[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 10th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23917 41 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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 816)
---------------------------------------
Vector Time (GMT): 2015/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5948298
80 A = 6785333
55 meter
Y = 1949481
56 meter E =
0012080
Z = 2613245
92 I = 51
66662
XDOT = -3690
976300 Wp = 75
61168
YDOT = -4213
064826 meter/sec RA = 1
12885 deg
ZDOT = -5235
283192 TA = 74
97320
MA = 74
83954
Ha = 221
104 n
mi
Hp = 214
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19515416
02 X = -5982350
29
Y = 6395936
89 feet Y = 1882773
63 meter
Z = 8573641
47 Z = 2584267
72
XDOT = -12109
502297 XDOT = -3618
159752
YDOT = -13822
391163 feet/sec YDOT = -4253
933011 meter/sec
ZDOT = -17176
125958 ZDOT = -5253
035820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18884927
39 X = -5756125
87
Y = -8199762
26 feet Y = -2499287
54 meter
Z = 8449273
08 Z = 2575338
43
XDOT = -402
891981 XDOT = -122
801476
YDOT = -16927
914866 feet/sec YDOT = -5159
628451 meter/sec
ZDOT = -17251
256328 ZDOT = -5258
182929
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 15040
53735063
00016717 00000-0 10270-3 0 9009
2 25544 51
6447 1
5113 0006290 345
9571 14
1406 15
54536346 8175
Satellite: ISS
Catalog Number: 25544
Epoch time: 15040
53735063 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 1
5113 deg
Eccentricity:
0006290
Arg of perigee: 345
9571 deg
Mean anomaly: 14
1406 deg
Mean motion: 15
54536346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 817
Checksum: 278
Coasting Arc #2 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2015/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6624320
01 A = 6787724
92 meter
Y = -1141190
52 meter E =
0014964
Z = -877412
48 I = 51
64348
XDOT = 1573
018066 Wp = 20
46774
YDOT = 4601
693863 meter/sec RA = 356
15443 deg
ZDOT = 5935
173796 TA = 330
03167
MA = 330
11724
Ha = 221
136 n
mi
Hp = 214
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21733333
36 X = 6640850
83
Y = -3744063
37 feet Y = -1067020
69 meter
Z = -2878649
88 Z = -845192
91
XDOT = 5160
820428 XDOT = 1492
613365
YDOT = 15097
420812 feet/sec YDOT = 4618
835245 meter/sec
ZDOT = 19472
354973 ZDOT = 5942
619503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18954499
97 X = 5777331
59
Y = 11307456
24 feet Y = 3446512
66 meter
Z = -2740579
98 Z = -835328
78
XDOT = -5173
233275 XDOT = -1576
801502
YDOT = 13361
843642 feet/sec YDOT = 4072
689942 meter/sec
ZDOT = 19503
307511 ZDOT = 5944
608129
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 15041
50161569
00016717 00000-0 10270-3 0 9012
2 25544 51
6446 356
7017 0006206 349
5401 10
5622 15
54579081 8321
Satellite: ISS
Catalog Number: 25544
Epoch time: 15041
50161569 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 356
7017 deg
Eccentricity:
0006206
Arg of perigee: 349
5401 deg
Mean anomaly: 10
5622 deg
Mean motion: 15
54579081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 287
Coasting Arc #3 (Orbit 847)
---------------------------------------
Vector Time (GMT): 2015/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6707633
89 A = 6787406
81 meter
Y = 230589
20 meter E =
0005336
Z = -1010396
06 I = 51
61245
XDOT = 717
943895 Wp = 103
79415
YDOT = -4840
025749 meter/sec RA = 351
18130 deg
ZDOT = -5898
165104 TA = 87
15417
MA = 87
09310
Ha = 221
127 n
mi
Hp = 213
