[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 4th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
314/23:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
9
000/00:00:00
000 0
0 0
0 221
0
Coasting Arc #1 (Orbit 1646)
---------------------------------------
Vector Time (GMT): 2013/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3625843
93 A = 6790114
48 meter
Y = 2206143
28 meter E =
0015456
Z = -5313588
04 I = 51
88560
XDOT = -4687
797379 Wp = 86
67102
YDOT = 6003
913669 meter/sec RA = 132
15782 deg
ZDOT = -706
964782 TA = 176
58881
MA = 176
57826
Ha = 228
136 n
mi
Hp = 221
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11895813
43 X = 3626717
62
Y = 7238002
90 feet Y = 2246694
63 meter
Z = -17433031
63 Z = -5295971
38
XDOT = -15379
912662 XDOT = -4751
151708
YDOT = 19697
879493 feet/sec YDOT = 5951
137497 meter/sec
ZDOT = -2319
438262 ZDOT = -729
892294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13710701
50 X = -4179021
82
Y = 2912294
21 feet Y = 887667
28 meter
Z = -17359287
48 Z = -5291110
82
XDOT = -2016
885013 XDOT = -614
746552
YDOT = -23882
288009 feet/sec YDOT = -7279
321385 meter/sec
ZDOT = -2416
626752 ZDOT = -736
587834
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 13308
51740836
00016717 00000-0 10270-3 0 9006
2 25544 51
6442 133
0750 0001047 116
3835 243
7423 15
49818948 16472
Satellite: ISS
Catalog Number: 25544
Epoch time: 13308
51740836 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 133
0750 deg
Eccentricity:
0001047
Arg of perigee: 116
3835 deg
Mean anomaly: 243
7423 deg
Mean motion: 15
49818948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1647
Checksum: 302
Coasting Arc #2 (Orbit 1662)
---------------------------------------
Vector Time (GMT): 2013/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3594354
18 A = 6790048
56 meter
Y = -2176803
76 meter E =
0003720
Z = 5330639
61 I = 51
90537
XDOT = 4382
415705 Wp = 110
86787
YDOT = -6275
758450 meter/sec RA = 127
22034 deg
ZDOT = 390
724182 TA = 335
40922
MA = 335
42695
Ha = 228
307 n
mi
Hp = 221
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11792500
59 X = -3595641
04
Y = -7141744
61 feet Y = -2217005
37 meter
Z = 17488975
08 Z = 5313174
94
XDOT = 14378
004283 XDOT = 4450
368823
YDOT = -20589
758695 feet/sec YDOT = -6226
371547 meter/sec
ZDOT = 1281
903485 ZDOT = 412
179123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13517646
52 X = 4120178
66
Y = -3145284
54 feet Y = -958682
73 meter
Z = 17415862
13 Z = 5308354
78
XDOT = 3763
182496 XDOT = 1147
018025
YDOT = 23803
046107 feet/sec YDOT = 7255
168454 meter/sec
ZDOT = 1372
963018 ZDOT = 418
479128
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 13309
54909843
00016717 00000-0 10270-3 0 9016
2 25544 51
6443 127
9647 0001067 116
4600 243
6660 15
49795298 16635
Satellite: ISS
Catalog Number: 25544
Epoch time: 13309
54909843 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 127
9647 deg
Eccentricity:
0001067
Arg of perigee: 116
4600 deg
Mean anomaly: 243
6660 deg
Mean motion: 15
49795298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1663
Checksum: 325
Coasting Arc #3 (Orbit 1677)
---------------------------------------
Vector Time (GMT): 2013/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3582399
73 A = 6789810
79 meter
Y = 2181476
35 meter E =
0015797
Z = -5353012
92 I = 51
92344
XDOT = -4044
873555 Wp = 91
79878
YDOT = 6492
755983 meter/sec RA = 122
28391 deg
ZDOT = -61
643919 TA = 177
61846
MA = 177
61093
Ha = 228
078 n
mi
Hp = 221
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11753279
95 X = 3583743
79
Y = 7157074
63 feet Y = 2221544
65 meter
Z = -17562378
33 Z = -5335606
24
XDOT = -13270
582530 XDOT = -4116
876902
YDOT = 21301
692856 feet/sec YDOT = 6447
121041 meter/sec
ZDOT = -202
243828 ZDOT = -81
468750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13445003
74 X = -4098037
14
Y = 3339089
30 feet Y = 1017754
42 meter
Z = -17489505
