[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 21st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
274/22:54:04
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 214
7
Coasting Arc #1 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2015/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5966344
53 A = 6787540
29 meter
Y = 2491089
80 meter E =
0001922
Z = -2061671
01 I = 51
43851
XDOT = -307
382836 Wp = 192
50005
YDOT = -5306
061801 meter/sec RA = 322
61203 deg
ZDOT = -5522
570046 TA = 10
36252
MA = 10
35856
Ha = 220
088 n
mi
Hp = 216
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19574621
16 X = -5983742
20
Y = 8172866
78 feet Y = 2424272
76 meter
Z = -6764012
49 Z = -2090696
92
XDOT = -1008
473871 XDOT = -221
199632
YDOT = -17408
339242 feet/sec YDOT = -5309
017727 meter/sec
ZDOT = -18118
668131 ZDOT = -5523
853497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19642452
39 X = 5987019
49
Y = -7900701
13 feet Y = -2408133
71 meter
Z = -6889586
05 Z = -2099945
83
XDOT = 75
198114 XDOT = 22
920385
YDOT = 15988
316785 feet/sec YDOT = 4873
238956 meter/sec
ZDOT = -18123
177530 ZDOT = -5523
944511
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 15264
52801562
00016717 00000-0 10270-3 0 9004
2 25544 51
6434 323
0629 0005533 302
5152 57
5466 15
54100033 3035
Satellite: ISS
Catalog Number: 25544
Epoch time: 15264
52801562 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 323
0629 deg
Eccentricity:
0005533
Arg of perigee: 302
5152 deg
Mean anomaly: 57
5466 deg
Mean motion: 15
54100033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 303
Checksum: 263
Coasting Arc #2 (Orbit 318)
---------------------------------------
Vector Time (GMT): 2015/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5642654
47 A = 6784061
41 meter
Y = -1367369
03 meter E =
0008186
Z = 3499682
31 I = 51
40231
XDOT = -1323
325367 Wp = 69
43443
YDOT = 6069
900397 meter/sec RA = 317
61785 deg
ZDOT = 4499
502449 TA = 331
90655
MA = 331
95070
Ha = 220
087 n
mi
Hp = 216
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18512645
90 X = 5640525
18
Y = -4486118
87 feet Y = -1304280
77 meter
Z = 11481897
35 Z = 3527088
20
XDOT = -4341
618659 XDOT = -1412
959040
YDOT = 19914
371380 feet/sec YDOT = 6054
601301 meter/sec
ZDOT = 14762
147141 ZDOT = 4492
855770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18423879
84 X = -5615598
58
Y = 4546613
45 feet Y = 1385807
78 meter
Z = 11600269
18 Z = 3535762
04
XDOT = 4700
817831 XDOT = 1432
809275
YDOT = -18586
898648 feet/sec YDOT = -5665
286708 meter/sec
ZDOT = 14732
340753 ZDOT = 4490
417462
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 15265
55686357
00016717 00000-0 10270-3 0 9012
2 25544 51
6434 317
9338 0005545 306
8182 53
2462 15
54115931 3196
Satellite: ISS
Catalog Number: 25544
Epoch time: 15265
55686357 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 317
9338 deg
Eccentricity:
0005545
Arg of perigee: 306
8182 deg
Mean anomaly: 53
2462 deg
Mean motion: 15
54115931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 319
Checksum: 312
Coasting Arc #3 (Orbit 333)
---------------------------------------
Vector Time (GMT): 2015/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5000886
08 A = 6780328
99 meter
Y = 21361
87 meter E =
0008991
Z = -4586914
91 I = 51
36725
XDOT = 2725
592306 Wp = 37
14354
YDOT = -6501
853956 meter/sec RA = 312
61175 deg
ZDOT = -2997
910375 TA = 202
77374
MA = 202
81365
Ha = 220
378 n
mi
Hp = 216
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16407106
55 X = -4978471
78
Y = 70084
88 feet Y = -34436
43 meter
Z = -15048933
45 Z = -4611153
78
XDOT = 8942
231975 XDOT = 2812
657754
YDOT = -21331
541851 feet/sec YDOT = -6470
888054 meter/sec
ZDOT = -9835
663959 ZDOT = -2984
457916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16305827
36 X = 4970016
18
Y = -403723
66 feet Y = -123054
97 meter
Z = -15153397
53 Z = -4618755
57
XDOT = -8594
241965 XDOT = -2619
524951
YDOT = 20323