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22006672
87 X = -6704805
79
Y = 756526
26 feet Y = 155595
82 meter
Z = -3314947
72 Z = -1042973
29
XDOT = 2355
458974 XDOT = 800
663658
YDOT = -15879
349571 feet/sec YDOT = -4831
535093 meter/sec
ZDOT = -19350
935381 ZDOT = -5894
476282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17421882
45 X = -5310189
77
Y = -13431316
31 feet Y = -4093865
21 meter
Z = -3454361
79 Z = -1052889
47
XDOT = 11052
933759 XDOT = 3368
934210
YDOT = -9386
567280 feet/sec YDOT = -2861
025707 meter/sec
ZDOT = -19334
204558 ZDOT = -5893
065549
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 15042
53013540
00016717 00000-0 10270-3 0 9022
2 25544 51
6455 351
5707 0006258 352
8247 7
2816 15
54626097 8487
Satellite: ISS
Catalog Number: 25544
Epoch time: 15042
53013540 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 351
5707 deg
Eccentricity:
0006258
Arg of perigee: 352
8247 deg
Mean anomaly: 7
2816 deg
Mean motion: 15
54626097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 848
Checksum: 303
Coasting Arc #4 (Orbit 863)
---------------------------------------
Vector Time (GMT): 2015/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6144483
20 A = 6784430
20 meter
Y = 742277
41 meter E =
0015380
Z = 2755753
05 I = 51
57190
XDOT = -2902
415071 Wp = 55
89170
YDOT = 4909
589990 meter/sec RA = 346
20130 deg
ZDOT = 5136
999113 TA = 335
38873
MA = 335
46205
Ha = 221
036 n
mi
Hp = 213
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20159065
60 X = 6122339
92
Y = 2435293
35 feet Y = 810865
36 meter
Z = 9041184
55 Z = 2785547
64
XDOT = -9522
359157 XDOT = -2982
052920
YDOT = 16107
578707 feet/sec YDOT = 4876
688276 meter/sec
ZDOT = 16853
671631 ZDOT = 5122
706203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14186107
75 X = 4323925
64
Y = 14448341
96 feet Y = 4403854
63 meter
Z = 9168498
21 Z = 2794558
25
XDOT = -16523
433893 XDOT = -5036
342651
YDOT = 5543
318088 feet/sec YDOT = 1689
603353 meter/sec
ZDOT = 16791
564634 ZDOT = 5118
068900
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 15043
55862398
00016717 00000-0 10270-3 0 9039
2 25544 51
6455 346
4400 0006175 356
4715 3
6394 15
54673769 8645
Satellite: ISS
Catalog Number: 25544
Epoch time: 15043
55862398 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 346
4400 deg
Eccentricity:
0006175
Arg of perigee: 356
4715 deg
Mean anomaly: 3
6394 deg
Mean motion: 15
54673769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 864
Checksum: 328
Coasting Arc #5 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2015/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5032025
26 A = 6780063
73 meter
Y = -1800296
65 meter E =
0011696
Z = -4184734
62 I = 51
52779
XDOT = 4764
720971 Wp = 39
55993
YDOT = -4722
618192 meter/sec RA = 341
20717 deg
ZDOT = -3694
624381 TA = 192
38849
MA = 192
41727
Ha = 221
165 n
mi
Hp = 213
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16509269
23 X = -4991192
30
Y = -5906485
09 feet Y = -1856339
90 meter
Z = -13729444
29 Z = -4209079
68
XDOT = 15632
286649 XDOT = 4835
123162
YDOT = -15494
154173 feet/sec YDOT = -4668
942485 meter/sec
ZDOT = -12121
471067 ZDOT = -3671
307384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9398924
79 X = -2864792
28
Y = -14705168
75 feet Y = -4482135
44 meter
Z = -13833235
41 Z = -4216370
15
XDOT = 20829
278921 XDOT = 6348
764215
YDOT = -1995
603476 feet/sec YDOT = -608
259939 meter/sec
ZDOT = -12020
800515 ZDOT = -3663
939997
