[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 30th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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
There are no maneuvers
Coasting Arc #1 (Orbit 1339)
---------------------------------------
Vector Time (GMT): 2014/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3629077
54 A = 6796977
69 meter
Y = 5001033
95 meter E =
0011935
Z = 2822676
06 I = 51
85452
XDOT = -5588
060470 Wp = 94
48040
YDOT = 1158
304130 meter/sec RA = 33
00796 deg
ZDOT = 5112
761778 TA = 297
41317
MA = 297
53453
Ha = 226
907 n
mi
Hp = 221
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11906422
37 X = 3559173
62
Y = 16407591
70 feet Y = 5041225
47 meter
Z = 9260748
23 Z = 2840136
16
XDOT = -18333
531727 XDOT = -5625
433443
YDOT = 3800
210400 feet/sec YDOT = 1095
605322 meter/sec
ZDOT = 16774
152814 ZDOT = 5085
525423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14684823
87 X = 4475934
32
Y = -13927236
18 feet Y = -4245021
59 meter
Z = 9333887
56 Z = 2844968
93
XDOT = 5207
246929 XDOT = 1587
168864
YDOT = 16697
343954 feet/sec YDOT = 5089
350437 meter/sec
ZDOT = 16658
341135 ZDOT = 5077
462378
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
55868062
00016717 00000-0 10270-3 0 9002
2 25544 51
6462 33
2843 0003440 201
6747 158
4259 15
50331148 13400
Satellite: ISS
Catalog Number: 25544
Epoch time: 14181
55868062 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 33
2843 deg
Eccentricity:
0003440
Arg of perigee: 201
6747 deg
Mean anomaly: 158
4259 deg
Mean motion: 15
50331148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1340
Checksum: 286
Coasting Arc #2 (Orbit 1354)
---------------------------------------
Vector Time (GMT): 2014/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3606829
40 A = 6795991
65 meter
Y = -4782184
17 meter E =
0004917
Z = -3208770
59 I = 51
82380
XDOT = 5838
651645 Wp = 140
63478
YDOT = -1177
704681 meter/sec RA = 28
06559 deg
ZDOT = -4815
514333 TA = 76
28463
MA = 76
22989
Ha = 226
826 n
mi
Hp = 221
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11833429
78 X = -3537498
85
Y = -15689580
60 feet Y = -4822130
10 meter
Z = -10527462
57 Z = -3226123
93
XDOT = 19155
681251 XDOT = 5874
779028
YDOT = -3863
860502 feet/sec YDOT = -1112
210667 meter/sec
ZDOT = -15798
931538 ZDOT = -4787
063655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13745481
65 X = -4189622
81
Y = 13989933
09 feet Y = 4264131
61 meter
Z = -10600187
47 Z = -3230937
14
XDOT = -5692
774100 XDOT = -1735
157546
YDOT = -17453
385386 feet/sec YDOT = -5319
791866 meter/sec
ZDOT = -15677
965545 ZDOT = -4778
643898
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
52557861
00016717 00000-0 10270-3 0 9013
2 25544 51
6454 28
4916 0003428 204
9034 155
1952 15
50328227 13553
Satellite: ISS
Catalog Number: 25544
Epoch time: 14182
52557861 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 28
4916 deg
Eccentricity:
0003428
Arg of perigee: 204
9034 deg
Mean anomaly: 155
1952 deg
Mean motion: 15
50328227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1355
Checksum: 300
Coasting Arc #3 (Orbit 1370)
---------------------------------------
Vector Time (GMT): 2014/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3571633
11 A = 6794956
01 meter
Y = 4560344
02 meter E =
0010913
Z = 3546641
09 I = 51
79260
XDOT = -6077
531886 Wp = 108
64405
YDOT = 1252
495244 meter/sec RA = 23
11970 deg
ZDOT = 4495
140345 TA = 293
00250
MA = 293
11757
Ha = 226
668 n
mi
Hp = 221
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11717956
39 X = 3503144
57
Y = 14961758
61 feet Y = 4599901
09 meter
Z = 11635961
57 Z = 3563825
44
