[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 26th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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
272/11:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 219
2
275/19:19:20
777 2
0 6
2 6
3
N/A -5
9 -0
9 227
7
000/00:14:41
553 0
6 0
3 222
9
Coasting Arc #1 (Orbit 1038)
---------------------------------------
Vector Time (GMT): 2013/269/06:20:13
647
Vector Time (MET): N/A
Weight (LBS) : 927888
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2105602
25 A = 6788090
78 meter
Y = 3672887
37 meter E =
0005541
Z = 5301359
71 I = 51
43603
XDOT = -6509
958137 Wp = 80
97055
YDOT = 4044
563646 meter/sec RA = 326
86340 deg
ZDOT = -215
473089 TA = 11
09533
MA = 11
08311
Ha = 227
831 n
mi
Hp = 219
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6908143
86 X = 2038621
98
Y = 12050155
42 feet Y = 3696059
45 meter
Z = 17392912
45 Z = 5311425
63
XDOT = -21358
130371 XDOT = -6553
654781
YDOT = 13269
565767 feet/sec YDOT = 3971
520819 meter/sec
ZDOT = -706
932707 ZDOT = -247
204532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10769803
72 X = 3282636
17
Y = -8688450
77 feet Y = -2648239
79 meter
Z = 17434570
59 Z = 5314057
12
XDOT = 15965
435287 XDOT = 4866
264675
YDOT = 18096
315786 feet/sec YDOT = 5515
757051 meter/sec
ZDOT = -840
627620 ZDOT = -256
223299
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 13269
31197808
00016717 00000-0 10270-3 0 9005
2 25544 51
6475 327
2060 0003045 84
1591 275
9907 15
50451347 10397
Satellite: ISS
Catalog Number: 25544
Epoch time: 13269
31197808 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 327
2060 deg
Eccentricity:
0003045
Arg of perigee: 84
1591 deg
Mean anomaly: 275
9907 deg
Mean motion: 15
50451347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1039
Checksum: 306
Coasting Arc #2 (Orbit 1053)
---------------------------------------
Vector Time (GMT): 2013/270/06:20:13
647
Vector Time (MET): N/A
Weight (LBS) : 927888
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1897016
08 A = 6788142
11 meter
Y = -3856260
64 meter E =
0017520
Z = -5269805
22 I = 51
41232
XDOT = 6351
739800 Wp = 94
57659
YDOT = -4190
540439 meter/sec RA = 321
88844 deg
ZDOT = 780
886194 TA = 182
92248
MA = 182
93273
Ha = 227
813 n
mi
Hp = 219
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6223806
04 X = -1828154
13
Y = -12651773
75 feet Y = -3877089
67 meter
Z = -17289387
22 Z = -5278853
23
XDOT = 20839
041338 XDOT = 6394
333913
YDOT = -13748
492253 feet/sec YDOT = -4119
273029 meter/sec
ZDOT = 2561
962579 ZDOT = 811
846306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11334361
76 X = -3454713
47
Y = 8309151
08 feet Y = 2532629
25 meter
Z = -17326751
07 Z = -5281193
73
XDOT = -16690
066808 XDOT = -5087
132363
YDOT = -17158
206378 feet/sec YDOT = -5229
821304 meter/sec
ZDOT = 2692
439392 ZDOT = 820
655527
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 13270
27877671
00016717 00000-0 10270-3 0 9016
2 25544 51
6484 322
4144 0003047 88
3175 271
8325 15
50508282 10540
Satellite: ISS
Catalog Number: 25544
Epoch time: 13270
27877671 = yrday
fracday
Element set: 901
Inclination: 51
6484 deg
RA of node: 322
4144 deg
Eccentricity:
0003047
Arg of perigee: 88
3175 deg
Mean anomaly: 271
8325 deg
Mean motion: 15
50508282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1054
Checksum: 300
Coasting Arc #3 (Orbit 1069)
---------------------------------------
Vector Time (GMT): 2013/271/06:20:13
647
Vector Time (MET): N/A
Weight (LBS) : 927888
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1696500
57 A = 6788615
63 meter
Y = 4060032
97 meter E =
0007194
Z = 5164135
