[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 27th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 1262)
---------------------------------------
Vector Time (GMT): 2014/176/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1414055
75 A = 6797585
21 meter
Y = -6085195
56 meter E =
0007542
Z = -2673051
21 I = 51
96322
XDOT = 5505
845529 Wp = 148
00502
YDOT = 1011
814379 meter/sec RA = 57
36175 deg
ZDOT = -5228
968549 TA = 61
95865
MA = 61
88238
Ha = 227
504 n
mi
Hp = 220
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4639290
53 X = -1332919
79
Y = -19964552
35 feet Y = -6100554
39 meter
Z = -8769853
06 Z = -2679724
31
XDOT = 18063
797668 XDOT = 5519
522628
YDOT = 3319
600981 feet/sec YDOT = 1073
461519 meter/sec
ZDOT = -17155
408625 ZDOT = -5202
188553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15620207
76 X = -4761039
32
Y = 13252850
91 feet Y = 4039468
96 meter
Z = -8797030
31 Z = -2681334
84
XDOT = -4444
380932 XDOT = -1354
647308
YDOT = -16522
320816 feet/sec YDOT = -5036
003385 meter/sec
ZDOT = -17041
951139 ZDOT = -5194
386707
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 14176
59516829
00016717 00000-0 10270-3 0 9001
2 25544 51
6478 57
8830 0003609 181
3265 178
7887 15
50251603 12634
Satellite: ISS
Catalog Number: 25544
Epoch time: 14176
59516829 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 57
8830 deg
Eccentricity:
0003609
Arg of perigee: 181
3265 deg
Mean anomaly: 178
7887 deg
Mean motion: 15
50251603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1263
Checksum: 329
Coasting Arc #2 (Orbit 1278)
---------------------------------------
Vector Time (GMT): 2014/177/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1542663
69 A = 6796646
88 meter
Y = 5884909
43 meter E =
0012807
Z = 3021791
57 I = 51
94241
XDOT = -5730
685799 Wp = 98
81048
YDOT = -1062
142415 meter/sec RA = 52
42694 deg
ZDOT = 4974
216294 TA = 295
58924
MA = 295
72154
Ha = 227
333 n
mi
Hp = 220
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5061232
59 X = 1462063
80
Y = 19307445
65 feet Y = 5901709
38 meter
Z = 9914014
33 Z = 3029090
69
XDOT = -18801
462596 XDOT = -5742
545826
YDOT = -3484
719210 feet/sec YDOT = -1126
293677 meter/sec
ZDOT = 16319
607263 ZDOT = 4946
348549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14614764
37 X = 4454580
18
Y = -13572367
68 feet Y = -4136857
67 meter
Z = 9943878
06 Z = 3030894
03
XDOT = 4926
704693 XDOT = 1501
659590
YDOT = 17222
902300 feet/sec YDOT = 5249
540621 meter/sec
ZDOT = 16201
541457 ZDOT = 4938
229836
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 14177
62656049
00016717 00000-0 10270-3 0 9016
2 25544 51
6474 52
7706 0003519 185
9026 174
2084 15
50286628 12793
Satellite: ISS
Catalog Number: 25544
Epoch time: 14177
62656049 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 52
7706 deg
Eccentricity:
0003519
Arg of perigee: 185
9026 deg
Mean anomaly: 174
2084 deg
Mean motion: 15
50286628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1279
Checksum: 323
Coasting Arc #3 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2014/178/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1598125
96 A = 6795655
30 meter
Y = -5670769
02 meter E =
0005576
Z = -3386607
74 I = 51
91835
XDOT = 5970
827554 Wp = 129
46130
YDOT = 1100
200834 meter/sec RA = 47
49091 deg
ZDOT = -4668
429785 TA = 89
81944
MA = 89
75554
Ha = 227
277 n
mi
Hp = 220
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5243195
40 X = -1518144
40
Y = -18604885
24 feet Y = -5688192
60 meter
Z = -11110917
79 Z = -3394177
72
XDOT = 19589
329244 XDOT = 5980
758676
YDOT = 3609
582790 feet/sec YDOT = 1167
026668 meter/sec
ZDOT = -15316
