[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 4th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19913 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
281/17:02:13
834 -0
9 3
7 3
8
N/A -3
6 -0
6 226
2
000/00:08:27
669 0
9 0
2 221
4
Coasting Arc #1 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2014/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -838801
10 A = 6795918
15 meter
Y = -6211909
24 meter E =
0005711
Z = -2627646
27 I = 51
30224
XDOT = 4853
856634 Wp = 72
84518
YDOT = -2847
515281 meter/sec RA = 281
93180 deg
ZDOT = 5193
281676 TA = 257
46160
MA = 257
52550
Ha = 226
708 n
mi
Hp = 219
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2751972
11 X = -756511
45
Y = -20380279
65 feet Y = -6220829
40 meter
Z = -8620886
72 Z = -2631520
58
XDOT = 15924
726490 XDOT = 4860
110083
YDOT = -9342
241737 feet/sec YDOT = -2793
200845 meter/sec
ZDOT = 17038
325709 ZDOT = 5216
876564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6633631
57 X = 2021930
90
Y = 19459134
30 feet Y = 5931144
13 meter
Z = -8636310
64 Z = -2632347
48
XDOT = -12264
467490 XDOT = -3738
209691
YDOT = 11771
564154 feet/sec YDOT = 3587
972754 meter/sec
ZDOT = 17139
132103 ZDOT = 5224
007465
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 14276
50530546
00016717 00000-0 10270-3 0 9005
2 25544 51
6443 282
6939 0001939 132
7540 227
3775 15
50859940 28131
Satellite: ISS
Catalog Number: 25544
Epoch time: 14276
50530546 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 282
6939 deg
Eccentricity:
0001939
Arg of perigee: 132
7540 deg
Mean anomaly: 227
3775 deg
Mean motion: 15
50859940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 320
Coasting Arc #2 (Orbit 2828)
---------------------------------------
Vector Time (GMT): 2014/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 867255
69 A = 6796993
61 meter
Y = 6416165
16 meter E =
0015563
Z = 2043499
44 I = 51
29909
XDOT = -4746
898419 Wp = 113
56628
YDOT = 2407
710594 meter/sec RA = 276
94950 deg
ZDOT = -5517
761762 TA = 43
74826
MA = 43
62505
Ha = 226
586 n
mi
Hp = 219
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2845327
06 X = 785517
49
Y = 21050410
62 feet Y = 6425406
59 meter
Z = 6704394
49 Z = 2047513
17
XDOT = -15573
813710 XDOT = -4746
665602
YDOT = 7899
312971 feet/sec YDOT = 2354
628361 meter/sec
ZDOT = -18102
892921 ZDOT = -5540
821303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7212774
69 X = -2198453
73
Y = -19974403
89 feet Y = -6088198
31 meter
Z = 6720390
56 Z = 2048375
04
XDOT = 11971
285160 XDOT = 3648
847717
YDOT = -10476
837608 feet/sec YDOT = -3193
340103 meter/sec
ZDOT = -18201
345524 ZDOT = -5547
770116
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 14277
53631015
00016717 00000-0 10270-3 0 9013
2 25544 51
6429 277
5785 0001785 134
2050 225
9248 15
50889055 28295
Satellite: ISS
Catalog Number: 25544
Epoch time: 14277
53631015 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 277
5785 deg
Eccentricity:
0001785
Arg of perigee: 134
2050 deg
Mean anomaly: 225
9248 deg
Mean motion: 15
50889055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2829
Checksum: 322
Coasting Arc #3 (Orbit 2843)
---------------------------------------
Vector Time (GMT): 2014/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -943063
56 A = 6797720
43 meter
Y = -6569928
83 meter E =
0008214
Z = -1458112
66 I = 51
29880
XDOT = 4675
314797 Wp = 51
14918
YDOT = -1940
990846 meter/sec RA = 271
96880 deg
ZDOT = 5748
820232 TA = 292
89230
MA = 292
97899
Ha = 226
548 n
mi
Hp = 219
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3094040
56 X = -862443
93
Y = -21554884
62 feet Y = -6580024
21 meter
Z = -4783834
19 Z = -1462497
25
XDOT = 15338
959307 XDOT = 4668
745869
YDOT = -6368
080203 feet/sec YDOT = -1888
744404 meter/sec
ZDOT = 18860
958768 ZDOT = 5771
516661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7924792
31 X = 2415476
70
Y = 20278448
59 feet Y = 6180871
