[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 11th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3166)
---------------------------------------
Vector Time (GMT): 2015/191/11:58:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5974693
94 A = 6782887
95 meter
Y = 969629
20 meter E =
0004110
Z = -3060192
88 I = 51
45446
XDOT = 1583
892306 Wp = 133
78559
YDOT = -5680
101681 meter/sec RA = 327
02783 deg
ZDOT = -4899
036475 TA = 81
44634
MA = 81
39977
Ha = 219
267 n
mi
Hp = 213
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19602014
23 X = -5970227
28
Y = 3181198
16 feet Y = 902841
51 meter
Z = -10040002
88 Z = -3089205
78
XDOT = 5196
497067 XDOT = 1671
088477
YDOT = -18635
504204 feet/sec YDOT = -5661
901579 meter/sec
ZDOT = -16072
954315 ZDOT = -4891
130968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8703843
61 X = 2652931
53
Y = 17778574
71 feet Y = 5418909
57 meter
Z = -10164941
18 Z = -3098274
07
XDOT = -18076
422994 XDOT = -5509
693729
YDOT = -307
186261 feet/sec YDOT = -93
630372 meter/sec
ZDOT = -16037
786758 ZDOT = -4888
317404
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 15191
52465072
00016717 00000-0 10270-3 0 9005
2 25544 51
6429 327
4691 0002174 220
3487 139
7505 15
54942574 31674
Satellite: ISS
Catalog Number: 25544
Epoch time: 15191
52465072 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 327
4691 deg
Eccentricity:
0002174
Arg of perigee: 220
3487 deg
Mean anomaly: 139
7505 deg
Mean motion: 15
54942574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 313
Coasting Arc #2 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2015/192/11:58:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5107573
70 A = 6778369
65 meter
Y = 492426
92 meter E =
0008446
Z = 4425746
38 I = 51
41446
XDOT = -3439
138353 Wp = 124
55657
YDOT = 6015
601442 meter/sec RA = 322
02116 deg
ZDOT = 3290
462321 TA = 292
11647
MA = 292
20610
Ha = 219
049 n
mi
Hp = 213
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16757131
58 X = 5080189
12
Y = 1615573
89 feet Y = 549389
57 meter
Z = 14520165
27 Z = 4450491
44
XDOT = -11283
262312 XDOT = -3522
134429
YDOT = 19736
225202 feet/sec YDOT = 5976
678338 meter/sec
ZDOT = 10795
480057 ZDOT = 3273
554752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3561889
64 X = -1085663
96
Y = -16359298
65 feet Y = -4986314
23 meter
Z = 14626449
57 Z = 4458141
83
XDOT = 21071
756252 XDOT = 6422
671305
YDOT = 5024
694789 feet/sec YDOT = 1531
526972 meter/sec
ZDOT = 10721
544268 ZDOT = 3267
926693
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 15192
55293463
00016717 00000-0 10270-3 0 9013
2 25544 51
6437 322
3363 0002231 226
0452 134
0518 15
54994930 31835
Satellite: ISS
Catalog Number: 25544
Epoch time: 15192
55293463 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 322
3363 deg
Eccentricity:
0002231
Arg of perigee: 226
0452 deg
Mean anomaly: 134
0518 deg
Mean motion: 15
54994930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 292
Coasting Arc #3 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2015/193/11:58:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3823315
00 A = 6775274
75 meter
Y = -2106555
39 meter E =
0012411
Z = -5192515
50 I = 51
37989
XDOT = 4834
891370 Wp = 85
33477
YDOT = -5819
757885 meter/sec RA = 317
00071 deg
ZDOT = -1200
463241 TA = 173
10366
MA = 173
08656
Ha = 219
102 n
mi
Hp = 213
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12543684
39 X = -3774251
69
Y = -6911270
97 feet Y = -2149035
27 meter
Z = -17035812
00 Z = -5210969
39
XDOT = 15862
504495 XDOT = 4905
441327
YDOT = -19093
693847 feet/sec YDOT = -5765
296354 meter/sec