370687 ZDOT = -4639
400245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13681359
83 X = -4170078
48
Y = 13629465
90 feet Y = 4154261
21 meter
Z = -11141965
68 Z = -3396071
14
XDOT = -5510
449569 XDOT = -1679
585029
YDOT = -17928
962540 feet/sec YDOT = -5464
747782 meter/sec
ZDOT = -15193
380248 ZDOT = -4630
942300
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
59348517
00016717 00000-0 10270-3 0 9022
2 25544 51
6463 47
9784 0003528 188
8812 171
2278 15
50285527 12944
Satellite: ISS
Catalog Number: 25544
Epoch time: 14178
59348517 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 47
9784 deg
Eccentricity:
0003528
Arg of perigee: 188
8812 deg
Mean anomaly: 171
2278 deg
Mean motion: 15
50285527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1294
Checksum: 340
Coasting Arc #4 (Orbit 1309)
---------------------------------------
Vector Time (GMT): 2014/179/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1647971
11 A = 6794667
98 meter
Y = 5451885
53 meter E =
0011712
Z = 3699856
86 I = 51
89321
XDOT = -6217
510529 Wp = 112
32964
YDOT = -1080
485689 meter/sec RA = 42
55183 deg
ZDOT = 4346
187065 TA = 291
48416
MA = 291
60901
Ha = 227
130 n
mi
Hp = 220
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5406729
35 X = 1568911
85
Y = 17886763
55 feet Y = 5469871
66 meter
Z = 12138637
99 Z = 3707671
11
XDOT = -20398
656590 XDOT = -6226
078380
YDOT = -3544
900554 feet/sec YDOT = -1150
062383 meter/sec
ZDOT = 14259
143913 ZDOT = 4315
962584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12745850
12 X = 3884935
12
Y = -13635669
01 feet Y = -4156151
91 meter
Z = 12170760
05 Z = 3709647
66
XDOT = 6295
776159 XDOT = 1918
952573
YDOT = 18542
632920 feet/sec YDOT = 5651
794514 meter/sec
ZDOT = 14131
077906 ZDOT = 4307
152546
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
62486420
00016717 00000-0 10270-3 0 9034
2 25544 51
6460 42
8656 0003530 194
2100 165
8952 15
50302518 13104
Satellite: ISS
Catalog Number: 25544
Epoch time: 14179
62486420 = yrday
fracday
Element set: 903
Inclination: 51
6460 deg
RA of node: 42
8656 deg
Eccentricity:
0003530
Arg of perigee: 194
2100 deg
Mean anomaly: 165
8952 deg
Mean motion: 15
50302518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1310
Checksum: 282
Coasting Arc #5 (Orbit 1324)
---------------------------------------
Vector Time (GMT): 2014/180/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1623673
11 A = 6793590
73 meter
Y = -5234076
72 meter E =
0005892
Z = -4019182
68 I = 51
86527
XDOT = 6462
420669 Wp = 101
60318
YDOT = 1041
358813 meter/sec RA = 37
61089 deg
ZDOT = -3972
911112 TA = 127
15078
MA = 127
09695
Ha = 227
088 n
mi
Hp = 220
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5327011
51 X = -1545500
11
Y = -17172167
73 feet Y = -5251796
10 meter
Z = -13186294
87 Z = -4026880
94
XDOT = 21202
167550 XDOT = 6469
594572
YDOT = 3416
531540 feet/sec YDOT = 1113
666355 meter/sec
ZDOT = -13034
485277 ZDOT = -3941
500363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11943918
36 X = -3640506
31
Y = 13407722
83 feet Y = 4086673
92 meter
Z = -13217963
21 Z = -4028835
19
XDOT = -7169
550171 XDOT = -2185
278892
YDOT = -19085
965747 feet/sec YDOT = -5817
402360 meter/sec
ZDOT = -12901
377998 ZDOT = -3932
340014
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
59177615
00016717 00000-0 10270-3 0 9046
2 25544 51
6450 38
0729 0003500 195
3266 164
7779 15
50315159 13259
Satellite: ISS
Catalog Number: 25544
Epoch time: 14180
59177615 = yrday
fracday
Element set: 904
Inclination: 51
6450 deg
RA of node: 38
0729 deg
Eccentricity:
0003500
Arg of perigee: 195
3266 deg
Mean anomaly: 164
7779 deg
Mean motion: 15