47 I = 51
39024
XDOT = -6192
640485 Wp = 69
15614
YDOT = 4313
588174 meter/sec RA = 316
90964 deg
ZDOT = -1352
912265 TA = 33
91759
MA = 33
87161
Ha = 227
810 n
mi
Hp = 219
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5565946
75 X = 1625888
25
Y = 13320318
14 feet Y = 4078609
95 meter
Z = 16942701
69 Z = 5172205
08
XDOT = -20317
061960 XDOT = -6233
843619
YDOT = 14152
192171 feet/sec YDOT = 4244
107635 meter/sec
ZDOT = -4438
688534 ZDOT = -1383
096102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11974975
17 X = 3649972
43
Y = -7992706
72 feet Y = -2436177
01 meter
Z = 16975935
56 Z = 5174265
16
XDOT = 17309
723306 XDOT = 5276
003664
YDOT = 16208
285499 feet/sec YDOT = 4940
285420 meter/sec
ZDOT = -4565
921720 ZDOT = -1391
692940
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 13271
31001955
00016717 00000-0 10270-3 0 9027
2 25544 51
6486 317
3010 0003089 90
6217 269
5287 15
50484297 10704
Satellite: ISS
Catalog Number: 25544
Epoch time: 13271
31001955 = yrday
fracday
Element set: 902
Inclination: 51
6486 deg
RA of node: 317
3010 deg
Eccentricity:
0003089
Arg of perigee: 90
6217 deg
Mean anomaly: 269
5287 deg
Mean motion: 15
50484297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1070
Checksum: 295
Coasting Arc #4 (Orbit 1084)
---------------------------------------
Vector Time (GMT): 2013/272/06:20:13
647
Vector Time (MET): N/A
Weight (LBS) : 927888
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1544527
93 A = 6789073
01 meter
Y = -4301407
20 meter E =
0015868
Z = -5034810
56 I = 51
37087
XDOT = 5978
558512 Wp = 102
17361
YDOT = -4376
039811 meter/sec RA = 311
93168 deg
ZDOT = 1906
391503 TA = 186
41772
MA = 186
43807
Ha = 227
751 n
mi
Hp = 219
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5067348
84 X = -1471856
04
Y = -14112228
33 feet Y = -4318273
25 meter
Z = -16518407
35 Z = -5042136
82
XDOT = 19614
693282 XDOT = 6017
787251
YDOT = -14357
085993 feet/sec YDOT = -4308
964243 meter/sec
ZDOT = 6254
565298 ZDOT = 1935
530580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12715719
12 X = -3875751
19
Y = 7883442
29 feet Y = 2402873
21 meter
Z = -16548492
95 Z = -5043980
65
XDOT = -17655
372414 XDOT = -5381
357512
YDOT = -15102
992346 feet/sec YDOT = -4603
392067 meter/sec
ZDOT = 6377
418376 ZDOT = 1943
837121
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 13272
27679684
00016717 00000-0 10270-3 0 9034
2 25544 51
6490 312
5091 0003023 94
0557 266
0940 15
50540894 10858
Satellite: ISS
Catalog Number: 25544
Epoch time: 13272
27679684 = yrday
fracday
Element set: 903
Inclination: 51
6490 deg
RA of node: 312
5091 deg
Eccentricity:
0003023
Arg of perigee: 94
0557 deg
Mean anomaly: 266
0940 deg
Mean motion: 15
50540894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1085
Checksum: 306
Coasting Arc #5 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2013/272/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5458086
48 A = 6796680
54 meter
Y = -2995476
05 meter E =
0016558
Z = 2707790
69 I = 51
39158
XDOT = 537
861453 Wp = 80
33352
YDOT = 5655
364005 meter/sec RA = 310
91964 deg
ZDOT = 5147
816280 TA = 310
35576
MA = 310
50023
Ha = 227
770 n
mi
Hp = 219
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17907107
88 X = 5478023
15
Y = -9827677
33 feet Y = -2934328
51 meter
Z = 8883827
72 Z = 2734354
37
XDOT = 1764
637312 XDOT = 449
575195
YDOT = 18554
343849 feet/sec YDOT = 5660
885593 meter/sec
ZDOT = 16889
161022 ZDOT = 5150
214157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18050207
43 X = -5501703
22
Y = 9457167
44 feet Y = 2882544
64 meter
Z = 8995673
69 Z = 2741881
34
XDOT = -587
444138 XDOT = -179
052973