13 meter
Z = -4801395
35 Z = -1463465
30
XDOT = -11875
743396 XDOT = -3619
726587
YDOT = 9108
823059 feet/sec YDOT = 2776
369268 meter/sec
ZDOT = 18957
786517 ZDOT = 5778
333330
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 14278
50285799
00016717 00000-0 10270-3 0 9026
2 25544 51
6425 272
7839 0001957 139
5292 220
6005 15
50934293 28440
Satellite: ISS
Catalog Number: 25544
Epoch time: 14278
50285799 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 272
7839 deg
Eccentricity:
0001957
Arg of perigee: 139
5292 deg
Mean anomaly: 220
6005 deg
Mean motion: 15
50934293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2844
Checksum: 330
Coasting Arc #4 (Orbit 2859)
---------------------------------------
Vector Time (GMT): 2014/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 994616
11 A = 6798325
08 meter
Y = 6669614
84 meter E =
0014986
Z = 802206
89 I = 51
30012
XDOT = -4668
880642 Wp = 127
87693
YDOT = 1415
432513 meter/sec RA = 266
98714 deg
ZDOT = -5912
546125 TA = 43
41708
MA = 43
29914
Ha = 226
441 n
mi
Hp = 219
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3263176
20 X = 916064
11
Y = 21881938
47 feet Y = 6680298
19 meter
Z = 2631912
37 Z = 806846
87
XDOT = -15317
849875 XDOT = -4655
639838
YDOT = 4643
807458 feet/sec YDOT = 1363
295240 meter/sec
ZDOT = -19398
117208 ZDOT = -5935
195120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8529926
50 X = -2599921
60
Y = -20411012
27 feet Y = -6221276
54 meter
Z = 2650555
53 Z = 807889
33
XDOT = 12097
929230 XDOT = 3687
448829
YDOT = -7615
625842 feet/sec YDOT = -2321
242757 meter/sec
ZDOT = -19494
654460 ZDOT = -5941
970679
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 14279
53382131
00016717 00000-0 10270-3 0 9039
2 25544 51
6419 267
6677 0001705 140
2034 219
9242 15
50945422 28608
Satellite: ISS
Catalog Number: 25544
Epoch time: 14279
53382131 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 267
6677 deg
Eccentricity:
0001705
Arg of perigee: 140
2034 deg
Mean anomaly: 219
9242 deg
Mean motion: 15
50945422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2860
Checksum: 301
Coasting Arc #5 (Orbit 2874)
---------------------------------------
Vector Time (GMT): 2014/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1073853
48 A = 6798402
58 meter
Y = -6706582
48 meter E =
0011453
Z = -163360
05 I = 51
30321
XDOT = 4709
868352 Wp = 53
63366
YDOT = -892
425307 meter/sec RA = 262
00704 deg
ZDOT = 5977
344817 TA = 304
60087
MA = 304
70885
Ha = 226
361 n
mi
Hp = 219
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3523141
33 X = -997985
55
Y = -22003223
37 feet Y = -6718166
83 meter
Z = -535958
16 Z = -168391
48
XDOT = 15452
323988 XDOT = 4690
461201
YDOT = -2927
904549 feet/sec YDOT = -839
864144 meter/sec
ZDOT = 19610
711341 ZDOT = 6000
177982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9175146
39 X = 2796584
62
Y = 20306375
03 feet Y = 6189383
11 meter
Z = -556270
07 Z = -169551
12
XDOT = -12540
984588 XDOT = -3822
492102
YDOT = 6180
345108 feet/sec YDOT = 1883
769189 meter/sec
ZDOT = 19707
945593 ZDOT = 6006
981817
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 14280
50032946
00016717 00000-0 10270-3 0 9045
2 25544 51
6416 262
8727 0001929 147
6196 212
5074 15
51007136 28756
Satellite: ISS
Catalog Number: 25544
Epoch time: 14280
50032946 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 262
8727 deg
Eccentricity:
0001929
Arg of perigee: 147
6196 deg
Mean anomaly: 212
5074 deg
Mean motion: 15
51007136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2875
Checksum: 305
Coasting Arc #6 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2014/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1104447
89 A = 6798310
01 meter
Y = 6681048
83 meter E =
0012576
Z = -529017
10 I = 51
30862
XDOT = -4815
850347 Wp = 139
82825
YDOT = 331
809738 meter/sec RA = 257
02608 deg
ZDOT = -5952
530585 TA = 45
89850
MA = 45
79508
Ha = 226
284 n
mi
Hp = 219
