[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 30th 2015
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) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3462)
---------------------------------------
Vector Time (GMT): 2015/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4065241
85 A = 6775423
45 meter
Y = -1553314
71 meter E =
0004686
Z = 5190508
11 I = 51
33215
XDOT = 3944
420440 Wp = 48
23806
YDOT = 6480
060125 meter/sec RA = 231
72577 deg
ZDOT = -1146
333889 TA = 52
81566
MA = 52
77289
Ha = 219
726 n
mi
Hp = 213
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13337407
66 X = 4057096
14
Y = -5096176
88 feet Y = -1507900
47 meter
Z = 17029226
09 Z = 5210236
03
XDOT = 12941
011941 XDOT = 3877
234058
YDOT = 21260
039781 feet/sec YDOT = 6523
793651 meter/sec
ZDOT = -3760
937955 ZDOT = -1127
335653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11894834
16 X = -3625545
45
Y = -7711236
50 feet Y = -2350384
88 meter
Z = 17114372
76 Z = 5216460
82
XDOT = 9023
648527 XDOT = 2750
408071
YDOT = -22114
524577 feet/sec YDOT = -6740
507091 meter/sec
ZDOT = -3680
342913 ZDOT = -1121
768520
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 15210
54630617
00016717 00000-0 10270-3 0 9008
2 25544 51
6412 232
5206 0001041 14
5956 345
5227 15
54932361 34630
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
54630617 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 232
5206 deg
Eccentricity:
0001041
Arg of perigee: 14
5956 deg
Mean anomaly: 345
5227 deg
Mean motion: 15
54932361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 272
Coasting Arc #2 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2015/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5098379
36 A = 6778441
69 meter
Y = -198366
30 meter E =
0009496
Z = -4471829
19 I = 51
36322
XDOT = -2563
554580 Wp = 104
00273
YDOT = -6465
517711 meter/sec RA = 226
70154 deg
ZDOT = 3213
036812 TA = 198
45219
MA = 198
48666
Ha = 219
859 n
mi
Hp = 213
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16726966
41 X = -5074060
24
Y = -650808
08 feet Y = -255243
46 meter
Z = -14671355
61 Z = -4496536
57
XDOT = -8410
612140 XDOT = -2506
672484
YDOT = -21212
328448 feet/sec YDOT = -6493
867220 meter/sec
ZDOT = 10541
459357 ZDOT = 3200
721559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9481608
55 X = 2889994
29
Y = 13681534
07 feet Y = 4170131
58 meter
Z = -14777630
27 Z = -4504221
71
XDOT = -10851
330855 XDOT = -3307
485645
YDOT = 18837
879969 feet/sec YDOT = 5741
785815 meter/sec
ZDOT = 10489
594044 ZDOT = 3197
228265
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 15211
51034084
00016717 00000-0 10270-3 0 9013
2 25544 51
6418 227
7090 0001129 11
9170 348
2009 15
54916617 34789
Satellite: ISS
Catalog Number: 25544
Epoch time: 15211
51034084 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 227
7090 deg
Eccentricity:
0001129
Arg of perigee: 11
9170 deg
Mean anomaly: 348
2009 deg
Mean motion: 15
54916617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 286
Coasting Arc #3 (Orbit 3493)
---------------------------------------
Vector Time (GMT): 2015/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5749216
76 A = 6782707
58 meter
Y = 1803433
43 meter E =
0013268
Z = 3102890
81 I = 51
39894
XDOT = 783
175927 Wp = 89
84225
YDOT = 5888
179412 meter/sec RA = 221
69018 deg
ZDOT = -4855
345736 TA = 54
29660
MA = 54
17320
Ha = 219
788 n
mi
Hp = 213
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18862259
73 X = 5713550
71
Y = 5916776
34 feet Y = 1867525
39 meter
Z = 10180087
96 Z = 3130732
20
XDOT = 2569
474825 XDOT = 740
859586
YDOT = 19318