50315159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1325
Checksum: 309
Coasting Arc #6 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2014/181/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1591450
27 A = 6792645
19 meter
Y = 5021305
44 meter E =
0010234
Z = 4285687
35 I = 51
83682
XDOT = -6703
663815 Wp = 127
02426
YDOT = -948
250013 meter/sec RA = 32
66707 deg
ZDOT = 3588
437426 TA = 286
36285
MA = 286
47535
Ha = 226
949 n
mi
Hp = 221
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5221293
54 X = 1514364
36
Y = 16474099
20 feet Y = 5038670
58 meter
Z = 14060654
05 Z = 4293231
62
XDOT = -21993
647687 XDOT = -6709
993312
YDOT = -3111
056472 feet/sec YDOT = -1023
250471 meter/sec
ZDOT = 11773
088669 ZDOT = 3555
856862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11181037
28 X = 3407980
16
Y = -13144125
57 feet Y = -4006329
47 meter
Z = 14091707
19 Z = 4295152
35
XDOT = 8207
734758 XDOT = 2501
717554
YDOT = 19497
518806 feet/sec YDOT = 5942
843732 meter/sec
ZDOT = 11635
001228 ZDOT = 3546
348374
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
62314188
00016717 00000-0 10270-3 0 9050
2 25544 51
6450 32
9600 0003548 201
1467 158
9537 15
50316872 13419
Satellite: ISS
Catalog Number: 25544
Epoch time: 14181
62314188 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 32
9600 deg
Eccentricity:
0003548
Arg of perigee: 201
1467 deg
Mean anomaly: 158
9537 deg
Mean motion: 15
50316872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 293
Coasting Arc #7 (Orbit 1355)
---------------------------------------
Vector Time (GMT): 2014/182/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1489248
80 A = 6791609
27 meter
Y = -4825118
08 meter E =
0007980
Z = -4548620
85 I = 51
80672
XDOT = 6924
756072 Wp = 88
59844
YDOT = 833
757303 meter/sec RA = 27
72116 deg
ZDOT = -3156
246980 TA = 149
78523
MA = 149
73919
Ha = 226
925 n
mi
Hp = 220
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4885986
89 X = -1413087
05
Y = -15830439
90 feet Y = -4841345
55 meter
Z = -14923296
77 Z = -4555670
80
XDOT = 22719
015985 XDOT = 6930
250010
YDOT = 2735
424223 feet/sec YDOT = 911
225394 meter/sec
ZDOT = -10355
141010 ZDOT = -3122
594431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10602382
95 X = -3231606
32
Y = 12696418
94 feet Y = 3869868
49 meter
Z = -14952287
57 Z = -4557457
25
XDOT = -9295
597991 XDOT = -2833
298268
YDOT = -19771
753299 feet/sec YDOT = -6026
430406 meter/sec
ZDOT = -10212
486361 ZDOT = -3112
765843
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
59004122
00016717 00000-0 10270-3 0 9062
2 25544 51
6448 28
1672 0003502 201
0983 159
0024 15
50339963 13569
Satellite: ISS
Catalog Number: 25544
Epoch time: 14182
59004122 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 28
1672 deg
Eccentricity:
0003502
Arg of perigee: 201
0983 deg
Mean anomaly: 159
0024 deg
Mean motion: 15
50339963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1356
Checksum: 285
Coasting Arc #8 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2014/183/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1380099
33 A = 6790800
31 meter
Y = 4643306
24 meter E =
0008445
Z = 4757668
06 I = 51
77583
XDOT = -7132
957625 Wp = 142
36525
YDOT = -673
349822 meter/sec RA = 22
77232 deg
ZDOT = 2717
213865 TA = 280
75463
MA = 280
84969
Ha = 226
785 n
mi
Hp = 221
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4527884
95 X = 1304963
25
Y = 15233944
36 feet Y = 4658318
90 meter
Z = 15609147
19 Z = 4764190
21
XDOT = -23402
091944 XDOT = -7138
097162
YDOT = -2209
152958 feet/sec YDOT = -753
144101 meter/sec
ZDOT = 8914
743652 ZDOT = 2682
