[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 3rd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3211)
---------------------------------------
Vector Time (GMT): 2013/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1666761
04 A = 6787818
66 meter
Y = -3946560
10 meter E =
0012849
Z = 5261404
21 I = 51
56072
XDOT = 7360
172303 Wp = 27
10272
YDOT = 1973
866722 meter/sec RA = 189
99888 deg
ZDOT = -839
033863 TA = 70
99897
MA = 70
85979
Ha = 229
357 n
mi
Hp = 218
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5468376
11 X = 1685209
91
Y = -12948031
84 feet Y = -3927818
53 meter
Z = 17261824
85 Z = 5269545
76
XDOT = 24147
546926 XDOT = 7341
628882
YDOT = 6475
940690 feet/sec YDOT = 2056
069186 meter/sec
ZDOT = -2752
735771 ZDOT = -803
323626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10052674
11 X = -3064055
07
Y = -9762522
74 feet Y = -2975616
93 meter
Z = 17296304
69 Z = 5271913
67
XDOT = 14227
442378 XDOT = 4336
524437
YDOT = -19333
224656 feet/sec YDOT = -5892
766875 meter/sec
ZDOT = -2603
866254 ZDOT = -793
658434
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 13151
54701579
00016717 00000-0 10270-3 0 9006
2 25544 51
6467 190
8608 0010353 16
6734 343
4755 15
50610454 32122
Satellite: ISS
Catalog Number: 25544
Epoch time: 13151
54701579 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 190
8608 deg
Eccentricity:
0010353
Arg of perigee: 16
6734 deg
Mean anomaly: 343
4755 deg
Mean motion: 15
50610454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 292
Coasting Arc #2 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2013/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1963295
67 A = 6788306
02 meter
Y = 3946409
98 meter E =
0018664
Z = -5176026
98 I = 51
59356
XDOT = -7303
954696 Wp = 67
51574
YDOT = -1777
979471 meter/sec RA = 185
03241 deg
ZDOT = 1425
916956 TA = 216
17907
MA = 216
30546
Ha = 229
544 n
mi
Hp = 218
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6441258
75 X = -1982135
48
Y = 12947539
31 feet Y = 3924350
15 meter
Z = -16981715
81 Z = -5185610
07
XDOT = -23963
105958 XDOT = -7290
456854
YDOT = -5833
265981 feet/sec YDOT = -1859
581517 meter/sec
ZDOT = 4678
205237 ZDOT = 1390
467478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9874499
79 X = 3009747
53
Y = 10499790
90 feet Y = 3200336
27 meter
Z = -17022218
00 Z = -5188372
05
XDOT = -13163
969593 XDOT = -4012
377932
YDOT = 19665
821273 feet/sec YDOT = 5994
142324 meter/sec
ZDOT = 4530
386276 ZDOT = 1380
861737
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 13152
51374457
00016717 00000-0 10270-3 0 9016
2 25544 51
6478 186
0673 0010424 19
9831 340
1727 15
50588890 32273
Satellite: ISS
Catalog Number: 25544
Epoch time: 13152
51374457 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 186
0673 deg
Eccentricity:
0010424
Arg of perigee: 19
9831 deg
Mean anomaly: 340
1727 deg
Mean motion: 15
50588890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 313
Coasting Arc #3 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2013/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2314516
79 A = 6788847
14 meter
Y = -3958369
25 meter E =
0015798
Z = 5002201
81 I = 51
62528
XDOT = 7210
159773 Wp = 36
06718
YDOT = 1621
658156 meter/sec RA = 180
06777 deg
ZDOT = -2037
106960 TA = 73
83345
MA = 73
65964
Ha = 229
542 n
mi
Hp = 217
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7593559
03 X = 2334308
55
Y = -12986775
76 feet Y = -3932376
52 meter
Z = 16411423
27 Z = 5013493
45
XDOT = 23655
379834 XDOT = 7201
385966
YDOT = 5320
400774 feet/sec YDOT = 1702
237785 meter/sec
ZDOT = -6683
421785 ZDOT = -2002
101543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9701123
31 X = -2956902
39
Y = -11429812
58 feet Y = -3483806
87 meter
Z = 16459067
04 Z = 5016723
64
XDOT = 12160
892201 XDOT = 3706
639943
YDOT = -19809
899492 feet/sec YDOT = -6038
057365 meter/sec
ZDOT = -6537
424984 ZDOT = -1992
