[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
169/11:15:28
720 0
9 1
9 1
9
N/A 1
6 -0
2 220
3
000/00:04:57
440 -0
3 -0
2 212
4
Coasting Arc #1 (Orbit 2777)
---------------------------------------
Vector Time (GMT): 2015/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 284592
06 A = 6785678
38 meter
Y = -6775074
06 meter E =
0012678
Z = -120626
44 I = 52
02824
XDOT = 4710
552837 Wp = 115
64915
YDOT = 296
613259 meter/sec RA = 91
60982 deg
ZDOT = -6043
656530 TA = 65
64367
MA = 65
51137
Ha = 220
369 n
mi
Hp = 211
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 933700
99 X = 360917
37
Y = -22227933
28 feet Y = -6771464
79 meter
Z = -395756
04 Z = -119059
50
XDOT = 15454
569675 XDOT = 4736
243939
YDOT = 973
140615 feet/sec YDOT = 349
434238 meter/sec
ZDOT = -19828
269457 ZDOT = -6020
710986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21923294
23 X = -6682220
08
Y = -3785272
33 feet Y = -1153751
00 meter
Z = -387713
70 Z = -118175
14
XDOT = 2689
660446 XDOT = 819
808504
YDOT = -13727
668179 feet/sec YDOT = -4184
193261 meter/sec
ZDOT = -19729
647706 ZDOT = -6013
596621
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 15166
53194865
00016717 00000-0 10270-3 0 9007
2 25544 51
6439 92
3000 0004304 46
1123 314
0385 15
55382367 27785
Satellite: ISS
Catalog Number: 25544
Epoch time: 15166
53194865 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 92
3000 deg
Eccentricity:
0004304
Arg of perigee: 46
1123 deg
Mean anomaly: 314
0385 deg
Mean motion: 15
55382367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2778
Checksum: 296
Coasting Arc #2 (Orbit 2793)
---------------------------------------
Vector Time (GMT): 2015/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1344290
06 A = 6783607
31 meter
Y = 6269151
25 meter E =
0018009
Z = 2187109
80 I = 52
02149
XDOT = -4483
207458 Wp = 65
50901
YDOT = -2895
785736 meter/sec RA = 86
65830 deg
ZDOT = 5516
699369 TA = 318
66945
MA = 318
80560
Ha = 220
406 n
mi
Hp = 211
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4410400
44 X = -1424917
48
Y = 20568081
54 feet Y = 6253667
39 meter
Z = 7175557
10 Z = 2180384
57
XDOT = -14708
685885 XDOT = -4477
291010
YDOT = -9500
609369 feet/sec YDOT = -2945
887627 meter/sec
ZDOT = 18099
407378 ZDOT = 5494
934700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19944018
38 X = 6078936
80
Y = 6720522
89 feet Y = 2048415
38 meter
Z = 7145413
45 Z = 2177922
02
XDOT = -10601
702794 XDOT = -3231
399012
YDOT = 12218
225353 feet/sec YDOT = 3724
115087 meter/sec
ZDOT = 18006
363215 ZDOT = 5488
339508
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 15167
55993642
00016717 00000-0 10270-3 0 9011
2 25544 51
6439 87
1658 0004355 48
7947 311
3582 15
55406429 27947
Satellite: ISS
Catalog Number: 25544
Epoch time: 15167
55993642 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 87
1658 deg
Eccentricity:
0004355
Arg of perigee: 48
7947 deg
Mean anomaly: 311
3582 deg
Mean motion: 15
55406429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2794
Checksum: 342
Coasting Arc #3 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2015/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2389792
23 A = 6778936
89 meter
Y = -4975593
81 meter E =
0010787
Z = -3947276
75 I = 52
00456
XDOT = 3965
702449 Wp = 64
96474
YDOT = 5133
532366 meter/sec RA = 81
69467 deg
ZDOT = -4074
187536 TA = 162
60722
MA = 162
57024
Ha = 220
339 n
mi
Hp = 211
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7840525
68 X = 2464427
26
Y = -16324126
66 feet Y = -4948451
69 meter
Z = -12950383
04 Z = -3935487
07
XDOT = 13010
834807 XDOT = 3927
794170
YDOT = 16842
297788 feet/sec YDOT = 5177
668090 meter/sec
ZDOT = -13366
757007 ZDOT = -4055
014260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15505137
08 X = -4725965
78
Y = -9427497
68 feet Y = -2873501
29 meter
Z = -12898697
09 Z = -3931522