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 15044
52280402
00016717 00000-0 10270-3 0 9048
2 25544 51
6459 341
6292 0006239
1547 359
9607 15
54727514 8790
Satellite: ISS
Catalog Number: 25544
Epoch time: 15044
52280402 = yrday
fracday
Element set: 904
Inclination: 51
6459 deg
RA of node: 341
6292 deg
Eccentricity:
0006239
Arg of perigee:
1547 deg
Mean anomaly: 359
9607 deg
Mean motion: 15
54727514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 312
Coasting Arc #6 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2015/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3460486
60 A = 6776402
40 meter
Y = 2876427
21 meter E =
0005495
Z = 5061882
22 I = 51
48672
XDOT = -6134
527616 Wp = 55
47844
YDOT = 4252
918316 meter/sec RA = 336
19884 deg
ZDOT = 1778
731416 TA = 17
29880
MA = 17
28008
Ha = 220
988 n
mi
Hp = 213
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11353302
50 X = 3403476
17
Y = 9437097
15 feet Y = 2914806
03 meter
Z = 16607225
15 Z = 5078553
77
XDOT = -20126
402941 XDOT = -6190
269101
YDOT = 13953
144083 feet/sec YDOT = 4184
006423 meter/sec
ZDOT = 5835
732992 ZDOT = 1748
795997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3391624
42 X = 1033767
12
Y = 14286289
24 feet Y = 4354460
96 meter
Z = 16677980
41 Z = 5083448
43
XDOT = -23464
303335 XDOT = -7151
919657
YDOT = -1085
320875 feet/sec YDOT = -330
805803 meter/sec
ZDOT = 5706
846800 ZDOT = 1739
446905
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 15045
55123138
00016717 00000-0 10270-3 0 9055
2 25544 51
6460 336
4981 0006094 2
4139 357
7042 15
54794523 8951
Satellite: ISS
Catalog Number: 25544
Epoch time: 15045
55123138 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 336
4981 deg
Eccentricity:
0006094
Arg of perigee: 2
4139 deg
Mean anomaly: 357
7042 deg
Mean motion: 15
54794523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 895
Checksum: 310
Coasting Arc #7 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2015/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1658133
05 A = 6775442
22 meter
Y = -3904084
05 meter E =
0016368
Z = -5296589
86 I = 51
45538
XDOT = 6843
210344 Wp = 70
74857
YDOT = -3417
174386 meter/sec RA = 331
18001 deg
ZDOT = 382
718386 TA = 202
87825
MA = 202
95126
Ha = 221
171 n
mi
Hp = 212
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5440069
05 X = -1588625
06
Y = -12808674
71 feet Y = -3922237
91 meter
Z = -17377263
34 Z = -5304475
64
XDOT = 22451
477506 XDOT = 6879
054326
YDOT = -11211
202054 feet/sec YDOT = -3340
448722 meter/sec
ZDOT = 1255
637750 ZDOT = 416
047916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3137061
55 X = 956176
36
Y = -13515480
69 feet Y = -4119518
51 meter
Z = -17410238
56 Z = -5306640
71
XDOT = 23785
142079 XDOT = 7249
711306
YDOT = 3745
127611 feet/sec YDOT = 1141
514896 meter/sec
ZDOT = 1398
875160 ZDOT = 426
377149
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 15046
51535646
00016717 00000-0 10270-3 0 9064
2 25544 51
6465 331
6869 0006177 6
7635 353
3600 15
54806064 9102
Satellite: ISS
Catalog Number: 25544
Epoch time: 15046
51535646 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 331
6869 deg
Eccentricity:
0006177
Arg of perigee: 6
7635 deg
Mean anomaly: 353
3600 deg
Mean motion: 15
54806064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 310
Coasting Arc #8 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2015/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -240924
97 A = 6777416
71 meter
Y = 4772422
