[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 21st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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 3820)
---------------------------------------
Vector Time (GMT): 2015/233/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4791839
83 A = 6777277
45 meter
Y = -1662118
18 meter E =
0010561
Z = -4505835
43 I = 51
95927
XDOT = -651
320553 Wp = 68
00558
YDOT = 6909
835714 meter/sec RA = 116
83474 deg
ZDOT = -3243
797020 TA = 169
48395
MA = 169
46185
Ha = 219
440 n
mi
Hp = 212
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15721259
30 X = 4831957
47
Y = -5453143
64 feet Y = -1608308
60 meter
Z = -14782924
65 Z = -4482460
18
XDOT = -2136
878454 XDOT = -712
782515
YDOT = 22670
064678 feet/sec YDOT = 6902
208396 meter/sec
ZDOT = -10642
378676 ZDOT = -3247
110640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16723651
27 X = -5097368
91
Y = -439007
91 feet Y = -133809
61 meter
Z = -14681838
82 Z = -4475024
47
XDOT = 9856
378935 XDOT = 3004
224299
YDOT = -19283
864279 feet/sec YDOT = -5877
721832 meter/sec
ZDOT = -10657
848778 ZDOT = -3248
512308
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 15233
55189609
00016717 00000-0 10270-3 0 9004
2 25544 51
6439 117
6767 0001168 54
0611 306
0650 15
55355492 38216
Satellite: ISS
Catalog Number: 25544
Epoch time: 15233
55189609 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 117
6767 deg
Eccentricity:
0001168
Arg of perigee: 54
0611 deg
Mean anomaly: 306
0650 deg
Mean motion: 15
55355492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3821
Checksum: 304
Coasting Arc #2 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2015/234/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4237709
69 A = 6774062
78 meter
Y = -486444
01 meter E =
0004376
Z = 5259046
80 I = 51
96253
XDOT = 2087
542770 Wp = 108
17675
YDOT = -7315
948588 meter/sec RA = 111
84814 deg
ZDOT = 1003
417338 TA = 332
25512
MA = 332
27846
Ha = 219
603 n
mi
Hp = 212
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13903247
02 X = -4257501
57
Y = -1595944
92 feet Y = -533943
32 meter
Z = 17254090
55 Z = 5238412
87
XDOT = 6848
893602 XDOT = 2164
322119
YDOT = -24002
455996 feet/sec YDOT = -7292
174973 meter/sec
ZDOT = 3292
051634 ZDOT = 1013
744952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12672004
49 X = 3862426
97
Y = 6190926
53 feet Y = 1886994
41 meter
Z = 17165188
31 Z = 5231949
40
XDOT = -14013
354762 XDOT = -4271
270531
YDOT = 19410
421140 feet/sec YDOT = 5916
296363 meter/sec
ZDOT = 3337
854345 ZDOT = 1017
378004
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 15234
57990988
00016717 00000-0 10270-3 0 9018
2 25544 51
6441 112
5421 0001244 61
2342 298
8936 15
55373788 38376
Satellite: ISS
Catalog Number: 25544
Epoch time: 15234
57990988 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 112
5421 deg
Eccentricity:
0001244
Arg of perigee: 61
2342 deg
Mean anomaly: 298
8936 deg
Mean motion: 15
55373788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 328
Coasting Arc #3 (Orbit 3851)
---------------------------------------
Vector Time (GMT): 2015/235/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3429744
51 A = 6774251
38 meter
Y = 2694400
72 meter E =
0014748
Z = -5196375
47 I = 51
97381
XDOT = -3214
612520 Wp = 97
76713
YDOT = 6807
865827 meter/sec RA = 106
85602 deg
ZDOT = 1409
730680 TA = 185
73623
MA = 185
75314
Ha = 219
346 n
mi
Hp = 212
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11252442
63 X = 3424602
07
Y = 8839897
37 feet Y = 2732725
48 meter
Z = -17048475
96 Z = -5179727
10
XDOT = -10546
629001 XDOT = -3297
348709
YDOT = 22335