550747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10093714
84 X = 3076564
28
Y = -12241522
20 feet Y = -3731215
97 meter
Z = 15635930
86 Z = 4765831
73
XDOT = 10495
040757 XDOT = 3198
888423
YDOT = 19890
567810 feet/sec YDOT = 6062
645069 meter/sec
ZDOT = 8767
775487 ZDOT = 2672
417968
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
62139373
00016717 00000-0 10270-3 0 9075
2 25544 51
6446 23
0542 0003542 207
0955 153
0011 15
50331019 13728
Satellite: ISS
Catalog Number: 25544
Epoch time: 14183
62139373 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 23
0542 deg
Eccentricity:
0003542
Arg of perigee: 207
0955 deg
Mean anomaly: 153
0011 deg
Mean motion: 15
50331019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1372
Checksum: 267
Coasting Arc #9 (Orbit 1386)
---------------------------------------
Vector Time (GMT): 2014/184/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1210425
02 A = 6789927
48 meter
Y = -4492434
74 meter E =
0010297
Z = -4954331
32 I = 51
74487
XDOT = 7303
523628 Wp = 87
93165
YDOT = 495
183956 meter/sec RA = 17
82175 deg
ZDOT = -2237
048226 TA = 160
23860
MA = 160
19868
Ha = 226
759 n
mi
Hp = 221
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3971210
69 X = -1136033
25
Y = -14738959
13 feet Y = -4505554
19 meter
Z = -16254367
85 Z = -4960030
99
XDOT = 23961
691694 XDOT = 7308
310337
YDOT = 1624
619277 feet/sec YDOT = 576
883583 meter/sec
ZDOT = -7339
397068 ZDOT = -2201
557324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9801298
88 X = -2987435
90
Y = 11669760
96 feet Y = 3556943
14 meter
Z = -16277687
93 Z = -4961439
28
XDOT = -11684
380312 XDOT = -3561
399119
YDOT = -19824
353189 feet/sec YDOT = -6042
462852 meter/sec
ZDOT = -7188
889245 ZDOT = -2191
173442
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
58828034
00016717 00000-0 10270-3 0 9081
2 25544 51
6454 18
2619 0003499 206
9937 153
1032 15
50362521 13879
Satellite: ISS
Catalog Number: 25544
Epoch time: 14184
58828034 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 18
2619 deg
Eccentricity:
0003499
Arg of perigee: 206
9937 deg
Mean anomaly: 153
1032 deg
Mean motion: 15
50362521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1387
Checksum: 314
Coasting Arc #10 (Orbit 1402)
---------------------------------------
Vector Time (GMT): 2014/185/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1037683
64 A = 6789352
14 meter
Y = 4363640
90 meter E =
0006369
Z = 5096246
16 I = 51
71253
XDOT = -7453
976147 Wp = 157
74476
YDOT = -282
892589 meter/sec RA = 12
86770 deg
ZDOT = 1753
510264 TA = 275
26837
MA = 275
34105
Ha = 226
622 n
mi
Hp = 221
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3404473
89 X = 964055
47
Y = 14316407
14 feet Y = 4374832
91 meter
Z = 16719967
72 Z = 5101108
52
XDOT = -24455
302319 XDOT = -7458
776733
YDOT = -928
125292 feet/sec YDOT = -366
274709 meter/sec
ZDOT = 5752
986431 ZDOT = 1717
288371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9595246
44 X = 2924631
11
Y = -11127401
15 feet Y = -3391631
87 meter
Z = 16739757
04 Z = 5102277
95
XDOT = 12922
923648 XDOT = 3938
907128
YDOT = 19598
952580 feet/sec YDOT = 5973
760746 meter/sec
ZDOT = 5599
344118 ZDOT = 1706
680087
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
61961968
00016717 00000-0 10270-3 0 9091
2 25544 51
6450 13
1489 0003506 212
9355 147
1578 15
50345817 14030
Satellite: ISS
Catalog Number: 25544
Epoch time: 14185
61961968 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 13
1489 deg
Eccentricity:
0003506
Arg of perigee: 212
9355 deg
Mean anomaly: 147
1578 deg
Mean motion: 15
50345817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1403
Checksum: 315
Coasting Arc #11 (Orbit 1417)