829920 feet/sec YDOT = 6194
703360 meter/sec
ZDOT = -9776
455572 ZDOT = -2979
863658
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 15266
52139997
00016717 00000-0 10270-3 0 9024
2 25544 51
6437 313
1254 0005545 311
0739 48
9934 15
54118105 3348
Satellite: ISS
Catalog Number: 25544
Epoch time: 15266
52139997 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 313
1254 deg
Eccentricity:
0005545
Arg of perigee: 311
0739 deg
Mean anomaly: 48
9934 deg
Mean motion: 15
54118105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 334
Checksum: 306
Coasting Arc #4 (Orbit 349)
---------------------------------------
Vector Time (GMT): 2015/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4105670
54 A = 6777717
54 meter
Y = 1471721
55 meter E =
0001911
Z = 5188174
38 I = 51
33739
XDOT = -3835
690571 Wp = 341
42128
YDOT = 6534
049152 meter/sec RA = 307
59524 deg
ZDOT = 1183
775717 TA = 97
18749
MA = 97
16577
Ha = 220
410 n
mi
Hp = 215
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13470047
71 X = 4063706
10
Y = 4828482
77 feet Y = 1517399
80 meter
Z = 17021569
49 Z = 5208016
79
XDOT = -12584
286650 XDOT = -3914
221144
YDOT = 21437
169134 feet/sec YDOT = 6490
716973 meter/sec
ZDOT = 3883
778598 ZDOT = 1164
951261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13533820
73 X = -4125108
56
Y = -4322405
15 feet Y = -1317469
09 meter
Z = 17106804
76 Z = 5214154
09
XDOT = 11475
734409 XDOT = 3497
803848
YDOT = -20911
120286 feet/sec YDOT = -6373
709463 meter/sec
ZDOT = 3801
426779 ZDOT = 1158
674882
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 15267
55022673
00016717 00000-0 10270-3 0 9031
2 25544 51
6431 307
9966 0005568 316
1441 43
9270 15
54153300 3506
Satellite: ISS
Catalog Number: 25544
Epoch time: 15267
55022673 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 307
9966 deg
Eccentricity:
0005568
Arg of perigee: 316
1441 deg
Mean anomaly: 43
9270 deg
Mean motion: 15
54153300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 350
Checksum: 291
Coasting Arc #5 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2015/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3085746
92 A = 6777509
34 meter
Y = -2983557
14 meter E =
0011208
Z = -5254215
78 I = 51
31845
XDOT = 4600
448319 Wp = 75
35917
YDOT = -6079
215745 meter/sec RA = 302
57282 deg
ZDOT = 754
362900 TA = 201
86347
MA = 201
91134
Ha = 220
640 n
mi
Hp = 215
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10123841
60 X = -3026631
75
Y = -9788573
28 feet Y = -3017734
15 meter
Z = -17238240
73 Z = -5269061
73
XDOT = 15093
334380 XDOT = 4664
421264
YDOT = -19944
933548 feet/sec YDOT = -6027
412708 meter/sec
ZDOT = 2474
943896 ZDOT = 776
867117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10536093
20 X = 3211401
21
Y = 9225422
99 feet Y = 2811908
93 meter
Z = -17301664
36 Z = -5273547
30
XDOT = -13286
429195 XDOT = -4049
703619
YDOT = 19974
303740 feet/sec YDOT = 6088
167780 meter/sec
ZDOT = 2573
053386 ZDOT = 784
266672
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 15268
51474304
00016717 00000-0 10270-3 0 9041
2 25544 51
6437 303
1880 0005638 320
0426 40
0312 15
54144168 3653
Satellite: ISS
Catalog Number: 25544
Epoch time: 15268
51474304 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 303
1880 deg
Eccentricity:
0005638
Arg of perigee: 320
0426 deg
Mean anomaly: 40
0312 deg
Mean motion: 15
54144168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 365
Checksum: 278
Coasting Arc #6 (Orbit 380)
---------------------------------------
Vector Time (GMT): 2015/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1993147
84 A = 6779494
15 meter
Y = 4406708
31 meter E =
0008886
Z = 4751290
59 I = 51
30787
XDOT = -5053
298163 Wp = 22
60516
YDOT = 5131
814377 meter/sec RA = 297
55170 deg
ZDOT = -2630
092075 TA = 93
51655
MA = 93
41491
Ha = 220
749 n
mi
Hp = 215
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6539198
96 X = 1920642
82
Y = 14457704
44 feet Y = 4428592
32 meter
Z = 15588223