517806 feet/sec YDOT = 6771
455351 meter/sec
ZDOT = 4625
100657 ZDOT = 1393
913659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7956637
65 X = -2425183
16
Y = -11995011
78 feet Y = -3656079
59 meter
Z = -16977143
25 Z = -5174633
26
XDOT = 16261
014097 XDOT = 4956
357097
YDOT = -17227
419979 feet/sec YDOT = -5250
917610 meter/sec
ZDOT = 4555
694534 ZDOT = 1388
575694
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 15235
54365756
00016717 00000-0 10270-3 0 9026
2 25544 51
6434 107
7275 0001134 58
5417 301
5847 15
55414780 38529
Satellite: ISS
Catalog Number: 25544
Epoch time: 15235
54365756 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 107
7275 deg
Eccentricity:
0001134
Arg of perigee: 58
5417 deg
Mean anomaly: 301
5847 deg
Mean motion: 15
55414780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3852
Checksum: 309
Coasting Arc #4 (Orbit 3867)
---------------------------------------
Vector Time (GMT): 2015/236/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2434953
97 A = 6777731
56 meter
Y = -4655596
52 meter E =
0010964
Z = 4275107
13 I = 51
99484
XDOT = 4030
198450 Wp = 71
55804
YDOT = -5437
853488 meter/sec RA = 101
87275 deg
ZDOT = -3615
424528 TA = 55
21616
MA = 55
11301
Ha = 219
295 n
mi
Hp = 212
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7988694
11 X = -2403479
69
Y = -15274266
81 feet Y = -4682649
71 meter
Z = 14025942
03 Z = 4263355
23
XDOT = 13222
435859 XDOT = 4108
268545
YDOT = -17840
726667 feet/sec YDOT = -5392
348715 meter/sec
ZDOT = -11861
629030 ZDOT = -3595
657036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3089057
11 X = 941544
61
Y = 16999311
28 feet Y = 5181390
08 meter
Z = 13976074
28 Z = 4259907
44
XDOT = -16825
046177 XDOT = -5128
274075
YDOT = 12768
223877 feet/sec YDOT = 3891
754638 meter/sec
ZDOT = -11775
408314 ZDOT = -3589
144454
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 15236
57163977
00016717 00000-0 10270-3 0 9032
2 25544 51
6439 102
5932 0001067 53
8155 306
3097 15
55464725 38680
Satellite: ISS
Catalog Number: 25544
Epoch time: 15236
57163977 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 102
5932 deg
Eccentricity:
0001067
Arg of perigee: 53
8155 deg
Mean anomaly: 306
3097 deg
Mean motion: 15
55464725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3868
Checksum: 326
Coasting Arc #5 (Orbit 3882)
---------------------------------------
Vector Time (GMT): 2015/237/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1376447
66 A = 6782463
12 meter
Y = 6074092
50 meter E =
0005939
Z = -2684952
64 I = 52
01490
XDOT = -4514
179494 Wp = 56
07665
YDOT = 3328
273924 meter/sec RA = 96
90381 deg
ZDOT = 5226
730816 TA = 273
77238
MA = 273
84029
Ha = 219
277 n
mi
Hp = 212
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4515904
41 X = 1321465
74
Y = 19928125
01 feet Y = 6089177
37 meter
Z = -8808899
73 Z = -2678399
86
XDOT = -14810
300178 XDOT = -4576
450768
YDOT = 10919
533871 feet/sec YDOT = 3277
445323 meter/sec
ZDOT = 17148
066982 ZDOT = 5204
650744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1307948
44 X = 398662
68
Y = -20403211
40 feet Y = -6218898
83 meter
Z = -8781714
48 Z = -2676666
57
XDOT = 15928
715859 XDOT = 4855
072594
YDOT = -6302
058128 feet/sec YDOT = -1920
867317 meter/sec
ZDOT = 17052
231656 ZDOT = 5197
520209
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 15237
53536116
00016717 00000-0 10270-3 0 9049
2 25544 51
6427 97
7787 0001013 60
2720 299
8534 15
55443500 38838
Satellite: ISS
Catalog Number: 25544
Epoch time: 15237
53536116 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 97
7787 deg
Eccentricity:
0001013
Arg of perigee: 60
2720 deg
Mean anomaly: 299