87
XDOT = 17313
865230 XDOT = 5277
266122
YDOT = -10317
842813 feet/sec YDOT = -3144
878489 meter/sec
ZDOT = -13285
296862 ZDOT = -4049
358484
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 15168
52366114
00016717 00000-0 10270-3 0 9028
2 25544 51
6448 82
3523 0004357 52
0913 308
0634 15
55450505 28090
Satellite: ISS
Catalog Number: 25544
Epoch time: 15168
52366114 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 82
3523 deg
Eccentricity:
0004357
Arg of perigee: 52
0913 deg
Mean anomaly: 308
0634 deg
Mean motion: 15
55450505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 292
Coasting Arc #4 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2015/169/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3989315
20 A = 6774518
36 meter
Y = -1274495
72 meter E =
0017136
Z = -5339627
63 I = 51
98065
XDOT = 1965
209477 Wp = 80
99822
YDOT = 7395
199062 meter/sec RA = 76
84590 deg
ZDOT = -295
094710 TA = 186
18736
MA = 186
20855
Ha = 220
330 n
mi
Hp = 212
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13088304
47 X = 4029208
21
Y = -4181416
41 feet Y = -1229660
78 meter
Z = -17518463
35 Z = -5320151
68
XDOT = 6447
537654 XDOT = 1883
801986
YDOT = 24262
464115 feet/sec YDOT = 7416
720186 meter/sec
ZDOT = -968
158498 ZDOT = -285
744831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -632224
47 X = -192702
02
Y = -13832035
32 feet Y = -4216004
37 meter
Z = -17434437
37 Z = -5314016
51
XDOT = 24097
336623 XDOT = 7344
868203
YDOT = 77
513770 feet/sec YDOT = 23
626197 meter/sec
ZDOT = -929
403010 ZDOT = -283
282038
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 15169
48737518
00016717 00000-0 10270-3 0 9035
2 25544 51
6443 77
5380 0002952 45
2777 314
8616 15
55113440 28249
Satellite: ISS
Catalog Number: 25544
Epoch time: 15169
48737518 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 77
5380 deg
Eccentricity:
0002952
Arg of perigee: 45
2777 deg
Mean anomaly: 314
8616 deg
Mean motion: 15
55113440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 318
Coasting Arc #5 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2015/170/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4439386
55 A = 6775713
42 meter
Y = -910096
19 meter E =
0008811
Z = 5032799
07 I = 51
97653
XDOT = -767
130540 Wp = 52
96921
YDOT = -7368
223216 meter/sec RA = 71
85951 deg
ZDOT = -2001
521903 TA = 56
40859
MA = 56
32452
Ha = 220
415 n
mi
Hp = 212
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14564916
50 X = -4453326
97
Y = -2985879
90 feet Y = -959818
91 meter
Z = 16511807
98 Z = 5011199
56
XDOT = -2516
832480 XDOT = -674
957714
YDOT = -24173
960683 feet/sec YDOT = -7376
286147 meter/sec
ZDOT = -6566
672909 ZDOT = -2005
025514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6440200
55 X = -1962973
13
Y = 13514059
37 feet Y = 4119085
30 meter
Z = 16419077
02 Z = 5004534
68
XDOT = -23070
909590 XDOT = -7032
013243
YDOT = -2969
414382 feet/sec YDOT = -905
077504 meter/sec
ZDOT = -6580
277692 ZDOT = -2005
668640
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 15170
51555248
00016717 00000-0 10270-3 0 9040
2 25544 51
6440 72
4052 0002919 46
7111 313
4285 15
55148093 28404
Satellite: ISS
Catalog Number: 25544
Epoch time: 15170
51555248 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 72
4052 deg
Eccentricity:
0002919
Arg of perigee: 46
7111 deg
Mean anomaly: 313
4285 deg
Mean motion: 15
55148093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 288
Coasting Arc #6 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2015/171/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4644337
27 A = 6779629
28 meter
Y = 2895348
84 meter E =
0008803
Z = -4008997
63 I = 51
97950
XDOT = -616
624023 Wp = 90
98609
YDOT = 6509
866265 meter/sec RA = 66
88051 deg
ZDOT = 3994
567104 TA = 220
41350
MA = 220
47893
Ha = 220
339 n
mi
Hp = 212
