[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 7th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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
191/02:58:39
135 3
2 3
9 3
9
N/A -2
1 -0
4 219
4
000/00:11:54
271 0
6 0
0 214
0
Coasting Arc #1 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2015/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3191407
64 A = 6777611
18 meter
Y = 4198003
15 meter E =
0011991
Z = 4247951
96 I = 51
55753
XDOT = -6636
084060 Wp = 85
34006
YDOT = -1396
552447 meter/sec RA = 346
99317 deg
ZDOT = -3595
734396 TA = 41
43947
MA = 41
34859
Ha = 219
764 n
mi
Hp = 211
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10470497
50 X = -3258748
21
Y = 13772976
23 feet Y = 4161937
92 meter
Z = 13936850
26 Z = 4232285
66
XDOT = -21771
929330 XDOT = -6602
507768
YDOT = -4581
864985 feet/sec YDOT = -1470
573494 meter/sec
ZDOT = -11797
028858 ZDOT = -3627
889331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15835613
66 X = 4826695
04
Y = 7103326
52 feet Y = 2165093
92 meter
Z = 13868600
50 Z = 4227149
43
XDOT = 1054
396959 XDOT = 321
380193
YDOT = 21013
877749 feet/sec YDOT = 6405
029938 meter/sec
ZDOT = -11935
008776 ZDOT = -3637
790675
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 15187
54157560
00016717 00000-0 10270-3 0 9002
2 25544 51
6407 347
3666 0002960 129
9602 230
1812 15
55544982 31050
Satellite: ISS
Catalog Number: 25544
Epoch time: 15187
54157560 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 347
3666 deg
Eccentricity:
0002960
Arg of perigee: 129
9602 deg
Mean anomaly: 230
1812 deg
Mean motion: 15
55544982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 306
Coasting Arc #2 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2015/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4967142
51 A = 6782247
13 meter
Y = -3804075
83 meter E =
0006337
Z = -2621922
27 I = 51
54396
XDOT = 4875
906651 Wp = 79
57822
YDOT = 2775
772843 meter/sec RA = 341
99348 deg
ZDOT = 5221
819830 TA = 250
84643
MA = 250
91504
Ha = 219
644 n
mi
Hp = 211
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16296399
31 X = 5022047
62
Y = -12480563
76 feet Y = -3748222
84 meter
Z = -8602107
17 Z = -2597659
96
XDOT = 15997
069065 XDOT = 4819
139511
YDOT = 9106
866282 feet/sec YDOT = 2829
980700 meter/sec
ZDOT = 17131
954822 ZDOT = 5245
368099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16133084
09 X = -4917364
03
Y = -12761590
85 feet Y = -3889732
89 meter
Z = -8496984
56 Z = -2589880
89
XDOT = 3971
701757 XDOT = 1210
574696
YDOT = -16468
643255 feet/sec YDOT = -5019
642464 meter/sec
ZDOT = 17232
631062 ZDOT = 5252
505948
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 15188
50520785
00016717 00000-0 10270-3 0 9013
2 25544 51
6420 342
5523 0003010 132
7661 227
3746 15
55584669 31205
Satellite: ISS
Catalog Number: 25544
Epoch time: 15188
50520785 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 342
5523 deg
Eccentricity:
0003010
Arg of perigee: 132
7661 deg
Mean anomaly: 227
3746 deg
Mean motion: 15
55584669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 292
Coasting Arc #3 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2015/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6052357
16 A = 6784906
47 meter
Y = 3006955
47 meter E =
0015721
Z = 507972
22 I = 51
52247
XDOT = -2540
309588 Wp = 130
47083
YDOT = -4084
187618 meter/sec RA = 337
00562 deg
ZDOT = -5978
918697 TA = 44
03507
MA = 43
90995
Ha = 219
467 n
mi
Hp = 211
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19856814
82 X = -6087999
35
Y = 9865339
46 feet Y = 2939074
72 meter
Z = 1666575
52 Z = 478484
84
XDOT = -8334
349042 XDOT = -2465
407253
YDOT = -13399
565677 feet/sec YDOT = -4112
175848 meter/sec
ZDOT = -19615
874990 ZDOT = -5991
077279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14753789
61 X = 4496955
07
Y = 16563579
52 feet Y = 5048579
04 meter
Z = 1539161