XDOT = -19939
409074 XDOT = -6112
921614
YDOT = 4109
236366 feet/sec YDOT = 1184
334129 meter/sec
ZDOT = 14747
835778 ZDOT = 4465
530975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12805782
23 X = 3903202
42
Y = -13981945
97 feet Y = -4261697
13 meter
Z = 11708008
06 Z = 3568600
86
XDOT = 6381
556180 XDOT = 1945
098324
YDOT = 18128
886748 feet/sec YDOT = 5525
684681 meter/sec
ZDOT = 14621
942716 ZDOT = 4456
768140
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
55692719
00016717 00000-0 10270-3 0 9020
2 25544 51
6453 23
3785 0003456 210
2708 149
8243 15
50352283 13719
Satellite: ISS
Catalog Number: 25544
Epoch time: 14183
55692719 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 23
3785 deg
Eccentricity:
0003456
Arg of perigee: 210
2708 deg
Mean anomaly: 149
8243 deg
Mean motion: 15
50352283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1371
Checksum: 303
Coasting Arc #4 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2014/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3468263
80 A = 6793846
41 meter
Y = -4363064
33 meter E =
0004597
Z = -3887741
23 I = 51
75933
XDOT = 6311
023742 Wp = 103
32802
YDOT = -1347
882869 meter/sec RA = 18
17180 deg
ZDOT = -4122
539836 TA = 123
42456
MA = 123
38058
Ha = 226
612 n
mi
Hp = 221
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11378818
24 X = -3400331
99
Y = -14314515
51 feet Y = -4401468
57 meter
Z = -12755056
52 Z = -3904424
76
XDOT = 20705
458471 XDOT = 6345
652852
YDOT = -4422
187891 feet/sec YDOT = -1277
115018 meter/sec
ZDOT = -13525
393162 ZDOT = -4091
797980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11991020
35 X = -3654863
00
Y = 13740773
08 feet Y = 4188187
64 meter
Z = -12825011
18 Z = -3909063
41
XDOT = -7173
054428 XDOT = -2186
346990
YDOT = -18745
976000 feet/sec YDOT = -5713
773485 meter/sec
ZDOT = -13394
681798 ZDOT = -4082
699012
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
52380913
00016717 00000-0 10270-3 0 9039
2 25544 51
6446 18
5856 0003369 211
8302 148
2645 15
50364485 13868
Satellite: ISS
Catalog Number: 25544
Epoch time: 14184
52380913 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 18
5856 deg
Eccentricity:
0003369
Arg of perigee: 211
8302 deg
Mean anomaly: 148
2645 deg
Mean motion: 15
50364485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1386
Checksum: 311
Coasting Arc #5 (Orbit 1401)
---------------------------------------
Vector Time (GMT): 2014/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3352404
41 A = 6792831
49 meter
Y = 4173897
07 meter E =
0009454
Z = 4178118
91 I = 51
72619
XDOT = -6523
507931 Wp = 124
41483
YDOT = 1492
355790 meter/sec RA = 13
22057 deg
ZDOT = 3732
185210 TA = 287
18563
MA = 287
28911
Ha = 226
456 n
mi
Hp = 221
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10998702
13 X = 3285185
91
Y = 13693888
04 feet Y = 4211009
69 meter
Z = 13707739
21 Z = 4194241
37
XDOT = -21402
585077 XDOT = -6557
840626
YDOT = 4896
180412 feet/sec YDOT = 1419
213504 meter/sec
ZDOT = 12244
702131 ZDOT = 3700
411778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11222598
10 X = 3420647
90
Y = -13442072
40 feet Y = -4097143
67 meter
Z = 13775344
42 Z = 4198724
98
XDOT = 8133
817105 XDOT = 2479
187453
YDOT = 19238
260608 feet/sec YDOT = 5863
821833 meter/sec
ZDOT = 12109
592214 ZDOT = 3691
003707
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
55514085
00016717 00000-0 10270-3 0 9043
2 25544 51
6446 13
4727 0003453 217
4910 142
6001 15
50371552 14026
Satellite: ISS
Catalog Number: 25544
Epoch time: 14185
55514085 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 13
4727 deg
Eccentricity:
0003453
Arg of perigee: 217
4910 deg
