[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 14th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19913 23 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
8
000/00:00:00
000 0
0 0
0 223
1
Coasting Arc #1 (Orbit 1512)
---------------------------------------
Vector Time (GMT): 2014/192/16:06:41
206
Vector Time (MET): N/A
Weight (LBS) : 887933
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4342992
04 A = 6797816
01 meter
Y = 4315620
24 meter E =
0009714
Z = 2939860
36 I = 51
52277
XDOT = -5433
508236 Wp = 121
46909
YDOT = -2058
299535 meter/sec RA = 337
61579 deg
ZDOT = -4998
034323 TA = 24
96369
MA = 24
91674
Ha = 226
669 n
mi
Hp = 222
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14248661
55 X = -4405208
23
Y = 14158859
05 feet Y = 4266705
83 meter
Z = 9645211
15 Z = 2918612
44
XDOT = -17826
470589 XDOT = -5385
809482
YDOT = -6752
951231 feet/sec YDOT = -2118
793132 meter/sec
ZDOT = -16397
750404 ZDOT = -5024
313655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16483397
43 X = 5024139
54
Y = -11556040
87 feet Y = -3522281
26 meter
Z = 9554227
97 Z = 2912128
69
XDOT = 15494
633538 XDOT = 4722
764302
YDOT = 8432
426559 feet/sec YDOT = 2570
203615 meter/sec
ZDOT = -16508
842023 ZDOT = -5031
895048
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
70949796
00016717 00000-0 10270-3 0 9005
2 25544 51
6480 338
0112 0005811 236
7279 123
3315 15
49987100 15137
Satellite: ISS
Catalog Number: 25544
Epoch time: 14192
70949796 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 338
0112 deg
Eccentricity:
0005811
Arg of perigee: 236
7279 deg
Mean anomaly: 123
3315 deg
Mean motion: 15
49987100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1513
Checksum: 306
Coasting Arc #2 (Orbit 1527)
---------------------------------------
Vector Time (GMT): 2014/193/16:06:41
206
Vector Time (MET): N/A
Weight (LBS) : 887933
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266065
99 A = 6798456
22 meter
Y = -4580741
79 meter E =
0001220
Z = -2651171
02 I = 51
49671
XDOT = 5288
893484 Wp = 283
75963
YDOT = 1917
728472 meter/sec RA = 332
65322 deg
ZDOT = 5195
272073 TA = 46
34910
MA = 46
33898
Ha = 226
351 n
mi
Hp = 223
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13996279
50 X = 4329850
15
Y = -15028680
40 feet Y = -4532678
93 meter
Z = -8698067
66 Z = -2630293
06
XDOT = 17352
012743 XDOT = 5241
819396
YDOT = 6291
760080 feet/sec YDOT = 1976
608439 meter/sec
ZDOT = 17044
855881 ZDOT = 5220
850236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16158082
20 X = -4924983
45
Y = 12736628
96 feet Y = 3882124
51 meter
Z = -8608607
19 Z = -2623903
47
XDOT = -15168
408715 XDOT = -4623
330976
YDOT = -7645
623191 feet/sec YDOT = -2330
385949 meter/sec
ZDOT = 17153
003589 ZDOT = 5228
235494
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
67659833
00016717 00000-0 10270-3 0 9013
2 25544 51
6481 333
2202 0005885 242
4662 117
5890 15
49998399 15287
Satellite: ISS
Catalog Number: 25544
Epoch time: 14193
67659833 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 333
2202 deg
Eccentricity:
0005885
Arg of perigee: 242
4662 deg
Mean anomaly: 117
5890 deg
Mean motion: 15
49998399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1528
Checksum: 344
Coasting Arc #3 (Orbit 1543)
---------------------------------------
Vector Time (GMT): 2014/194/16:06:41
206
Vector Time (MET): N/A
Weight (LBS) : 887933