8534 deg
Mean motion: 15
55443500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3883
Checksum: 311
Coasting Arc #6 (Orbit 3898)
---------------------------------------
Vector Time (GMT): 2015/238/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -251866
53 A = 6785253
97 meter
Y = -6746399
12 meter E =
0013604
Z = 616642
17 I = 52
02750
XDOT = 4715
653268 Wp = 124
27992
YDOT = -732
963362 meter/sec RA = 91
95012 deg
ZDOT = -6006
279242 TA = 49
09409
MA = 48
97635
Ha = 219
248 n
mi
Hp = 212
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -826333
77 X = -179403
32
Y = -22133855
37 feet Y = -6748810
47 meter
Z = 2023104
25 Z = 615594
87
XDOT = 15471
303373 XDOT = 4752
674794
YDOT = -2404
735440 feet/sec YDOT = -680
022999 meter/sec
ZDOT = -19705
640558 ZDOT = -5983
281908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5145490
96 X = -1568345
64
Y = 21543622
79 feet Y = 6566496
23 meter
Z = 2019794
97 Z = 615633
51
XDOT = -14098
213677 XDOT = -4297
135529
YDOT = -1502
369320 feet/sec YDOT = -457
922169 meter/sec
ZDOT = -19606
302951 ZDOT = -5976
001139
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 15238
56331456
00016717 00000-0 10270-3 0 9054
2 25544 51
6427 92
6441 0001079 62
6458 297
4805 15
55476595 38997
Satellite: ISS
Catalog Number: 25544
Epoch time: 15238
56331456 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 92
6441 deg
Eccentricity:
0001079
Arg of perigee: 62
6458 deg
Mean anomaly: 297
4805 deg
Mean motion: 15
55476595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3899
Checksum: 345
Coasting Arc #7 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2015/239/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -846844
14 A = 6784360
36 meter
Y = 6549554
42 meter E =
0014846
Z = 1522704
16 I = 52
02361
XDOT = -4632
903461 Wp = 62
49312
YDOT = -1954
904416 meter/sec RA = 86
99827 deg
ZDOT = 5795
603236 TA = 314
06726
MA = 314
18940
Ha = 219
186 n
mi
Hp = 212
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2778360
03 X = -927416
50
Y = 21488039
45 feet Y = 6539634
02 meter
Z = 4995748
56 Z = 1518394
42
XDOT = -15199
814503 XDOT = -4638
851306
YDOT = -6413
728398 feet/sec YDOT = -2006
745573 meter/sec
ZDOT = 19014
446312 ZDOT = 5773
083525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8142580
85 X = 2481858
64
Y = -20083591
94 feet Y = -6121478
82 meter
Z = 4975976
21 Z = 1516677
55
XDOT = 11742
037696 XDOT = 3578
973090
YDOT = 9477
425951 feet/sec YDOT = 2888
719430 meter/sec
ZDOT = 18917
647743 ZDOT = 5766
099032
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 15239
59125167
00016717 00000-0 10270-3 0 9069
2 25544 51
6414 87
5079 0000951 70
0369 290
0887 15
55504334 39156
Satellite: ISS
Catalog Number: 25544
Epoch time: 15239
59125167 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 87
5079 deg
Eccentricity:
0000951
Arg of perigee: 70
0369 deg
Mean anomaly: 290
0887 deg
Mean motion: 15
55504334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 319
Coasting Arc #8 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2015/240/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1953598
78 A = 6780263
17 meter
Y = -5502106
11 meter E =
0005928
Z = -3452648
75 I = 52
00662
XDOT = 4253
612553 Wp = 85
23295
YDOT = 4400
926389 meter/sec RA = 82
03839 deg
ZDOT = -4612
781541 TA = 134
99882
MA = 134
95077
Ha = 219
185 n
mi
Hp = 212
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6409444
83 X = 2031750
84
Y = -18051529
24 feet Y = -5479822
96 meter
Z = -11327587
75 Z = -3442968
51
XDOT = 13955
421761 XDOT = 4226
490952
YDOT = 14438
734872 feet/sec YDOT = 4448
341110 meter/sec
ZDOT = -15133
797707 ZDOT = -4592