24 meter E =
0012216
Z = 4803621
47 I = 51
43516
XDOT = -6900
637646 Wp = 37
50936
YDOT = 2204
330895 meter/sec RA = 326
16136 deg
ZDOT = -2523
216473 TA = 77
43627
MA = 77
29966
Ha = 221
203 n
mi
Hp = 212
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -790436
26 X = -317607
08
Y = 15657553
29 feet Y = 4769299
53 meter
Z = 15759912
97 Z = 4802264
67
XDOT = -22639
887289 XDOT = -6912
517565
YDOT = 7232
056742 feet/sec YDOT = 2127
096930 meter/sec
ZDOT = -8278
269267 ZDOT = -2556
766620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9640265
91 X = -2938353
05
Y = 12371778
70 feet Y = 3770918
15 meter
Z = 15753189
72 Z = 4801572
23
XDOT = -21787
569221 XDOT = -6640
851099
YDOT = -6199
139338 feet/sec YDOT = -1889
497670 meter/sec
ZDOT = -8422
210649 ZDOT = -2567
089806
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 15047
54372520
00016717 00000-0 10270-3 0 9079
2 25544 51
6465 326
5555 0006164 10
3647 349
7632 15
54857733 9267
Satellite: ISS
Catalog Number: 25544
Epoch time: 15047
54372520 = yrday
fracday
Element set: 907
Inclination: 51
6465 deg
RA of node: 326
5555 deg
Eccentricity:
0006164
Arg of perigee: 10
3647 deg
Mean anomaly: 349
7632 deg
Mean motion: 15
54857733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 926
Checksum: 320
Coasting Arc #9 (Orbit 940)
---------------------------------------
Vector Time (GMT): 2015/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1956371
15 A = 6781351
80 meter
Y = -5348179
09 meter E =
0008567
Z = -3683394
55 I = 51
42365
XDOT = 6302
319902 Wp = 54
12191
YDOT = -657
684684 meter/sec RA = 321
15016 deg
ZDOT = 4314
278885 TA = 261
87490
MA = 261
97209
Ha = 221
194 n
mi
Hp = 212
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6418540
52 X = 2033922
45
Y = -17546519
32 feet Y = -5325868
30 meter
Z = -12084627
80 Z = -3673702
41
XDOT = 20676
902566 XDOT = 6288
249267
YDOT = -2157
758151 feet/sec YDOT = -587
286424 meter/sec
ZDOT = 14154
458283 ZDOT = 4344
859422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15137143
68 X = 4613801
39
Y = -10998626
16 feet Y = -3352381
25 meter
Z = -12042148
30 Z = -3670446
80
XDOT = 17524
001236 XDOT = 5341
315577
YDOT = 8520
259453 feet/sec YDOT = 2596
975081 meter/sec
ZDOT = 14285
395743 ZDOT = 4354
188622
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 15048
50779297
00016717 00000-0 10270-3 0 9089
2 25544 51
6471 321
7442 0006125 13
8522 346
2798 15
54905300 9419
Satellite: ISS
Catalog Number: 25544
Epoch time: 15048
50779297 = yrday
fracday
Element set: 908
Inclination: 51
6471 deg
RA of node: 321
7442 deg
Eccentricity:
0006125
Arg of perigee: 13
8522 deg
Mean anomaly: 346
2798 deg
Mean motion: 15
54905300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 941
Checksum: 312
Coasting Arc #10 (Orbit 956)
---------------------------------------
Vector Time (GMT): 2015/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3414350
52 A = 6785332
11 meter
Y = 5504134
96 meter E =
0014779
Z = 2010319
73 I = 51
41297
XDOT = -5168
336455 Wp = 87
42132
YDOT = -1168
336258 meter/sec RA = 316
15093 deg
ZDOT = -5543
153555 TA = 70
29323
MA = 70
13386
Ha = 221
217 n
mi
Hp = 212
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11201937
40 X = -3485410
43
Y = 18058185
56 feet Y = 5465556
33 meter
Z = 6595537
17 Z = 1993560
80
XDOT = -16956
484434 XDOT = -5127
961847
YDOT = -3833
124206 feet/sec YDOT = -1225
906726 meter/sec
ZDOT = -18186
199328 ZDOT = -5568
161515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19217762