YDOT = -17269
647131 feet/sec YDOT = -5263
788446 meter/sec
ZDOT = 16898
378533 ZDOT = 5150
625777
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 13272
53460278
00016717 00000-0 10270-3 0 9041
2 25544 51
6488 311
2340 0003137 88
0056 272
1454 15
50515804 10896
Satellite: ISS
Catalog Number: 25544
Epoch time: 13272
53460278 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 311
2340 deg
Eccentricity:
0003137
Arg of perigee: 88
0056 deg
Mean anomaly: 272
1454 deg
Mean motion: 15
50515804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1089
Checksum: 291
Coasting Arc #6 (Orbit 1103)
---------------------------------------
Vector Time (GMT): 2013/273/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5252006
30 A = 6795417
65 meter
Y = 2935493
85 meter E =
0007678
Z = -3164271
35 I = 51
36910
XDOT = -433
715541 Wp = 96
39961
YDOT = -5944
094303 meter/sec RA = 305
94463 deg
ZDOT = -4805
382352 TA = 120
17364
MA = 120
09756
Ha = 227
744 n
mi
Hp = 219
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17230991
81 X = -5269070
08
Y = 9630885
34 feet Y = 2876666
80 meter
Z = -10381467
67 Z = -3189826
97
XDOT = -1422
951249 XDOT = -343
871824
YDOT = -19501
621729 feet/sec YDOT = -5948
442593 meter/sec
ZDOT = -15765
690131 ZDOT = -4807
270399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17198785
48 X = 5242189
81
Y = -9571681
27 feet Y = -2917448
45 meter
Z = -10489070
40 Z = -3197068
66
XDOT = 560
687934 XDOT = 170
897682
YDOT = 18253
063653 feet/sec YDOT = 5563
533801 meter/sec
ZDOT = -15772
735865 ZDOT = -4807
529892
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 13273
50136793
00016717 00000-0 10270-3 0 9052
2 25544 51
6495 306
4408 0003149 90
9187 269
2325 15
50556822 11042
Satellite: ISS
Catalog Number: 25544
Epoch time: 13273
50136793 = yrday
fracday
Element set: 905
Inclination: 51
6495 deg
RA of node: 306
4408 deg
Eccentricity:
0003149
Arg of perigee: 90
9187 deg
Mean anomaly: 269
2325 deg
Mean motion: 15
50556822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1104
Checksum: 308
Coasting Arc #7 (Orbit 1119)
---------------------------------------
Vector Time (GMT): 2013/274/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5028621
28 A = 6794312
53 meter
Y = -2856609
76 meter E =
0015286
Z = 3553302
17 I = 51
34679
XDOT = 395
866439 Wp = 92
79316
YDOT = 6239
068175 meter/sec RA = 300
96743 deg
ZDOT = 4438
243414 TA = 309
29952
MA = 309
43497
Ha = 227
733 n
mi
Hp = 219
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16498101
32 X = 5042929
72
Y = -9372079
28 feet Y = -2800296
05 meter
Z = 11657815
53 Z = 3577765
99
XDOT = 1298
774407 XDOT = 304
510506
YDOT = 20469
383777 feet/sec YDOT = 6242
984785 meter/sec
ZDOT = 14561
166055 ZDOT = 4439
943789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16294431
08 X = -4966542
59
Y = 9597004
26 feet Y = 2925166
90 meter
Z = 11760820
76 Z = 3584698
17
XDOT = -790
881440 XDOT = -241
060663
YDOT = -19263
660354 feet/sec YDOT = -5871
563676 meter/sec
ZDOT = 14567
391417 ZDOT = 4440
140904
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 13274
53257342
00016717 00000-0 10270-3 0 9061
2 25544 51
6482 301
3282 0003270 93
1491 267
0034 15
50553988 11201
Satellite: ISS
Catalog Number: 25544
Epoch time: 13274
53257342 = yrday
fracday
Element set: 906
Inclination: 51
6482 deg
RA of node: 301
3282 deg
Eccentricity:
0003270
Arg of perigee: 93
1491 deg
Mean anomaly: 267
0034 deg
Mean motion: 15
50553988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1120
Checksum: 286
Coasting Arc #8 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2013/275/11:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 939475