Mean anomaly: 142
6001 deg
Mean motion: 15
50371552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1402
Checksum: 273
Coasting Arc #6 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2014/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3177261
62 A = 6791737
41 meter
Y = -4023030
15 meter E =
0006799
Z = -4461357
95 I = 51
69200
XDOT = 6711
479375 Wp = 84
01594
YDOT = -1653
225764 meter/sec RA = 8
26699 deg
ZDOT = -3292
572869 TA = 152
76846
MA = 152
73279
Ha = 226
434 n
mi
Hp = 221
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10424086
69 X = -3110367
24
Y = -13198917
82 feet Y = -4058185
99 meter
Z = -14637001
16 Z = -4476630
42
XDOT = 22019
289289 XDOT = 6745
461543
YDOT = -5423
969041 feet/sec YDOT = -1577
983444 meter/sec
ZDOT = -10802
404427 ZDOT = -3259
887076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10633124
38 X = -3240976
31
Y = 12958834
30 feet Y = 3949852
69 meter
Z = -14701023
69 Z = -4480872
02
XDOT = -9160
040644 XDOT = -2791
980388
YDOT = -19599
632055 feet/sec YDOT = -5973
967850 meter/sec
ZDOT = -10663
398909 ZDOT = -3250
203987
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
52200666
00016717 00000-0 10270-3 0 9059
2 25544 51
6444 8
6798 0003330 217
8175 142
2742 15
50395438 14172
Satellite: ISS
Catalog Number: 25544
Epoch time: 14186
52200666 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 8
6798 deg
Eccentricity:
0003330
Arg of perigee: 217
8175 deg
Mean anomaly: 142
2742 deg
Mean motion: 15
50395438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 305
Coasting Arc #7 (Orbit 1432)
---------------------------------------
Vector Time (GMT): 2014/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2993401
97 A = 6790850
95 meter
Y = 3890046
72 meter E =
0007658
Z = 4691482
57 I = 51
65779
XDOT = -6871
400596 Wp = 141
41688
YDOT = 1852
542637 meter/sec RA = 3
30998 deg
ZDOT = 2839
869596 TA = 280
34067
MA = 280
42699
Ha = 226
271 n
mi
Hp = 221
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9820872
59 X = 2926890
37
Y = 12762620
48 feet Y = 3923148
61 meter
Z = 15392003
18 Z = 4705862
86
XDOT = -22543
965211 XDOT = -6905
400632
YDOT = 6077
895790 feet/sec YDOT = 1775
511882 meter/sec
ZDOT = 9317
157466 ZDOT = 2806
406841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10127174
86 X = 3086762
90
Y = -12446515
12 feet Y = -3793697
81 meter
Z = 15452261
09 Z = 4709849
18
XDOT = 10302
811633 XDOT = 3140
296986
YDOT = 19807
307170 feet/sec YDOT = 6037
267226 meter/sec
ZDOT = 9174
822831 ZDOT = 2796
485999
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
55332130
00016717 00000-0 10270-3 0 9066
2 25544 51
6441 3
5667 0003408 223
7050 136
3832 15
50390478 14333
Satellite: ISS
Catalog Number: 25544
Epoch time: 14187
55332130 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 3
5667 deg
Eccentricity:
0003408
Arg of perigee: 223
7050 deg
Mean anomaly: 136
3832 deg
Mean motion: 15
50390478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1433
Checksum: 283
Coasting Arc #8 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2014/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2764172
31 A = 6789911
59 meter
Y = -3806231
43 meter E =
0009381
Z = -4904907
02 I = 51
62422
XDOT = 6990
270636 Wp = 82
81404
YDOT = -2058
683342 meter/sec RA = 358
35081 deg
ZDOT = -2344
546766 TA = 164
20372
MA = 164
17444
Ha = 226
267 n
mi
Hp = 221
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9068806
79 X = -2697578
22
Y = -12487635
92 feet Y = -3836769
37 meter
Z = -16092214
63 Z = -4918173
61
XDOT = 22933
958781 XDOT = 7024
160842
YDOT = -6754
210440 feet/sec YDOT = -1980
323925 meter/sec
ZDOT = -7692