184881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10554024
22 X = -3216866
58
Y = 16016183
27 feet Y = 4881732
66 meter
Z = -11284829
69 Z = -3439616
09
XDOT = -9084
949419 XDOT = -2769
092583
YDOT = -16573
029225 feet/sec YDOT = -5051
459308 meter/sec
ZDOT = -15045
737018 ZDOT = -4585
940643
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 15240
55492956
00016717 00000-0 10270-3 0 9071
2 25544 51
6405 82
6934 0001049 68
9904 291
1362 15
55520518 39301
Satellite: ISS
Catalog Number: 25544
Epoch time: 15240
55492956 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 82
6934 deg
Eccentricity:
0001049
Arg of perigee: 68
9904 deg
Mean anomaly: 291
1362 deg
Mean motion: 15
55520518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 316
Coasting Arc #9 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2015/241/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2971233
91 A = 6775656
70 meter
Y = 3763025
44 meter E =
0008269
Z = 4782401
05 I = 51
98542
XDOT = -3580
166380 Wp = 112
94328
YDOT = -6237
640025 meter/sec RA = 77
06105 deg
ZDOT = 2676
970266 TA = 310
74063
MA = 310
81239
Ha = 219
281 n
mi
Hp = 212
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9748142
74 X = -3036322
86
Y = 12345884
00 feet Y = 3729435
67 meter
Z = 15690292
15 Z = 4767809
17
XDOT = -11745
952689 XDOT = -3523
152996
YDOT = -20464
698245 feet/sec YDOT = -6277
356769 meter/sec
ZDOT = 8782
710846 ZDOT = 2659
717872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12312574
17 X = 3752872
61
Y = -9891438
50 feet Y = -3014910
45 meter
Z = 15626655
69 Z = 4763004
65
XDOT = 6313
494617 XDOT = 1924
353159
YDOT = 21653
541133 feet/sec YDOT = 6599
999337 meter/sec
ZDOT = 8709
415128 ZDOT = 2654
629731
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 15241
58283756
00016717 00000-0 10270-3 0 9082
2 25544 51
6402 77
5569 0001015 70
2886 289
8377 15
55512511 39464
Satellite: ISS
Catalog Number: 25544
Epoch time: 15241
58283756 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 77
5569 deg
Eccentricity:
0001015
Arg of perigee: 70
2886 deg
Mean anomaly: 289
8377 deg
Mean motion: 15
55512511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 330
Coasting Arc #10 (Orbit 3960)
---------------------------------------
Vector Time (GMT): 2015/242/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3877779
25 A = 6773211
32 meter
Y = -1577945
12 meter E =
0015925
Z = -5338121
19 I = 51
96917
XDOT = 2558
975505 Wp = 87
46504
YDOT = 7213
826252 meter/sec RA = 72
07026 deg
ZDOT = -273
499107 TA = 179
93671
MA = 179
93651
Ha = 219
137 n
mi
Hp = 212
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12722372
86 X = 3921066
26
Y = -5176985
31 feet Y = -1534339
80 meter
Z = -17513520
98 Z = -5319178
63
XDOT = 8395
588926 XDOT = 2479
447104
YDOT = 23667
408963 feet/sec YDOT = 7241
997700 meter/sec
ZDOT = -897
306780 ZDOT = -261
262228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13615722
42 X = -4150072
19
Y = 2477471
10 feet Y = 755133
19 meter
Z = -17431511
84 Z = -5313124
81
XDOT = -3263
059905 XDOT = -994
580659
YDOT = -23884
076551 feet/sec YDOT = -7279
866533 meter/sec
ZDOT = -845
834657 ZDOT = -257
810403
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 15242
54648524
00016717 00000-0 10270-3 0 9098
2 25544 51
6397 72
7415 0001076 82
2445 277
8831 15
55561430 39618
Satellite: ISS
Catalog Number: 25544
Epoch time: 15242
54648524 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 72
7415 deg
Eccentricity:
0001076
Arg of perigee: 82
2445 deg
Mean anomaly: 277
8831 deg
Mean motion: 15
55561430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3961
Checksum: 320
Coasting Arc #11 (Orbit 3976)