11 Z = 469136
31
XDOT = -9555
435643 XDOT = -2912
496784
YDOT = 10375
840417 feet/sec YDOT = 3162
556159 meter/sec
ZDOT = -19667
301952 ZDOT = -5994
593635
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 15189
53306993
00016717 00000-0 10270-3 0 9021
2 25544 51
6412 337
4164 0002808 135
4775 224
6604 15
55620135 31369
Satellite: ISS
Catalog Number: 25544
Epoch time: 15189
53306993 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 337
4164 deg
Eccentricity:
0002808
Arg of perigee: 135
4775 deg
Mean anomaly: 224
6604 deg
Mean motion: 15
55620135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 304
Coasting Arc #4 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2015/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6304804
15 A = 6783708
07 meter
Y = -1857664
48 meter E =
0014941
Z = 1655877
30 I = 51
49114
XDOT = 5
083277 Wp = 75
04932
YDOT = 5133
786798 meter/sec RA = 332
01907 deg
ZDOT = 5700
787780 TA = 303
14223
MA = 303
28550
Ha = 219
426 n
mi
Hp = 211
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20685053
00 X = 6317064
81
Y = -6094699
75 feet Y = -1787091
60 meter
Z = 5432668
31 Z = 1686534
36
XDOT = 16
677418 XDOT = -80
016535
YDOT = 16843
132541 feet/sec YDOT = 5133
367405 meter/sec
ZDOT = 18703
371981 ZDOT = 5700
606151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11635633
30 X = -3546541
03
Y = -18115600
51 feet Y = -5521635
04 meter
Z = 5564865
08 Z = 1696170
88
XDOT = 14877
940287 XDOT = 4534
796200
YDOT = -3772
613421 feet/sec YDOT = -1149
892571 meter/sec
ZDOT = 18701
523230 ZDOT = 5700
224280
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 15190
56092059
00016717 00000-0 10270-3 0 9032
2 25544 51
6424 332
2810 0002978 140
8775 219
2594 15
55644453 31526
Satellite: ISS
Catalog Number: 25544
Epoch time: 15190
56092059 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 332
2810 deg
Eccentricity:
0002978
Arg of perigee: 140
8775 deg
Mean anomaly: 219
2594 deg
Mean motion: 15
55644453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 312
Coasting Arc #5 (Orbit 3160)
---------------------------------------
Vector Time (GMT): 2015/191/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 869706
24 A = 6777979
77 meter
Y = -4859778
99 meter E =
0009795
Z = -4653730
27 I = 51
44856
XDOT = 6936
677952 Wp = 119
35214
YDOT = -1514
526230 meter/sec RA = 328
83904 deg
ZDOT = 2877
812092 TA = 179
35511
MA = 179
35385
Ha = 219
400 n
mi
Hp = 213
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2853366
91 X = 946590
83
Y = -15944156
81 feet Y = -4849623
10 meter
Z = -15268143
93 Z = -4649319
07
XDOT = 22758
129763 XDOT = 6939
118900
YDOT = -4968
918078 feet/sec YDOT = -1436
942344 meter/sec
ZDOT = 9441
640721 ZDOT = 2911
514852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9858970
44 X = 3005014
19
Y = -12875096
18 feet Y = -3924329
31 meter
Z = -15248169
01 Z = -4647641
92
XDOT = 21544
384508 XDOT = 6566
728398
YDOT = 5143
049443 feet/sec YDOT = 1567
601470 meter/sec
ZDOT = 9586
857263 ZDOT = 2922
074094
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
13908314
00016717 00000-0 10270-3 0 9047
2 25544 51
6440 329
3958 0001887 225
1426 134
9574 15
54885070 31614
Satellite: ISS
Catalog Number: 25544
Epoch time: 15191
13908314 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 329
3958 deg
Eccentricity:
0001887
Arg of perigee: 225
1426 deg
Mean anomaly: 134
9574 deg
Mean motion: 15
54885070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3161
Checksum: 315
Coasting Arc #6 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2015/192/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2601488
81 A = 6782275
93 meter
Y = 5255799
38 meter E =
0011181
Z = 3396107
26 I = 51
43590
XDOT = -6138
730448 Wp = 96
57147
YDOT = -57
212344 meter/sec RA = 323
83114 deg
ZDOT = -4602
065600 TA = 43
56842
MA = 43
48017
Ha = 219
396 n
mi
Hp = 213