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15237327
00 X = 4631089
66
Y = 9499175
98 feet Y = 2947211
23 meter
Z = -13152879
35 Z = -3986468
36
XDOT = -2023
044694 XDOT = -708
777033
YDOT = 21357
828954 feet/sec YDOT = 6502
455069 meter/sec
ZDOT = 13105
535119 ZDOT = 3991
348584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12699970
42 X = 3870950
98
Y = -12792423
31 feet Y = -3899130
63 meter
Z = -13056545
13 Z = -3979634
95
XDOT = 19405
466855 XDOT = 5914
786297
YDOT = 5929
538360 feet/sec YDOT = 1807
323292 meter/sec
ZDOT = 13090
387133 ZDOT = 3989
949998
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 15171
47945698
00016717 00000-0 10270-3 0 9059
2 25544 51
6446 67
5923 0002931 50
8293 309
3120 15
55155003 28550
Satellite: ISS
Catalog Number: 25544
Epoch time: 15171
47945698 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 67
5923 deg
Eccentricity:
0002931
Arg of perigee: 50
8293 deg
Mean anomaly: 309
3120 deg
Mean motion: 15
55155003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 313
Coasting Arc #7 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2015/172/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4486856
29 A = 6784073
27 meter
Y = -4503168
52 meter E =
0015790
Z = 2351623
57 I = 51
98071
XDOT = 2145
727897 Wp = 98
69165
YDOT = -4984
866451 meter/sec RA = 61
91539 deg
ZDOT = -5422
965970 TA = 55
17865
MA = 55
03021
Ha = 220
375 n
mi
Hp = 212
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14720657
13 X = -4447590
53
Y = -14774174
95 feet Y = -4553124
17 meter
Z = 7715300
43 Z = 2329922
39
XDOT = 7039
789687 XDOT = 2227
652929
YDOT = -16354
548723 feet/sec YDOT = -4960
412926 meter/sec
ZDOT = -17791
883105 ZDOT = -5412
344010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17523371
49 X = -5341123
63
Y = 11372044
35 feet Y = 3466199
12 meter
Z = 7622854
53 Z = 2323446
06
XDOT = -13680
532154 XDOT = -4169
826201
YDOT = -9121
944253 feet/sec YDOT = -2780
368608 meter/sec
ZDOT = -17745
187396 ZDOT = -5408
733118
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 15172
50760865
00016717 00000-0 10270-3 0 9066
2 25544 51
6443 62
4587 0002898 55
6039 304
5388 15
55149885 28712
Satellite: ISS
Catalog Number: 25544
Epoch time: 15172
50760865 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 62
4587 deg
Eccentricity:
0002898
Arg of perigee: 55
6039 deg
Mean anomaly: 304
5388 deg
Mean motion: 15
55149885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 342
Coasting Arc #8 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2015/173/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3935049
14 A = 6786187
45 meter
Y = 5508092
69 meter E =
0014179
Z = -377981
30 I = 51
97304
XDOT = -3660
311203 Wp = 44
92422
YDOT = 3018
539957 meter/sec RA = 56
96027 deg
ZDOT = 6028
029669 TA = 311
01731
MA = 311
13981
Ha = 220
282 n
mi
Hp = 212
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12910266
22 X = 3874999
95
Y = 18071170
24 feet Y = 5551761
26 meter
Z = -1240096
14 Z = -359011
10
XDOT = -12008
895022 XDOT = -3723
074928
YDOT = 9903
346316 feet/sec YDOT = 2977
256517 meter/sec
ZDOT = 19777
000228 ZDOT = 6010
096503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20207840
48 X = 6159349
78
Y = -9223800
75 feet Y = -2811414
47 meter
Z = -1159607
23 Z = -353448
28
XDOT = 6729
324731 XDOT = 2051
098178
YDOT = 12331
151862 feet/sec YDOT = 3758
535088 meter/sec
ZDOT = 19699
246979 ZDOT = 6004
330479
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 15173
47148690
00016717 00000-0 10270-3 0 9070
2 25544 51
6449 57
6457 0002856 55
4313 304
7109 15
55191332 28860
Satellite: ISS
Catalog Number: 25544
Epoch time: 15173
47148690 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 57
6457 deg
Eccentricity:
0002856
Arg of perigee: 55
4313 deg
Mean anomaly: 304
7109 deg
Mean motion: 15
55191332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 324