---------------------------------------
Vector Time (GMT): 2015/243/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4536605
67 A = 6774769
01 meter
Y = -740303
08 meter E =
0007291
Z = 4972504
27 I = 51
96370
XDOT = -1214
633639 Wp = 60
99631
YDOT = -7256
166709 meter/sec RA = 67
07746 deg
ZDOT = -2182
598285 TA = 50
20378
MA = 50
13961
Ha = 219
264 n
mi
Hp = 212
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14883876
86 X = -4552144
61
Y = -2428815
86 feet Y = -791120
69 meter
Z = 16313990
40 Z = 4950428
86
XDOT = -3985
018502 XDOT = -1122
800997
YDOT = -23806
321224 feet/sec YDOT = -7269
236329 meter/sec
ZDOT = -7160
755529 ZDOT = -2188
274796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14278549
82 X = 4352101
99
Y = 5161950
03 feet Y = 1573362
37 meter
Z = 16218893
51 Z = 4943518
74
XDOT = -162
992256 XDOT = -49
680040
YDOT = 23083
431342 feet/sec YDOT = 7035
829873 meter/sec
ZDOT = -7183
907313 ZDOT = -2189
654949
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 15243
57436125
00016717 00000-0 10270-3 0 9106
2 25544 51
6398 67
6052 0001010 84
8525 275
2744 15
55560815 39772
Satellite: ISS
Catalog Number: 25544
Epoch time: 15243
57436125 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 67
6052 deg
Eccentricity:
0001010
Arg of perigee: 84
8525 deg
Mean anomaly: 275
2744 deg
Mean motion: 15
55560815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3977
Checksum: 312
Coasting Arc #12 (Orbit 3991)
---------------------------------------
Vector Time (GMT): 2015/244/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4856729
67 A = 6779050
41 meter
Y = 2847522
08 meter E =
0006963
Z = -3783118
58 I = 51
96595
XDOT = -408
778658 Wp = 100
29782
YDOT = 6354
825679 meter/sec RA = 62
09459 deg
ZDOT = 4263
877666 TA = 214
62067
MA = 214
66602
Ha = 219
097 n
mi
Hp = 212
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15934152
46 X = 4842903
92
Y = 9342264
04 feet Y = 2901755
50 meter
Z = -12411806
38 Z = -3759559
53
XDOT = -1341
137329 XDOT = -500
521710
YDOT = 20849
165615 feet/sec YDOT = 6349
741952 meter/sec
ZDOT = 13989
099955 ZDOT = 4261
668372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14212164
36 X = -4331867
70
Y = -11903317
36 feet Y = -3628131
13 meter
Z = -12310705
48 Z = -3752303
03
XDOT = 4051
682273 XDOT = 1234
952757
YDOT = -19275
762595 feet/sec YDOT = -5875
252439 meter/sec
ZDOT = 13978
388320 ZDOT = 4260
612760
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 15244
53797977
00016717 00000-0 10270-3 0 9119
2 25544 51
6405 62
7897 0001097 90
3824 269
7455 15
55609766 39926
Satellite: ISS
Catalog Number: 25544
Epoch time: 15244
53797977 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 62
7897 deg
Eccentricity:
0001097
Arg of perigee: 90
3824 deg
Mean anomaly: 269
7455 deg
Mean motion: 15
55609766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3992
Checksum: 359
Coasting Arc #13 (Orbit 4007)
---------------------------------------
Vector Time (GMT): 2015/245/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4689670
51 A = 6783415
53 meter
Y = -4503321
44 meter E =
0014791
Z = 1910536
53 I = 51
96509
XDOT = 2211
161439 Wp = 111
31796
YDOT = -4708
434112 meter/sec RA = 57
12806 deg
ZDOT = -5640
894932 TA = 47
70808
MA = 47
58279
Ha = 218
987 n
mi
Hp = 211
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15386058
11 X = -4648245
39
Y = -14774676
63 feet Y = -4555532
61 meter
Z = 6268164
46 Z = 1887856
11
XDOT = 7254
466662 XDOT = 2291
049267
YDOT = -15447
618477 feet/sec YDOT = -4683
261317 meter/sec
ZDOT = -18506
873137 ZDOT = -5629
959060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13012026
