[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 13th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 381)
---------------------------------------
Vector Time (GMT): 2015/012/12:56:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4760254
06 A = 6782580
03 meter
Y = 877302
31 meter E =
0004461
Z = -4755283
60 I = 51
86227
XDOT = -3845
094950 Wp = 81
13879
YDOT = 6036
812567 meter/sec RA = 139
96667 deg
ZDOT = -2736
901483 TA = 161
86174
MA = 161
84582
Ha = 221
410 n
mi
Hp = 218
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15617631
44 X = 4773189
36
Y = 2878288
42 feet Y = 930606
92 meter
Z = -15601324
13 Z = -4732127
88
XDOT = -12615
140912 XDOT = -3899
019441
YDOT = 19805
815509 feet/sec YDOT = 5993
512725 meter/sec
ZDOT = -8979
335573 ZDOT = -2755
711067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6681942
15 X = 2036655
97
Y = 14512813
32 feet Y = 4423505
50 meter
Z = -15502456
89 Z = -4725148
86
XDOT = -22366
199712 XDOT = -6817
217672
YDOT = 624
479261 feet/sec YDOT = 190
341279 meter/sec
ZDOT = -9060
786655 ZDOT = -2761
727772
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 15012
56050350
00016717 00000-0 10270-3 0 9000
2 25544 51
6451 140
8965 0006570 244
3047 115
7427 15
53199199 3821
Satellite: ISS
Catalog Number: 25544
Epoch time: 15012
56050350 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 140
8965 deg
Eccentricity:
0006570
Arg of perigee: 244
3047 deg
Mean anomaly: 115
7427 deg
Mean motion: 15
53199199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 295
Coasting Arc #2 (Orbit 397)
---------------------------------------
Vector Time (GMT): 2015/013/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2640232
72 A = 6779896
90 meter
Y = -3268477
57 meter E =
0003877
Z = 5323984
08 I = 51
87803
XDOT = 5626
069032 Wp = 246
15135
YDOT = -5190
374747 meter/sec RA = 134
96728 deg
ZDOT = -398
167853 TA = 207
62442
MA = 207
64502
Ha = 221
020 n
mi
Hp = 218
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8662180
85 X = -2629349
48
Y = -10723351
60 feet Y = -3297941
58 meter
Z = 17467139
37 Z = 5311184
76
XDOT = 18458
231732 XDOT = 5685
625024
YDOT = -17028
788541 feet/sec YDOT = -5127
127385 meter/sec
ZDOT = -1306
324976 ZDOT = -370
692964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3263644
88 X = 994758
96
Y = -13463359
30 feet Y = -4103631
91 meter
Z = 17412960
20 Z = 5307470
27
XDOT = 23737
867334 XDOT = 7235
301964
YDOT = 4225
313735 feet/sec YDOT = 1287
875626 meter/sec
ZDOT = -1187
946618 ZDOT = -362
086129
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 15013
58993395
00016717 00000-0 10270-3 0 9019
2 25544 51
6455 135
7716 0006457 249
2010 110
8451 15
53268382 3981
Satellite: ISS
Catalog Number: 25544
Epoch time: 15013
58993395 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 135
7716 deg
Eccentricity:
0006457
Arg of perigee: 249
2010 deg
Mean anomaly: 110
8451 deg
Mean motion: 15
53268382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 398
Checksum: 314
Coasting Arc #3 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2015/014/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1594430
58 A = 6781036
67 meter
Y = 4251521
26 meter E =
0008229
Z = -5043435
38 I = 51
90364
XDOT = -5840
519313 Wp = 128
55248
YDOT = 4544
436199 meter/sec RA = 129
99515 deg
ZDOT = 1981
641296 TA = 160
65218
MA = 160
62092
Ha = 220
681 n
mi
Hp = 218
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5231071
47 X = 1571269
67
Y = 13948560
57 feet Y = 4269221
83 meter
Z = -16546703
99 Z = -5035746
11
XDOT = -19161
808771 XDOT = -5900
528245
YDOT = 14909
567582 feet/sec YDOT = 4478
788142 meter/sec
