417107
84 meter
Z = -4616601
06 Z = -1407140
00
XDOT = -12805
683715 XDOT = -3903
172396
YDOT = -7617
293287 feet/sec YDOT = -2321
750994 meter/sec
ZDOT = -19020
475757 ZDOT = -5797
441011
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
42077450
00016717 00000-0 10270-3 0 9136
2 25544 51
6452 344
3960 0003318 243
8549 116
2261 15
50426554 14937
Satellite: ISS
Catalog Number: 25544
Epoch time: 14191
42077450 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 344
3960 deg
Eccentricity:
0003318
Arg of perigee: 243
8549 deg
Mean anomaly: 116
2261 deg
Mean motion: 15
50426554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1493
Checksum: 297
Coasting Arc #15 (Orbit 1508)
---------------------------------------
Vector Time (GMT): 2014/192/09:23:25
066
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6478889
37 A = 6798623
50 meter
Y = -935644
38 meter E =
0010541
Z = 1817245
74 I = 51
53493
XDOT = -847
803591 Wp = 66
18579
YDOT = 5120
422628 meter/sec RA = 339
04157 deg
ZDOT = 5637
178034 TA = 313
79038
MA = 313
87752
Ha = 225
784 n
mi
Hp = 221
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21256198
73 X = 6480042
94
Y = -3069699
42 feet Y = -863187
08 meter
Z = 5962092
33 Z = 1848721
62
XDOT = -2781
507846 XDOT = -932
381623
YDOT = 16799
286836 feet/sec YDOT = 5110
468250 meter/sec
ZDOT = 18494
678590 ZDOT = 5632
854851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4650899
72 X = 1417594
23
Y = -20928588
02 feet Y = -6379033
63 meter
Z = 6095811
64 Z = 1858003
39
XDOT = 13156
931527 XDOT = 4010
232729
YDOT = 8325
446314 feet/sec YDOT = 2537
596036 meter/sec
ZDOT = 18475
341819 ZDOT = 5631
284186
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
45206518
00016717 00000-0 10270-3 0 9140
2 25544 51
6446 339
2820 0003382 245
8755 114
2042 15
50438012 15095
Satellite: ISS
Catalog Number: 25544
Epoch time: 14192
45206518 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 339
2820 deg
Eccentricity:
0003382
Arg of perigee: 245
8755 deg
Mean anomaly: 114
2042 deg
Mean motion: 15
50438012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1509
Checksum: 289
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