11 X = 3966065
56
Y = 16938581
35 feet Y = 5162879
60 meter
Z = 6171173
11 Z = 1880973
56
XDOT = -8390
524793 XDOT = -2557
431957
YDOT = 13206
659058 feet/sec YDOT = 4025
389681 meter/sec
ZDOT = -18458
815129 ZDOT = -5626
246851
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 15245
56582257
00016717 00000-0 10270-3 0 9127
2 25544 51
6404 57
6536 0000931 84
8905 275
2355 15
55648216 40085
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
56582257 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 57
6536 deg
Eccentricity:
0000931
Arg of perigee: 84
8905 deg
Mean anomaly: 275
2355 deg
Mean motion: 15
55648216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4008
Checksum: 316
Coasting Arc #14 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2015/246/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3990207
80 A = 6784819
94 meter
Y = 5473728
97 meter E =
0013397
Z = 262420
00 I = 51
95321
XDOT = -3965
740594 Wp = 51
52661
YDOT = 2592
096442 meter/sec RA = 52
17152 deg
ZDOT = 6033
814177 TA = 311
29103
MA = 311
40631
Ha = 218
997 n
mi
Hp = 211
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13091232
94 X = 3927427
94
Y = 17958428
37 feet Y = 5517999
09 meter
Z = 860958
00 Z = 281650
71
XDOT = -13010
959955 XDOT = -4023
741298
YDOT = 8504
253420 feet/sec YDOT = 2547
425111 meter/sec
ZDOT = 19795
978272 ZDOT = 6014
408303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10554667
81 X = -3217062
75
Y = -19553433
32 feet Y = -5959886
48 meter
Z = 942873
65 Z = 287387
89
XDOT = 12734
664450 XDOT = 3881
525724
YDOT = -5894
691714 feet/sec YDOT = -1796
702035 meter/sec
ZDOT = 19711
777596 ZDOT = 6008
149811
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 15246
59365042
00016717 00000-0 10270-3 0 9133
2 25544 51
6417 52
5178 0001108 97
1252 263
0027 15
55669754 40243
Satellite: ISS
Catalog Number: 25544
Epoch time: 15246
59365042 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 52
5178 deg
Eccentricity:
0001108
Arg of perigee: 97
1252 deg
Mean anomaly: 263
0027 deg
Mean motion: 15
55669754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4024
Checksum: 300
Coasting Arc #15 (Orbit 4038)
---------------------------------------
Vector Time (GMT): 2015/247/12:43:08
739
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700108
50 A = 6782207
81 meter
Y = -5724764
94 meter E =
0006297
Z = -2434532
30 I = 51
92476
XDOT = 5461
177443 Wp = 124
90901
YDOT = -296
510334 meter/sec RA = 47
21208 deg
ZDOT = -5373
006914 TA = 82
22237
MA = 82
15088
Ha = 218
921 n
mi
Hp = 211
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8858623
70 X = -2624066
09
Y = -18782037
20 feet Y = -5754534
32 meter
Z = -7987310
71 Z = -2447463
80
XDOT = 17917
248830 XDOT = 5490
187231
YDOT = -972
802932 feet/sec YDOT = -235
278017 meter/sec
ZDOT = -17627
975440 ZDOT = -5346
407127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6544310
00 X = 1994705
69
Y = 19685923
53 feet Y = 6000269
49 meter
Z = -8041995
35 Z = -2451200
18
XDOT = -16583
745799 XDOT = -5054
725719
YDOT = -1623
625417 feet/sec YDOT = -494
881027 meter/sec
ZDOT = -17513
179986 ZDOT = -5338
017260
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 15247
55722274
00016717 00000-0 10270-3 0 9145
2 25544 51
6418 47
7029 0001102 89
6151 270
5128 15
55700469 40393
Satellite: ISS
Catalog Number: 25544
Epoch time: 15247
55722274 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 47
7029 deg
Eccentricity:
0001102
Arg of perigee: 89
6151 deg
Mean anomaly: 270
5128 deg
Mean motion: 15
55700469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4039
Checksum: 302
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