ZDOT = -3938
527692 ZDOT = -1176
805732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2534051
64 X = -772378
94
Y = 13999773
14 feet Y = 4267130
85 meter
Z = -17114716
16 Z = -5216565
49
XDOT = -22176
109725 XDOT = -6759
278244
YDOT = -8697
101371 feet/sec YDOT = -2650
876498 meter/sec
ZDOT = -3835
617113 ZDOT = -1169
096096
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 15193
51693751
00016717 00000-0 10270-3 0 9025
2 25544 51
6440 317
5252 0002068 232
0281 128
0685 15
54998324 31982
Satellite: ISS
Catalog Number: 25544
Epoch time: 15193
51693751 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 317
5252 deg
Eccentricity:
0002068
Arg of perigee: 232
0281 deg
Mean anomaly: 128
0685 deg
Mean motion: 15
54998324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 311
Coasting Arc #4 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2015/194/11:58:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2295057
69 A = 6775155
11 meter
Y = 3674485
80 meter E =
0001814
Z = 5207848
84 I = 51
35762
XDOT = -5678
523978 Wp = 55
78629
YDOT = 5048
064308 meter/sec RA = 311
97176 deg
ZDOT = -1058
000445 TA = 44
39148
MA = 44
37694
Ha = 218
954 n
mi
Hp = 213
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7529716
84 X = 2228500
60
Y = 12055399
61 feet Y = 3699777
86 meter
Z = 17086118
25 Z = 5218836
47
XDOT = -18630
328013 XDOT = -5729
411285
YDOT = 16561
890775 feet/sec YDOT = 4984
278934 meter/sec
ZDOT = -3471
130068 ZDOT = -1085
708343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8831193
98 X = 2691747
92
Y = -11065650
63 feet Y = -3372810
31 meter
Z = 17132604
04 Z = 5222017
71
XDOT = 21077
990424 XDOT = 6424
571481
YDOT = 11255
070234 feet/sec YDOT = 3430
545407 meter/sec
ZDOT = -3591
291122 ZDOT = -1094
625534
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 15194
54519082
00016717 00000-0 10270-3 0 9034
2 25544 51
6446 312
3919 0001987 237
5244 122
5718 15
55017282 32140
Satellite: ISS
Catalog Number: 25544
Epoch time: 15194
54519082 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 312
3919 deg
Eccentricity:
0001987
Arg of perigee: 237
5244 deg
Mean anomaly: 122
5718 deg
Mean motion: 15
55017282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 308
Coasting Arc #5 (Orbit 3228)
---------------------------------------
Vector Time (GMT): 2015/195/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 721328
83 A = 6781323
03 meter
Y = -5718764
62 meter E =
0003678
Z = -3576673
43 I = 51
35795
XDOT = 5930
982479 Wp = 113
23016
YDOT = -2013
096114 meter/sec RA = 306
93085 deg
ZDOT = 4417
089864 TA = 204
31210
MA = 204
32945
Ha = 218
950 n
mi
Hp = 213
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2366564
42 X = 802597
73
Y = -18762351
11 feet Y = -5710243
42 meter
Z = -11734492
88 Z = -3572972
69
XDOT = 19458
603933 XDOT = 5931
596315
YDOT = -6604
646043 feet/sec YDOT = -1946
769079 meter/sec
ZDOT = 14491
764645 ZDOT = 4445
902304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18329446
77 X = -5586815
38
Y = 4696624
87 feet Y = 1431531
26 meter
Z = -11717417
17 Z = -3571468
75
XDOT = -12976
337154 XDOT = -3955
187564
YDOT = -14195
617746 feet/sec YDOT = -4326
824289 meter/sec
ZDOT = 14616
051352 ZDOT = 4454
972452
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 15195
50916278
00016717 00000-0 10270-3 0 9040
2 25544 51
6449 307
5806 0002057 245
1908 114
9031 15
55021380 32298
Satellite: ISS
Catalog Number: 25544
Epoch time: 15195
50916278 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 307
5806 deg
Eccentricity:
0002057
Arg of perigee: 245
1908 deg
Mean anomaly: 114
9031 deg
Mean motion: 15