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4165073
25 A = 6798957
71 meter
Y = 4832151
13 meter E =
0010183
Z = 2333065
85 I = 51
47168
XDOT = -5138
414257 Wp = 128
67915
YDOT = -1824
119817 meter/sec RA = 327
68941 deg
ZDOT = -5385
545907 TA = 25
27774
MA = 25
22794
Ha = 226
106 n
mi
Hp = 223
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13664938
48 X = -4230130
97
Y = 15853514
20 feet Y = 4785210
61 meter
Z = 7654415
52 Z = 2312675
37
XDOT = -16858
314492 XDOT = -5091
473908
YDOT = -5984
645070 feet/sec YDOT = -1881
317878 meter/sec
ZDOT = -17669
113868 ZDOT = -5410
393274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15712191
92 X = 4789076
10
Y = -13875241
81 feet Y = -4229173
70 meter
Z = 7566982
44 Z = 2306416
25
XDOT = 14782
759800 XDOT = 4505
785187
YDOT = 7029
008993 feet/sec YDOT = 2142
441941 meter/sec
ZDOT = -17774
182137 ZDOT = -5417
570715
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
70815544
00016717 00000-0 10270-3 0 9022
2 25544 51
6481 328
1100 0005725 246
7312 113
3236 15
50053309 15440
Satellite: ISS
Catalog Number: 25544
Epoch time: 14194
70815544 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 328
1100 deg
Eccentricity:
0005725
Arg of perigee: 246
7312 deg
Mean anomaly: 113
3236 deg
Mean motion: 15
50053309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1544
Checksum: 276
Coasting Arc #4 (Orbit 1558)
---------------------------------------
Vector Time (GMT): 2014/195/16:06:41
206
Vector Time (MET): N/A
Weight (LBS) : 887933
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4039329
31 A = 6799573
01 meter
Y = -5084846
25 meter E =
0003595
Z = -2007280
74 I = 51
44742
XDOT = 4978
390224 Wp = 341
43345
YDOT = 1765
530183 meter/sec RA = 322
72366 deg
ZDOT = 5546
353899 TA = 356
38020
MA = 356
38280
Ha = 225
857 n
mi
Hp = 223
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13252392
74 X = 4105639
54
Y = -16682566
43 feet Y = -5039304
95 meter
Z = -6585566
74 Z = -1987497
96
XDOT = 16333
301261 XDOT = 4931
335797
YDOT = 5792
421859 feet/sec YDOT = 1820
938235 meter/sec
ZDOT = 18196
699145 ZDOT = 5570
423577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15151664
93 X = -4618227
47
Y = 15015722
27 feet Y = 4576792
15 meter
Z = -6500673
78 Z = -1981405
37
XDOT = -14335
622370 XDOT = -4369
497698
YDOT = -6544
394341 feet/sec YDOT = -1994
731395 meter/sec
ZDOT = 18298
480888 ZDOT = 5577
376975
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
67522359
00016717 00000-0 10270-3 0 9039
2 25544 51
6477 323
3189 0005773 251
9401 108
1121 15
50042793 15595
Satellite: ISS
Catalog Number: 25544
Epoch time: 14195
67522359 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 323
3189 deg
Eccentricity:
0005773
Arg of perigee: 251
9401 deg
Mean anomaly: 108
1121 deg
Mean motion: 15
50042793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1559
Checksum: 308
Coasting Arc #5 (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 = 1423514
50 A = 6790020
93 meter
Y = 4206843
68 meter E =
0001672
Z = 5137584
86 I = 51
39527
XDOT = -6366
791837 Wp = 306
24718
YDOT = 3987
338345 meter/sec RA = 318
76731 deg
ZDOT = -1500
251202 TA = 158
26956
MA = 158
26247
Ha = 225
795 n
mi
Hp = 223
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4670323
17 X = 1351410
54
Y = 13801980
56 feet Y = 4222358
87 meter
Z = 16855593
38 Z = 5144325
08
XDOT = -20888