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4831575
44 A = 6792959
22 meter
Y = 2697887
36 meter E =
0009811
Z = -3949465
66 I = 51
32856
XDOT = -379
590885 Wp = 80
18760
YDOT = -6517
618623 meter/sec RA = 295
98773 deg
ZDOT = -3994
701634 TA = 147
89129
MA = 147
83150
Ha = 227
715 n
mi
Hp = 218
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15851625
45 X = -4842199
14
Y = 8851336
48 feet Y = 2643797
64 meter
Z = -12957564
50 Z = -3972963
37
XDOT = -1245
376920 XDOT = -287
275912
YDOT = -21383
263199 feet/sec YDOT = -6521
347861 meter/sec
ZDOT = -13105
976490 ZDOT = -3996
320498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15488859
61 X = 4721004
41
Y = -9334988
50 feet Y = -2845304
49 meter
Z = -13056488
13 Z = -3979617
58
XDOT = 1145
560289 XDOT = 349
166776
YDOT = 20208
438814 feet/sec YDOT = 6159
532150 meter/sec
ZDOT = -13111
829626 ZDOT = -3996
485670
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 13275
49931687
00016717 00000-0 10270-3 0 9079
2 25544 51
6491 296
5349 0003205 96
5336 263
6179 15
50589989 11351
Satellite: ISS
Catalog Number: 25544
Epoch time: 13275
49931687 = yrday
fracday
Element set: 907
Inclination: 51
6491 deg
RA of node: 296
5349 deg
Eccentricity:
0003205
Arg of perigee: 96
5336 deg
Mean anomaly: 263
6179 deg
Mean motion: 15
50589989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 354
Coasting Arc #9 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2013/275/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2222952
26 A = 6793691
69 meter
Y = -4326387
98 meter E =
0009209
Z = -4751849
45 I = 51
31435
XDOT = 4759
522788 Wp = 114
12438
YDOT = -5368
873600 meter/sec RA = 294
27389 deg
ZDOT = 2662
036021 TA = 182
33723
MA = 182
34154
Ha = 227
748 n
mi
Hp = 222
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7293150
45 X = -2151325
03
Y = -14194186
27 feet Y = -4350846
65 meter
Z = -15590057
24 Z = -4762473
82
XDOT = 15615
232245 XDOT = 4806
273415
YDOT = -17614
414699 feet/sec YDOT = -5315
387801 meter/sec
ZDOT = 8733
713981 ZDOT = 2685
271880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8098771
79 X = 2468505
64
Y = -13700477
39 feet Y = -4175905
51 meter
Z = -15633990
75 Z = -4765240
38
XDOT = 22218
830404 XDOT = 6772
299507
YDOT = 3057
422622 feet/sec YDOT = 931
902415 meter/sec
ZDOT = 8831
919194 ZDOT = 2691
968970
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 13275
82156520
00016717 00000-0 10270-3 0 9082
2 25544 51
6492 294
9352 0002113 263
9073 96
1837 15
49353262 11400
Satellite: ISS
Catalog Number: 25544
Epoch time: 13275
82156520 = yrday
fracday
Element set: 908
Inclination: 51
6492 deg
RA of node: 294
9352 deg
Eccentricity:
0002113
Arg of perigee: 263
9073 deg
Mean anomaly: 96
1837 deg
Mean motion: 15
49353262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 306
Coasting Arc #10 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2013/276/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2488282
62 A = 6793838
08 meter
Y = 4243920
12 meter E =
0006132
Z = 4682759
47 I = 51
30292
XDOT = -4354
336525 Wp = 54
79735
YDOT = 5648
592024 meter/sec RA = 289
30154 deg
ZDOT = -2799
394906 TA = 63
14794
MA = 63
08527
Ha = 227
606 n
mi
Hp = 222
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8163656
88 X = 2417893
38
Y = 13923622
43 feet Y = 4271352
80 meter
Z = 15363384
09 Z = 4694675
86
XDOT = -14285
880988 XDOT = -4403
577828
YDOT = 18532
126063 feet/sec YDOT = 5599
623322 meter/sec
ZDOT = -9184
366491 ZDOT = -2820
668580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7154890
71 X = -2180810
69
Y = 14415295
90 feet Y = 4393782
19 meter
Z = 15412751