33 Z = -5330801
22
XDOT = -5456
410934 XDOT = -1663
114053
YDOT = -23460
123620 feet/sec YDOT = -7150
645679 meter/sec
ZDOT = -286
503173 ZDOT = -87
326167
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 13310
51629262
00016717 00000-0 10270-3 0 9020
2 25544 51
6447 123
1738 0001131 122
3134 237
8126 15
49862286 16788
Satellite: ISS
Catalog Number: 25544
Epoch time: 13310
51629262 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 123
1738 deg
Eccentricity:
0001131
Arg of perigee: 122
3134 deg
Mean anomaly: 237
8126 deg
Mean motion: 15
49862286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1678
Checksum: 292
Coasting Arc #4 (Orbit 1693)
---------------------------------------
Vector Time (GMT): 2013/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3571430
20 A = 6789891
61 meter
Y = -2194068
24 meter E =
0003422
Z = 5338729
23 I = 51
93919
XDOT = 3707
963275 Wp = 91
86890
YDOT = -6702
326180 meter/sec RA = 117
34834 deg
ZDOT = -273
923111 TA =
73296
MA =
73246
Ha = 228
254 n
mi
Hp = 221
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11717290
67 X = -3572564
76
Y = -7198386
62 feet Y = -2234012
70 meter
Z = 17515515
85 Z = 5321376
43
XDOT = 12165
233842 XDOT = 3783
965247
YDOT = -21989
259121 feet/sec YDOT = -6660
436419 meter/sec
ZDOT = -898
697872 ZDOT = -255
725371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13390130
81 X = 4081311
87
Y = -3515078
46 feet Y = -1071395
91 meter
Z = 17442866
35 Z = 5316585
66
XDOT = 7120
692334 XDOT = 2170
387024
YDOT = 23049
256390 feet/sec YDOT = 7025
413348 meter/sec
ZDOT = -821
230072 ZDOT = -250
310926
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 13311
54795496
00016717 00000-0 10270-3 0 9038
2 25544 51
6447 118
0633 0001140 121
9259 238
2003 15
49836040 16944
Satellite: ISS
Catalog Number: 25544
Epoch time: 13311
54795496 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 118
0633 deg
Eccentricity:
0001140
Arg of perigee: 121
9259 deg
Mean anomaly: 238
2003 deg
Mean motion: 15
49836040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1694
Checksum: 296
Coasting Arc #5 (Orbit 1708)
---------------------------------------
Vector Time (GMT): 2013/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3589061
59 A = 6789795
63 meter
Y = 2232358
52 meter E =
0015668
Z = -5327389
52 I = 51
95394
XDOT = -3347
093834 Wp = 97
10028
YDOT = 6851
287248 meter/sec RA = 112
41444 deg
ZDOT = 615
657442 TA = 178
76710
MA = 178
76324
Ha = 228
007 n
mi
Hp = 221
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11775136
44 X = 3589711
49
Y = 7324010
89 feet Y = 2272497
38 meter
Z = -17478312
08 Z = -5309952
34
XDOT = -10981
278984 XDOT = -3426
448414
YDOT = 22477
976537 feet/sec YDOT = 6813
414212 meter/sec
ZDOT = 2019
873497 ZDOT = 599
204661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13458874
27 X = -4102264
88
Y = 3701391
15 feet Y = 1128184
02 meter
Z = -17405308
78 Z = -5305138
12
XDOT = -8679
296111 XDOT = -2645
449455
YDOT = -22386
023060 feet/sec YDOT = -6823
259829 meter/sec
ZDOT = 1949
705143 ZDOT = 594
270128
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 13312
51512297
00016717 00000-0 10270-3 0 9043
2 25544 51
6458 113
2731 0001182 127
0822 233
0437 15
49906490 17099
Satellite: ISS
Catalog Number: 25544
Epoch time: 13312
51512297 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 113
2731 deg
Eccentricity:
0001182
Arg of perigee: 127
0822 deg
Mean anomaly: 233
0437 deg
Mean motion: 15
49906490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1709
Checksum: 286
Coasting Arc #6 (Orbit 1724)
---------------------------------------
Vector Time (GMT): 2013/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3610615
31 A = 6790040
53 meter
Y = -2277579
20 meter E =
0004108
Z = 5276968
12 I = 51
96502
XDOT = 2993
763442 Wp = 74
30477
YDOT = -6989
324430 meter/sec RA = 107
48013 deg
ZDOT = -966
542013 TA = 24
91806
MA = 24
89823
Ha = 228
187 n
mi
Hp = 221