424663 XDOT = -6403
618371
YDOT = 13081
818718 feet/sec YDOT = 3915
934958 meter/sec
ZDOT = -4922
083995 ZDOT = -1531
268825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12709422
88 X = 3873832
09
Y = -7059680
69 feet Y = -2151790
67 meter
Z = 16883396
95 Z = 5146059
39
XDOT = 16228
497920 XDOT = 4946
446166
YDOT = 17123
198746 feet/sec YDOT = 5219
150978 meter/sec
ZDOT = -5054
424759 ZDOT = -1540
588666
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
51333906
00016717 00000-0 10270-3 0 9042
2 25544 51
6467 319
1625 0005551 251
7329 108
3218 15
50054682 15727
Satellite: ISS
Catalog Number: 25544
Epoch time: 14196
51333906 = yrday
fracday
Element set: 904
Inclination: 51
6467 deg
RA of node: 319
1625 deg
Eccentricity:
0005551
Arg of perigee: 251
7329 deg
Mean anomaly: 108
3218 deg
Mean motion: 15
50054682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1572
Checksum: 303
Coasting Arc #6 (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 = -1401055
41 A = 6790282
95 meter
Y = -4347820
70 meter E =
0008367
Z = -5031527
51 I = 51
37436
XDOT = 6121
583044 Wp = 122
81389
YDOT = -4182
587389 meter/sec RA = 313
79375 deg
ZDOT = 1907
526794 TA = 165
79688
MA = 165
77334
Ha = 225
568 n
mi
Hp = 222
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4596638
49 X = -1327891
79
Y = -14264503
60 feet Y = -4363078
89 meter
Z = -16507636
18 Z = -5038156
03
XDOT = 20083
933870 XDOT = 6158
632712
YDOT = -13722
399571 feet/sec YDOT = -4113
924836 meter/sec
ZDOT = 6258
290007 ZDOT = 1937
353932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13053470
08 X = -3978697
68
Y = 7301349
18 feet Y = 2225451
23 meter
Z = -16534945
41 Z = -5039851
36
XDOT = -16980
563847 XDOT = -5175
675861
YDOT = -15881
253358 feet/sec YDOT = -4840
606024 meter/sec
ZDOT = 6385
605967 ZDOT = 1946
332699
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
48037658
00016717 00000-0 10270-3 0 9055
2 25544 51
6470 314
3722 0005627 256
1079 103
9446 15
50127370 15876
Satellite: ISS
Catalog Number: 25544
Epoch time: 14197
48037658 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 314
3722 deg
Eccentricity:
0005627
Arg of perigee: 256
1079 deg
Mean anomaly: 103
9446 deg
Mean motion: 15
50127370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 315
Coasting Arc #7 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2014/198/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1397668
06 A = 6790903
55 meter
Y = 4500486
64 meter E =
0002613
Z = 4890276
36 I = 51
35556
XDOT = -5870
616105 Wp = 7
65002
YDOT = 4342
788230 meter/sec RA = 308
81725 deg
ZDOT = -2316
099019 TA = 105
13789
MA = 105
10899
Ha = 225
383 n
mi
Hp = 223
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4585525
13 X = 1323483
59
Y = 14765376
10 feet Y = 4515701
26 meter
Z = 16044213
78 Z = 4896885
97
XDOT = -19260
551526 XDOT = -5907
491105
YDOT = 14247
992881 feet/sec YDOT = 4276
933140 meter/sec
ZDOT = -7598
750063 ZDOT = -2344
706698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13416282
67 X = 4089282
96
Y = -7627122
77 feet Y = -2324747
02 meter
Z = 16071419
52 Z = 4898568
67
XDOT = 17573
120368 XDOT = 5356
287088
YDOT = 14623
950378 feet/sec YDOT = 4457
380075 meter/sec
ZDOT = -7720
912590 ZDOT = -2353
334157
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
51186898
00016717 00000-0 10270-3 0 9062
2 25544 51
6472 309
2607 0005524 260
6657 99
3869 15