71 Z = 4760796
15
XDOT = -16579
062215 XDOT = -5097
531773
YDOT = 16836
661342 feet/sec YDOT = 5075
057349 meter/sec
ZDOT = -8628
911007 ZDOT = -2654
748231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7465049
30 X = -2275347
03
Y = -13957289
80 feet Y = -4254181
93 meter
Z = 15628376
74 Z = 4763529
23
XDOT = 14249
245148 XDOT = 4343
169921
YDOT = -17438
825222 feet/sec YDOT = -5315
353928 meter/sec
ZDOT = -8736
104213 ZDOT = -2662
764564
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 15269
54354817
00016717 00000-0 10270-3 0 9052
2 25544 51
6422 298
0588 0005637 325
0800 34
9982 15
54201273 3818
Satellite: ISS
Catalog Number: 25544
Epoch time: 15269
54354817 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 298
0588 deg
Eccentricity:
0005637
Arg of perigee: 325
0800 deg
Mean anomaly: 34
9982 deg
Mean motion: 15
54201273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 381
Checksum: 314
Coasting Arc #7 (Orbit 395)
---------------------------------------
Vector Time (GMT): 2015/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -948328
97 A = 6783108
77 meter
Y = -5566732
97 meter E =
0004620
Z = -3757482
09 I = 51
30684
XDOT = 5204
181353 Wp = 39
34560
YDOT = -3728
652715 meter/sec RA = 292
53760 deg
ZDOT = 4216
933439 TA = 275
43901
MA = 275
49171
Ha = 220
892 n
mi
Hp = 215
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3111315
53 X = -867757
40
Y = -18263559
63 feet Y = -5576887
91 meter
Z = -12327697
14 Z = -3761892
33
XDOT = 17074
085805 XDOT = 5225
004878
YDOT = -12233
112582 feet/sec YDOT = -3670
339030 meter/sec
ZDOT = 13835
083461 ZDOT = 4242
265632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4650199
07 X = 1417380
68
Y = 17921205
67 feet Y = 5462383
49 meter
Z = -12345689
42 Z = -3762966
14
XDOT = -14519
342637 XDOT = -4425
495636
YDOT = 13359
597539 feet/sec YDOT = 4072
005330 meter/sec
ZDOT = 13944
921328 ZDOT = 4250
412021
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 15270
50804425
00016717 00000-0 10270-3 0 9066
2 25544 51
6430 293
2499 0005633 329
7273 30
3553 15
54201842 3968
Satellite: ISS
Catalog Number: 25544
Epoch time: 15270
50804425 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 293
2499 deg
Eccentricity:
0005633
Arg of perigee: 329
7273 deg
Mean anomaly: 30
3553 deg
Mean motion: 15
54201842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 396
Checksum: 298
Coasting Arc #8 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2015/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -51437
15 A = 6786741
84 meter
Y = 6369676
28 meter E =
0010779
Z = 2334436
05 I = 51
30630
XDOT = -5120
329333 Wp = 84
33367
YDOT = 1934
292491 meter/sec RA = 287
53267 deg
ZDOT = -5368
189509 TA = 69
50679
MA = 69
39112
Ha = 221
051 n
mi
Hp = 215
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -168757
05 X = -134000
52
Y = 20897888
05 feet Y = 6368639
80 meter
Z = 7658910
94 Z = 2333984
65
XDOT = -16798
980751 XDOT = -5115
501586
YDOT = 6346
103972 feet/sec YDOT = 1877
059756 meter/sec
ZDOT = -17612
170305 ZDOT = -5393
051892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2006137
30 X = -611470
65
Y = -20803196
69 feet Y = -6340814
35 meter
Z = 7655817
47 Z = 2333493
16
XDOT = 14399
804585 XDOT = 4389
060438
YDOT = -7936
831727 feet/sec YDOT = -2419
146311 meter/sec
ZDOT = -17719
650992 ZDOT = -5400
949622
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 15271
53682818
00016717 00000-0 10270-3 0 9071
2 25544 51
6414 288
1197 0005664 334
1746 25
9123 15
54225014 4126
Satellite: ISS
Catalog Number: 25544
Epoch time: 15271
53682818 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 288
1197 deg
Eccentricity:
0005664
Arg of perigee: 334
1746 deg
Mean anomaly: 25
9123 deg
Mean motion: 15
54225014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 412
Checksum: 301
Coasting Arc #9 (Orbit 426)
---------------------------------------
Vector Time (GMT): 2015/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892142