Coasting Arc #9 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2015/174/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2908674
20 A = 6785016
41 meter
Y = -5887343
37 meter E =
0008420
Z = -1701670
54 I = 51
95136
XDOT = 5030
276322 Wp = 123
15025
YDOT = -837
918407 meter/sec RA = 52
00646 deg
ZDOT = -5724
192496 TA = 75
42481
MA = 75
33145
Ha = 220
235 n
mi
Hp = 212
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9542894
35 X = -2834358
29
Y = -19315431
01 feet Y = -5919454
41 meter
Z = -5582908
60 Z = -1715620
22
XDOT = 16503
531239 XDOT = 5067
078139
YDOT = -2749
076139 feet/sec YDOT = -781
460343 meter/sec
ZDOT = -18780
159109 ZDOT = -5699
667159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20677482
57 X = -6302496
69
Y = 5994525
25 feet Y = 1827131
30 meter
Z = -5641715
88 Z = -1719595
00
XDOT = 626
027781 XDOT = 190
813268
YDOT = -15339
904978 feet/sec YDOT = -4675
603037 meter/sec
ZDOT = -18674
491217 ZDOT = -5691
984923
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 15174
49961175
00016717 00000-0 10270-3 0 9085
2 25544 51
6452 52
5119 0002689 59
9777 300
1642 15
55179291 29021
Satellite: ISS
Catalog Number: 25544
Epoch time: 15174
49961175 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 52
5119 deg
Eccentricity:
0002689
Arg of perigee: 59
9777 deg
Mean anomaly: 300
1642 deg
Mean motion: 15
55179291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 330
Coasting Arc #10 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2015/175/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1492201
80 A = 6780984
60 meter
Y = 5612300
89 meter E =
0014786
Z = 3487156
18 I = 51
91800
XDOT = -6043
256122 Wp = 85
42347
YDOT = -1239
843806 meter/sec RA = 47
04185 deg
ZDOT = 4565
965465 TA = 315
42190
MA = 315
54073
Ha = 220
263 n
mi
Hp = 212
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4895675
18 X = 1412393
52
Y = 18413060
65 feet Y = 5628541
16 meter
Z = 11440801
11 Z = 3494211
58
XDOT = -19826
955782 XDOT = -6051
122463
YDOT = -4067
729023 feet/sec YDOT = -1307
467786 meter/sec
ZDOT = 14980
201656 ZDOT = 4536
589332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18943616
31 X = 5774014
25
Y = -1865172
02 feet Y = -568504
43 meter
Z = 11470000
10 Z = 3496056
03
XDOT = -7286
451969 XDOT = -2220
910560
YDOT = 17652
475544 feet/sec YDOT = 5380
474546 meter/sec
ZDOT = 14854
096195 ZDOT = 4527
528520
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 15175
52772313
00016717 00000-0 10270-3 0 9095
2 25544 51
6452 47
3779 0002898 60
4542 299
6900 15
55213210 29180
Satellite: ISS
Catalog Number: 25544
Epoch time: 15175
52772313 = yrday
fracday
Element set: 909
Inclination: 51
6452 deg
RA of node: 47
3779 deg
Eccentricity:
0002898
Arg of perigee: 60
4542 deg
Mean anomaly: 299
6900 deg
Mean motion: 15
55213210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 319
Coasting Arc #11 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2015/176/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 265731
62 A = 6776385
60 meter
Y = -4810525
23 meter E =
0013926
Z = -4778600
01 I = 51
88071
XDOT = 6501
961379 Wp = 69
05444
YDOT = 3027
029151 meter/sec RA = 42
06113 deg
ZDOT = -2687
148893 TA = 174
46824
MA = 174
45284
Ha = 220
134 n
mi
Hp = 212
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 871822
90 X = 342716
99
Y = -15782563
09 feet Y = -4807122
81 meter
Z = -15677821
56 Z = -4777122
53
XDOT = 21331
894289 XDOT = 6480
682351
YDOT = 9931
198002 feet/sec YDOT = 3099
619576 meter/sec
ZDOT = -8816
105292 ZDOT = -2655
615028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15491464
82 X = -4721798
48
Y = -3177136
76 feet Y = -968391
28 meter
Z = -15670474
84 Z = -4776360
73
XDOT = 12602
003328 XDOT = 3841
090614
YDOT = -18652
591528 feet/sec YDOT = -5685
309898 meter/sec
ZDOT = -8681
093526 ZDOT = -2645
997307