50111777 16031
Satellite: ISS
Catalog Number: 25544
Epoch time: 14198
51186898 = yrday
fracday
Element set: 906
Inclination: 51
6472 deg
RA of node: 309
2607 deg
Eccentricity:
0005524
Arg of perigee: 260
6657 deg
Mean anomaly: 99
3869 deg
Mean motion: 15
50111777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 337
Coasting Arc #8 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2014/199/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1420032
52 A = 6791393
28 meter
Y = -4671769
31 meter E =
0006200
Z = -4726179
28 I = 51
33910
XDOT = 5603
570047 Wp = 130
37915
YDOT = -4453
885644 meter/sec RA = 303
84044 deg
ZDOT = 2717
380691 TA = 166
66301
MA = 166
64661
Ha = 225
205 n
mi
Hp = 222
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4658899
34 X = -1344728
12
Y = -15327327
12 feet Y = -4687227
74 meter
Z = -15505837
53 Z = -4732894
86
XDOT = 18384
416164 XDOT = 5639
757895
YDOT = -14612
485708 feet/sec YDOT = -4391
020709 meter/sec
ZDOT = 8915
290980 ZDOT = 2744
689497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13810802
20 X = -4209532
51
Y = 8064519
82 feet Y = 2458065
64 meter
Z = -15533465
81 Z = -4734600
38
XDOT = -17951
301452 XDOT = -5471
556682
YDOT = -13335
467665 feet/sec YDOT = -4064
650544 meter/sec
ZDOT = 9031
955990 ZDOT = 2752
940186
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
47887496
00016717 00000-0 10270-3 0 9071
2 25544 51
6473 304
4696 0005635 265
1889 94
8618 15
50176462 16187
Satellite: ISS
Catalog Number: 25544
Epoch time: 14199
47887496 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 304
4696 deg
Eccentricity:
0005635
Arg of perigee: 265
1889 deg
Mean anomaly: 94
8618 deg
Mean motion: 15
50176462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 362
Coasting Arc #9 (Orbit 1633)
---------------------------------------
Vector Time (GMT): 2014/200/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1461873
72 A = 6792193
26 meter
Y = 4850001
95 meter E =
0004264
Z = 4524334
83 I = 51
32537
XDOT = -5341
079028 Wp = 38
25518
YDOT = 4522
043403 meter/sec RA = 298
86195 deg
ZDOT = -3116
902187 TA = 83
17739
MA = 83
12888
Ha = 225
167 n
mi
Hp = 222
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4796173
62 X = 1385553
62
Y = 15912079
89 feet Y = 4865922
56 meter
Z = 14843618
21 Z = 4531251
28
XDOT = -17523
225156 XDOT = -5376
107780
YDOT = 14836
100403 feet/sec YDOT = 4462
120347 meter/sec
ZDOT = -10226
057044 ZDOT = -3142
933041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14199725
96 X = 4328076
47
Y = -8586027
71 feet Y = -2617021
25 meter
Z = 14872070
47 Z = 4533007
08
XDOT = 18152
864172 XDOT = 5532
993000
YDOT = 12088
411065 feet/sec YDOT = 3684
547693 meter/sec
ZDOT = -10337
307543 ZDOT = -3150
811339
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
51033382
00016717 00000-0 10270-3 0 9087
2 25544 51
6475 299
3582 0005495 269
7784 90
2737 15
50168631 16342
Satellite: ISS
Catalog Number: 25544
Epoch time: 14200
51033382 = yrday
fracday
Element set: 908
Inclination: 51
6475 deg
RA of node: 299
3582 deg
Eccentricity:
0005495
Arg of perigee: 269
7784 deg
Mean anomaly: 90
2737 deg
Mean motion: 15
50168631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1634
Checksum: 323
Coasting Arc #10 (Orbit 1648)
---------------------------------------
Vector Time (GMT): 2014/201/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1537240