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 927298
72 A = 6788740
06 meter
Y = -6681965
54 meter E =
0014013
Z = -680580
99 I = 51
30531
XDOT = 4856
682712 Wp = 19
41280
YDOT = 74
019569 meter/sec RA = 282
53596 deg
ZDOT = 5938
790334 TA = 333
19804
MA = 333
27038
Ha = 221
020 n
mi
Hp = 215
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3042318
64 X = 1005255
22
Y = -21922459
13 feet Y = -6671160
09 meter
Z = -2232877
27 Z = -675886
01
XDOT = 15933
998399 XDOT = 4826
645219
YDOT = 242
846354 feet/sec YDOT = 128
163077 meter/sec
ZDOT = 19484
220256 ZDOT = 5962
310513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -327048
12 X = -99684
27
Y = 22132288
30 feet Y = 6745921
47 meter
Z = -2211450
26 Z = -674050
04
XDOT = -14104
625323 XDOT = -4299
089798
YDOT = 1732
591938 feet/sec YDOT = 528
094023 meter/sec
ZDOT = 19585
553376 ZDOT = 5969
676669
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 15272
50130269
00016717 00000-0 10270-3 0 9088
2 25544 51
6420 283
3109 0005572 336
8956 23
1946 15
54265345 4273
Satellite: ISS
Catalog Number: 25544
Epoch time: 15272
50130269 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 283
3109 deg
Eccentricity:
0005572
Arg of perigee: 336
8956 deg
Mean anomaly: 23
1946 deg
Mean motion: 15
54265345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 427
Checksum: 305
Coasting Arc #10 (Orbit 442)
---------------------------------------
Vector Time (GMT): 2015/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892142
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1729491
52 A = 6788497
74 meter
Y = 6474280
39 meter E =
0004561
Z = -1079502
89 I = 51
29724
XDOT = -4446
688398 Wp = 116
80022
YDOT = -2160
681849 meter/sec RA = 277
54054 deg
ZDOT = -5855
715459 TA = 74
95850
MA = 74
90802
Ha = 221
261 n
mi
Hp = 214
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5674184
78 X = -1796516
05
Y = 21241077
40 feet Y = 6454565
19 meter
Z = -3541676
15 Z = -1088068
12
XDOT = -14588
872696 XDOT = -4393
751312
YDOT = -7088
851210 feet/sec YDOT = -2210
112356 meter/sec
ZDOT = -19211
664891 ZDOT = -5877
188110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2611295
06 X = 795922
73
Y = -21824065
60 feet Y = -6651975
19 meter
Z = -3579736
13 Z = -1091103
57
XDOT = 13727
136247 XDOT = 4184
031128
YDOT = 4797
525441 feet/sec YDOT = 1462
285754 meter/sec
ZDOT = -19303
803880 ZDOT = -5883
799423
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 15273
53006402
00016717 00000-0 10270-3 0 9094
2 25544 51
6410 278
1802 0005684 341
5418 18
5527 15
54239076 4437
Satellite: ISS
Catalog Number: 25544
Epoch time: 15273
53006402 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 278
1802 deg
Eccentricity:
0005684
Arg of perigee: 341
5418 deg
Mean anomaly: 18
5527 deg
Mean motion: 15
54239076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 443
Checksum: 295
Coasting Arc #11 (Orbit 458)
---------------------------------------
Vector Time (GMT): 2015/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892142
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2421940
73 A = 6785757
92 meter
Y = -5723703
74 meter E =
0014249
Z = 2701889
78 I = 51
28510
XDOT = 3946
409233 Wp = 54
84406
YDOT = 4104
111062 meter/sec RA = 272
54127 deg
ZDOT = 5145
475681 TA = 335
88405
MA = 335
95069
Ha = 221
217 n
mi
Hp = 214
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7945999
77 X = 2472639
60
Y = -18778555
59 feet Y = -5696336
27 meter
Z = 8864467
77 Z = 2713778
98
XDOT = 12947
536854 XDOT = 3875
227576
YDOT = 13464
931307 feet/sec YDOT = 4147
844918 meter/sec
ZDOT = 16881
481893 ZDOT = 5164
473565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4833273
56 X = -1473181
78
Y = 19785943
43 feet Y = 6030755
56 meter
Z = 8916712
42 Z = 2717813
95
XDOT = -13357
363137 XDOT = -4071
324284
YDOT = -10923
717307 feet/sec YDOT = -3329
549035 meter/sec
ZDOT = 16962
617095 ZDOT = 5170
205691
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 15274