55021380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3229
Checksum: 302
Coasting Arc #6 (Orbit 3244)
---------------------------------------
Vector Time (GMT): 2015/196/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2107246
38 A = 6785232
66 meter
Y = 6172620
90 meter E =
0012747
Z = 1845720
43 I = 51
35292
XDOT = -5227
882764 Wp = 120
39078
YDOT = -99
155627 meter/sec RA = 301
92748 deg
ZDOT = -5614
353451 TA = 39
20515
MA = 39
11290
Ha = 218
924 n
mi
Hp = 213
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6913537
99 X = -2185079
17
Y = 20251380
92 feet Y = 6148620
90 meter
Z = 6055513
22 Z = 1835295
65
XDOT = -17151
846338 XDOT = -5199
113456
YDOT = -325
313737 feet/sec YDOT = -157
455751 meter/sec
ZDOT = -18419
794788 ZDOT = -5639
679217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21364258
74 X = 6511826
06
Y = -1428176
03 feet Y = -435308
05 meter
Z = 6009445
77 Z = 1831679
07
XDOT = 6187
207789 XDOT = 1885
860934
YDOT = 14275
224459 feet/sec YDOT = 4351
088415 meter/sec
ZDOT = -18528
663210 ZDOT = -5647
536546
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 15196
53738486
00016717 00000-0 10270-3 0 9058
2 25544 51
6449 302
4481 0001976 245
2683 114
8265 15
55049158 32450
Satellite: ISS
Catalog Number: 25544
Epoch time: 15196
53738486 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 302
4481 deg
Eccentricity:
0001976
Arg of perigee: 245
2683 deg
Mean anomaly: 114
8265 deg
Mean motion: 15
55049158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 332
Coasting Arc #7 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2015/197/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3166698
80 A = 6786567
18 meter
Y = -5994621
82 meter E =
0010807
Z = 135178
73 I = 51
34222
XDOT = 4179
049226 Wp = 41
92896
YDOT = 2348
707807 meter/sec RA = 296
93165 deg
ZDOT = 5987
453553 TA = 319
53387
MA = 319
61419
Ha = 218
852 n
mi
Hp = 213
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10389431
76 X = 3232840
11
Y = -19667394
44 feet Y = -5958839
92 meter
Z = 443499
77 Z = 150721
71
XDOT = 13710
791425 XDOT = 4123
390553
YDOT = 7705
734275 feet/sec YDOT = 2395
128878 meter/sec
ZDOT = 19643
876486 ZDOT = 6007
619233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22185003
69 X = -6761989
13
Y = -1583458
45 feet Y = -482638
14 meter
Z = 511525
87 Z = 155913
08
XDOT = 1466
252930 XDOT = 446
913893
YDOT = -13921
448527 feet/sec YDOT = -4243
257511 meter/sec
ZDOT = 19730
111706 ZDOT = 6013
738048
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 15197
56559046
00016717 00000-0 10270-3 0 9066
2 25544 51
6455 297
3152 0001876 256
3600 103
7344 15
55076115 32611
Satellite: ISS
Catalog Number: 25544
Epoch time: 15197
56559046 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 297
3152 deg
Eccentricity:
0001876
Arg of perigee: 256
3600 deg
Mean anomaly: 103
7344 deg
Mean motion: 15
55076115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 311
Coasting Arc #8 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2015/198/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3900639
56 A = 6784515
37 meter
Y = 5123214
94 meter E =
0005550
Z = -2129189
36 I = 51
32142
XDOT = -2919
750551 Wp = 155
23302
YDOT = -4496
904741 meter/sec RA = 291
93472 deg
ZDOT = -5481
578340 TA = 48
47981
MA = 48
43221
Ha = 218
744 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12797373
89 X = -3947296
08
Y = 16808447
96 feet Y = 5079334
73 meter
Z = -6985529
39 Z = -2148250
44
XDOT = -9579
234092 XDOT = -2842
621154
YDOT = -14753
624477 feet/sec YDOT = -4529
123602 meter/sec
ZDOT = -17984
180904 ZDOT = -5495
574674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20602223