ZDOT = 6501
447822 ZDOT = 1953
123562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7689952
56 X = -2343897
54
Y = 12800554
01 feet Y = 3901608
86 meter
Z = -16514548
44 Z = -5033634
37
XDOT = -22645
403220 XDOT = -6902
318902
YDOT = -5362
893870 feet/sec YDOT = -1634
610052 meter/sec
ZDOT = 6378
701864 ZDOT = 1944
228328
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 15014
55500957
00016717 00000-0 10270-3 0 9026
2 25544 51
6454 130
9678 0006318 252
8210 107
2251 15
53293848 4133
Satellite: ISS
Catalog Number: 25544
Epoch time: 15014
55500957 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 130
9678 deg
Eccentricity:
0006318
Arg of perigee: 252
8210 deg
Mean anomaly: 107
2251 deg
Mean motion: 15
53293848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 293
Coasting Arc #4 (Orbit 428)
---------------------------------------
Vector Time (GMT): 2015/015/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -600811
20 A = 6783589
06 meter
Y = -5134484
42 meter E =
0003332
Z = 4391017
10 I = 51
93192
XDOT = 5820
970196 Wp = 57
99634
YDOT = -3620
172914 meter/sec RA = 125
02780 deg
ZDOT = -3433
032928 TA = 66
68717
MA = 66
65211
Ha = 220
486 n
mi
Hp = 218
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1971165
34 X = -564681
42
Y = -16845421
34 feet Y = -5141001
23 meter
Z = 14406224
07 Z = 4388186
04
XDOT = 19097
671246 XDOT = 5877
695555
YDOT = -11877
207722 feet/sec YDOT = -3554
761745 meter/sec
ZDOT = -11263
231390 ZDOT = -3404
618177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11780757
46 X = 3590774
87
Y = -12214359
54 feet Y = -3722936
79 meter
Z = 14395005
36 Z = 4387597
64
XDOT = 20410
719429 XDOT = 6221
187282
YDOT = 6542
033805 feet/sec YDOT = 1994
011904 meter/sec
ZDOT = -11141
066819 ZDOT = -3395
797166
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 15015
58440521
00016717 00000-0 10270-3 0 9031
2 25544 51
6455 125
8427 0006249 257
6557 102
3896 15
53297363 4293
Satellite: ISS
Catalog Number: 25544
Epoch time: 15015
58440521 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 125
8427 deg
Eccentricity:
0006249
Arg of perigee: 257
6557 deg
Mean anomaly: 102
3896 deg
Mean motion: 15
53297363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 429
Checksum: 318
Coasting Arc #5 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2015/016/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -299817
19 A = 6786726
97 meter
Y = 5855352
18 meter E =
0001685
Z = -3418008
67 I = 51
96005
XDOT = -5597
713156 Wp = 237
04775
YDOT = 2423
311468 meter/sec RA = 120
06866 deg
ZDOT = 4639
816517 TA = 83
19930
MA = 83
18013
Ha = 220
148 n
mi
Hp = 218
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -983652
19 X = -348667
48
Y = 19210473
04 feet Y = 5851726
47 meter
Z = -11213939
20 Z = -3419583
46
XDOT = -18365
200643 XDOT = -5646
933574
YDOT = 7950
496942 feet/sec YDOT = 2360
438751 meter/sec
ZDOT = 15222
495135 ZDOT = 4612
504577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15293669
57 X = -4661510
49
Y = 11659304
05 feet Y = 3553755
88 meter
Z = -11221701
23 Z = -3420374
54
XDOT = -17114
297709 XDOT = -5216
437942
YDOT = -7902
726819 feet/sec YDOT = -2408
751134 meter/sec
ZDOT = 15105
238840 ZDOT = 4604
076799
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 15016
54944593
00016717 00000-0 10270-3 0 9047
2 25544 51
6456 121
0382 0006358 261
9398 98
1029 15
53319504 4443
Satellite: ISS
Catalog Number: 25544
Epoch time: 15016
54944593 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 121
0382 deg
Eccentricity:
0006358
Arg of perigee: 261
9398 deg
Mean anomaly: 98
1029 deg
Mean motion: 15