88 A = 6792877
66 meter
Y = -5032193
27 meter E =
0003403
Z = -4299751
17 I = 51
31417
XDOT = 5075
877990 Wp = 137
57260
YDOT = -4541
696945 meter/sec RA = 293
88309 deg
ZDOT = 3499
795222 TA = 168
26950
MA = 168
26157
Ha = 225
095 n
mi
Hp = 222
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5043441
22 X = -1459968
82
Y = -16509820
44 feet Y = -5048951
32 meter
Z = -14106795
17 Z = -4307031
50
XDOT = 16653
143012 XDOT = 5109
286259
YDOT = -14900
580528 feet/sec YDOT = -4484
748668 meter/sec
ZDOT = 11482
267788 ZDOT = 3524
533787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14557280
24 X = -4437059
02
Y = 9233074
40 feet Y = 2814241
08 meter
Z = -14136763
05 Z = -4308885
38
XDOT = -18153
315441 XDOT = -5533
130546
YDOT = -10874
689888 feet/sec YDOT = -3314
605478 meter/sec
ZDOT = 11588
035911 ZDOT = 3532
033346
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
47730917
00016717 00000-0 10270-3 0 9092
2 25544 51
6477 294
5666 0005645 274
2197 85
8308 15
50222573 16496
Satellite: ISS
Catalog Number: 25544
Epoch time: 14201
47730917 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 294
5666 deg
Eccentricity:
0005645
Arg of perigee: 274
2197 deg
Mean anomaly: 85
8308 deg
Mean motion: 15
50222573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1649
Checksum: 332
Coasting Arc #11 (Orbit 1664)
---------------------------------------
Vector Time (GMT): 2014/202/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1630392
72 A = 6793794
37 meter
Y = 5215200
77 meter E =
0005928
Z = 4035080
24 I = 51
30554
XDOT = -4827
071322 Wp = 58
80202
YDOT = 4513
418454 meter/sec RA = 288
90369 deg
ZDOT = -3875
781149 TA = 71
63493
MA = 71
57046
Ha = 225
241 n
mi
Hp = 222
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5349057
47 X = 1552353
00
Y = 17110238
75 feet Y = 5232996
19 meter
Z = 13238452
23 Z = 4042811
29
XDOT = -15836
848168 XDOT = -4858
355483
YDOT = 14807
803326 feet/sec YDOT = 4459
264442 meter/sec
ZDOT = -12715
817417 ZDOT = -3899
305814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14882207
99 X = 4536097
00
Y = -9952295
35 feet Y = -3033459
62 meter
Z = 13270305
42 Z = 4044789
09
XDOT = 17978
072713 XDOT = 5479
716563
YDOT = 9762
612576 feet/sec YDOT = 2975
644313 meter/sec
ZDOT = -12816
428137 ZDOT = -3906
447296
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
50873546
00016717 00000-0 10270-3 0 9105
2 25544 51
6478 289
4554 0005492 279
0373 81
0156 15
50225862 16656
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
50873546 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 289
4554 deg
Eccentricity:
0005492
Arg of perigee: 279
0373 deg
Mean anomaly: 81
0156 deg
Mean motion: 15
50225862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1665
Checksum: 315
Coasting Arc #12 (Orbit 1679)
---------------------------------------
Vector Time (GMT): 2014/203/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1759796
34 A = 6794618
41 meter
Y = -5386129
35 meter E =
0000234
Z = -3749783
41 I = 51
29962
XDOT = 4589
935056 Wp = 82
20901
YDOT = -4441
978689 meter/sec RA = 283
92410 deg
ZDOT = 4226
562083 TA = 232
78861
MA = 232
79075
Ha = 225
264 n
mi
Hp = 222
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5773610
03 X = -1681221
56
Y = -17671028
04 feet Y = -5405368
84 meter
Z = -12302439
01 Z = -3758141
81
XDOT = 15058
842048 XDOT = 4618
734070
YDOT = -14573