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 15176
49156390
00016717 00000-0 10270-3 0 9105
2 25544 51
6452 42
5649 0002713 61
0727 299
0698 15
55258611 29330
Satellite: ISS
Catalog Number: 25544
Epoch time: 15176
49156390 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 42
5649 deg
Eccentricity:
0002713
Arg of perigee: 61
0727 deg
Mean anomaly: 299
0698 deg
Mean motion: 15
55258611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 319
Coasting Arc #12 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2015/177/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2148850
55 A = 6774054
21 meter
Y = 3606375
74 meter E =
0004988
Z = 5312112
79 I = 51
84909
XDOT = -6303
570289 Wp = 85
24755
YDOT = -4358
723798 meter/sec RA = 37
06700 deg
ZDOT = 409
282745 TA =
86438
MA =
86352
Ha = 220
229 n
mi
Hp = 211
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7050034
62 X = -2214822
54
Y = 11831941
41 feet Y = 3581976
55 meter
Z = 17428191
56 Z = 5301514
13
XDOT = -20681
004886 XDOT = -6256
349648
YDOT = -14300
274928 feet/sec YDOT = -4428
950458 meter/sec
ZDOT = 1342
791159 ZDOT = 378
775432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10860430
85 X = 3310259
32
Y = 8565149
13 feet Y = 2610657
45 meter
Z = 17381856
89 Z = 5297989
98
XDOT = -16117
251417 XDOT = -4912
538232
YDOT = 17976
259185 feet/sec YDOT = 5479
163800 meter/sec
ZDOT = 1212
480395 ZDOT = 369
564024
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 15177
51964952
00016717 00000-0 10270-3 0 9111
2 25544 51
6455 37
4312 0002726 65
8631 294
2807 15
55273601 29495
Satellite: ISS
Catalog Number: 25544
Epoch time: 15177
51964952 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 37
4312 deg
Eccentricity:
0002726
Arg of perigee: 65
8631 deg
Mean anomaly: 294
2807 deg
Mean motion: 15
55273601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2949
Checksum: 320
Coasting Arc #13 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2015/178/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3957001
95 A = 6775232
40 meter
Y = -2206742
24 meter E =
0015035
Z = -5050933
48 I = 51
82650
XDOT = 5336
359656 Wp = 98
06660
YDOT = 5140
807917 meter/sec RA = 32
06812 deg
ZDOT = 1937
475569 TA = 190
68847
MA = 190
72046
Ha = 220
079 n
mi
Hp = 212
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12982289
85 X = 4005919
82
Y = -7239967
98 feet Y = -2162218
42 meter
Z = -16571304
05 Z = -5031592
45
XDOT = 17507
741655 XDOT = 5269
065729
YDOT = 16866
167707 feet/sec YDOT = 5200
106124 meter/sec
ZDOT = 6356
547142 ZDOT = 1963
235757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5810644
28 X = -1771084
38
Y = -13782549
46 feet Y = -4200921
08 meter
Z = -16487657
43 Z = -5025437
99
XDOT = 17621
371775 XDOT = 5370
994117
YDOT = -15153
139809 feet/sec YDOT = -4618
677014 meter/sec
ZDOT = 6466
266604 ZDOT = 1970
918061
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 15178
48346734
00016717 00000-0 10270-3 0 9121
2 25544 51
6447 32
6174 0002635 66
7494 293
3937 15
55299687 29648
Satellite: ISS
Catalog Number: 25544
Epoch time: 15178
48346734 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 32
6174 deg
Eccentricity:
0002635
Arg of perigee: 66
7494 deg
Mean anomaly: 293
3937 deg
Mean motion: 15
55299687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 353
Coasting Arc #14 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2015/179/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5433807
25 A = 6779171
14 meter
Y = 735411
36 meter E =
0013583
Z = 3977155
10 I = 51
81298
XDOT = -3675
161273 Wp = 77
01279
YDOT = -5416
899418 meter/sec RA = 27
07759 deg
ZDOT = -4005
103404 TA = 54
65657
MA = 54
52968
Ha = 220
083 n
mi
Hp = 211
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17827451
61 X = -5460946
55
Y = 2412766
91 feet Y = 674494
75 meter
Z = 13048409
11 Z = 3950692
78
XDOT = -12057
615724 XDOT = -3594