50 Z = 4697806
66
XDOT = -22255
587457 XDOT = -6783
503057
YDOT = -1108
984493 feet/sec YDOT = -338
018474 meter/sec
ZDOT = -9274
373293 ZDOT = -2826
828980
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 13276
85356703
00016717 00000-0 10270-3 0 9092
2 25544 51
6487 289
8278 0002136 269
5648 90
5258 15
49386621 11566
Satellite: ISS
Catalog Number: 25544
Epoch time: 13276
85356703 = yrday
fracday
Element set: 909
Inclination: 51
6487 deg
RA of node: 289
8278 deg
Eccentricity:
0002136
Arg of perigee: 269
5648 deg
Mean anomaly: 90
5258 deg
Mean motion: 15
49386621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 352
Coasting Arc #11 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2013/277/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2765807
14 A = 6794076
06 meter
Y = -4146751
45 meter E =
0008275
Z = -4624967
13 I = 51
29501
XDOT = 3924
029840 Wp = 113
99875
YDOT = -5882
169810 meter/sec RA = 284
32758 deg
ZDOT = 2928
195821 TA = 185
35626
MA = 185
36512
Ha = 227
662 n
mi
Hp = 222
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9074170
42 X = -2696764
49
Y = -13604827
59 feet Y = -4177295
08 meter
Z = -15173776
66 Z = -4638235
09
XDOT = 12874
113648 XDOT = 3975
289297
YDOT = -19298
457381 feet/sec YDOT = -5838
001788 meter/sec
ZDOT = 9606
941669 ZDOT = 2947
384053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6126749
11 X = 1867433
13
Y = -15106989
39 feet Y = -4604610
37 meter
Z = -15228828
51 Z = -4641746
93
XDOT = 22060
156871 XDOT = 6723
935814
YDOT = -816
841746 feet/sec YDOT = -248
973364 meter/sec
ZDOT = 9688
228424 ZDOT = 2952
972024
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 13277
82105865
00016717 00000-0 10270-3 0 9103
2 25544 51
6492 285
0388 0002167 273
1794 86
9109 15
49388279 11711
Satellite: ISS
Catalog Number: 25544
Epoch time: 13277
82105865 = yrday
fracday
Element set: 910
Inclination: 51
6492 deg
RA of node: 285
0388 deg
Eccentricity:
0002167
Arg of perigee: 273
1794 deg
Mean anomaly: 86
9109 deg
Mean motion: 15
49388279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 338
Coasting Arc #12 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2013/278/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3025408
19 A = 6794233
85 meter
Y = 4041180
28 meter E =
0006911
Z = 4544160
83 I = 51
28917
XDOT = -3498
840962 Wp = 56
95627
YDOT = 6083
806450 meter/sec RA = 279
35338 deg
ZDOT = -3073
838080 TA = 64
01937
MA = 63
94819
Ha = 227
520 n
mi
Hp = 222
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9925879
87 X = 2957919
22
Y = 13258465
49 feet Y = 4074635
54 meter
Z = 14908664
13 Z = 4558693
83
XDOT = -11479
137013 XDOT = -3551
679210
YDOT = 19959
994915 feet/sec YDOT = 6044
384358 meter/sec
ZDOT = -10084
770603 ZDOT = -3090
964583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5088571
92 X = -1550996
72
Y = 15703904
05 feet Y = 4786549
96 meter
Z = 14969037
97 Z = 4562562
77
XDOT = -21733
965982 XDOT = -6624
512831
YDOT = 2661
763970 feet/sec YDOT = 811
305658 meter/sec
ZDOT = -10157
434596 ZDOT = -3095
986065
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 13278
85303769
00016717 00000-0 10270-3 0 9111
2 25544 51
6491 279
9310 0002205 279
2239 80
8662 15
49432202 11871
Satellite: ISS
Catalog Number: 25544
Epoch time: 13278
85303769 = yrday
fracday
Element set: 911
Inclination: 51
6491 deg
RA of node: 279
9310 deg
Eccentricity:
0002205
Arg of perigee: 279
2239 deg
Mean anomaly: 80
8662 deg
Mean motion: 15
49432202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 316
Coasting Arc #13 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2013/279/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3297290