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8535068
28 X = -2676564
05
Y = 17243436
29 feet Y = 5226287
72 meter
Z = 11142084
18 Z = 3383287
94
XDOT = -20140
191759 XDOT = -6115
279392
YDOT = -187
704540 feet/sec YDOT = -125
728067 meter/sec
ZDOT = -15098
640421 ZDOT = -4631
829333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15288999
98 X = -4660087
19
Y = 11733680
15 feet Y = 3576425
71 meter
Z = 11085880
90 Z = 3378976
50
XDOT = -17080
644697 XDOT = -5206
180504
YDOT = -7833
422452 feet/sec YDOT = -2387
627163 meter/sec
ZDOT = -15226
591969 ZDOT = -4641
065232
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
16741098
00016717 00000-0 10270-3 0 9056
2 25544 51
6437 324
2636 0001860 228
3288 131
7706 15
54887399 31774
Satellite: ISS
Catalog Number: 25544
Epoch time: 15192
16741098 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 324
2636 deg
Eccentricity:
0001860
Arg of perigee: 228
3288 deg
Mean anomaly: 131
7706 deg
Mean motion: 15
54887399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3177
Checksum: 334
Coasting Arc #7 (Orbit 3191)
---------------------------------------
Vector Time (GMT): 2015/193/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3953187
90 A = 6785831
28 meter
Y = -5246868
51 meter E =
0006018
Z = -1689668
22 I = 51
42384
XDOT = 4819
952381 Wp = 32
00323
YDOT = 1806
182877 meter/sec RA = 318
83381 deg
ZDOT = 5682
502067 TA = 309
41698
MA = 309
47023
Ha = 219
238 n
mi
Hp = 213
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12969776
59 X = 4019773
57
Y = -17214135
53 feet Y = -5202288
88 meter
Z = -5543530
89 Z = -1670303
35
XDOT = 15813
492064 XDOT = 4771
793648
YDOT = 5925
796839 feet/sec YDOT = 1859
812826 meter/sec
ZDOT = 18643
379484 ZDOT = 5705
799586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19059502
01 X = 5809336
21
Y = -10109644
16 feet Y = -3081419
54 meter
Z = -5459192
21 Z = -1663961
79
XDOT = 10984
165001 XDOT = 3347
973492
YDOT = 10612
669704 feet/sec YDOT = 3234
741726 meter/sec
ZDOT = 18743
168882 ZDOT = 5712
917875
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
13145673
00016717 00000-0 10270-3 0 9062
2 25544 51
6445 319
4514 0001888 235
9786 124
1188 15
54926475 31927
Satellite: ISS
Catalog Number: 25544
Epoch time: 15193
13145673 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 319
4514 deg
Eccentricity:
0001888
Arg of perigee: 235
9786 deg
Mean anomaly: 124
1188 deg
Mean motion: 15
54926475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3192
Checksum: 333
Coasting Arc #8 (Orbit 3207)
---------------------------------------
Vector Time (GMT): 2015/194/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4852310
61 A = 6787037
51 meter
Y = 4728284
44 meter E =
0011243
Z = -281143
29 I = 51
40472
XDOT = -3168
011068 Wp = 146
52367
YDOT = -3599
731279 meter/sec RA = 313
84366 deg
ZDOT = -5986
786525 TA = 36
51720
MA = 36
44059
Ha = 219
190 n
mi
Hp = 214
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15919654
24 X = -4903457
11
Y = 15512744
23 feet Y = 4673736
78 meter
Z = -922386
14 Z = -304838
35
XDOT = -10393
737099 XDOT = -3098
441225
YDOT = -11810
141991 feet/sec YDOT = -3634
768344 meter/sec
ZDOT = -19641
688073 ZDOT = -6002
007444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20847565
27 X = -6354337
89
Y = 7698009
19 feet Y = 2346353
20 meter
Z = -1025230
62 Z = -312490
29
XDOT = -4014
285681 XDOT = -1223
554275
YDOT = -13447
303357 feet/sec YDOT = -4098
738063 meter/sec
ZDOT = -19706
387429 ZDOT = -6006
506888
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
15976263
00016717 00000-0 10270-3 0 9073
2 25544 51
6448 314
3188 0001948 238
6954 121
4008 15
54903043 32080
Satellite: ISS
Catalog Number: 25544
Epoch time: 15194
15976263 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 314
3188 deg
Eccentricity:
0001948
Arg of perigee: 238
6954 deg
Mean anomaly: 121
4008 deg
Mean motion: 15