22 X = -5857573
92
Y = 9122122
29 feet Y = 2780422
87 meter
Z = 6522812
13 Z = 1988153
14
XDOT = -11434
703551 XDOT = -3485
297642
YDOT = -10923
935634 feet/sec YDOT = -3329
615581 meter/sec
ZDOT = -18292
950878 ZDOT = -5575
691428
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 15049
53610268
00016717 00000-0 10270-3 0 9096
2 25544 51
6469 316
6122 0006052 17
6306 342
5057 15
54927738 9578
Satellite: ISS
Catalog Number: 25544
Epoch time: 15049
53610268 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 316
6122 deg
Eccentricity:
0006052
Arg of perigee: 17
6306 deg
Mean anomaly: 342
5057 deg
Mean motion: 15
54927738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 957
Checksum: 318
Coasting Arc #11 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2015/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4408002
07 A = 6786857
56 meter
Y = -5147162
75 meter E =
0017750
Z = -86293
60 I = 51
39659
XDOT = 3681
509468 Wp = 36
29016
YDOT = 3063
121941 meter/sec RA = 311
15908 deg
ZDOT = 5996
784002 TA = 322
77627
MA = 322
89919
Ha = 221
185 n
mi
Hp = 212
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14461949
06 X = 4465650
43
Y = -16887016
89 feet Y = -5097547
28 meter
Z = -283115
50 Z = -64740
28
XDOT = 12078
443138 XDOT = 3617
853841
YDOT = 10049
612667 feet/sec YDOT = 3103
935748 meter/sec
ZDOT = 19674
488195 ZDOT = 6014
512683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21181137
21 X = 6456010
62
Y = -6761864
02 feet Y = -2061016
15 meter
Z = -189963
78 Z = -57900
96
XDOT = 4391
419636 XDOT = 1338
504705
YDOT = 13289
800941 feet/sec YDOT = 4050
731327 meter/sec
ZDOT = 19749
748598 ZDOT = 6019
723373
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 15050
50011421
00016717 00000-0 10270-3 0 9103
2 25544 51
6470 311
8007 0006135 19
8795 340
2596 15
54979827 9723
Satellite: ISS
Catalog Number: 25544
Epoch time: 15050
50011421 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 311
8007 deg
Eccentricity:
0006135
Arg of perigee: 19
8795 deg
Mean anomaly: 340
2596 deg
Mean motion: 15
54979827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 300
Coasting Arc #12 (Orbit 987)
---------------------------------------
Vector Time (GMT): 2015/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4966746
53 A = 6785177
77 meter
Y = 4214694
71 meter E =
0006731
Z = -1905232
92 I = 51
37128
XDOT = -1982
429922 Wp = 88
74860
YDOT = -4854
328712 meter/sec RA = 306
16611 deg
ZDOT = -5587
600935 TA = 112
31127
MA = 112
23990
Ha = 221
146 n
mi
Hp = 212
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16295100
18 X = -5004252
37
Y = 13827738
55 feet Y = 4158943
36 meter
Z = -6250764
17 Z = -1929451
58
XDOT = -6504
035176 XDOT = -1900
858374
YDOT = -15926
275303 feet/sec YDOT = -4876
042159 meter/sec
ZDOT = -18332
024064 ZDOT = -5597
032263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21038263
92 X = -6412462
84
Y = 3579451
11 feet Y = 1091016
70 meter
Z = -6355129
98 Z = -1937043
62
XDOT = 2909
195717 XDOT = 886
722855
YDOT = -15421
342037 feet/sec YDOT = -4700
425053 meter/sec
ZDOT = -18371
466894 ZDOT = -5599
623109
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 15051
52836441
00016717 00000-0 10270-3 0 9114
2 25544 51
6470 306
6681 0005940 23
0708 337
0711 15
55007416 9884
Satellite: ISS
Catalog Number: 25544
Epoch time: 15051
52836441 = yrday
fracday
Element set: 911
Inclination: 51
6470 deg
RA of node: 306
6681 deg
Eccentricity:
0005940