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3623516
70 X = 1032226
61
Y = 21919451
53 feet Y = 6692995
59 meter
Z = -1735620
41 Z = -523828
10
XDOT = -15800
033946 XDOT = -4790
286798
YDOT = 1088
614626 feet/sec YDOT = 278
097894 meter/sec
ZDOT = -19529
299820 ZDOT = -5975
863669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9609769
13 X = -2929057
63
Y = -20032897
95 feet Y = -6106027
29 meter
Z = -1714626
50 Z = -522618
16
XDOT = 13288
933888 XDOT = 4050
467049
YDOT = -4719
912222 feet/sec YDOT = -1438
629245 meter/sec
ZDOT = -19628
570244 ZDOT = -5982
788210
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 14281
53125000
00016717 00000-0 10270-3 0 9054
2 25544 51
6420 257
7562 0001635 147
6091 212
5161 15
51004326 28912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
53125000 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 257
7562 deg
Eccentricity:
0001635
Arg of perigee: 147
6091 deg
Mean anomaly: 212
5161 deg
Mean motion: 15
51004326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 270
Coasting Arc #7 (Orbit 2893)
---------------------------------------
Vector Time (GMT): 2014/281/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4437016
50 A = 6790579
36 meter
Y = -1816717
92 meter E =
0009863
Z = -4818230
41 I = 51
28106
XDOT = 251
044123 Wp = 116
56473
YDOT = -7231
514571 meter/sec RA = 255
94008 deg
ZDOT = 2495
119903 TA = 178
13387
MA = 178
13019
Ha = 226
242 n
mi
Hp = 221
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14557140
76 X = -4392965
92
Y = -5960360
64 feet Y = -1866089
86 meter
Z = -15807842
56 Z = -4839677
97
XDOT = 823
635574 XDOT = 319
769220
YDOT = -23725
441506 feet/sec YDOT = -7228
322632 meter/sec
ZDOT = 8186
088922 ZDOT = 2496
507369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5187226
32 X = 1581066
58
Y = -14752847
39 feet Y = -4496667
88 meter
Z = -15898751
82 Z = -4845939
56
XDOT = 22656
522881 XDOT = 6905
708174
YDOT = -864
530919 feet/sec YDOT = -263
509024 meter/sec
ZDOT = 8193
146362 ZDOT = 2497
271011
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 14281
72454564
00016717 00000-0 10270-3 0 9066
2 25544 51
6456 256
7967 0002378 249
2215 110
8681 15
50303610 28948
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
72454564 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 256
7967 deg
Eccentricity:
0002378
Arg of perigee: 249
2215 deg
Mean anomaly: 110
8681 deg
Mean motion: 15
50303610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2894
Checksum: 318
Coasting Arc #8 (Orbit 2909)
---------------------------------------
Vector Time (GMT): 2014/282/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4583573
16 A = 6791231
95 meter
Y = 1967741
35 meter E =
0005962
Z = 4605495
11 I = 51
29240
XDOT = -62
754699 Wp = 61
54083
YDOT = 7071
443780 meter/sec RA = 250
95697 deg
ZDOT = -2953
170006 TA = 58
08013
MA = 58
02215
Ha = 225
972 n
mi
Hp = 221
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15037969
69 X = 4538856
27
Y = 6455844
31 feet Y = 2018748
34 meter
Z = 15109892
09 Z = 4627653
08
XDOT = -205
888120 XDOT = -127
478703
YDOT = 23200
274868 feet/sec YDOT = 7070
379776 meter/sec
ZDOT = -9688
877971 ZDOT = -2953
632910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5392853
44 X = -1643741
73
Y = 15358672
21 feet Y = 4681323
29 meter
Z = 15203802
71 Z = 4634119
06
XDOT = -22032
461550 XDOT = -6715
494280
YDOT = 1876
485800 feet/sec YDOT = 571
952872 meter/sec
ZDOT = -9691
972902 ZDOT = -2954
113341
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 14282
75590917
00016717 00000-0 10270-3 0 9074
2 25544 51
6457 251
6847 0002395 254
5329 105
5557 15
50360961 29108
Satellite: ISS
Catalog Number: 25544
Epoch time: 14282
75590917 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 251
6847 deg
Eccentricity:
0002395
Arg of perigee: 254
5329 deg
Mean anomaly: 105
5557 deg
Mean motion: 15
50360961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2910