55881193
00016717 00000-0 10270-3 0 9107
2 25544 51
6409 273
0506 0005766 344
2953 15
8021 15
54279396 4590
Satellite: ISS
Catalog Number: 25544
Epoch time: 15274
55881193 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 273
0506 deg
Eccentricity:
0005766
Arg of perigee: 344
2953 deg
Mean anomaly: 15
8021 deg
Mean motion: 15
54279396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 459
Checksum: 321
Coasting Arc #12 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2015/274/22:54:04
000
Vector Time (MET): N/A
Weight (LBS) : 907268
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3446682
74 A = 6781102
71 meter
Y = -3969952
53 meter E =
0008189
Z = 4274418
50 I = 51
26849
XDOT = 2794
495604 Wp = 69
43820
YDOT = 6218
906767 meter/sec RA = 270
26455 deg
ZDOT = 3519
935517 TA = 344
52900
MA = 344
55402
Ha = 221
268 n
mi
Hp = 214
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11308014
24 X = 3470055
72
Y = -13024778
63 feet Y = -3931278
37 meter
Z = 14023682
75 Z = 4291219
20
XDOT = 9168
292664 XDOT = 2707
647802
YDOT = 20403
237423 feet/sec YDOT = 6249
671384 meter/sec
ZDOT = 11548
344873 ZDOT = 3533
299317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12716498
37 X = 3875988
70
Y = -11565084
99 feet Y = -3525037
91 meter
Z = 14096779
79 Z = 4296698
48
XDOT = 5706
315793 XDOT = 1739
285054
YDOT = 20430
222627 feet/sec YDOT = 6227
131857 meter/sec
ZDOT = 11604
832160 ZDOT = 3537
152842
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 15275
00888587
00016717 00000-0 10270-3 0 9113
2 25544 51
6405 270
8042 0006056 343
9901 16
1060 15
54260273 4667
Satellite: ISS
Catalog Number: 25544
Epoch time: 15275
00888587 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 270
8042 deg
Eccentricity:
0006056
Arg of perigee: 343
9901 deg
Mean anomaly: 16
1060 deg
Mean motion: 15
54260273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 294
Coasting Arc #13 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2015/275/22:54:04
000
Vector Time (MET): N/A
Weight (LBS) : 907268
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3886413
75 A = 6777892
88 meter
Y = 2303541
69 meter E =
0014703
Z = -5065223
27 I = 51
25811
XDOT = -1994
107270 Wp = 53
29738
YDOT = -7187
790402 meter/sec RA = 265
24202 deg
ZDOT = -1733
689385 TA = 199
80118
MA = 199
85831
Ha = 221
426 n
mi
Hp = 214
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12750701
28 X = -3887278
40
Y = 7557551
49 feet Y = 2260076
01 meter
Z = -16618186
58 Z = -5084105
23
XDOT = -6542
346687 XDOT = -1905
161726
YDOT = -23581
989508 feet/sec YDOT = -7209
592640 meter/sec
ZDOT = -5687
957299 ZDOT = -1743
159864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13363593
74 X = -4073223
37
Y = 6195710
46 feet Y = 1888452
55 meter
Z = -16699958
90 Z = -5090147
47
XDOT = -3558
355091 XDOT = -1084
586632
YDOT = -23158
056047 feet/sec YDOT = -7058
575483 meter/sec
ZDOT = -5727
507646 ZDOT = -1745
744330
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 15275
97332133
00016717 00000-0 10270-3 0 9121
2 25544 51
6398 265
9946 0005888 348
7739 11
3282 15
54292902 4814
Satellite: ISS
Catalog Number: 25544
Epoch time: 15275
97332133 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 265
9946 deg
Eccentricity:
0005888
Arg of perigee: 348
7739 deg
Mean anomaly: 11
3282 deg
Mean motion: 15
54292902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 339
Coasting Arc #14 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2015/276/22:54:04
000
Vector Time (MET): N/A
Weight (LBS) : 907268
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4224269
15 A = 6776951
41 meter
Y = -434018
41 meter E =
0006530
Z = 5280243
13 I = 51
25841
XDOT = 1102
990130 Wp = 15
21374
YDOT = 7586
418072 meter/sec RA = 260
21304 deg
ZDOT = -252
561805 TA = 77
24223
MA = 77
16926
Ha = 221
447 n
mi
Hp = 214
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13859150
76 X = 4203158
81
Y = -1423944
93 feet Y = -386897
47 meter
Z = 17323632