082566 ZDOT = -2310
506835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9835524
97 X = -2997868
01
Y = 11817613
61 feet Y = 3602008
63 meter
Z = -16147759
48 Z = -4921837
09
XDOT = -11450
326449 XDOT = -3490
059502
YDOT = -19830
420582 feet/sec YDOT = -6044
312193 meter/sec
ZDOT = -7547
263752 ZDOT = -2300
405992
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
52017058
00016717 00000-0 10270-3 0 9074
2 25544 51
6445 358
7741 0003292 223
8218 136
2672 15
50423769 14480
Satellite: ISS
Catalog Number: 25544
Epoch time: 14188
52017058 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 358
7741 deg
Eccentricity:
0003292
Arg of perigee: 223
8218 deg
Mean anomaly: 136
2672 deg
Mean motion: 15
50423769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1448
Checksum: 318
Coasting Arc #9 (Orbit 1463)
---------------------------------------
Vector Time (GMT): 2014/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2532674
48 A = 6789267
76 meter
Y = 3747526
24 meter E =
0005564
Z = 5062935
72 I = 51
59025
XDOT = -7077
216195 Wp = 159
41987
YDOT = 2289
176142 meter/sec RA = 353
38771 deg
ZDOT = 1840
163213 TA = 272
70117
MA = 272
76485
Ha = 226
103 n
mi
Hp = 221
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8309299
49 X = 2465986
42
Y = 12295033
60 feet Y = 3775474
79 meter
Z = 16610681
51 Z = 5075077
56
XDOT = -23219
213238 XDOT = -7111
227219
YDOT = 7510
420413 feet/sec YDOT = 2209
843782 meter/sec
ZDOT = 6037
280882 ZDOT = 1805
700702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9649574
88 X = 2941190
42
Y = -11198589
44 feet Y = -3413330
06 meter
Z = 16661462
98 Z = 5078413
92
XDOT = 12649
149332 XDOT = 3855
460716
YDOT = 19691
458148 feet/sec YDOT = 6001
956444 meter/sec
ZDOT = 5890
627154 ZDOT = 1795
463156
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
55146795
00016717 00000-0 10270-3 0 9080
2 25544 51
6439 353
6606 0003331 229
8065 130
2794 15
50409962 14643
Satellite: ISS
Catalog Number: 25544
Epoch time: 14189
55146795 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 353
6606 deg
Eccentricity:
0003331
Arg of perigee: 229
8065 deg
Mean anomaly: 130
2794 deg
Mean motion: 15
50409962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1464
Checksum: 327
Coasting Arc #10 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2014/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2273788
95 A = 6788602
79 meter
Y = -3744260
94 meter E =
0011316
Z = -5195967
49 I = 51
55857
XDOT = 7111
451435 Wp = 88
11138
YDOT = -2512
810111 meter/sec RA = 348
42328 deg
ZDOT = -1303
360759 TA = 169
34390
MA = 169
31990
Ha = 226
087 n
mi
Hp = 221
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7459937
50 X = -2206510
47
Y = -12284320
66 feet Y = -3769311
05 meter
Z = -17047137
45 Z = -5206850
30
XDOT = 23331
533581 XDOT = 7145
353010
YDOT = -8244
127661 feet/sec YDOT = -2433
095562 meter/sec
ZDOT = -4276
117975 ZDOT = -1268
732355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9687604
32 X = -2952781
80
Y = 10542970
87 feet Y = 3213497
52 meter
Z = -17092576
88 Z = -5209817
43
XDOT = -13777
847811 XDOT = -4199
488013
YDOT = -19342
505111 feet/sec YDOT = -5895
595558 meter/sec
ZDOT = -4128
717794 ZDOT = -1258
433184
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
51830029
00016717 00000-0 10270-3 0 9099
2 25544 51
6449 348
8682 0003252 230
7555 129
3307 15
50452196 14793
Satellite: ISS
Catalog Number: 25544
Epoch time: 14190
51830029 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 348
8682 deg
Eccentricity:
0003252
Arg of perigee: 230
7555 deg
Mean anomaly: 129
3307 deg
Mean motion: 15
50452196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1479