53319504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 444
Checksum: 314
Coasting Arc #6 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2015/017/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1088617
97 A = 6789582
97 meter
Y = -6332657
69 meter E =
0008531
Z = 2177803
54 I = 51
98466
XDOT = 5231
448698 Wp = 125
75637
YDOT = -1001
095107 meter/sec RA = 115
11789 deg
ZDOT = -5515
802942 TA = 30
20004
MA = 30
15089
Ha = 220
022 n
mi
Hp = 218
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3571581
28 X = 1148771
45
Y = -20776436
00 feet Y = -6320147
86 meter
Z = 7145024
74 Z = 2183237
50
XDOT = 17163
545598 XDOT = 5269
047888
YDOT = -3284
432766 feet/sec YDOT = -942
383068 meter/sec
ZDOT = -18096
466346 ZDOT = -5490
298489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17988103
21 X = 5482773
86
Y = -10977059
29 feet Y = -3345807
67 meter
Z = 7169391
66 Z = 2185230
58
XDOT = 13019
778009 XDOT = 3968
428337
YDOT = 9565
757307 feet/sec YDOT = 2915
642827 meter/sec
ZDOT = -17987
177447 ZDOT = -5482
491686
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 15017
57880604
00016717 00000-0 10270-3 0 9054
2 25544 51
6454 115
9134 0006184 266
3899 93
6546 15
53345904 4605
Satellite: ISS
Catalog Number: 25544
Epoch time: 15017
57880604 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 115
9134 deg
Eccentricity:
0006184
Arg of perigee: 266
3899 deg
Mean anomaly: 93
6546 deg
Mean motion: 15
53345904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 460
Checksum: 323
Coasting Arc #7 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2015/018/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1747551
49 A = 6791371
23 meter
Y = 6511117
92 meter E =
0008201
Z = -774509
45 I = 52
00347
XDOT = -4766
452482 Wp = 2
54245
YDOT = -569
362020 meter/sec RA = 110
17291 deg
ZDOT = 5978
594686 TA = 349
12996
MA = 349
14768
Ha = 219
977 n
mi
Hp = 218
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5733436
66 X = -1816468
23
Y = 21361935
42 feet Y = 6491190
37 meter
Z = -2541041
50 Z = -783165
58
XDOT = -15637
967462 XDOT = -4788
772930
YDOT = -1867
985630 feet/sec YDOT = -622
788784 meter/sec
ZDOT = 19614
811961 ZDOT = 5955
386196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19698332
68 X = -6004051
80
Y = 10049113
98 feet Y = 3062969
94 meter
Z = -2579238
35 Z = -786151
85
XDOT = -8429
744445 XDOT = -2569
386107
YDOT = -11523
706168 feet/sec YDOT = -3512
425640 meter/sec
ZDOT = 19515
612997 ZDOT = 5948
358842
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 15018
54381337
00016717 00000-0 10270-3 0 9062
2 25544 51
6458 111
1084 0006255 272
3879 87
6557 15
53335763 4758
Satellite: ISS
Catalog Number: 25544
Epoch time: 15018
54381337 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 111
1084 deg
Eccentricity:
0006255
Arg of perigee: 272
3879 deg
Mean anomaly: 87
6557 deg
Mean motion: 15
53335763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 324
Coasting Arc #8 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2015/019/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2299256
54 A = 6791247
05 meter
Y = -6345752
72 meter E =
0007505
Z = -706020
06 I = 52
01319
XDOT = 4247
704159 Wp = 174
52989
YDOT = 2204
102754 meter/sec RA = 105
23144 deg
ZDOT = -5989
834407 TA = 13
05531
MA = 13
03589
Ha = 219
992 n
mi
Hp = 218
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7543492
59 X = 2373474
88
Y = -20819398
68 feet Y = -6319625
92 meter
Z = -2316338
78 Z = -694671
00
XDOT = 13936
037266 XDOT = 4251
837559
YDOT = 7231
308248 feet/sec YDOT = 2251
626795 meter/sec
ZDOT = -19651
687686 ZDOT = -5969
190057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20381421