Arg of perigee: 23
0708 deg
Mean anomaly: 337
0711 deg
Mean motion: 15
55007416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 988
Checksum: 292
Coasting Arc #13 (Orbit 1003)
---------------------------------------
Vector Time (GMT): 2015/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5030958
04 A = 6781013
09 meter
Y = -2759113
55 meter E =
0015378
Z = 3596612
61 I = 51
33960
XDOT = 302
244737 Wp = 72
17880
YDOT = 6289
872565 meter/sec RA = 301
16140 deg
ZDOT = 4391
574192 TA = 330
67691
MA = 330
76312
Ha = 221
081 n
mi
Hp = 211
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16505767
85 X = 5043966
44
Y = -9052209
80 feet Y = -2702780
89 meter
Z = 11799910
14 Z = 3621083
62
XDOT = 991
616590 XDOT = 210
555117
YDOT = 20636
064847 feet/sec YDOT = 6292
740365 meter/sec
ZDOT = 14408
051811 ZDOT = 4392
818900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18756439
18 X = 5716962
66
Y = 293036
96 feet Y = 89317
66 meter
Z = 11905077
60 Z = 3628667
65
XDOT = -9435
711626 XDOT = -2876
004904
YDOT = 16997
276478 feet/sec YDOT = 5180
769871 meter/sec
ZDOT = 14412
223782 ZDOT = 4392
845809
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 15052
55658435
00016717 00000-0 10270-3 0 9124
2 25544 51
6466 301
5350 0006141 27
0332 333
1140 15
55063636 10046
Satellite: ISS
Catalog Number: 25544
Epoch time: 15052
55658435 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 301
5350 deg
Eccentricity:
0006141
Arg of perigee: 27
0332 deg
Mean anomaly: 333
1140 deg
Mean motion: 15
55063636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1004
Checksum: 264
Coasting Arc #14 (Orbit 1018)
---------------------------------------
Vector Time (GMT): 2015/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4715602
49 A = 6776523
58 meter
Y = 878694
89 meter E =
0016529
Z = -4802372
29 I = 51
30947
XDOT = 1244
549572 Wp = 57
20737
YDOT = -7121
502044 meter/sec RA = 296
14091 deg
ZDOT = -2522
655650 TA = 187
81270
MA = 187
83848
Ha = 221
094 n
mi
Hp = 211
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15471136
78 X = -4701749
92
Y = 2882857
26 feet Y = 826038
83 meter
Z = -15755814
61 Z = -4825245
98
XDOT = 4083
167886 XDOT = 1336
345374
YDOT = -23364
508019 feet/sec YDOT = -7107
071723 meter/sec
ZDOT = -8276
429298 ZDOT = -2516
386119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14861367
39 X = -4529744
78
Y = -4869226
02 feet Y = -1484140
09 meter
Z = -15853801
77 Z = -4832238
78
XDOT = 14511
834588 XDOT = 4423
207182
YDOT = -17409
862149 feet/sec YDOT = -5306
525983 meter/sec
ZDOT = -8248
321041 ZDOT = -2514
088253
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 15053
52051152
00016717 00000-0 10270-3 0 9136
2 25544 51
6464 296
7225 0006069 28
5931 331
5554 15
55135775 10191
Satellite: ISS
Catalog Number: 25544
Epoch time: 15053
52051152 = yrday
fracday
Element set: 913
Inclination: 51
6464 deg
RA of node: 296
7225 deg
Eccentricity:
0006069
Arg of perigee: 28
5931 deg
Mean anomaly: 331
5554 deg
Mean motion: 15
55135775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1019
Checksum: 301
Coasting Arc #15 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2015/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4058529
98 A = 6774309
82 meter
Y = 1231060
26 meter E =
0007263
Z = 5277346
38 I = 51
28939
XDOT = -2551
990734 Wp = 51
03614
YDOT = 7233
129735 meter/sec RA = 291
10767 deg
ZDOT = 279
543598 TA = 36
31321
MA = 36
26395
Ha = 220
947 n
mi
Hp = 211