43 A = 6794531
63 meter
Y = -3916205
54 meter E =
0007234
Z = -4474682
36 I = 51
28642
XDOT = 3057
584284 Wp = 113
07630
YDOT = -6239
660837 meter/sec RA = 274
37832 deg
ZDOT = 3209
214971 TA = 189
42122
MA = 189
43479
Ha = 227
590 n
mi
Hp = 222
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10817881
98 X = -3231516
22
Y = -12848443
37 feet Y = -3952710
66 meter
Z = -14680716
41 Z = -4490540
46
XDOT = 10031
444500 XDOT = 3111
540455
YDOT = -20471
328204 feet/sec YDOT = -6205
166952 meter/sec
ZDOT = 10528
920510 ZDOT = 3224
200496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3956900
27 X = 1206063
20
Y = -16263802
03 feet Y = -4957206
86 meter
Z = -14746666
93 Z = -4494784
08
XDOT = 21199
337798 XDOT = 6461
558161
YDOT = -4442
741800 feet/sec YDOT = -1354
147701 meter/sec
ZDOT = 10592
625232 ZDOT = 3228
632171
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 13279
82050813
00016717 00000-0 10270-3 0 9129
2 25544 51
6495 275
1419 0002261 281
9126 78
1771 15
49424990 12024
Satellite: ISS
Catalog Number: 25544
Epoch time: 13279
82050813 = yrday
fracday
Element set: 912
Inclination: 51
6495 deg
RA of node: 275
1419 deg
Eccentricity:
0002261
Arg of perigee: 281
9126 deg
Mean anomaly: 78
1771 deg
Mean motion: 15
49424990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1202
Checksum: 307
Coasting Arc #14 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2013/280/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3550811
34 A = 6794710
46 meter
Y = 3786777
87 meter E =
0007691
Z = 4380556
39 I = 51
28639
XDOT = -2628
556476 Wp = 59
98780
YDOT = 6363
276433 meter/sec RA = 269
40351 deg
ZDOT = -3361
847689 TA = 64
26955
MA = 64
19018
Ha = 227
459 n
mi
Hp = 222
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11649643
51 X = 3486922
82
Y = 12423811
91 feet Y = 3826128
46 meter
Z = 14371904
18 Z = 4397650
78
XDOT = -8623
872952 XDOT = -2683
185359
YDOT = 20876
891185 feet/sec YDOT = 6333
576502 meter/sec
ZDOT = -11029
684019 ZDOT = -3374
750512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2832456
29 X = -863332
68
Y = 16732964
83 feet Y = 5100207
68 meter
Z = 14443060
81 Z = 4402244
94
XDOT = -20554
340732 XDOT = -6264
963055
YDOT = 6111
604469 feet/sec YDOT = 1862
817042 meter/sec
ZDOT = -11084
670645 ZDOT = -3378
607613
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 13280
85246382
00016717 00000-0 10270-3 0 9133
2 25544 51
6498 270
0340 0002312 287
9813 72
1086 15
49476820 12189
Satellite: ISS
Catalog Number: 25544
Epoch time: 13280
85246382 = yrday
fracday
Element set: 913
Inclination: 51
6498 deg
RA of node: 270
0340 deg
Eccentricity:
0002312
Arg of perigee: 287
9813 deg
Mean anomaly: 72
1086 deg
Mean motion: 15
49476820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 306
Coasting Arc #15 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2013/281/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3815452
47 A = 6795062
03 meter
Y = -3632885
07 meter E =
0006140
Z = -4297913
21 I = 51
28848
XDOT = 2191
948897 Wp = 110
64733
YDOT = -6443
486099 meter/sec RA = 264
42818 deg
ZDOT = 3502
531428 TA = 195
24621
MA = 195
26472
Ha = 227
543 n
mi
Hp = 222
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12517888
67 X = -3753666
64
Y = -11918914
28 feet Y = -3675206
72 meter
Z = -14100765
14 Z = -4316298
39
XDOT = 7191
433390 XDOT = 2246
823760
YDOT = -21140
046256 feet/sec YDOT = -6418
667269 meter/sec
ZDOT = 11491
244844 ZDOT = 3513
313672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1607891
28 X = 490085
26
Y = -17146624
33 feet Y = -5226291
10 meter
Z = -14177361
94 Z = -4321259
92
XDOT = 19733