54903043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3208
Checksum: 317
Coasting Arc #9 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2015/195/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5234428
60 A = 6784884
77 meter
Y = -3710336
05 meter E =
0012071
Z = 2189234
65 I = 51
37670
XDOT = 1401
410205 Wp = 71
24353
YDOT = 5208
074161 meter/sec RA = 308
84991 deg
ZDOT = 5455
048042 TA = 313
17143
MA = 313
27224
Ha = 219
081 n
mi
Hp = 213
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17173322
19 X = 5264895
08
Y = -12173018
54 feet Y = -3651631
16 meter
Z = 7182528
36 Z = 2214735
74
XDOT = 4597
802511 XDOT = 1316
569847
YDOT = 17086
857484 feet/sec YDOT = 5223
270617 meter/sec
ZDOT = 17897
139247 ZDOT = 5461
650307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20523127
84 X = 6255449
37
Y = -4506501
28 feet Y = -1373581
59 meter
Z = 7292925
29 Z = 2222883
63
XDOT = -2883
534309 XDOT = -878
901257
YDOT = 15984
682249 feet/sec YDOT = 4872
131149 meter/sec
ZDOT = 17924
461074 ZDOT = 5463
375735
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
18805660
00016717 00000-0 10270-3 0 9080
2 25544 51
6449 309
1860 0001808 250
5635 109
5323 15
54937373 32242
Satellite: ISS
Catalog Number: 25544
Epoch time: 15195
18805660 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 309
1860 deg
Eccentricity:
0001808
Arg of perigee: 250
5635 deg
Mean anomaly: 109
5323 deg
Mean motion: 15
54937373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3224
Checksum: 316
Coasting Arc #10 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2015/196/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5155054
47 A = 6780621
27 meter
Y = 2201805
07 meter E =
0004268
Z = -3819526
43 I = 51
34371
XDOT = 321
794244 Wp = 74
64534
YDOT = -6436
930033 meter/sec RA = 303
84487 deg
ZDOT = -4147
719318 TA = 151
49760
MA = 151
47426
Ha = 218
959 n
mi
Hp = 213
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16912908
36 X = -5160738
90
Y = 7223769
91 feet Y = 2144126
53 meter
Z = -12531254
69 Z = -3844581
86
XDOT = 1055
755395 XDOT = 413
897385
YDOT = -21118
536854 feet/sec YDOT = -6432
816061 meter/sec
ZDOT = -13608
003013 ZDOT = -4145
933165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18312875
38 X = -5581764
42
Y = 381010
80 feet Y = 116132
09 meter
Z = -12639426
05 Z = -3852497
06
XDOT = 9009
103332 XDOT = 2745
974696
YDOT = -17813
690993 feet/sec YDOT = -5429
613015 meter/sec
ZDOT = -13599
019512 ZDOT = -4144
981147
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
15207136
00016717 00000-0 10270-3 0 9093
2 25544 51
6451 304
3745 0002016 255
7013 104
3917 15
54958743 32395
Satellite: ISS
Catalog Number: 25544
Epoch time: 15196
15207136 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 304
3745 deg
Eccentricity:
0002016
Arg of perigee: 255
7013 deg
Mean anomaly: 104
3917 deg
Mean motion: 15
54958743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 302
Coasting Arc #11 (Orbit 3254)
---------------------------------------
Vector Time (GMT): 2015/197/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4671801
02 A = 6776573
66 meter
Y = -361752
37 meter E =
0005308
Z = 4893511
98 I = 51
31339
XDOT = -1831
680634 Wp = 134
92820
YDOT = 7095
463151 meter/sec RA = 298
82430 deg
ZDOT = 2268
027153 TA = 292
78603
MA = 292
84211
Ha = 218
869 n
mi
Hp = 213
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15327431
15 X = 4651728
58
Y = -1186851
60 feet Y = -309621
97 meter
Z = 16054829
33 Z = 4916157
49
XDOT = -6009
450899 XDOT = -1921
904703
YDOT = 23279
078580 feet/sec YDOT = 7074
475390 meter/sec
ZDOT = 7441
033965 ZDOT = 2258
910958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14634920
75 X = 4460723
85
Y = 4361151
43 feet Y = 1329278
96 meter
Z = 16152267
95 Z = 4923211
27
XDOT = -13694
746094 XDOT = -4174
158609
YDOT = 18484
639006 feet/sec YDOT = 5634
117969 meter/sec
ZDOT = 7400
415101 ZDOT = 2255
646523