Checksum: 316
Coasting Arc #11 (Orbit 1494)
---------------------------------------
Vector Time (GMT): 2014/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2020689
28 A = 6788305
60 meter
Y = 3769844
55 meter E =
0003207
Z = 5271564
96 I = 51
52661
XDOT = -7113
659862 Wp = 178
96056
YDOT = 2744
293320 meter/sec RA = 343
45447 deg
ZDOT = 761
131932 TA = 263
73203
MA = 263
76856
Ha = 225
939 n
mi
Hp = 221
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6629557
99 X = 1952776
41
Y = 12368256
39 feet Y = 3792060
73 meter
Z = 17295160
61 Z = 5281216
70
XDOT = -23338
779076 XDOT = -7147
515786
YDOT = 9003
587008 feet/sec YDOT = 2664
554393 meter/sec
ZDOT = 2497
152009 ZDOT = 726
493118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9835156
81 X = 2997755
80
Y = -9939915
31 feet Y = -3029686
19 meter
Z = 17335373
08 Z = 5283821
72
XDOT = 14887
485904 XDOT = 4537
705704
YDOT = 18846
388282 feet/sec YDOT = 5744
379148 meter/sec
ZDOT = 2349
662339 ZDOT = 716
177081
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
54958034
00016717 00000-0 10270-3 0 9102
2 25544 51
6445 343
7542 0003255 236
6542 123
4297 15
50430824 14957
Satellite: ISS
Catalog Number: 25544
Epoch time: 14191
54958034 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 343
7542 deg
Eccentricity:
0003255
Arg of perigee: 236
6542 deg
Mean anomaly: 123
4297 deg
Mean motion: 15
50430824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1495
Checksum: 303
Coasting Arc #12 (Orbit 1509)
---------------------------------------
Vector Time (GMT): 2014/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1760703
16 A = 6788003
21 meter
Y = -3851217
20 meter E =
0012149
Z = -5315637
88 I = 51
49770
XDOT = 7058
215966 Wp = 95
97019
YDOT = -2953
272256 meter/sec RA = 338
48546 deg
ZDOT = -199
862525 TA = 172
12718
MA = 172
10809
Ha = 225
891 n
mi
Hp = 221
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5776585
16 X = -1691685
74
Y = -12635227
05 feet Y = -3870519
88 meter
Z = -17439756
81 Z = -5324023
93
XDOT = 23156
876528 XDOT = 7091
686406
YDOT = -9689
213437 feet/sec YDOT = -2874
155572 meter/sec
ZDOT = -655
716945 ZDOT = -165
494196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10186758
38 X = -3104923
95
Y = 9382525
86 feet Y = 2859793
88 meter
Z = -17474586
65 Z = -5326254
01
XDOT = -15851
041389 XDOT = -4831
397415
YDOT = -18148
401489 feet/sec YDOT = -5531
632774 meter/sec
ZDOT = -509
334156 ZDOT = -155
245051
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
51639568
00016717 00000-0 10270-3 0 9119
2 25544 51
6457 338
9621 0003223 238
9398 121
1437 15
50481092 15105
Satellite: ISS
Catalog Number: 25544
Epoch time: 14192
51639568 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 338
9621 deg
Eccentricity:
0003223
Arg of perigee: 238
9398 deg
Mean anomaly: 121
1437 deg
Mean motion: 15
50481092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1510
Checksum: 308
Coasting Arc #13 (Orbit 1525)
---------------------------------------
Vector Time (GMT): 2014/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1514765
11 A = 6788121
34 meter
Y = 3961140
83 meter E =
0000679
Z = 5300609
41 I = 51
46930
XDOT = -6974
713517 Wp = 212
30086
YDOT = 3152
444847 meter/sec RA = 333
51221 deg
ZDOT = -363
226405 TA = 241
16971
MA = 241
17653
Ha = 225
779 n
mi
Hp = 221
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4969701
80 X = 1444609
91
Y = 12995868
87 feet Y = 3977686
98 meter
Z = 17390450
83 Z = 5307797
91
XDOT = -22882
918363 XDOT = -7007
682093
YDOT = 10342
666820 feet/sec YDOT = 3074
264821 meter/sec
ZDOT = -1191
687681 ZDOT = -397
187714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10632808