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11845850
76 X = -3610512
96
Y = -7472372
72 feet Y = -2317954
81 meter
Z = 17312887
52 Z = 5259428
12
XDOT = 9822
058538 XDOT = 3076
392362
YDOT = -22930
854430 feet/sec YDOT = -6955
384262 meter/sec
ZDOT = -3171
069595 ZDOT = -951
797673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13550113
48 X = 4130074
59
Y = -3884870
72 feet Y = -1184108
60 meter
Z = 17239455
12 Z = 5254585
92
XDOT = 10173
993304 XDOT = 3101
033159
YDOT = 21668
870547 feet/sec YDOT = 6604
671743 meter/sec
ZDOT = -3108
051993 ZDOT = -947
334247
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 13313
54675741
00016717 00000-0 10270-3 0 9052
2 25544 51
6454 108
1623 0001190 126
4128 233
7132 15
49879702 17251
Satellite: ISS
Catalog Number: 25544
Epoch time: 13313
54675741 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 108
1623 deg
Eccentricity:
0001190
Arg of perigee: 126
4128 deg
Mean anomaly: 233
7132 deg
Mean motion: 15
49879702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1725
Checksum: 297
Coasting Arc #7 (Orbit 1739)
---------------------------------------
Vector Time (GMT): 2013/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902570
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3667525
98 A = 6790109
71 meter
Y = 2337841
72 meter E =
0014966
Z = -5227565
68 I = 51
97541
XDOT = -2626
653491 Wp = 102
35375
YDOT = 7063
697694 meter/sec RA = 102
54790 deg
ZDOT = 1316
261468 TA = 180
26160
MA = 180
26238
Ha = 227
914 n
mi
Hp = 221
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12032565
56 X = 3666505
54
Y = 7670084
40 feet Y = 2378848
52 meter
Z = -17150806
05 Z = -5209751
49
XDOT = -8617
629563 XDOT = -2711
840216
YDOT = 23174
861202 feet/sec YDOT = 7033
848505 meter/sec
ZDOT = 4318
443138 ZDOT = 1303
294207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13752345
97 X = -4191715
05
Y = 4127760
46 feet Y = 1258141
39 meter
Z = -17076227
65 Z = -5204834
19
XDOT = -11514
304399 XDOT = -3509
559981
YDOT = -20727
628480 feet/sec YDOT = -6317
781161 meter/sec
ZDOT = 4262
876211 ZDOT = 1299
324669
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 13314
51389881
00016717 00000-0 10270-3 0 9068
2 25544 51
6465 103
3724 0001160 131
4831 228
6419 15
49950042 17401
Satellite: ISS
Catalog Number: 25544
Epoch time: 13314
51389881 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 103
3724 deg
Eccentricity:
0001160
Arg of perigee: 131
4831 deg
Mean anomaly: 228
6419 deg
Mean motion: 15
49950042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1740
Checksum: 293
Coasting Arc #8 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2013/314/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206078
86 A = 6792048
66 meter
Y = 2429103
24 meter E =
0008607
Z = 4742780
67 I = 51
98425
XDOT = -936
187580 Wp = 116
82150
YDOT = -7078
131558 meter/sec RA = 100
23435 deg
ZDOT = 2787
280697 TA = 305
64877
MA = 305
72889
Ha = 227
918 n
mi
Hp = 220
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13799471
32 X = -4255968
45
Y = 7969498
81 feet Y = 2381789
37 meter
Z = 15560304
03 Z = 4722226
41
XDOT = -3071
481561 XDOT = -870
508794
YDOT = -23222
216396 feet/sec YDOT = -7088
233295 meter/sec
ZDOT = 9144
621709 ZDOT = 2782
892454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5269045
75 X = -1606005
14
Y = 15128425
48 feet Y = 4611144
09 meter
Z = 15473502
54 Z = 4716323
58
XDOT = -16481
335445 XDOT = -5023
511044
YDOT = -15101
521000 feet/sec YDOT = -4602
943601 meter/sec
ZDOT = 9127
204005 ZDOT = 2781
971781
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 13315
02970181
00016717 00000-0 10270-3 0 9075
2 25544 51
6456 100
8208 0000734 115
8350 244
2877 15
49970108 17483
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
02970181 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 100
8208 deg
Eccentricity:
0000734
Arg of perigee: 115
8350 deg
Mean anomaly: 244
2877 deg
Mean motion: 15