173925 feet/sec YDOT = 5896
701004 meter/sec
ZDOT = -15929
611994 ZDOT = -4851
643833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6894466
58 X = -2101433
41
Y = -18461097
71 feet Y = -5626942
58 meter
Z = 10299586
26 Z = 3139313
89
XDOT = 12242
420968 XDOT = 3731
489911
YDOT = -13483
612031 feet/sec YDOT = -4109
804947 meter/sec
ZDOT = -15914
692885 ZDOT = -4850
798391
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 15212
53863657
00016717 00000-0 10270-3 0 9023
2 25544 51
6403 222
5754 0001217 18
3157 341
8039 15
54967928 34948
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
53863657 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 222
5754 deg
Eccentricity:
0001217
Arg of perigee: 18
3157 deg
Mean anomaly: 341
8039 deg
Mean motion: 15
54967928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3494
Checksum: 315
Coasting Arc #4 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2015/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5897167
31 A = 6786013
06 meter
Y = -3075004
12 meter E =
0009761
Z = -1327252
37 I = 51
43505
XDOT = 1231
787482 Wp = 36
88762
YDOT = -4855
645897 meter/sec RA = 216
69451 deg
ZDOT = 5806
517010 TA = 308
61744
MA = 308
70479
Ha = 219
801 n
mi
Hp = 213
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19347661
78 X = -5855896
44
Y = -10088596
19 feet Y = -3140719
33 meter
Z = -4354502
53 Z = -1355798
82
XDOT = 4041
297513 XDOT = 1257
787710
YDOT = -15930
596774 feet/sec YDOT = -4841
725979 meter/sec
ZDOT = 19050
252659 ZDOT = 5812
563711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4294945
49 X = 1309099
39
Y = 21367846
49 feet Y = 6512919
61 meter
Z = -4476836
09 Z = -1364539
64
XDOT = -13295
015864 XDOT = -4052
320835
YDOT = 6649
230768 feet/sec YDOT = 2026
685538 meter/sec
ZDOT = 19077
099348 ZDOT = 5814
699881
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 15213
50265760
00016717 00000-0 10270-3 0 9033
2 25544 51
6407 217
7638 0001078 27
4510 332
6700 15
54996520 35098
Satellite: ISS
Catalog Number: 25544
Epoch time: 15213
50265760 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 217
7638 deg
Eccentricity:
0001078
Arg of perigee: 27
4510 deg
Mean anomaly: 332
6700 deg
Mean motion: 15
54996520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 295
Coasting Arc #5 (Orbit 3524)
---------------------------------------
Vector Time (GMT): 2015/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5441095
48 A = 6786729
54 meter
Y = 3992903
81 meter E =
0010251
Z = -674626
09 I = 51
46224
XDOT = -3315
035581 Wp = 133
47295
YDOT = 3522
837094 meter/sec RA = 211
70611 deg
ZDOT = -5950
101261 TA = 53
83254
MA = 53
73774
Ha = 219
938 n
mi
Hp = 213
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17851363
12 X = 5399318
49
Y = 13100078
11 feet Y = 4053516
12 meter
Z = -2213340
18 Z = -648296
34
XDOT = -10876
100989 XDOT = -3325
279672
YDOT = 11557
864483 feet/sec YDOT = 3485
708907 meter/sec
ZDOT = -19521
329598 ZDOT = -5966
229600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1419462
52 X = -432652
18
Y = -22107789
11 feet Y = -6738454
12 meter
Z = -2100683
98 Z = -640288
48
XDOT = 14150
140034 XDOT = 4312
962682
YDOT = 932
095692 feet/sec YDOT = 284
102767 meter/sec
ZDOT = -19591
338505 ZDOT = -5971
439976
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 15214
53093926
00016717 00000-0 10270-3 0 9041
2 25544 51
6399 212
6298 0001243 25
4261 334
6953 15
54962525 35257
Satellite: ISS
Catalog Number: 25544
Epoch time: 15214
53093926 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 212
6298 deg
Eccentricity:
0001243
Arg of perigee: 25
4261 deg
Mean anomaly: 334