Checksum: 326
Coasting Arc #9 (Orbit 2924)
---------------------------------------
Vector Time (GMT): 2014/283/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4765845
17 A = 6792121
38 meter
Y = -2095544
26 meter E =
0007004
Z = -4369541
76 I = 51
30713
XDOT = -88
253007 Wp = 121
69041
YDOT = -6863
964877 meter/sec RA = 245
97456 deg
ZDOT = 3388
492584 TA = 182
85647
MA = 182
86047
Ha = 226
044 n
mi
Hp = 221
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15635974
96 X = -4720831
80
Y = -6875145
21 feet Y = -2148587
77 meter
Z = -14335766
93 Z = -4392584
52
XDOT = -289
543987 XDOT = -27
952568
YDOT = -22519
569807 feet/sec YDOT = -6864
614289 meter/sec
ZDOT = 11117
101654 ZDOT = 3388
210993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5492866
83 X = 1674225
81
Y = -16086334
87 feet Y = -4903114
87 meter
Z = -14433426
22 Z = -4399308
31
XDOT = 21228
189226 XDOT = 6470
352076
YDOT = -2724
866901 feet/sec YDOT = -830
539431 meter/sec
ZDOT = 11116
993191 ZDOT = 3388
459525
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 14283
72279298
00016717 00000-0 10270-3 0 9089
2 25544 51
6463 246
8917 0002453 257
5571 102
5305 15
50369545 29257
Satellite: ISS
Catalog Number: 25544
Epoch time: 14283
72279298 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 246
8917 deg
Eccentricity:
0002453
Arg of perigee: 257
5571 deg
Mean anomaly: 102
5305 deg
Mean motion: 15
50369545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2925
Checksum: 330
Coasting Arc #10 (Orbit 2940)
---------------------------------------
Vector Time (GMT): 2014/284/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4958237
26 A = 6792980
07 meter
Y = 2213106
88 meter E =
0008105
Z = 4076652
53 I = 51
32419
XDOT = 184
569427 Wp = 75
28062
YDOT = 6640
683118 meter/sec RA = 240
99409 deg
ZDOT = -3821
120751 TA = 54
44871
MA = 54
37317
Ha = 225
827 n
mi
Hp = 221
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16267182
60 X = 4913317
80
Y = 7260849
35 feet Y = 2268302
27 meter
Z = 13374844
26 Z = 4100630
15
XDOT = 605
542739 XDOT = 128
860208
YDOT = 21787
018105 feet/sec YDOT = 6642
435301 meter/sec
ZDOT = -12536
485405 ZDOT = -3820
359966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5532314
59 X = -1686249
49
Y = 16852474
34 feet Y = 5136634
18 meter
Z = 13476469
33 Z = 4107627
85
XDOT = -20366
421220 XDOT = -6207
685188
YDOT = 3359
378443 feet/sec YDOT = 1023
938549 meter/sec
ZDOT = -12534
299117 ZDOT = -3820
454371
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 14284
75411304
00016717 00000-0 10270-3 0 9090
2 25544 51
6464 241
7796 0002431 262
7647 97
3228 15
50428635 29414
Satellite: ISS
Catalog Number: 25544
Epoch time: 14284
75411304 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 241
7796 deg
Eccentricity:
0002431
Arg of perigee: 262
7647 deg
Mean anomaly: 97
3228 deg
Mean motion: 15
50428635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2941
Checksum: 318
Coasting Arc #11 (Orbit 2955)
---------------------------------------
Vector Time (GMT): 2014/285/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5174989
30 A = 6794016
99 meter
Y = -2293623
20 meter E =
0003661
Z = -3761568
85 I = 51
34346
XDOT = -235
054347 Wp = 115
81842
YDOT = -6385
629385 meter/sec RA = 236
01458 deg
ZDOT = 4218
679144 TA = 199
04813
MA = 199
06182
Ha = 225
860 n
mi
Hp = 221
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16978311
34 X = -5130684
03
Y = -7525010
48 feet Y = -2351245
80 meter
Z = -12341105
14 Z = -3786600
89
XDOT = -771
175678 XDOT = -184
124645
YDOT = -20950
227642 feet/sec YDOT = -6387
972867 meter/sec
ZDOT = 13840
810840 ZDOT = 4217
661399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5416519
37 X = 1650955
10
Y = -17689542
76 feet Y = -5391772
63 meter
Z = -12447212
93 Z = -3793910
50
XDOT = 19399
509776 XDOT = 5912
970580
YDOT = -3792
825973 feet/sec YDOT = -1156
053357 meter/sec
ZDOT = 13837
486116 ZDOT = 4217
665768