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
18034486
00016717 00000-0 10270-3 0 9105
2 25544 51
6452 299
2419 0001834 260
7672 99
3274 15
54973796 32552
Satellite: ISS
Catalog Number: 25544
Epoch time: 15197
18034486 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 299
2419 deg
Eccentricity:
0001834
Arg of perigee: 260
7672 deg
Mean anomaly: 99
3274 deg
Mean motion: 15
54973796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3255
Checksum: 341
Coasting Arc #12 (Orbit 3269)
---------------------------------------
Vector Time (GMT): 2015/198/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3906487
99 A = 6774763
88 meter
Y = -1654279
67 meter E =
0012918
Z = -5293277
79 I = 51
29242
XDOT = 3050
022026 Wp = 89
87087
YDOT = -7026
993233 meter/sec RA = 293
79216 deg
ZDOT = -54
923975 TA = 179
60321
MA = 179
60218
Ha = 218
878 n
mi
Hp = 213
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12816561
64 X = -3861986
84
Y = -5427426
73 feet Y = -1697715
29 meter
Z = -17366396
94 Z = -5312146
44
XDOT = 10006
633942 XDOT = 3128
639664
YDOT = -23054
439741 feet/sec YDOT = -6992
446306 meter/sec
ZDOT = -180
196768 ZDOT = -39
917515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10072650
73 X = -3070143
94
Y = -9457798
93 feet Y = -2882737
11 meter
Z = -17447197
56 Z = -5317905
82
XDOT = 16618
574046 XDOT = 5065
341369
YDOT = -17488
659735 feet/sec YDOT = -5330
543487 meter/sec
ZDOT = -114
280543 ZDOT = -34
832709
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
14433992
00016717 00000-0 10270-3 0 9118
2 25544 51
6444 294
4296 0001971 267
5719 92
5209 15
55018798 32705
Satellite: ISS
Catalog Number: 25544
Epoch time: 15198
14433992 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 294
4296 deg
Eccentricity:
0001971
Arg of perigee: 267
5719 deg
Mean anomaly: 92
5209 deg
Mean motion: 15
55018798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3270
Checksum: 337
Coasting Arc #13 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2015/199/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2947705
61 A = 6776272
42 meter
Y = 3598394
04 meter E =
0004839
Z = 4925836
39 I = 51
28578
XDOT = -3946
212686 Wp = 43
18783
YDOT = 6209
837661 meter/sec RA = 288
75956 deg
ZDOT = -2170
157258 TA = 68
09598
MA = 68
04454
Ha = 218
698 n
mi
Hp = 213
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9670950
17 X = 2883321
03
Y = 11805754
72 feet Y = 3630996
87 meter
Z = 16160880
56 Z = 4939999
37
XDOT = -12946
892016 XDOT = -4004
817692
YDOT = 20373
483139 feet/sec YDOT = 6165
380996 meter/sec
ZDOT = -7119
938510 ZDOT = -2189
468722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5183884
84 X = 1580048
10
Y = 14285703
99 feet Y = 4354282
58 meter
Z = 16221072
14 Z = 4944182
79
XDOT = -17808
948814 XDOT = -5428
167599
YDOT = 14660
133942 feet/sec YDOT = 4468
408826 meter/sec
ZDOT = -7204
189210 ZDOT = -2195
836871
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
17259121
00016717 00000-0 10270-3 0 9123
2 25544 51
6444 289
2972 0002077 272
7332 87
3583 15
55046902 32867
Satellite: ISS
Catalog Number: 25544
Epoch time: 15199
17259121 = yrday
fracday
Element set: 912
Inclination: 51
6444 deg
RA of node: 289
2972 deg
Eccentricity:
0002077
Arg of perigee: 272
7332 deg
Mean anomaly: 87
3583 deg
Mean motion: 15
55046902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3286
Checksum: 324
Coasting Arc #14 (Orbit 3300)
---------------------------------------
Vector Time (GMT): 2015/200/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1912795
14 A = 6780305
03 meter
Y = -5233073
28 meter E =
0004350
Z = -3868512
45 I = 51
28845
XDOT = 4508
140157 Wp = 109
58268
YDOT = -4663
936354 meter/sec RA = 283
73438 deg
ZDOT = 4082
338280 TA = 203
45548
MA = 203
47533
Ha = 218
802 n
mi
Hp = 213
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6275574
61 X = -1835344
06
Y = -17168875
59 feet Y = -5254030
15 meter