6953 deg
Mean motion: 15
54962525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3525
Checksum: 312
Coasting Arc #6 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2015/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4394457
18 A = 6784078
59 meter
Y = -4484613
19 meter E =
0014379
Z = 2550492
76 I = 51
48133
XDOT = 5185
305251 Wp = 72
47190
YDOT = -2077
782093 meter/sec RA = 206
71737 deg
ZDOT = 5260
523246 TA = 316
27944
MA = 316
39324
Ha = 219
839 n
mi
Hp = 213
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14417510
45 X = -4356371
67
Y = -14713297
87 feet Y = -4533541
91 meter
Z = 8367758
41 Z = 2529238
30
XDOT = 17012
156334 XDOT = 5182
600935
YDOT = -6816
870384 feet/sec YDOT = -2019
811650 meter/sec
ZDOT = 17258
934533 ZDOT = 5285
705462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1642220
63 X = -500548
85
Y = 20570835
29 feet Y = 6269990
60 meter
Z = 8277014
50 Z = 2522834
02
XDOT = -14719
127846 XDOT = -4486
390167
YDOT = -8190
249153 feet/sec YDOT = -2496
387942 meter/sec
ZDOT = 17367
676278 ZDOT = 5293
667729
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 15215
55921134
00016717 00000-0 10270-3 0 9056
2 25544 51
6400 207
4973 0001131 21
6310 338
4891 15
55006762 35415
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
55921134 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 207
4973 deg
Eccentricity:
0001131
Arg of perigee: 21
6310 deg
Mean anomaly: 338
4891 deg
Mean motion: 15
55006762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 275
Coasting Arc #7 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2015/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2795996
96 A = 6779791
80 meter
Y = 4625982
67 meter E =
0008332
Z = -4101499
18 I = 51
49538
XDOT = -6618
157674 Wp = 65
50330
YDOT = 625
590078 meter/sec RA = 201
71755 deg
ZDOT = -3808
740990 TA = 165
06949
MA = 165
04488
Ha = 219
937 n
mi
Hp = 213
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9173218
37 X = 2763983
57
Y = 15177108
50 feet Y = 4657070
27 meter
Z = -13456362
14 Z = -4087994
80
XDOT = -21713
115727 XDOT = -6606
160119
YDOT = 2052
460885 feet/sec YDOT = 551
648505 meter/sec
ZDOT = -12495
869390 ZDOT = -3840
861138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5113340
43 X = 1558546
16
Y = -17026068
25 feet Y = -5189545
60 meter
Z = -13398992
10 Z = -4084012
79
XDOT = 14731
513995 XDOT = 4490
165466
YDOT = 14359
932177 feet/sec YDOT = 4376
907327 meter/sec
ZDOT = -12634
245266 ZDOT = -3850
917957
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 15216
52321221
00016717 00000-0 10270-3 0 9066
2 25544 51
6398 202
6842 0001313 28
0350 332
0873 15
54978097 35564
Satellite: ISS
Catalog Number: 25544
Epoch time: 15216
52321221 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 202
6842 deg
Eccentricity:
0001313
Arg of perigee: 28
0350 deg
Mean anomaly: 332
0873 deg
Mean motion: 15
54978097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 294
Coasting Arc #8 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2015/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -827230
24 A = 6775980
65 meter
Y = -4438980
37 meter E =
0005524
Z = 5048309
76 I = 51
51272
XDOT = 7417
650841 Wp = 110
85172
YDOT = 705
462271 meter/sec RA = 196
70733 deg
ZDOT = 1832
241537 TA = 321
36650
MA = 321
40600
Ha = 219
890 n
mi
Hp = 213
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2714009
97 X = -802053
55
Y = -14563583
89 feet Y = -4448090
16 meter
Z = 16562696
06 Z = 5044352
48
XDOT = 24336
124807 XDOT = 7400
310648
YDOT = 2314
508762 feet/sec YDOT = 788
314382 meter/sec
ZDOT = 6011
291132 ZDOT = 1868