859692
YDOT = -17771
979717 feet/sec YDOT = -5457
548005 meter/sec
ZDOT = -13140
103032 ZDOT = -4022
762301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 808909
92 X = 246555
74
Y = 18053982
85 feet Y = 5502853
97 meter
Z = 12934443
30 Z = 3942418
32
XDOT = -17452
693212 XDOT = -5319
580891
YDOT = 10283
861638 feet/sec YDOT = 3134
521027 meter/sec
ZDOT = -13214
911917 ZDOT = -4027
905152
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 15179
51152618
00016717 00000-0 10270-3 0 9133
2 25544 51
6450 27
4836 0002587 66
6746 293
4679 15
55351006 29800
Satellite: ISS
Catalog Number: 25544
Epoch time: 15179
51152618 = yrday
fracday
Element set: 913
Inclination: 51
6450 deg
RA of node: 27
4836 deg
Eccentricity:
0002587
Arg of perigee: 66
6746 deg
Mean anomaly: 293
4679 deg
Mean motion: 15
55351006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 327
Coasting Arc #15 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2015/180/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6346683
93 A = 6783677
19 meter
Y = 613292
48 meter E =
0008255
Z = -2311917
58 I = 51
79769
XDOT = 1468
283281 Wp = 51
57168
YDOT = 5208
897931 meter/sec RA = 22
09913 deg
ZDOT = 5430
631255 TA = 282
72144
MA = 282
81370
Ha = 220
065 n
mi
Hp = 211
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20822453
84 X = 6350584
70
Y = 2012114
44 feet Y = 684287
38 meter
Z = -7585031
42 Z = -2281076
99
XDOT = 4817
202364 XDOT = 1383
546985
YDOT = 17089
560142 feet/sec YDOT = 5224
842710 meter/sec
ZDOT = 17817
031676 ZDOT = 5437
558797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3507531
99 X = 1069095
75
Y = -20671551
14 feet Y = -6300688
79 meter
Z = -7452521
89 Z = -2271528
67
XDOT = 15877
935582 XDOT = 4839
594765
YDOT = -3717
798260 feet/sec YDOT = -1133
184910 meter/sec
ZDOT = 17845
723422 ZDOT = 5439
376499
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 15180
47532139
00016717 00000-0 10270-3 0 9141
2 25544 51
6436 22
6697 0002521 71
2132 288
9295 15
55318172 29951
Satellite: ISS
Catalog Number: 25544
Epoch time: 15180
47532139 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 22
6697 deg
Eccentricity:
0002521
Arg of perigee: 71
2132 deg
Mean anomaly: 288
9295 deg
Mean motion: 15
55318172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 316
Coasting Arc #16 (Orbit 3009)
---------------------------------------
Vector Time (GMT): 2015/181/11:17:57
440
Vector Time (MET): N/A
Weight (LBS) : 877531
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6528073
46 A = 6785797
40 meter
Y = -1816231
52 meter E =
0014051
Z = 237815
87 I = 51
77510
XDOT = 1060
992810 Wp = 123
38609
YDOT = -4634
269320 meter/sec RA = 17
13159 deg
ZDOT = -6019
585028 TA = 54
05490
MA = 53
92463
Ha = 220
008 n
mi
Hp = 211
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21417563
84 X = -6508433
96
Y = -5958764
84 feet Y = -1889122
94 meter
Z = 780235
78 Z = 206151
22
XDOT = 3480
947540 XDOT = 1141
976315
YDOT = -15204
295670 feet/sec YDOT = -4621
950919 meter/sec
ZDOT = -19749
294712 ZDOT = -6014
234913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7123022
87 X = -2171097
37
Y = 21063592
53 feet Y = 6420183
00 meter
Z = 644439
38 Z = 196425
12
XDOT = -13449
822943 XDOT = -4099
506033
YDOT = -3914
590351 feet/sec YDOT = -1193
167139 meter/sec
ZDOT = -19725
300317 ZDOT = -6012
271537
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 15181
50335616
00016717 00000-0 10270-3 0 9158
2 25544 51
6434 17
5355 0002567 75
9192 284
2246 15
55338780 30101
Satellite: ISS
Catalog Number: 25544
Epoch time: 15181
50335616 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 17
5355 deg
Eccentricity:
0002567
Arg of perigee: 75
9192 deg
Mean anomaly: 284
2246 deg
Mean motion: 15
55338780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3010
Checksum: 303
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