420896 feet/sec YDOT = -4390
490444 meter/sec
ZDOT = 13866
673500 ZDOT = 4248
928663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15112591
50 X = -4606317
89
Y = 10787007
01 feet Y = 3287879
74 meter
Z = -12336931
08 Z = -3760296
59
XDOT = -17639
470337 XDOT = -5376
510559
YDOT = -8745
330398 feet/sec YDOT = -2665
576705 meter/sec
ZDOT = 13962
356230 ZDOT = 4255
726179
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
47568118
00016717 00000-0 10270-3 0 9119
2 25544 51
6480 284
6637 0005667 283
2319 76
8200 15
50264532 16805
Satellite: ISS
Catalog Number: 25544
Epoch time: 14203
47568118 = yrday
fracday
Element set: 911
Inclination: 51
6480 deg
RA of node: 284
6637 deg
Eccentricity:
0005667
Arg of perigee: 283
2319 deg
Mean anomaly: 76
8200 deg
Mean motion: 15
50264532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1680
Checksum: 308
Coasting Arc #13 (Orbit 1695)
---------------------------------------
Vector Time (GMT): 2014/204/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1902614
40 A = 6795551
90 meter
Y = 5551091
23 meter E =
0007317
Z = 3422782
81 I = 51
29601
XDOT = -4381
421548 Wp = 75
66447
YDOT = 4321
464837 meter/sec RA = 278
94461 deg
ZDOT = -4563
082371 TA = 64
12262
MA = 64
04721
Ha = 225
496 n
mi
Hp = 222
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6242173
22 X = 1823772
86
Y = 18212241
57 feet Y = 5571926
34 meter
Z = 11229602
40 Z = 3431834
35
XDOT = -14374
742613 XDOT = -4407
253824
YDOT = 14178
034241 feet/sec YDOT = 4272
324951 meter/sec
ZDOT = -14970
742687 ZDOT = -4584
428764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15285641
35 X = 4659063
48
Y = -11668674
34 feet Y = -3556611
94 meter
Z = 11267015
90 Z = 3434186
45
XDOT = 17146
245556 XDOT = 5226
175646
YDOT = 7885
906532 feet/sec YDOT = 2403
624311 meter/sec
ZDOT = -15062
073507 ZDOT = -4590
920005
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
50707578
00016717 00000-0 10270-3 0 9120
2 25544 51
6476 279
5525 0005544 288
3857 71
6690 15
50284203 16966
Satellite: ISS
Catalog Number: 25544
Epoch time: 14204
50707578 = yrday
fracday
Element set: 912
Inclination: 51
6476 deg
RA of node: 279
5525 deg
Eccentricity:
0005544
Arg of perigee: 288
3857 deg
Mean anomaly: 71
6690 deg
Mean motion: 15
50284203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1696
Checksum: 330
Coasting Arc #14 (Orbit 1710)
---------------------------------------
Vector Time (GMT): 2014/205/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2078936
43 A = 6796441
27 meter
Y = -5688387
64 meter E =
0003540
Z = -3079149
68 I = 51
29495
XDOT = 4198
345814 Wp = 344
53698
YDOT = -4167
910975 meter/sec RA = 273
96515 deg
ZDOT = 4867
224017 TA = 339
95962
MA = 339
97352
Ha = 225
574 n
mi
Hp = 222
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6820657
57 X = -2000215
78
Y = -18662689
10 feet Y = -5711195
21 meter
Z = -10102197
12 Z = -3089058
01
XDOT = 13774
100438 XDOT = 4220
997289
YDOT = -13674
248605 feet/sec YDOT = -4120
836151 meter/sec
ZDOT = 15968
582734 ZDOT = 4887
673311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15310193
97 X = -4666547
12
Y = 12632675
44 feet Y = 3850439
47 meter
Z = -10143233
83 Z = -3091657
67
XDOT = -16549
672721 XDOT = -5044
340245
YDOT = -7170
776564 feet/sec YDOT = -2185
652697 meter/sec
ZDOT = 16056
077556 ZDOT = 4893
892439
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
47399278