---------------------------------------
Vector Time (GMT): 2014/186/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -818725
26 A = 6788743
78 meter
Y = -4277236
35 meter E =
0012023
Z = -5218169
84 I = 51
68146
XDOT = 7552
540457 Wp = 92
68200
YDOT = 61
561326 meter/sec RA = 7
91264 deg
ZDOT = -1238
464295 TA = 165
43306
MA = 165
39838
Ha = 226
571 n
mi
Hp = 221
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2686106
50 X = -745487
23
Y = -14032927
64 feet Y = -4285981
99 meter
Z = -17119979
79 Z = -5221969
50
XDOT = 24778
676040 XDOT = 7557
306794
YDOT = 201
972855 feet/sec YDOT = 146
045432 meter/sec
ZDOT = -4063
203066 ZDOT = -1201
763586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9612974
34 X = -2930034
58
Y = 10545380
36 feet Y = 3214231
93 meter
Z = -17135273
90 Z = -5222831
49
XDOT = -14079
746325 XDOT = -4291
506680
YDOT = -19168
081584 feet/sec YDOT = -5842
431267 meter/sec
ZDOT = -3907
494706 ZDOT = -1191
004386
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
58649330
00016717 00000-0 10270-3 0 9106
2 25544 51
6462 8
3572 0003478 213
7466 146
3463 15
50385079 14186
Satellite: ISS
Catalog Number: 25544
Epoch time: 14186
58649330 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 8
3572 deg
Eccentricity:
0003478
Arg of perigee: 213
7466 deg
Mean anomaly: 146
3463 deg
Mean motion: 15
50385079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1418
Checksum: 316
Coasting Arc #12 (Orbit 1433)
---------------------------------------
Vector Time (GMT): 2014/187/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 602686
78 A = 6788487
41 meter
Y = 4217948
48 meter E =
0004037
Z = 5284753
13 I = 51
64897
XDOT = -7626
495931 Wp = 172
12971
YDOT = 179
158860 meter/sec RA = 2
95337 deg
ZDOT = 722
778730 TA = 270
93911
MA = 270
98537
Ha = 226
447 n
mi
Hp = 221
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1977318
83 X = 529804
27
Y = 13838413
66 feet Y = 4224280
18 meter
Z = 17338428
91 Z = 5287504
21
XDOT = -25021
312108 XDOT = -7631
443535
YDOT = 587
791534 feet/sec YDOT = 93
846753 meter/sec
ZDOT = 2371
321292 ZDOT = 685
718255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9716750
05 X = 2961665
42
Y = -10030939
84 feet Y = -3057430
46 meter
Z = 17349282
80 Z = 5288061
40
XDOT = 15220
711299 XDOT = 4639
272804
YDOT = 18595
865245 feet/sec YDOT = 5668
019727 meter/sec
ZDOT = 2214
047424 ZDOT = 674
841655
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
61781937
00016717 00000-0 10270-3 0 9112
2 25544 51
6457 3
2440 0003454 219
5015 140
5884 15
50361948 14346
Satellite: ISS
Catalog Number: 25544
Epoch time: 14187
61781937 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 3
2440 deg
Eccentricity:
0003454
Arg of perigee: 219
5015 deg
Mean anomaly: 140
5884 deg
Mean motion: 15
50361948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1434
Checksum: 302
Coasting Arc #13 (Orbit 1448)
---------------------------------------
Vector Time (GMT): 2014/188/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -358592
51 A = 6788215
58 meter
Y = -4208036
69 meter E =
0012753
Z = -5325304
59 I = 51
61833
XDOT = 7639
651259 Wp = 99
91935
YDOT = -416
498154 meter/sec RA = 357
99374 deg
ZDOT = -187
848513 TA = 168
30118
MA = 168
27151
Ha = 226
355 n
mi
Hp = 221
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1176484
61 X = -285641
97
Y = -13805894
64 feet Y = -4211638
30 meter
Z = -17471471
74 Z = -5326869
79
XDOT = 25064
472635 XDOT = 7644
653348
YDOT = -1366
463760 feet/sec YDOT = -331
038672 meter/sec
ZDOT = -616
300895 ZDOT = -150
723988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10024347
14 X = -3055421
01
Y = 9554885