91 X = 6212257
40
Y = -8670470
87 feet Y = -2642759
52 meter
Z = -2266636
95 Z = -690870
94
XDOT = 3668
737642 XDOT = 1118
231233
YDOT = 13727
411879 feet/sec YDOT = 4184
115141 meter/sec
ZDOT = -19563
744297 ZDOT = -5963
029262
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 15019
57313822
00016717 00000-0 10270-3 0 9071
2 25544 51
6454 105
9835 0006120 275
6169 84
4285 15
53399132 4919
Satellite: ISS
Catalog Number: 25544
Epoch time: 15019
57313822 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 105
9835 deg
Eccentricity:
0006120
Arg of perigee: 275
6169 deg
Mean anomaly: 84
4285 deg
Mean motion: 15
53399132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 314
Coasting Arc #9 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2015/020/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2748724
75 A = 6789507
81 meter
Y = 5824358
11 meter E =
0009204
Z = 2131438
51 I = 52
01511
XDOT = -3711
570168 Wp = 50
25062
YDOT = -3783
458620 meter/sec RA = 100
28769 deg
ZDOT = 5542
076091 TA = 333
24195
MA = 333
28940
Ha = 220
234 n
mi
Hp = 218
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9018125
84 X = -2824003
32
Y = 19108786
45 feet Y = 5793199
09 meter
Z = 6992908
51 Z = 2117903
40
XDOT = -12177
067479 XDOT = -3695
907572
YDOT = -12412
921982 feet/sec YDOT = -3824
876447 meter/sec
ZDOT = 18182
664341 ZDOT = 5524
084270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20043299
22 X = -6109197
60
Y = 6749798
29 feet Y = 2057338
52 meter
Z = 6933935
54 Z = 2113463
55
XDOT = 886
584437 XDOT = 270
230936
YDOT = -16001
964613 feet/sec YDOT = -4877
398814 meter/sec
ZDOT = 18106
350929 ZDOT = 5518
815763
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 15020
60244425
00016717 00000-0 10270-3 0 9080
2 25544 51
6455 100
8577 0006089 280
6759 79
3708 15
53416961 5073
Satellite: ISS
Catalog Number: 25544
Epoch time: 15020
60244425 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 100
8577 deg
Eccentricity:
0006089
Arg of perigee: 280
6759 deg
Mean anomaly: 79
3708 deg
Mean motion: 15
53416961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 317
Coasting Arc #10 (Orbit 521)
---------------------------------------
Vector Time (GMT): 2015/021/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3136789
03 A = 6786442
98 meter
Y = -4960521
50 meter E =
0001758
Z = -3407901
04 I = 52
00950
XDOT = 3165
024277 Wp = 324
61824
YDOT = 5200
803036 meter/sec RA = 95
33876 deg
ZDOT = -4654
433657 TA = 254
96083
MA = 254
98029
Ha = 220
297 n
mi
Hp = 218
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10291302
60 X = 3208579
55
Y = -16274676
83 feet Y = -4925042
43 meter
Z = -11180777
69 Z = -3392489
17
XDOT = 10383
937916 XDOT = 3129
241435
YDOT = 17063
002088 feet/sec YDOT = 5235
996387 meter/sec
ZDOT = -15270
451630 ZDOT = -4639
145766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18837884
58 X = 5741787
22
Y = -4171411
60 feet Y = -1271446
26 meter
Z = -11113920
77 Z = -3387523
05
XDOT = -4968
439968 XDOT = -1514
380502
YDOT = 18098
922747 feet/sec YDOT = 5516
551653 meter/sec
ZDOT = -15205
964308 ZDOT = -4634
777921
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 15021
56740253
00016717 00000-0 10270-3 0 9097
2 25544 51
6451 96
0525 0006033 284
7824 75
2660 15
53449827 5221
Satellite: ISS
Catalog Number: 25544
Epoch time: 15021
56740253 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 96
0525 deg
Eccentricity:
0006033
Arg of perigee: 284
7824 deg
Mean anomaly: 75
2660 deg
Mean motion: 15
53449827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 522
Checksum: 302