05 X = 3240879
89
Y = -8916216
84 feet Y = -2717662
89 meter
Z = 17420183
52 Z = 5309671
94
XDOT = 16728
229314 XDOT = 5098
764295
YDOT = 17341
590666 feet/sec YDOT = 5285
716835 meter/sec
ZDOT = -1336
380486 ZDOT = -407
328772
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
54765845
00016717 00000-0 10270-3 0 9122
2 25544 51
6458 333
8483 0003200 244
5612 115
5208 15
50453919 15260
Satellite: ISS
Catalog Number: 25544
Epoch time: 14193
54765845 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 333
8483 deg
Eccentricity:
0003200
Arg of perigee: 244
5612 deg
Mean anomaly: 115
5208 deg
Mean motion: 15
50453919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1526
Checksum: 306
Coasting Arc #14 (Orbit 1540)
---------------------------------------
Vector Time (GMT): 2014/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1282797
95 A = 6788227
56 meter
Y = -4120649
24 meter E =
0011663
Z = -5249921
52 I = 51
44361
XDOT = 6836
326819 Wp = 104
89629
YDOT = -3314
168866 meter/sec RA = 328
53943 deg
ZDOT = 929
652240 TA = 174
04604
MA = 174
03217
Ha = 225
697 n
mi
Hp = 221
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4208654
69 X = -1211122
64
Y = -13519190
43 feet Y = -4134593
01 meter
Z = -17224151
98 Z = -5255979
39
XDOT = 22428
893763 XDOT = 6868
362661
YDOT = -10873
257435 feet/sec YDOT = -3237
541634 meter/sec
ZDOT = 3050
040158 ZDOT = 962
938973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11233853
65 X = -3424078
59
Y = 8568724
25 feet Y = 2611747
15 meter
Z = -17249063
52 Z = -5257514
56
XDOT = -17396
766410 XDOT = -5302
534402
YDOT = -16374
394532 feet/sec YDOT = -4990
915453 meter/sec
ZDOT = 3191
897492 ZDOT = 972
890356
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
51445709
00016717 00000-0 10270-3 0 9135
2 25544 51
6467 329
0565 0003218 248
0882 111
9927 15
50508895 15414
Satellite: ISS
Catalog Number: 25544
Epoch time: 14194
51445709 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 329
0565 deg
Eccentricity:
0003218
Arg of perigee: 248
0882 deg
Mean anomaly: 111
9927 deg
Mean motion: 15
50508895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1541
Checksum: 323
Coasting Arc #15 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2014/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1071848
75 A = 6788772
75 meter
Y = 4304287
74 meter E =
0002035
Z = 5138881
47 I = 51
41945
XDOT = -6677
859880 Wp = 25
44536
YDOT = 3448
768217 meter/sec RA = 323
56312 deg
ZDOT = -1493
796974 TA = 79
00628
MA = 78
98340
Ha = 225
636 n
mi
Hp = 221
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3516564
15 X = 998675
03
Y = 14121678
94 feet Y = 4315864
30 meter
Z = 16859847
33 Z = 5143910
86
XDOT = -21908
989107 XDOT = -6708
672245
YDOT = 11314
856354 feet/sec YDOT = 3373
919925 meter/sec
ZDOT = -4900
908708 ZDOT = -1526
310991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11897771
76 X = 3626440
83
Y = -8338987
16 feet Y = -2541723
29 meter
Z = 16880367
65 Z = 5145136
06
XDOT = 17923
093188 XDOT = 5462
958804
YDOT = 15357
300451 feet/sec YDOT = 4680
905177 meter/sec
ZDOT = -5039
505781 ZDOT = -1536
041362
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
54570251
00016717 00000-0 10270-3 0 9141
2 25544 51
6471 323
9432 0003164 253
3492 106
7312 15
50479731 15574
Satellite: ISS
Catalog Number: 25544
Epoch time: 14195
54570251 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 323
9432 deg
Eccentricity:
0003164
Arg of perigee: 253
3492 deg
Mean anomaly: 106
7312 deg
Mean motion: 15
50479731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 299
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