99 X = 6279557
87
Y = 4547420
29 feet Y = 1386053
70 meter
Z = -7068497
54 Z = -2154478
05
XDOT = -9108
077829 XDOT = -2776
142122
YDOT = 13268
831432 feet/sec YDOT = 4044
339821 meter/sec
ZDOT = -18043
472614 ZDOT = -5499
650453
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 15198
52951860
00016717 00000-0 10270-3 0 9074
2 25544 51
6448 292
5038 0001927 258
5508 101
5429 15
55106219 32766
Satellite: ISS
Catalog Number: 25544
Epoch time: 15198
52951860 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 292
5038 deg
Eccentricity:
0001927
Arg of perigee: 258
5508 deg
Mean anomaly: 101
5429 deg
Mean motion: 15
55106219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 324
Coasting Arc #9 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2015/199/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4280826
66 A = 6780167
45 meter
Y = -3637689
82 meter E =
0009576
Z = 3789568
21 I = 51
29634
XDOT = 1596
711132 Wp = 99
94516
YDOT = 6236
718405 meter/sec RA = 286
92491 deg
ZDOT = 4172
418648 TA = 305
82991
MA = 305
91883
Ha = 218
606 n
mi
Hp = 213
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14044706
88 X = 4302778
08
Y = -11934677
88 feet Y = -3589696
31 meter
Z = 12432966
57 Z = 3810416
31
XDOT = 5238
553582 XDOT = 1506
584328
YDOT = 20461
674556 feet/sec YDOT = 6254
069681 meter/sec
ZDOT = 13689
037559 ZDOT = 4179
956503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16812682
13 X = -5124505
51
Y = -7400623
16 feet Y = -2255709
94 meter
Z = 12523317
51 Z = 3817107
18
XDOT = 15658
708675 XDOT = 4772
774404
YDOT = -12297
326102 feet/sec YDOT = -3748
224996 meter/sec
ZDOT = 13720
231580 ZDOT = 4181
926586
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 15199
55769300
00016717 00000-0 10270-3 0 9085
2 25544 51
6448 287
3703 0001909 264
9339 95
1596 15
55151887 32922
Satellite: ISS
Catalog Number: 25544
Epoch time: 15199
55769300 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 287
3703 deg
Eccentricity:
0001909
Arg of perigee: 264
9339 deg
Mean anomaly: 95
1596 deg
Mean motion: 15
55151887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3292
Checksum: 351
Coasting Arc #10 (Orbit 3306)
---------------------------------------
Vector Time (GMT): 2015/200/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4374610
56 A = 6776061
24 meter
Y = 1659711
01 meter E =
0010455
Z = -4911123
24 I = 51
27317
XDOT = -280
603612 Wp = 70
37371
YDOT = -7325
790904 meter/sec RA = 281
90062 deg
ZDOT = -2226
229756 TA = 177
76161
MA = 177
75693
Ha = 218
689 n
mi
Hp = 213
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14352396
84 X = -4368988
75
Y = 5445246
11 feet Y = 1610822
92 meter
Z = -16112609
06 Z = -4932360
13
XDOT = -920
615526 XDOT = -187
850009
YDOT = -24034
747062 feet/sec YDOT = -7328
410075 meter/sec
ZDOT = -7303
903400 ZDOT = -2227
367917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11268147
48 X = 3434531
35
Y = 10281514
46 feet Y = 3133805
61 meter
Z = -16204242
76 Z = -4939053
19
XDOT = -20327
473680 XDOT = -6195
813978
YDOT = 10763
510867 feet/sec YDOT = 3280
718112 meter/sec
ZDOT = -7307
385294 ZDOT = -2227
291038
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 15200
52159440
00016717 00000-0 10270-3 0 9094
2 25544 51
6439 282
5588 0001961 271
3907 88
7021 15
55137048 33072
Satellite: ISS
Catalog Number: 25544
Epoch time: 15200
52159440 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 282
5588 deg
Eccentricity:
0001961
Arg of perigee: 271
3907 deg
Mean anomaly: 88
7021 deg
Mean motion: 15
55137048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3307
Checksum: 310