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13315387
08 X = 4018827
20
Y = 4038911
63 feet Y = 1276223
96 meter
Z = 17314128
55 Z = 5296965
19
XDOT = -8372
673013 XDOT = -2634
041535
YDOT = 23730
740602 feet/sec YDOT = 7204
132968 meter/sec
ZDOT = 917
137789 ZDOT = 266
946582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9801424
17 X = 2987474
09
Y = 9728289
47 feet Y = 2965182
63 meter
Z = 17397811
82 Z = 5302853
04
XDOT = -17761
558170 XDOT = -5413
722930
YDOT = 16378
298160 feet/sec YDOT = 4992
105279 meter/sec
ZDOT = 861
956881 ZDOT = 262
724457
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 15054
54867264
00016717 00000-0 10270-3 0 9149
2 25544 51
6464 291
5889 0006009 32
5458 327
6064 15
55177487 10359
Satellite: ISS
Catalog Number: 25544
Epoch time: 15054
54867264 = yrday
fracday
Element set: 914
Inclination: 51
6464 deg
RA of node: 291
5889 deg
Eccentricity:
0006009
Arg of perigee: 32
5458 deg
Mean anomaly: 327
6064 deg
Mean motion: 15
55177487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1035
Checksum: 332
Coasting Arc #16 (Orbit 1049)
---------------------------------------
Vector Time (GMT): 2015/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3209711
02 A = 6775539
08 meter
Y = -3297595
90 meter E =
0015786
Z = -4986201
30 I = 51
28278
XDOT = 3546
463395 Wp = 83
94140
YDOT = -6483
550325 meter/sec RA = 286
07150 deg
ZDOT = 2012
078131 TA = 205
69493
MA = 205
77345
Ha = 221
006 n
mi
Hp = 211
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10530547
97 X = -3148377
09
Y = -10818884
19 feet Y = -3333146
50 meter
Z = -16358928
16 Z = -5001644
04
XDOT = 11635
378594 XDOT = 3608
926570
YDOT = -21271
490566 feet/sec YDOT = -6443
542025 meter/sec
ZDOT = 6601
306205 ZDOT = 2029
458307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4431220
95 X = -1350636
15
Y = -14358244
09 feet Y = -4376392
80 meter
Z = -16424382
30 Z = -5006151
72
XDOT = 18888
521341 XDOT = 5757
221305
YDOT = -13440
231857 feet/sec YDOT = -4096
582670 meter/sec
ZDOT = 6676
800953 ZDOT = 2035
088931
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 15055
51254631
00016717 00000-0 10270-3 0 9156
2 25544 51
6458 286
7755 0005994 34
5748 325
5794 15
55221812 10502
Satellite: ISS
Catalog Number: 25544
Epoch time: 15055
51254631 = yrday
fracday
Element set: 915
Inclination: 51
6458 deg
RA of node: 286
7755 deg
Eccentricity:
0005994
Arg of perigee: 34
5748 deg
Mean anomaly: 325
5794 deg
Mean motion: 15
55221812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1050
Checksum: 322
Coasting Arc #17 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2015/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2191493
15 A = 6779426
95 meter
Y = 5088313
38 meter E =
0016061
Z = 3899932
02 I = 51
28890
XDOT = -4260
248820 Wp = 65
34573
YDOT = 4943
037438 meter/sec RA = 281
04445 deg
ZDOT = -4035
594176 TA = 67
11990
MA = 66
95041
Ha = 220
933 n
mi
Hp = 211
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7189938
16 X = 2115487
34
Y = 16693941
53 feet Y = 5112395
42 meter
Z = 12795052
57 Z = 3910392
75
XDOT = -13977
194291 XDOT = -4295
603197
YDOT = 16217
314430 feet/sec YDOT = 4895
198562 meter/sec
ZDOT = -13240
138372 ZDOT = -4056
375684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -866657
18 X = -264157
11
Y = 18124794
50 feet Y = 5524437
36 meter
Z = 12838886
03 Z = 3913292
46
XDOT = -18244
461137 XDOT = -5560
911755
YDOT = 8615
646981 feet/sec YDOT = 2626
049200 meter/sec
ZDOT = -13329
899035 ZDOT = -4062
953226