093790 XDOT = 6014
646987
YDOT = -7683
727352 feet/sec YDOT = -2342
000097 meter/sec
ZDOT = 11537
348379 ZDOT = 3516
583786
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 13281
81991251
00016717 00000-0 10270-3 0 9143
2 25544 51
6495 265
2448 0002353 289
7130 70
3767 15
49463090 12336
Satellite: ISS
Catalog Number: 25544
Epoch time: 13281
81991251 = yrday
fracday
Element set: 914
Inclination: 51
6495 deg
RA of node: 265
2448 deg
Eccentricity:
0002353
Arg of perigee: 289
7130 deg
Mean anomaly: 70
3767 deg
Mean motion: 15
49463090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 313
Coasting Arc #16 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2013/282/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4061762
56 A = 6795276
72 meter
Y = 3478238
83 meter E =
0008452
Z = 4188717
02 I = 51
29390
XDOT = -1774
994772 Wp = 63
88462
YDOT = 6492
435209 meter/sec RA = 259
45372 deg
ZDOT = -3660
581372 TA = 63
91093
MA = 63
82397
Ha = 227
427 n
mi
Hp = 222
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13325992
66 X = 4002218
24
Y = 11411544
71 feet Y = 3523327
34 meter
Z = 13742509
90 Z = 4208304
21
XDOT = -5823
473662 XDOT = -1829
680260
YDOT = 21300
640448 feet/sec YDOT = 6472
280121 meter/sec
ZDOT = -12009
781403 ZDOT = -3669
337479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -406147
63 X = -123793
80
Y = 17475387
80 feet Y = 5326498
20 meter
Z = 13824177
25 Z = 4213609
23
XDOT = -18829
029745 XDOT = -5739
088266
YDOT = 9116
994746 feet/sec YDOT = 2778
859999 meter/sec
ZDOT = -12047
391893 ZDOT = -3672
045049
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 13282
85184411
00016717 00000-0 10270-3 0 9151
2 25544 51
6498 260
1371 0002431 295
4623 64
6275 15
49517917 12491
Satellite: ISS
Catalog Number: 25544
Epoch time: 13282
85184411 = yrday
fracday
Element set: 915
Inclination: 51
6498 deg
RA of node: 260
1371 deg
Eccentricity:
0002431
Arg of perigee: 295
4623 deg
Mean anomaly: 64
6275 deg
Mean motion: 15
49517917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1249
Checksum: 316
Coasting Arc #17 (Orbit 1263)
---------------------------------------
Vector Time (GMT): 2013/283/19:26:41
553
Vector Time (MET): N/A
Weight (LBS) : 938828
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4316649
57 A = 6795671
24 meter
Y = -3294128
03 meter E =
0005067
Z = -4091347
44 I = 51
30053
XDOT = 1357
952835 Wp = 105
43123
YDOT = -6502
163804 meter/sec RA = 254
47865 deg
ZDOT = 3805
087317 TA = 204
11838
MA = 204
14211
Ha = 227
525 n
mi
Hp = 222
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14162236
11 X = -4259618
15
Y = -10807506
66 feet Y = -3342080
88 meter
Z = -13423055
91 Z = -4112178
92
XDOT = 4455
225836 XDOT = 1412
076198
YDOT = -21332
558413 feet/sec YDOT = -6486
675495 meter/sec
ZDOT = 12483
882272 ZDOT = 3811
816018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -897848
46 X = -273664
21
Y = -17726362
81 feet Y = -5402995
39 meter
Z = -13509977
47 Z = -4117841
13
XDOT = 17786
769225 XDOT = 5421
407260
YDOT = -10431
014213 feet/sec YDOT = -3179
373132 meter/sec
ZDOT = 12512
986223 ZDOT = 3813
958201
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 13283
81927025
00016717 00000-0 10270-3 0 9165
2 25544 51
6487 255
3476 0002406 296
6541 63
4363 15
49501232 12640
Satellite: ISS
Catalog Number: 25544
Epoch time: 13283
81927025 = yrday
fracday
Element set: 916
Inclination: 51
6487 deg
RA of node: 255
3476 deg
Eccentricity:
0002406
Arg of perigee: 296
6541 deg
Mean anomaly: 63
4363 deg
Mean motion: 15
49501232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1264
Checksum: 309
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