Coasting Arc #11 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2015/201/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4201587
17 A = 6774211
48 meter
Y = 562394
93 meter E =
0000579
Z = 5283589
24 I = 51
26215
XDOT = -956
157861 Wp = 49
39157
YDOT = 7611
132911 meter/sec RA = 276
86422 deg
ZDOT = -49
418314 TA = 41
08382
MA = 41
07946
Ha = 218
438 n
mi
Hp = 213
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13784734
83 X = 4169320
78
Y = 1845127
72 feet Y = 609199
23 meter
Z = 17334610
37 Z = 5303921
06
XDOT = -3137
000857 XDOT = -1040
956264
YDOT = 24970
908502 feet/sec YDOT = 7599
966393 meter/sec
ZDOT = -162
133575 ZDOT = -54
268752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4720826
91 X = -1438908
04
Y = -12965431
20 feet Y = -3951863
43 meter
Z = 17421926
25 Z = 5310203
12
XDOT = 22621
534579 XDOT = 6895
043740
YDOT = -8486
174077 feet/sec YDOT = -2586
585859 meter/sec
ZDOT = -184
439350 ZDOT = -56
217114
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 15201
54973907
00016717 00000-0 10270-3 0 9101
2 25544 51
6440 277
4249 0001983 277
8029 82
2899 15
55205767 33235
Satellite: ISS
Catalog Number: 25544
Epoch time: 15201
54973907 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 277
4249 deg
Eccentricity:
0001983
Arg of perigee: 277
8029 deg
Mean anomaly: 82
2899 deg
Mean motion: 15
55205767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 330
Coasting Arc #12 (Orbit 3337)
---------------------------------------
Vector Time (GMT): 2015/202/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3824268
64 A = 6776024
41 meter
Y = -2760410
31 meter E =
0010205
Z = -4874715
02 I = 51
26417
XDOT = 2088
631455 Wp = 106
83520
YDOT = -6995
847288 meter/sec RA = 271
82827 deg
ZDOT = 2324
137910 TA = 186
04285
MA = 186
05517
Ha = 218
662 n
mi
Hp = 213
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12546813
12 X = -3769437
62
Y = -9056464
27 feet Y = -2802869
06 meter
Z = -15993159
50 Z = -4893159
23
XDOT = 6852
465403 XDOT = 2155
415829
YDOT = -22952
254881 feet/sec YDOT = -6972
117499 meter/sec
ZDOT = 7625
124375 ZDOT = 2334
445939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1973154
92 X = -601417
62
Y = 15265071
06 feet Y = 4652793
66 meter
Z = -16071947
02 Z = -4898729
45
XDOT = -22287
420073 XDOT = -6793
205638
YDOT = 5191
423373 feet/sec YDOT = 1582
345844 meter/sec
ZDOT = 7670
765472 ZDOT = 2338
049316
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 15202
51361353
00016717 00000-0 10270-3 0 9116
2 25544 51
6429 272
6127 0001841 287
3494 72
7457 15
55206974 33380
Satellite: ISS
Catalog Number: 25544
Epoch time: 15202
51361353 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 272
6127 deg
Eccentricity:
0001841
Arg of perigee: 287
3494 deg
Mean anomaly: 72
7457 deg
Mean motion: 15
55206974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3338
Checksum: 310
Coasting Arc #13 (Orbit 3353)
---------------------------------------
Vector Time (GMT): 2015/203/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3236501
12 A = 6780171
65 meter
Y = 4659310
04 meter E =
0009996
Z = 3706259
58 I = 51
27882
XDOT = -3113
844967 Wp = 78
60626
YDOT = 5564
866794 meter/sec RA = 266
80189 deg
ZDOT = -4264
940607 TA = 56
88527
MA = 56
78937
Ha = 218
540 n
mi
Hp = 213
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10618441
98 X = 3166155
61
Y = 15286450
25 feet Y = 4695109
28 meter
Z = 12159644
28 Z = 3721810
98
XDOT = -10216
026793 XDOT = -3155
123951
YDOT = 18257
436987 feet/sec YDOT = 5529
815055 meter/sec
ZDOT = -13992
587293 ZDOT = -4280
167005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8065595