33 feet Y = 2912329
05 meter
Z = -17477293
80 Z = -5327079
15
XDOT = -16208
673573 XDOT = -4940
403705
YDOT = -17828
942030 feet/sec YDOT = -5434
261531 meter/sec
ZDOT = -458
715077 ZDOT = -139
816355
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
58467976
00016717 00000-0 10270-3 0 9124
2 25544 51
6467 358
4526 0003448 221
6896 138
3993 15
50407924 14498
Satellite: ISS
Catalog Number: 25544
Epoch time: 14188
58467976 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 358
4526 deg
Eccentricity:
0003448
Arg of perigee: 221
6896 deg
Mean anomaly: 138
3993 deg
Mean motion: 15
50407924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1449
Checksum: 356
Coasting Arc #14 (Orbit 1464)
---------------------------------------
Vector Time (GMT): 2014/189/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 124434
44 A = 6788332
93 meter
Y = 4226884
05 meter E =
0001538
Z = 5310203
50 I = 51
58722
XDOT = -7626
901675 Wp = 178
56301
YDOT = 656
548711 meter/sec RA = 353
02961 deg
ZDOT = -345
387772 TA = 274
72587
MA = 274
74344
Ha = 226
256 n
mi
Hp = 221
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 408249
49 X = 51363
93
Y = 13867729
84 feet Y = 4227866
39 meter
Z = 17421927
49 Z = 5310630
99
XDOT = -25022
643291 XDOT = -7631
998719
YDOT = 2154
031205 feet/sec YDOT = 571
231331 meter/sec
ZDOT = -1133
161983 ZDOT = -382
450532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10401337
80 X = 3170327
76
Y = -9179231
15 feet Y = -2797829
65 meter
Z = 17422917
19 Z = 5310505
16
XDOT = 17120
204565 XDOT = 5218
238352
YDOT = 16959
380915 feet/sec YDOT = 5169
219303 meter/sec
ZDOT = -1290
528875 ZDOT = -393
353201
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
61599234
00016717 00000-0 10270-3 0 9133
2 25544 51
6465 353
3392 0003400 227
1156 132
9710 15
50380003 14652
Satellite: ISS
Catalog Number: 25544
Epoch time: 14189
61599234 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 353
3392 deg
Eccentricity:
0003400
Arg of perigee: 227
1156 deg
Mean anomaly: 132
9710 deg
Mean motion: 15
50380003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1465
Checksum: 289
Coasting Arc #15 (Orbit 1479)
---------------------------------------
Vector Time (GMT): 2014/190/13:38:21
794
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 117345
27 A = 6788432
31 meter
Y = -4296491
62 meter E =
0012301
Z = -5265069
11 I = 51
55784
XDOT = 7551
277239 Wp = 108
38679
YDOT = -879
152709 meter/sec RA = 348
06542 deg
ZDOT = 883
628765 TA = 170
10205
MA = 170
07780
Ha = 226
120 n
mi
Hp = 221
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 384991
06 X = 190956
87
Y = -14096101
12 feet Y = -4294767
11 meter
Z = -17273848
78 Z = -5264320
83
XDOT = 24774
531623 XDOT = 7556
254519
YDOT = -2884
359280 feet/sec YDOT = -794
681756 meter/sec
ZDOT = 2899
044504 ZDOT = 920
323726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10935450
40 X = -3333125
28
Y = 8910826
43 feet Y = 2716019
90 meter
Z = -17269835
95 Z = -5263846
00
XDOT = -17820
809653 XDOT = -5431
782782
YDOT = -15935
956115 feet/sec YDOT = -4857
279424 meter/sec
ZDOT = 3054
893188 ZDOT = 931
131444
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
58283950
00016717 00000-0 10270-3 0 9147
2 25544 51
6472 348
5475 0003420 230
6211 129
4637 15
50430080 14808
Satellite: ISS
Catalog Number: 25544
Epoch time: 14190
58283950 = yrday
fracday
Element set: 914
Inclination: 51
6472 deg
RA of node: 348
5475 deg
Eccentricity:
0003420
Arg of perigee: 230
6211 deg
Mean anomaly: 129
4637 deg
Mean motion: 15
50430080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1480
Checksum: 289
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