49970108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 302
Coasting Arc #9 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2013/315/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4066722
15 A = 6791464
29 meter
Y = -2389186
34 meter E =
0012425
Z = -4898049
80 I = 51
98698
XDOT = 1255
310074 Wp = 74
86531
YDOT = 7141
564570 meter/sec RA = 95
30159 deg
ZDOT = -2443
297533 TA = 171
23617
MA = 171
21445
Ha = 227
845 n
mi
Hp = 221
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13342264
26 X = 4116930
07
Y = -7838537
87 feet Y = -2343429
12 meter
Z = -16069717
19 Z = -4878171
69
XDOT = 4118
471373 XDOT = 1187
227282
YDOT = 23430
329955 feet/sec YDOT = 7155
221484 meter/sec
ZDOT = -8016
068021 ZDOT = -2437
364895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4757843
35 X = 1450190
65
Y = -14815968
90 feet Y = -4515907
32 meter
Z = -15985759
11 Z = -4872459
38
XDOT = 17680
566930 XDOT = 5389
036800
YDOT = 14293
779295 feet/sec YDOT = 4356
743929 meter/sec
ZDOT = -7992
174259 ZDOT = -2436
014714
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 13315
99682535
00016717 00000-0 10270-3 0 9085
2 25544 51
6458 96
0290 0000820 109
9254 250
1985 15
49966706 17637
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
99682535 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 96
0290 deg
Eccentricity:
0000820
Arg of perigee: 109
9254 deg
Mean anomaly: 250
1985 deg
Mean motion: 15
49966706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 336
Coasting Arc #10 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2013/316/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3933924
76 A = 6790786
54 meter
Y = 2337944
21 meter E =
0006734
Z = 5013493
27 I = 51
98747
XDOT = -1594
526337 Wp = 122
01397
YDOT = -7196
905472 meter/sec RA = 90
37020 deg
ZDOT = 2099
429663 TA = 307
61116
MA = 307
67227
Ha = 227
812 n
mi
Hp = 220
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12906577
31 X = -3984130
44
Y = 7670420
63 feet Y = 2293672
03 meter
Z = 16448468
72 Z = 4994260
22
XDOT = -5231
385619 XDOT = -1524
129092
YDOT = -23611
894594 feet/sec YDOT = -7214
342787 meter/sec
ZDOT = 6887
892595 ZDOT = 2091
854723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4299498
00 X = -1310486
99
Y = 14477411
84 feet Y = 4412715
13 meter
Z = 16367225
70 Z = 4988730
39
XDOT = -18887
750460 XDOT = -5756
986340
YDOT = -13382
111586 feet/sec YDOT = -4078
867611 meter/sec
ZDOT = 6857
112063 ZDOT = 2090
047757
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 13317
02840741
00016717 00000-0 10270-3 0 9097
2 25544 51
6461 90
9192 0000622 111
8864 248
2353 15
50018959 17798
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
02840741 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 90
9192 deg
Eccentricity:
0000622
Arg of perigee: 111
8864 deg
Mean anomaly: 248
2353 deg
Mean motion: 15
50018959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 309
Coasting Arc #11 (Orbit 1793)
---------------------------------------
Vector Time (GMT): 2013/317/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3845520
37 A = 6790334
93 meter
Y = -2257113
23 meter E =
0013923
Z = -5133619
91 I = 51
98557
XDOT = 1926
690734 Wp = 78
38595
YDOT = 7200
977936 meter/sec RA = 85
43673 deg
ZDOT = -1724
049275 TA = 175
00175
MA = 174
98784
Ha = 227
723 n
mi
Hp = 221
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12616536
64 X = 3895412
39
Y = -7405227
12 feet Y = -2213831
37 meter
Z = -16842585
01 Z = -5114817
05
XDOT = 6321
163827 XDOT = 1854
399761
YDOT = 23625
255697 feet/sec YDOT = 7222
119163 meter/sec
ZDOT = -5656
329644 ZDOT = -1714
865199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4026582
89 X = 1227302
46
Y = -14158750
78 feet Y = -4315587
24 meter
Z = -16763157
87 Z = -5109410
52
XDOT = 19932
455031 XDOT = 6075
412293
YDOT = 12316
088618 feet/sec YDOT = 3753
943811 meter/sec
ZDOT = -5618
796375 ZDOT = -1712
609135