88 X = 2458393
62
Y = -16726134
62 feet Y = -5098125
83 meter
Z = 12225645
34 Z = 3726376
70
XDOT = 19655
629408 XDOT = 5991
035843
YDOT = -825
977414 feet/sec YDOT = -251
757916 meter/sec
ZDOT = -14059
097723 ZDOT = -4285
212986
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 15203
54173018
00016717 00000-0 10270-3 0 9120
2 25544 51
6433 267
4785 0001985 293
8087 66
2858 15
55250446 33540
Satellite: ISS
Catalog Number: 25544
Epoch time: 15203
54173018 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 267
4785 deg
Eccentricity:
0001985
Arg of perigee: 293
8087 deg
Mean anomaly: 66
2858 deg
Mean motion: 15
55250446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 324
Coasting Arc #14 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2015/204/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2473897
84 A = 6784440
57 meter
Y = -5992836
94 meter E =
0006661
Z = -1987824
80 I = 51
29474
XDOT = 3988
585456 Wp = 23
52490
YDOT = -3482
395141 meter/sec RA = 261
79083 deg
ZDOT = 5547
171292 TA = 314
41163
MA = 314
46613
Ha = 218
674 n
mi
Hp = 213
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8116462
73 X = -2397044
60
Y = -19661538
53 feet Y = -6020071
92 meter
Z = -6521734
92 Z = -1999655
95
XDOT = 13085
910290 XDOT = 4000
284131
YDOT = -11425
180909 feet/sec YDOT = -3437
726928 meter/sec
ZDOT = 18199
380879 ZDOT = 5566
575217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12797255
80 X = -3900603
57
Y = 16971496
60 feet Y = 5172912
16 meter
Z = -6571501
95 Z = -2002993
80
XDOT = -15202
354685 XDOT = -4633
677708
YDOT = -4399
424547 feet/sec YDOT = -1340
944602 meter/sec
ZDOT = 18283
462444 ZDOT = 5572
799353
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 15204
50557808
00016717 00000-0 10270-3 0 9131
2 25544 51
6425 262
6656 0001940 299
6910 60
4050 15
55223630 33696
Satellite: ISS
Catalog Number: 25544
Epoch time: 15204
50557808 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 262
6656 deg
Eccentricity:
0001940
Arg of perigee: 299
6910 deg
Mean anomaly: 60
4050 deg
Mean motion: 15
55223630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 301
Coasting Arc #15 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2015/205/12:02:20
369
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1495267
84 A = 6785990
75 meter
Y = 6613786
74 meter E =
0010158
Z = -69463
73 I = 51
30642
XDOT = -4689
277321 Wp = 136
33192
YDOT = 1002
887747 meter/sec RA = 256
79041 deg
ZDOT = -5985
733408 TA = 44
42009
MA = 44
33866
Ha = 218
717 n
mi
Hp = 213
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4905734
40 X = 1421537
18
Y = 21698775
41 feet Y = 6630095
56 meter
Z = -227899
37 Z = -62378
87
XDOT = -15384
768114 XDOT = -4671
067067
YDOT = 3290
314131 feet/sec YDOT = 950
551232 meter/sec
ZDOT = -19638
232966 ZDOT = -6008
468596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15899035
48 X = 4846026
02
Y = -15560727
27 feet Y = -4742909
67 meter
Z = -198645
05 Z = -60547
01
XDOT = 9669
912008 XDOT = 2947
389180
YDOT = 10106
534517 feet/sec YDOT = 3080
471721 meter/sec
ZDOT = -19736
183478 ZDOT = -6015
588724
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 15205
53366774
00016717 00000-0 10270-3 0 9146
2 25544 51
6431 257
5313 0001857 308
2449 51
8537 15
55276876 33859
Satellite: ISS
Catalog Number: 25544
Epoch time: 15205
53366774 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 257
5313 deg
Eccentricity:
0001857
Arg of perigee: 308
2449 deg
Mean anomaly: 51
8537 deg
Mean motion: 15
55276876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 329
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