31 Z = 5300712
76
XDOT = 3618
734021 XDOT = 1019
301844
YDOT = 24889
823072 feet/sec YDOT = 7598
284486 meter/sec
ZDOT = -828
614846 ZDOT = -247
407516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13819887
13 X = 4212301
60
Y = -218095
37 feet Y = -66475
47 meter
Z = 17411923
21 Z = 5307154
19
XDOT = 1423
818025 XDOT = 433
979734
YDOT = 24103
190071 feet/sec YDOT = 7346
652334 meter/sec
ZDOT = -807
721573 ZDOT = -246
193535
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 15277
00204130
00016717 00000-0 10270-3 0 9133
2 25544 51
6398 260
8641 0005851 352
8964 7
2105 15
54271227 4978
Satellite: ISS
Catalog Number: 25544
Epoch time: 15277
00204130 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 260
8641 deg
Eccentricity:
0005851
Arg of perigee: 352
8964 deg
Mean anomaly: 7
2105 deg
Mean motion: 15
54271227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 295
Coasting Arc #15 (Orbit 511)
---------------------------------------
Vector Time (GMT): 2015/277/22:54:04
000
Vector Time (MET): N/A
Weight (LBS) : 907268
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4454471
62 A = 6778367
28 meter
Y = -1405782
30 meter E =
0011801
Z = -4921268
91 I = 51
26982
XDOT = -112
070389 Wp = 78
80793
YDOT = -7336
144394 meter/sec RA = 255
18512 deg
ZDOT = 2203
800172 TA = 212
79467
MA = 212
86797
Ha = 221
507 n
mi
Hp = 214
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14614408
19 X = -4414514
91
Y = -4612146
64 feet Y = -1455372
14 meter
Z = -16145895
37 Z = -4942810
84
XDOT = -367
685004 XDOT = -40
732818
YDOT = -24068
715205 feet/sec YDOT = -7336
998582 meter/sec
ZDOT = 7230
315525 ZDOT = 2203
429643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14152138
00 X = -4313571
66
Y = -5618807
48 feet Y = -1712612
52 meter
Z = -16238496
03 Z = -4949493
59
XDOT = 863
465643 XDOT = 263
184328
YDOT = -23005
939017 feet/sec YDOT = -7012
210212 meter/sec
ZDOT = 7229
981920 ZDOT = 2203
698489
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 15277
96645268
00016717 00000-0 10270-3 0 9140
2 25544 51
6396 256
0539 0005751 357
0174 3
0943 15
54330688 5127
Satellite: ISS
Catalog Number: 25544
Epoch time: 15277
96645268 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 256
0539 deg
Eccentricity:
0005751
Arg of perigee: 357
0174 deg
Mean anomaly: 3
0943 deg
Mean motion: 15
54330688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 512
Checksum: 321
Coasting Arc #16 (Orbit 527)
---------------------------------------
Vector Time (GMT): 2015/278/22:54:04
000
Vector Time (MET): N/A
Weight (LBS) : 907268
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4516333
88 A = 6781913
15 meter
Y = 3118212
32 meter E =
0013221
Z = 3980895
63 I = 51
29037
XDOT = -1006
891114 Wp = 53
61142
YDOT = 6504
247098 meter/sec RA = 250
16564 deg
ZDOT = -3935
559334 TA = 77
58561
MA = 77
43768
Ha = 221
577 n
mi
Hp = 213
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14817368
38 X = 4461791
82
Y = 10230355
39 feet Y = 3168412
36 meter
Z = 13060681
19 Z = 4002702
43
XDOT = -3303
448537 XDOT = -1060
430788
YDOT = 21339
393365 feet/sec YDOT = 6492
687649 meter/sec
ZDOT = -12911
940071 ZDOT = -3940
581292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14171946
34 X = 4319609
24
Y = 10996385
30 feet Y = 3351698
24 meter
Z = 13154140
70 Z = 4009382
09
XDOT = -3542
970452 XDOT = -1079
897394
YDOT = 20104
605914 feet/sec YDOT = 6127
883882 meter/sec
ZDOT = -12934
693217 ZDOT = -3942
494492
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 15278
99514590
00016717 00000-0 10270-3 0 9158
2 25544 51
6391 250
9236 0005745 359
9968
1184 15
54334718 5284
Satellite: ISS
Catalog Number: 25544
Epoch time: 15278
99514590 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 250
9236 deg
Eccentricity:
0005745
Arg of perigee: 359
9968 deg
Mean anomaly:
1184 deg
Mean motion: 15
54334718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 528
Checksum: 336
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