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 13317
99550342
00016717 00000-0 10270-3 0 9100
2 25544 51
6465 86
1273 0000679 105
0833 255
0393 15
50013497 17941
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
99550342 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 86
1273 deg
Eccentricity:
0000679
Arg of perigee: 105
0833 deg
Mean anomaly: 255
0393 deg
Mean motion: 15
50013497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1794
Checksum: 305
Coasting Arc #12 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2013/318/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3769164
41 A = 6789785
04 meter
Y = 2166842
81 meter E =
0004825
Z = 5212304
90 I = 51
98167
XDOT = -2270
541372 Wp = 122
48683
YDOT = -7195
727478 meter/sec RA = 80
50453 deg
ZDOT = 1346
065448 TA = 314
61274
MA = 314
65209
Ha = 227
716 n
mi
Hp = 220
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12366024
96 X = -3818434
98
Y = 7109064
35 feet Y = 2124418
23 meter
Z = 17100737
85 Z = 5193874
46
XDOT = -7449
282717 XDOT = -2196
447387
YDOT = -23608
029783 feet/sec YDOT = -7220
703809 meter/sec
ZDOT = 4416
225222 ZDOT = 1335
215198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3815177
39 X = -1162866
07
Y = 13840462
79 feet Y = 4218573
06 meter
Z = 17022885
05 Z = 5188575
36
XDOT = -20950
970648 XDOT = -6385
855854
YDOT = -11166
019942 feet/sec YDOT = -3403
402878 meter/sec
ZDOT = 4371
699440 ZDOT = 1332
493989
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 13319
02705617
00016717 00000-0 10270-3 0 9114
2 25544 51
6473 81
0176 0000534 105
3387 254
7823 15
50066869 18107
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
02705617 = yrday
fracday
Element set: 911
Inclination: 51
6473 deg
RA of node: 81
0176 deg
Eccentricity:
0000534
Arg of perigee: 105
3387 deg
Mean anomaly: 254
7823 deg
Mean motion: 15
50066869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 295
Coasting Arc #13 (Orbit 1824)
---------------------------------------
Vector Time (GMT): 2013/319/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3741151
99 A = 6789513
14 meter
Y = -2061939
16 meter E =
0014960
Z = -5290330
29 I = 51
97514
XDOT = 2597
869859 Wp = 83
31321
YDOT = 7133
935395 meter/sec RA = 75
57004 deg
ZDOT = -943
962091 TA = 177
67904
MA = 177
67209
Ha = 227
617 n
mi
Hp = 220
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12274120
72 X = 3789630
66
Y = -6764892
25 feet Y = -2019832
17 meter
Z = -17356726
66 Z = -5272037
87
XDOT = 8523
195075 XDOT = 2522
489166
YDOT = 23405
299852 feet/sec YDOT = 7162
564950 meter/sec
ZDOT = -3096
988489 ZDOT = -931
524662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3760764
52 X = 1146281
02
Y = -13599651
65 feet Y = -4145173
82 meter
Z = -17279464
46 Z = -5266780
77
XDOT = 21758
458255 XDOT = 6631
978076
YDOT = 9884
382074 feet/sec YDOT = 3012
759656 meter/sec
ZDOT = -3045
794146 ZDOT = -928
358056
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 13319
99412477
00016717 00000-0 10270-3 0 9120
2 25544 51
6478 76
2258 0000583 97
8915 262
2302 15
50060178 18254
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
99412477 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 76
2258 deg
Eccentricity:
0000583
Arg of perigee: 97
8915 deg
Mean anomaly: 262
2302 deg
Mean motion: 15
50060178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1825
Checksum: 318
Coasting Arc #14 (Orbit 1840)
---------------------------------------
Vector Time (GMT): 2013/320/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3729230
66 A = 6789149
93 meter
Y = 1950811
90 meter E =
0003251
Z = 5324700
90 I = 51
96673
XDOT = -2927
100040 Wp = 109
31716
YDOT = -7063
321616 meter/sec RA = 70
63655 deg
ZDOT = 536
441267 TA = 335
57722
MA = 335
59262
Ha = 227
632 n
mi
Hp = 220
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12235008
72 X = -3776634
52
Y = 6400301
50 feet Y = 1908844
13 meter
Z = 17469491
14 Z = 5306469
05
XDOT = -9603
346588 XDOT = -2850