Coasting Arc #11 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2015/022/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3475324
09 A = 6783007
22 meter
Y = 3796617
27 meter E =
0003387
Z = 4415746
20 I = 52
00015
XDOT = -2615
377593 Wp = 110
01639
YDOT = -6354
224777 meter/sec RA = 90
38191 deg
ZDOT = 3401
684950 TA = 305
70353
MA = 305
73504
Ha = 220
601 n
mi
Hp = 217
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11401981
92 X = -3538970
04
Y = 12456093
40 feet Y = 3757398
11 meter
Z = 14487356
30 Z = 4398709
49
XDOT = -8580
635146 XDOT = -2560
652533
YDOT = -20847
194150 feet/sec YDOT = -6383
165611 meter/sec
ZDOT = 11160
383695 ZDOT = 3389
113210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16922123
61 X = -5157863
28
Y = 963581
57 feet Y = 293699
66 meter
Z = 14413750
02 Z = 4393311
01
XDOT = 8344
890461 XDOT = 2543
522612
YDOT = -19764
491571 feet/sec YDOT = -6024
217031 meter/sec
ZDOT = 11107
731977 ZDOT = 3385
636707
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 15022
59667277
00016717 00000-0 10270-3 0 9107
2 25544 51
6448 90
9265 0006040 289
4149 70
6350 15
53489029 5381
Satellite: ISS
Catalog Number: 25544
Epoch time: 15022
59667277 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 90
9265 deg
Eccentricity:
0006040
Arg of perigee: 289
4149 deg
Mean anomaly: 70
6350 deg
Mean motion: 15
53489029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 538
Checksum: 322
Coasting Arc #12 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2015/023/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3792563
60 A = 6780349
06 meter
Y = -2413079
65 meter E =
0009088
Z = -5083832
46 I = 51
99078
XDOT = 2037
440887 Wp = 52
28866
YDOT = 7144
636130 meter/sec RA = 85
41718 deg
ZDOT = -1868
185087 TA = 199
66426
MA = 199
69932
Ha = 220
699 n
mi
Hp = 217
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12442793
95 X = 3843960
24
Y = -7916927
98 feet Y = -2370381
50 meter
Z = -16679240
37 Z = -5065284
38
XDOT = 6684
517345 XDOT = 1966
471232
YDOT = 23440
407251 feet/sec YDOT = 7167
023255 meter/sec
ZDOT = -6129
216165 ZDOT = -1858
460351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14574579
53 X = 4442331
84
Y = 2781915
55 feet Y = 847927
86 meter
Z = -16599412
83 Z = -5059501
03
XDOT = -10888
824785 XDOT = -3318
913794
YDOT = 20653
617602 feet/sec YDOT = 6295
222645 meter/sec
ZDOT = -6088
899024 ZDOT = -1855
896423
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 15023
56159899
00016717 00000-0 10270-3 0 9112
2 25544 51
6450 86
1205 0006013 293
7713 66
2808 15
53492062 5537
Satellite: ISS
Catalog Number: 25544
Epoch time: 15023
56159899 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 86
1205 deg
Eccentricity:
0006013
Arg of perigee: 293
7713 deg
Mean anomaly: 66
2808 deg
Mean motion: 15
53492062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 553
Checksum: 303
Coasting Arc #13 (Orbit 568)
---------------------------------------
Vector Time (GMT): 2015/024/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4084314
61 A = 6779067
45 meter
Y = 885356
83 meter E =
0003767
Z = 5339970
79 I = 51
98292
XDOT = -1406
923992 Wp = 312
08181
YDOT = -7533
691663 meter/sec RA = 80
44764 deg
ZDOT = 175
511348 TA = 136
26782
MA = 136
23797
Ha = 220
943 n
mi
Hp = 217
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13399982
31 X = -4119850
50
Y = 2904714
03 feet Y = 839484
86 meter
Z = 17519589
21 Z = 5320043
95
XDOT = -4615
892361 XDOT = -1323
428472
YDOT = -24716
836165 feet/sec YDOT = -7548
957946 meter/sec
ZDOT = 575
824633 ZDOT = 168
879947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11976095
60 X = -3650313
94
Y = -6896148
49 feet Y = -2101946