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 15056
54064827
00016717 00000-0 10270-3 0 9167
2 25544 51
6460 281
6419 0006046 36
8521 323
3047 15
55297922 10668
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
54064827 = yrday
fracday
Element set: 916
Inclination: 51
6460 deg
RA of node: 281
6419 deg
Eccentricity:
0006046
Arg of perigee: 36
8521 deg
Mean anomaly: 323
3047 deg
Mean motion: 15
55297922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1066
Checksum: 309
Coasting Arc #18 (Orbit 1080)
---------------------------------------
Vector Time (GMT): 2015/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1141451
33 A = 6783806
06 meter
Y = -6296439
68 meter E =
0011945
Z = -2242425
30 I = 51
29726
XDOT = 4662
233856 Wp = 41
68307
YDOT = -2767
737427 meter/sec RA = 276
03117 deg
ZDOT = 5423
692614 TA = 293
24397
MA = 293
36969
Ha = 220
969 n
mi
Hp = 211
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3744919
08 X = -1060065
50
Y = -20657610
51 feet Y = -6308749
25 meter
Z = -7357038
38 Z = -2247772
04
XDOT = 15296
042834 XDOT = 4666
490909
YDOT = -9080
503371 feet/sec YDOT = -2715
577087 meter/sec
ZDOT = 17794
267107 ZDOT = 5446
351094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5313694
17 X = 1619613
98
Y = -20302840
71 feet Y = -6188305
85 meter
Z = -7378795
16 Z = -2249056
76
XDOT = 16110
927416 XDOT = 4910
610676
YDOT = -2255
662678 feet/sec YDOT = -687
525984 meter/sec
ZDOT = 17891
667273 ZDOT = 5453
380185
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 15057
50446820
00016717 00000-0 10270-3 0 9172
2 25544 51
6450 276
8284 0005955 39
9052 320
2539 15
55288452 10811
Satellite: ISS
Catalog Number: 25544
Epoch time: 15057
50446820 = yrday
fracday
Element set: 917
Inclination: 51
6450 deg
RA of node: 276
8284 deg
Eccentricity:
0005955
Arg of perigee: 39
9052 deg
Mean anomaly: 320
2539 deg
Mean motion: 15
55288452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1081
Checksum: 317
Coasting Arc #19 (Orbit 1096)
---------------------------------------
Vector Time (GMT): 2015/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 16515
77 A = 6785831
46 meter
Y = 6780428
64 meter E =
0013929
Z = 172794
28 I = 51
30177
XDOT = -4795
196407 Wp = 107
72318
YDOT = 174
158957 meter/sec RA = 271
03024 deg
ZDOT = -5980
885812 TA = 70
40621
MA = 70
25589
Ha = 220
984 n
mi
Hp = 211
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 54185
61 X = -60145
16
Y = 22245500
78 feet Y = 6780184
70 meter
Z = 566910
37 Z = 172687
80
XDOT = -15732
271677 XDOT = -4767
735055
YDOT = 571
387653 feet/sec YDOT = 120
689042 meter/sec
ZDOT = -19622
328779 ZDOT = -6004
112892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8941628
96 X = -2725408
51
Y = 20369446
97 feet Y = 6208607
44 meter
Z = 565270
02 Z = 172294
30
XDOT = -13021
740488 XDOT = -3969
026501
YDOT = -5132
846372 feet/sec YDOT = -1564
491574 meter/sec
ZDOT = -19721
707234 ZDOT = -6011
176365
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 15058
53251313
00016717 00000-0 10270-3 0 9188
2 25544 51
6447 271
6945 0005913 44
6473 315
5155 15
55327382 10972
Satellite: ISS
Catalog Number: 25544
Epoch time: 15058
53251313 = yrday
fracday
Element set: 918
Inclination: 51
6447 deg
RA of node: 271
6945 deg
Eccentricity:
0005913
Arg of perigee: 44
6473 deg
Mean anomaly: 315
5155 deg
Mean motion: 15
55327382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1097
Checksum: 314
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