232540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8751790
43 X = -2667545
72
Y = 11975385
98 feet Y = 3650097
65 meter
Z = 16546389
98 Z = 5043339
67
XDOT = -13964
406767 XDOT = -4256
351182
YDOT = -18741
234459 feet/sec YDOT = -5712
328263 meter/sec
ZDOT = 6166
125369 ZDOT = 1879
435013
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 15217
55147021
00016717 00000-0 10270-3 0 9075
2 25544 51
6397 197
5515 0001351 24
0162 336
1054 15
54999774 35720
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
55147021 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 197
5515 deg
Eccentricity:
0001351
Arg of perigee: 24
0162 deg
Mean anomaly: 336
1054 deg
Mean motion: 15
54999774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 309
Coasting Arc #9 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2015/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1314848
56 A = 6774873
13 meter
Y = 4027182
81 meter E =
0015503
Z = -5300348
99 I = 51
53991
XDOT = -7414
290653 Wp = 88
73906
YDOT = -1872
869291 meter/sec RA = 191
69023 deg
ZDOT = 417
644186 TA = 185
24626
MA = 185
26252
Ha = 219
934 n
mi
Hp = 212
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4313807
61 X = -1334036
87
Y = 13212542
02 feet Y = 4012372
02 meter
Z = -17389596
42 Z = -5306782
82
XDOT = -24325
100568 XDOT = -7394
825474
YDOT = -6144
584289 feet/sec YDOT = -1955
671921 meter/sec
ZDOT = 1370
223708 ZDOT = 381
674585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12436892
82 X = 3790764
93
Y = -6125079
32 feet Y = -1866924
18 meter
Z = -17417961
04 Z = -5308994
52
XDOT = 11986
367889 XDOT = 3653
444933
YDOT = 20894
148076 feet/sec YDOT = 6368
536334 meter/sec
ZDOT = 1215
657214 ZDOT = 370
532319
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 15218
51545494
00016717 00000-0 10270-3 0 9089
2 25544 51
6398 192
7391 0001395 30
2522 329
8711 15
54997874 35871
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
51545494 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 192
7391 deg
Eccentricity:
0001395
Arg of perigee: 30
2522 deg
Mean anomaly: 329
8711 deg
Mean motion: 15
54997874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 344
Coasting Arc #10 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2015/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3376227
21 A = 6776936
27 meter
Y = -3418342
81 meter E =
0008586
Z = 4775241
98 I = 51
57842
XDOT = 6617
674427 Wp = 56
27285
YDOT = 2866
319556 meter/sec RA = 186
67740 deg
ZDOT = -2618
974720 TA = 59
59851
MA = 59
51368
Ha = 219
790 n
mi
Hp = 212
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11076860
92 X = 3391004
87
Y = -11215035
46 feet Y = -3380505
06 meter
Z = 15666804
40 Z = 4791678
75
XDOT = 21711
530272 XDOT = 6597
852605
YDOT = 9403
935551 feet/sec YDOT = 2940
211942 meter/sec
ZDOT = -8592
436744 ZDOT = -2586
875710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15691308
43 X = -4782710
81
Y = 127255
11 feet Y = 38787
36 meter
Z = 15738147
10 Z = 4796987
24
XDOT = -8675
953565 XDOT = -2644
430647
YDOT = -20917
947096 feet/sec YDOT = -6375
790275 meter/sec
ZDOT = -8454
682879 ZDOT = -2576
987341
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 15219
54369682
00016717 00000-0 10270-3 0 9097
2 25544 51
6397 187
6061 0001418 28
2721 331
8508 15
55027010 36034
Satellite: ISS
Catalog Number: 25544
Epoch time: 15219
54369682 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 187
6061 deg
Eccentricity:
0001418
Arg of perigee: 28
2721 deg
Mean anomaly: 331
8508 deg
Mean motion: 15
55027010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 305
Coasting Arc #11 (Orbit 3617)