504819
YDOT = -23173
627349 feet/sec YDOT = -7095
626052 meter/sec
ZDOT = 1759
977911 ZDOT = 522
407252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3766102
06 X = -1147907
91
Y = 13385066
96 feet Y = 4079768
41 meter
Z = 17392494
82 Z = 5301232
42
XDOT = -22509
194428 XDOT = -6860
802462
YDOT = -8550
609292 feet/sec YDOT = -2606
225712 meter/sec
ZDOT = 1702
073256 ZDOT = 518
791928
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 13321
02564835
00016717 00000-0 10270-3 0 9134
2 25544 51
6486 71
1162 0000484 96
4152 263
7053 15
50112799 18413
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
02564835 = yrday
fracday
Element set: 913
Inclination: 51
6486 deg
RA of node: 71
1162 deg
Eccentricity:
0000484
Arg of perigee: 96
4152 deg
Mean anomaly: 263
7053 deg
Mean motion: 15
50112799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1841
Checksum: 291
Coasting Arc #15 (Orbit 1855)
---------------------------------------
Vector Time (GMT): 2013/321/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3765488
24 A = 6789096
07 meter
Y = -1841326
12 meter E =
0015399
Z = -5353924
17 I = 51
95573
XDOT = 3229
036702 Wp = 89
11051
YDOT = 6934
814987 meter/sec RA = 65
70053 deg
ZDOT = -114
052627 TA = 179
80515
MA = 179
80454
Ha = 227
536 n
mi
Hp = 220
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12353964
06 X = 3811807
04
Y = -6041096
21 feet Y = -1798958
88 meter
Z = -17565368
00 Z = -5335518
87
XDOT = 10593
952433 XDOT = 3151
804126
YDOT = 22752
017675 feet/sec YDOT = 6970
492303 meter/sec
ZDOT = -374
188408 ZDOT = -98
553248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3881858
23 X = 1183190
39
Y = -13295509
79 feet Y = -4052471
38 meter
Z = -17487653
36 Z = -5330236
75
XDOT = 23010
389123 XDOT = 7013
566605
YDOT = 7125
962398 feet/sec YDOT = 2171
993339 meter/sec
ZDOT = -310
114297 ZDOT = -94
522838
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 13321
99268978
00016717 00000-0 10270-3 0 9140
2 25544 51
6490 66
3245 0000558 90
0612 270
0602 15
50106203 18569
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
99268978 = yrday
fracday
Element set: 914
Inclination: 51
6490 deg
RA of node: 66
3245 deg
Eccentricity:
0000558
Arg of perigee: 90
0612 deg
Mean anomaly: 270
0602 deg
Mean motion: 15
50106203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1856
Checksum: 293
Coasting Arc #16 (Orbit 1871)
---------------------------------------
Vector Time (GMT): 2013/322/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 887343
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3819877
09 A = 6788969
52 meter
Y = 1729649
19 meter E =
0003046
Z = 5336671
36 I = 51
94271
XDOT = -3522
154933 Wp = 76
39384
YDOT = -6800
121891 meter/sec RA = 60
76504 deg
ZDOT = -316
272945 TA = 16
61513
MA = 16
60515
Ha = 227
564 n
mi
Hp = 220
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12532405
14 X = -3864859
17
Y = 5674702
06 feet Y = 1686681
14 meter
Z = 17508764
32 Z = 5318005
16
XDOT = -11555
626421 XDOT = -3444
316288
YDOT = -22310
111191 feet/sec YDOT = -6839
073634 meter/sec
ZDOT = -1037
640895 ZDOT = -333
194871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4045653
63 X = -1233115
23
Y = 13253274
12 feet Y = 4039597
95 meter
Z = 17429964
48 Z = 5312653
17
XDOT = -23431
831698 XDOT = -7142
022302
YDOT = -5692
255069 feet/sec YDOT = -1734
999345 meter/sec
ZDOT = -1107
707939 ZDOT = -337
629380
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 13323
02418441
00016717 00000-0 10270-3 0 9159
2 25544 51
6494 61
2148 0000481 86
6845 273
4361 15
50156763 18726
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
02418441 = yrday
fracday
Element set: 915
Inclination: 51
6494 deg
RA of node: 61
2148 deg
Eccentricity:
0000481
Arg of perigee: 86
6845 deg
Mean anomaly: 273
4361 deg
Mean motion: 15
50156763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1872
Checksum: 299
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