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 14285
72095519
00016717 00000-0 10270-3 0 9106
2 25544 51
6462 236
9863 0002556 265
4858 94
6001 15
50434680 29567
Satellite: ISS
Catalog Number: 25544
Epoch time: 14285
72095519 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 236
9863 deg
Eccentricity:
0002556
Arg of perigee: 265
4858 deg
Mean anomaly: 94
6001 deg
Mean motion: 15
50434680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2956
Checksum: 327
Coasting Arc #12 (Orbit 2971)
---------------------------------------
Vector Time (GMT): 2014/286/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5391213
87 A = 6794968
16 meter
Y = 2360651
59 meter E =
0009882
Z = 3387528
33 I = 51
36538
XDOT = 219
105747 Wp = 90
05827
YDOT = 6122
996478 meter/sec RA = 231
03758 deg
ZDOT = -4603
943932 TA = 50
25306
MA = 50
16604
Ha = 225
710 n
mi
Hp = 221
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17687709
56 X = 5347960
06
Y = 7744919
92 feet Y = 2420698
01 meter
Z = 11113938
08 Z = 3413613
26
XDOT = 718
850875 XDOT = 172
985515
YDOT = 20088
571123 feet/sec YDOT = 6125
188497 meter/sec
ZDOT = -15104
802925 ZDOT = -4602
991942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5229740
52 X = -1594024
91
Y = 18520753
02 feet Y = 5645125
52 meter
Z = 11224526
51 Z = 3421235
68
XDOT = -18430
082384 XDOT = -5617
489110
YDOT = 3971
240072 feet/sec YDOT = 1210
433974 meter/sec
ZDOT = -15101
710452 ZDOT = -4603
001346
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 14286
75223052
00016717 00000-0 10270-3 0 9116
2 25544 51
6461 231
8740 0002500 270
5340 89
5524 15
50495848 29720
Satellite: ISS
Catalog Number: 25544
Epoch time: 14286
75223052 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 231
8740 deg
Eccentricity:
0002500
Arg of perigee: 270
5340 deg
Mean anomaly: 89
5524 deg
Mean motion: 15
50495848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2972
Checksum: 300
Coasting Arc #13 (Orbit 2986)
---------------------------------------
Vector Time (GMT): 2014/287/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5616236
78 A = 6796025
56 meter
Y = -2381374
02 meter E =
0002276
Z = -2994858
46 I = 51
38836
XDOT = -153
813714 Wp = 45
46751
YDOT = -5848
341166 meter/sec RA = 226
06144 deg
ZDOT = 4942
671738 TA = 280
20053
MA = 280
22620
Ha = 225
705 n
mi
Hp = 221
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18425973
69 X = -5574642
05
Y = -7812906
89 feet Y = -2443946
05 meter
Z = -9825651
11 Z = -3022040
49
XDOT = -504
638170 XDOT = -112
414987
YDOT = -19187
471016 feet/sec YDOT = -5849
829406 meter/sec
ZDOT = 16216
114626 ZDOT = 4942
025471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4861303
93 X = 1481725
44
Y = -19355808
64 feet Y = -5899650
47 meter
Z = -9940917
27 Z = -3029991
58
XDOT = 17446
529584 XDOT = 5317
702217
YDOT = -3939
197516 feet/sec YDOT = -1200
667403 meter/sec
ZDOT = 16214
273025 ZDOT = 4942
110418
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 14287
71903013
00016717 00000-0 10270-3 0 9126
2 25544 51
6452 227
0801 0002656 272
5680 87
5166 15
50498465 29870
Satellite: ISS
Catalog Number: 25544
Epoch time: 14287
71903013 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 227
0801 deg
Eccentricity:
0002656
Arg of perigee: 272
5680 deg
Mean anomaly: 87
5166 deg
Mean motion: 15
50498465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2987
Checksum: 320
Coasting Arc #14 (Orbit 3002)
---------------------------------------
Vector Time (GMT): 2014/288/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5826922
93 A = 6796907
61 meter
Y = 2388483
54 meter E =
0011033
Z = 2543485
37 I = 51
41425
XDOT = 15
174430 Wp = 105
29874
YDOT = 5577
444148 meter/sec RA = 221
08848 deg
ZDOT = -5256
064351 TA = 46
07477
MA = 45
98376
Ha = 225
618 n
mi
Hp = 221
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19117201
21 X = 5787425
71
Y = 7836232
10 feet Y = 2453423
32 meter
Z = 8344768
26 Z = 2571695
92