---------------------------------------
Vector Time (GMT): 2015/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5088061
21 A = 6781182
74 meter
Y = 2693707
58 meter E =
0006180
Z = -3588218
31 I = 51
62433
XDOT = -5063
068308 Wp = 85
98320
YDOT = -3663
061198 meter/sec RA = 181
67758 deg
ZDOT = 4436
510753 TA = 231
58549
MA = 231
64099
Ha = 219
905 n
mi
Hp = 212
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16693114
22 X = -5100374
70
Y = 8837623
29 feet Y = 2636740
78 meter
Z = -11772369
78 Z = -3612964
72
XDOT = -16611
116497 XDOT = -5043
281475
YDOT = -12017
917317 feet/sec YDOT = -3719
569229 meter/sec
ZDOT = 14555
481473 ZDOT = 4411
963555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18077475
39 X = 5510014
50
Y = 5238062
32 feet Y = 1596561
39 meter
Z = -11879390
75 Z = -3620838
30
XDOT = 3993
098156 XDOT = 1217
096318
YDOT = 18939
317555 feet/sec YDOT = 5772
703991 meter/sec
ZDOT = 14450
364843 ZDOT = 4404
471204
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 15220
50766607
00016717 00000-0 10270-3 0 9105
2 25544 51
6397 182
7939 0001496 32
0262 328
0982 15
55017588 36182
Satellite: ISS
Catalog Number: 25544
Epoch time: 15220
50766607 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 182
7939 deg
Eccentricity:
0001496
Arg of perigee: 32
0262 deg
Mean anomaly: 328
0982 deg
Mean motion: 15
55017588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3618
Checksum: 321
Coasting Arc #12 (Orbit 3633)
---------------------------------------
Vector Time (GMT): 2015/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6260815
41 A = 6785139
80 meter
Y = -1826670
21 meter E =
0014311
Z = 1849919
69 I = 51
67008
XDOT = 2929
394454 Wp = 107
74056
YDOT = 4296
898831 meter/sec RA = 176
69373 deg
ZDOT = -5639
629193 TA = 51
90262
MA = 51
77364
Ha = 219
876 n
mi
Hp = 212
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20540732
98 X = 6271790
26
Y = -5993012
51 feet Y = -1756596
36 meter
Z = 6069290
32 Z = 1880359
74
XDOT = 9610
874194 XDOT = 2908
522637
YDOT = 14097
437108 feet/sec YDOT = 4329
540715 meter/sec
ZDOT = -18502
720449 ZDOT = -5625
449504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19051245
20 X = -5806819
54
Y = -9657922
51 feet Y = -2943734
78 meter
Z = 6200708
39 Z = 1889975
92
XDOT = 1845
839969 XDOT = 562
612023
YDOT = -15546
934495 feet/sec YDOT = -4738
705634 meter/sec
ZDOT = -18442
350484 ZDOT = -5621
228428
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 15221
53589168
00016717 00000-0 10270-3 0 9115
2 25544 51
6402 177
6603 0001496 33
8761 326
2487 15
55049624 36347
Satellite: ISS
Catalog Number: 25544
Epoch time: 15221
53589168 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 177
6603 deg
Eccentricity:
0001496
Arg of perigee: 33
8761 deg
Mean anomaly: 326
2487 deg
Mean motion: 15
55049624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3634
Checksum: 316
Coasting Arc #13 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2015/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6721670
55 A = 6786590
41 meter
Y = 878199
56 meter E =
0013706
Z = 125079
67 I = 51
70677
XDOT = -498
535023 Wp = 45
85829
YDOT = -4729
870364 meter/sec RA = 171
72160 deg
ZDOT = 6019
002115 TA = 315
48862
MA = 315
59864
Ha = 219
865 n
mi
Hp = 212
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22052724
91 X = -6731598
81
Y = 2881232
16 feet Y = 802977
91 meter
Z = 410366
38 Z = 92403
53
XDOT = -1635
613592 XDOT = -474
845009
YDOT = -15517
947390 feet/sec YDOT = -4735
313028 meter/sec
ZDOT = 19747
382266 ZDOT = 6016
637768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18275968