Z = -12691969
98 Z = -3877616
43
XDOT = 14790
486081 XDOT = 4540
128266
YDOT = -15301
628459 feet/sec YDOT = -4613
344738 meter/sec
ZDOT = 13393
498294 ZDOT = 4104
314983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -557260
89 X = -169853
12
Y = -18244812
87 feet Y = -5561018
96 meter
Z = -12730101
78 Z = -3880135
02
XDOT = 17398
273257 XDOT = 5302
993689
YDOT = -9937
809276 feet/sec YDOT = -3029
044267 meter/sec
ZDOT = 13488
895699 ZDOT = 4111
415409
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
13656880
00016717 00000-0 10270-3 0 9136
2 25544 51
6431 284
4844 0002088 276
5915 83
5000 15
55036137 33018
Satellite: ISS
Catalog Number: 25544
Epoch time: 15200
13656880 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 284
4844 deg
Eccentricity:
0002088
Arg of perigee: 276
5915 deg
Mean anomaly: 83
5000 deg
Mean motion: 15
55036137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3301
Checksum: 288
Coasting Arc #15 (Orbit 3316)
---------------------------------------
Vector Time (GMT): 2015/201/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 835348
61 A = 6784468
41 meter
Y = 6346260
12 meter E =
0011797
Z = 2231759
60 I = 51
29599
XDOT = -4788
803957 Wp = 109
01925
YDOT = 2545
291231 meter/sec RA = 278
72382 deg
ZDOT = -5425
604934 TA = 46
02809
MA = 45
93086
Ha = 218
778 n
mi
Hp = 213
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2740645
05 X = 753480
25
Y = 20821063
37 feet Y = 6355143
69 meter
Z = 7322045
92 Z = 2235618
90
XDOT = -15711
299072 XDOT = -4790
554992
YDOT = 8350
693016 feet/sec YDOT = 2491
730115 meter/sec
ZDOT = -17800
541122 ZDOT = -5448
871773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3548756
72 X = -1081661
05
Y = 20693203
63 feet Y = 6307288
47 meter
Z = 7337426
06 Z = 2236447
46
XDOT = -15854
201638 XDOT = -4832
360659
YDOT = 3651
436187 feet/sec YDOT = 1112
957750 meter/sec
ZDOT = -17901
070631 ZDOT = -5456
246328
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
16480039
00016717 00000-0 10270-3 0 9142
2 25544 51
6430 279
3517 0002082 284
7738 75
3184 15
55071424 33172
Satellite: ISS
Catalog Number: 25544
Epoch time: 15201
16480039 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 279
3517 deg
Eccentricity:
0002082
Arg of perigee: 284
7738 deg
Mean anomaly: 75
3184 deg
Mean motion: 15
55071424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3317
Checksum: 298
Coasting Arc #16 (Orbit 3331)
---------------------------------------
Vector Time (GMT): 2015/202/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 205981
01 A = 6786608
23 meter
Y = -6771294
22 meter E =
0010730
Z = -292074
34 I = 51
29752
XDOT = 4806
059451 Wp = 32
90745
YDOT = -106
770294 meter/sec RA = 273
72201 deg
ZDOT = 5977
107256 TA = 323
92851
MA = 324
00086
Ha = 218
806 n
mi
Hp = 213
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 675790
71 X = 283102
71
Y = -22215532
23 feet Y = -6768559
59 meter
Z = -958249
13 Z = -290886
63
XDOT = 15767
911584 XDOT = 4777
862054
YDOT = -350
296241 feet/sec YDOT = -53
183640 meter/sec
ZDOT = 19609
931941 ZDOT = 6000
385336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6822359
86 X = 2079455
29
Y = -21153112
59 feet Y = -6447468
72 meter
Z = -951861
34 Z = -290127
34
XDOT = 13582
008104 XDOT = 4139
796070
YDOT = 3510
286834 feet/sec YDOT = 1069
935427 meter/sec
ZDOT = 19710
044050 ZDOT = 6007
621427
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
12875885
00016717 00000-0 10270-3 0 9157
2 25544 51
6415 274
5382 0002120 286
2583 73
8336 15
55052314 33326
Satellite: ISS
Catalog Number: 25544
Epoch time: 15202
12875885 = yrday
fracday
Element set: 915
Inclination: 51
6415 deg
RA of node: 274
5382 deg
Eccentricity:
0002120
Arg of perigee: 286
2583 deg
Mean anomaly: 73
8336 deg
Mean motion: 15
55052314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3332
Checksum: 297
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