00016717 00000-0 10270-3 0 9132
2 25544 51
6474 274
7606 0005707 292
3193 67
7352 15
50301379 17113
Satellite: ISS
Catalog Number: 25544
Epoch time: 14205
47399278 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 274
7606 deg
Eccentricity:
0005707
Arg of perigee: 292
3193 deg
Mean anomaly: 67
7352 deg
Mean motion: 15
50301379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1711
Checksum: 319
Coasting Arc #15 (Orbit 1726)
---------------------------------------
Vector Time (GMT): 2014/206/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2261300
63 A = 6797264
99 meter
Y = 5813406
55 meter E =
0008215
Z = 2693372
95 I = 51
29639
XDOT = -4055
021156 Wp = 90
68553
YDOT = 3968
555278 meter/sec RA = 268
98609 deg
ZDOT = -5147
689752 TA = 58
78598
MA = 58
70550
Ha = 225
803 n
mi
Hp = 222
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7418965
33 X = 2183042
43
Y = 19072856
13 feet Y = 5838256
09 meter
Z = 8836525
43 Z = 2704168
21
XDOT = -13303
875185 XDOT = -4074
091716
YDOT = 13020
194482 feet/sec YDOT = 3923
103200 meter/sec
ZDOT = -16888
745904 ZDOT = -5167
434114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15261039
78 X = 4651564
92
Y = -13605951
96 feet Y = -4147094
16 meter
Z = 8881317
78 Z = 2707025
66
XDOT = 15838
842949 XDOT = 4827
679331
YDOT = 6657
325547 feet/sec YDOT = 2029
152827 meter/sec
ZDOT = -16973
211606 ZDOT = -5173
434898
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
50535638
00016717 00000-0 10270-3 0 9140
2 25544 51
6469 269
6491 0005639 297
7354 62
3224 15
50342899 17272
Satellite: ISS
Catalog Number: 25544
Epoch time: 14206
50535638 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 269
6491 deg
Eccentricity:
0005639
Arg of perigee: 297
7354 deg
Mean anomaly: 62
3224 deg
Mean motion: 15
50342899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1727
Checksum: 336
Coasting Arc #16 (Orbit 1741)
---------------------------------------
Vector Time (GMT): 2014/207/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2469244
04 A = 6798124
18 meter
Y = -5897424
26 meter E =
0007192
Z = -2296733
54 I = 51
29988
XDOT = 3948
570846 Wp = 353
60760
YDOT = -3750
445876 meter/sec RA = 264
00720 deg
ZDOT = 5390
410605 TA = 340
72193
MA = 340
74913
Ha = 225
923 n
mi
Hp = 222
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8101194
34 X = -2391957
60
Y = -19348504
80 feet Y = -5924604
66 meter
Z = -7535215
01 Z = -2308541
20
XDOT = 12954
628759 XDOT = 3964
031374
YDOT = -12304
612454 feet/sec YDOT = -3706
204325 meter/sec
ZDOT = 17685
074162 ZDOT = 5409
629123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15026833
83 X = -4580178
95
Y = 14609792
77 feet Y = 4453064
84 meter
Z = -7584304
40 Z = -2311695
98
XDOT = -15101
011491 XDOT = -4602
788302
YDOT = -6317
747084 feet/sec YDOT = -1925
649311 meter/sec
ZDOT = 17767
267249 ZDOT = 5415
463057
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
47224532
00016717 00000-0 10270-3 0 9156
2 25544 51
6462 264
8568 0005759 301
6268 58
4320 15
50333920 17424
Satellite: ISS
Catalog Number: 25544
Epoch time: 14207
47224532 = yrday
fracday
Element set: 915
Inclination: 51
6462 deg
RA of node: 264
8568 deg
Eccentricity:
0005759
Arg of perigee: 301
6268 deg
Mean anomaly: 58
4320 deg
Mean motion: 15
50333920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1742
Checksum: 304
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