98 X = 5570515
34
Y = 12677102
54 feet Y = 3863980
85 meter
Z = 269452
55 Z = 82129
14
XDOT = -8190
933621 XDOT = -2496
596568
YDOT = 11346
550997 feet/sec YDOT = 3458
428744 meter/sec
ZDOT = 19737
975331 ZDOT = 6016
134881
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 15222
56410799
00016717 00000-0 10270-3 0 9123
2 25544 51
6402 172
5272 0001446 37
8959 322
2296 15
55071124 36503
Satellite: ISS
Catalog Number: 25544
Epoch time: 15222
56410799 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 172
5272 deg
Eccentricity:
0001446
Arg of perigee: 37
8959 deg
Mean anomaly: 322
2296 deg
Mean motion: 15
55071124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 300
Coasting Arc #14 (Orbit 3664)
---------------------------------------
Vector Time (GMT): 2015/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6439136
70 A = 6784714
45 meter
Y = 205824
84 meter E =
0006352
Z = -2124829
23 I = 51
73305
XDOT = -1974
559175 Wp = 125
92499
YDOT = 4938
686480 meter/sec RA = 166
75091 deg
ZDOT = -5520
542262 TA = 77
58698
MA = 77
51590
Ha = 219
910 n
mi
Hp = 212
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21125776
56 X = 6446677
97
Y = 675278
35 feet Y = 277873
71 meter
Z = -6971224
50 Z = -2093531
43
XDOT = -6478
212518 XDOT = -2002
821790
YDOT = 16203
039633 feet/sec YDOT = 4916
447755 meter/sec
ZDOT = -18112
015296 ZDOT = -5530
202646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15482975
65 X = -4719210
98
Y = -14453144
91 feet Y = -4405318
57 meter
Z = -6836408
00 Z = -2083737
16
XDOT = 14405
642011 XDOT = 4390
839685
YDOT = -6868
967933 feet/sec YDOT = -2093
661426 meter/sec
ZDOT = -18154
450703 ZDOT = -5533
476574
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 15223
52805349
00016717 00000-0 10270-3 0 9130
2 25544 51
6414 167
7145 0001515 37
2560 322
8698 15
55081167 36656
Satellite: ISS
Catalog Number: 25544
Epoch time: 15223
52805349 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 167
7145 deg
Eccentricity:
0001515
Arg of perigee: 37
2560 deg
Mean anomaly: 322
8698 deg
Mean motion: 15
55081167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3665
Checksum: 310
Coasting Arc #15 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2015/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5455016
13 A = 6780522
71 meter
Y = -1345288
58 meter E =
0012498
Z = 3785321
22 I = 51
75041
XDOT = 4147
268457 Wp = 91
38505
YDOT = -4877
287283 meter/sec RA = 161
77251 deg
ZDOT = 4230
905554 TA = 313
97132
MA = 314
07433
Ha = 219
962 n
mi
Hp = 212
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17897034
53 X = -5457954
64
Y = -4413676
43 feet Y = -1406306
61 meter
Z = 12419032
86 Z = 3758815
22
XDOT = 13606
523808 XDOT = 4180
947507
YDOT = -16001
598699 feet/sec YDOT = -4830
721527 meter/sec
ZDOT = 13880
923732 ZDOT = 4251
133515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10876873
67 X = 3315271
10
Y = 14976531
90 feet Y = 4564846
92 meter
Z = 12305034
46 Z = 3750574
50
XDOT = -19561
345404 XDOT = -5962
298079
YDOT = 2695
930727 feet/sec YDOT = 821
719686 meter/sec
ZDOT = 13968
891456 ZDOT = 4257
718116
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 15224
55625294
00016717 00000-0 10270-3 0 9144
2 25544 51
6419 162
5817 0001433 42
1563 317
9700 15
55102396 36812
Satellite: ISS
Catalog Number: 25544
Epoch time: 15224
55625294 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 162
5817 deg
Eccentricity:
0001433
Arg of perigee: 42
1563 deg
Mean anomaly: 317
9700 deg
Mean motion: 15
55102396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 300
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