06 meter
Z = 17434137
94 Z = 5313925
24
XDOT = 12630
838609 XDOT = 3849
879608
YDOT = -20568
806265 feet/sec YDOT = -6269
372150 meter/sec
ZDOT = 548
827529 ZDOT = 167
282631
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 15024
59083474
00016717 00000-0 10270-3 0 9122
2 25544 51
6444 80
9942 0005952 298
9365 61
1190 15
53541258 5698
Satellite: ISS
Catalog Number: 25544
Epoch time: 15024
59083474 = yrday
fracday
Element set: 912
Inclination: 51
6444 deg
RA of node: 80
9942 deg
Eccentricity:
0005952
Arg of perigee: 298
9365 deg
Mean anomaly: 61
1190 deg
Mean motion: 15
53541258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 569
Checksum: 324
Coasting Arc #14 (Orbit 583)
---------------------------------------
Vector Time (GMT): 2015/025/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4345166
72 A = 6779841
99 meter
Y = 654481
66 meter E =
0008344
Z = -5170125
69 I = 51
98039
XDOT = 696
842328 Wp = 86
20678
YDOT = 7473
888228 meter/sec RA = 75
47674 deg
ZDOT = 1534
430186 TA = 198
50561
MA = 198
53597
Ha = 221
111 n
mi
Hp = 217
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14255796
34 X = 4362639
45
Y = 2147249
54 feet Y = 703169
67 meter
Z = -16962354
62 Z = -5148975
55
XDOT = 2286
228111 XDOT = 605
762166
YDOT = 24520
630668 feet/sec YDOT = 7481
171561 meter/sec
ZDOT = 5034
219770 ZDOT = 1537
593812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9414968
37 X = 2869682
36
Y = 11056920
72 feet Y = 3370149
44 meter
Z = -16871951
84 Z = -5142570
92
XDOT = -13610
618173 XDOT = -4148
516419
YDOT = 19276
380252 feet/sec YDOT = 5875
440701 meter/sec
ZDOT = 5046
373719 ZDOT = 1538
134709
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 15025
55572812
00016717 00000-0 10270-3 0 9139
2 25544 51
6454 76
1879 0006021 303
1897 56
8678 15
53541426 5848
Satellite: ISS
Catalog Number: 25544
Epoch time: 15025
55572812 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 76
1879 deg
Eccentricity:
0006021
Arg of perigee: 303
1897 deg
Mean anomaly: 56
8678 deg
Mean motion: 15
53541426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 584
Checksum: 321
Coasting Arc #15 (Orbit 599)
---------------------------------------
Vector Time (GMT): 2015/026/13:00:54
035
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4540766
57 A = 6782127
67 meter
Y = -2136734
17 meter E =
0007848
Z = 4562915
14 I = 51
97895
XDOT = 127
979095 Wp = 25
64089
YDOT = -6992
695004 meter/sec RA = 70
50945 deg
ZDOT = -3138
301516 TA = 95
71455
MA = 95
62507
Ha = 221
173 n
mi
Hp = 217
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14897528
12 X = -4538700
34
Y = -7010282
71 feet Y = -2187500
33 meter
Z = 14970194
03 Z = 4540862
26
XDOT = 419
878919 XDOT = 221
408086
YDOT = -22941
912743 feet/sec YDOT = -6990
741534 meter/sec
ZDOT = -10296
264815 ZDOT = -3137
452746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6952245
05 X = -2119044
29
Y = -15018385
15 feet Y = -4577603
79 meter
Z = 14876206
29 Z = 4534267
68
XDOT = 14054
873644 XDOT = 4283
925487
YDOT = -16729
216037 feet/sec YDOT = -5099
065048 meter/sec
ZDOT = -10291
322047 ZDOT = -3136
794960
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 15026
58492930
00016717 00000-0 10270-3 0 9146
2 25544 51
6445 71
0614 0005967 308
1469 51
9145 15
53609571 6007
Satellite: ISS
Catalog Number: 25544
Epoch time: 15026
58492930 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 71
0614 deg
Eccentricity:
0005967
Arg of perigee: 308
1469 deg
Mean anomaly: 51
9145 deg
Mean motion: 15
53609571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 600
Checksum: 307
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