XDOT = 49
784875 XDOT = -21
662427
YDOT = 18298
701273 feet/sec YDOT = 5577
407472 meter/sec
ZDOT = -17244
305615 ZDOT = -5256
080534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4429599
48 X = -1350141
92
Y = 20130604
88 feet Y = 6135808
37 meter
Z = 8464423
70 Z = 2579956
34
XDOT = -16527
424730 XDOT = -5037
559058
YDOT = 3636
551159 feet/sec YDOT = 1108
420793 meter/sec
ZDOT = -17245
233491 ZDOT = -5256
347168
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 14288
75025992
00016717 00000-0 10270-3 0 9133
2 25544 51
6452 221
9673 0002595 277
4143 82
6713 15
50562178 30037
Satellite: ISS
Catalog Number: 25544
Epoch time: 14288
75025992 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 221
9673 deg
Eccentricity:
0002595
Arg of perigee: 277
4143 deg
Mean anomaly: 82
6713 deg
Mean motion: 15
50562178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3003
Checksum: 314
Coasting Arc #15 (Orbit 3017)
---------------------------------------
Vector Time (GMT): 2014/289/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6028382
42 A = 6797820
08 meter
Y = -2346247
95 meter E =
0005412
Z = -2079840
99 I = 51
44017
XDOT = 169
992589 Wp = 16
91074
YDOT = -5316
190442 meter/sec RA = 216
11624 deg
ZDOT = 5513
115921 TA = 320
04556
MA = 320
08537
Ha = 225
590 n
mi
Hp = 221
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19778157
53 X = -5991594
78
Y = -7697663
89 feet Y = -2413455
72 meter
Z = -6823625
31 Z = -2109036
75
XDOT = 557
718468 XDOT = 202
645616
YDOT = -17441
569693 feet/sec YDOT = -5314
106422 meter/sec
ZDOT = 18087
650660 ZDOT = 5514
021505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3819430
63 X = 1164162
46
Y = -20835922
97 feet Y = -6350789
32 meter
Z = -6947493
83 Z = -2117596
12
XDOT = 15688
757464 XDOT = 4781
933275
YDOT = -3147
423869 feet/sec YDOT = -959
334795 meter/sec
ZDOT = 18092
316243 ZDOT = 5514
537991
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 14289
71701670
00016717 00000-0 10270-3 0 9145
2 25544 51
6439 217
1726 0002723 278
6898 81
3945 15
50562063 30183
Satellite: ISS
Catalog Number: 25544
Epoch time: 14289
71701670 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 217
1726 deg
Eccentricity:
0002723
Arg of perigee: 278
6898 deg
Mean anomaly: 81
3945 deg
Mean motion: 15
50562063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3018
Checksum: 322
Coasting Arc #16 (Orbit 3033)
---------------------------------------
Vector Time (GMT): 2014/290/17:06:27
669
Vector Time (MET): N/A
Weight (LBS) : 946187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6199954
15 A = 6798439
60 meter
Y = 2294705
05 meter E =
0011291
Z = 1560947
00 I = 51
46888
XDOT = -428
374757 Wp = 120
54113
YDOT = 5071
802346 meter/sec RA = 211
14778 deg
ZDOT = -5729
089675 TA = 42
37598
MA = 42
28883
Ha = 225
546 n
mi
Hp = 221
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20341056
94 X = 6166250
78
Y = 7528559
89 feet Y = 2363848
66 meter
Z = 5121217
19 Z = 1590983
72
XDOT = -1405
428994 XDOT = -457
226622
YDOT = 16639
771478 feet/sec YDOT = 5066
850100 meter/sec
ZDOT = -18796
225967 ZDOT = -5731
241257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3176488
62 X = -968193
73
Y = 21424889
47 feet Y = 6530306
31 meter
Z = 5248686
32 Z = 1599799
59
XDOT = -14983
305307 XDOT = -4566
911458
YDOT = 2405
582420 feet/sec YDOT = 733
221522 meter/sec
ZDOT = -18806
150916 ZDOT = -5732
114799
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 14290
74820062
00016717 00000-0 10270-3 0 9158
2 25544 51
6442 212
0594 0002688 283
5365 76
5486 15
50629875 30347
Satellite: ISS
Catalog Number: 25544
Epoch time: 14290
74820062 = yrday
fracday
Element set: 915
Inclination: 51
6442 deg
RA of node: 212
0594 deg
Eccentricity:
0002688
Arg of perigee: 283
5365 deg
Mean anomaly: 76
5486 deg
Mean motion: 15
50629875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3034
Checksum: 319
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