607135
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 13153
54491158
00016717 00000-0 10270-3 0 9029
2 25544 51
6466 180
9540 0010498 24
2883 335
8761 15
50640297 32430
Satellite: ISS
Catalog Number: 25544
Epoch time: 13153
54491158 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 180
9540 deg
Eccentricity:
0010498
Arg of perigee: 24
2883 deg
Mean anomaly: 335
8761 deg
Mean motion: 15
50640297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 313
Coasting Arc #4 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2013/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2595517
93 A = 6789741
88 meter
Y = 4040940
67 meter E =
0016787
Z = -4810762
52 I = 51
65961
XDOT = -7051
107880 Wp = 70
21459
YDOT = -1455
739730 meter/sec RA = 175
10683 deg
ZDOT = 2594
369346 TA = 225
32500
MA = 225
46191
Ha = 229
702 n
mi
Hp = 217
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8515478
78 X = -2617142
04
Y = 13257679
35 feet Y = 4011795
40 meter
Z = -15783341
59 Z = -4823423
68
XDOT = -23133
556038 XDOT = -7046
908319
YDOT = -4776
048984 feet/sec YDOT = -1534
566379 meter/sec
ZDOT = 8511
710454 ZDOT = 2560
125385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9855977
97 X = 3004102
09
Y = 12225024
61 feet Y = 3726187
50 meter
Z = -15836722
64 Z = -4827033
06
XDOT = -11068
584374 XDOT = -3373
704517
YDOT = 19710
209344 feet/sec YDOT = 6007
671808 meter/sec
ZDOT = 8368
860626 ZDOT = 2550
828719
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 13154
51162350
00016717 00000-0 10270-3 0 9037
2 25544 51
6475 176
1609 0010542 27
3052 332
8651 15
50616013 32585
Satellite: ISS
Catalog Number: 25544
Epoch time: 13154
51162350 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 176
1609 deg
Eccentricity:
0010542
Arg of perigee: 27
3052 deg
Mean anomaly: 332
8651 deg
Mean motion: 15
50616013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 276
Coasting Arc #5 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2013/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2919891
69 A = 6790688
56 meter
Y = -4133456
33 meter E =
0018427
Z = 4522721
29 I = 51
69207
XDOT = 6848
641779 Wp = 47
90812
YDOT = 1350
072321 meter/sec RA = 170
14721 deg
ZDOT = -3167
281912 TA = 73
96711
MA = 73
76424
Ha = 229
689 n
mi
Hp = 217
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9579697
13 X = 2943925
42
Y = -13561208
44 feet Y = -4100670
29 meter
Z = 14838324
43 Z = 4536964
06
XDOT = 22469
297175 XDOT = 6848
421972
YDOT = 4429
371131 feet/sec YDOT = 1426
657208 meter/sec
ZDOT = -10391
344855 ZDOT = -3134
011789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10028258
83 X = -3056613
29
Y = -13165354
16 feet Y = -4012799
95 meter
Z = 14898332
73 Z = 4541011
82
XDOT = 10117
807302 XDOT = 3083
907666
YDOT = -19384
285187 feet/sec YDOT = -5908
330125 meter/sec
ZDOT = -10252
536409 ZDOT = -3124
973097
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 13155
54277268
00016717 00000-0 10270-3 0 9047
2 25544 51
6458 171
0469 0010604 31
3532 328
8249 15
50670085 32746
Satellite: ISS
Catalog Number: 25544
Epoch time: 13155
54277268 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 171
0469 deg
Eccentricity:
0010604
Arg of perigee: 31
3532 deg
Mean anomaly: 328
8249 deg
Mean motion: 15
50670085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 307
Coasting Arc #6 (Orbit 3288)
---------------------------------------
Vector Time (GMT): 2013/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3153297
36 A = 6791863
12 meter
Y = 4285363
88 meter E =
0014903
Z = -4229498
38 I = 51
72614
XDOT = -6600
672254 Wp = 66
73412
YDOT = -1250
394782 meter/sec RA = 165
19213 deg
ZDOT = 3670
233087 TA = 240
83176
MA = 240
98096
Ha = 229
833 n
mi
Hp = 217
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10345463
78 X = -3180436
82
Y = 14059592
77 feet Y = 4249950
42 meter
Z = -13876307
00 Z = -4244882
49
XDOT = -21655
748864 XDOT = -6604
028730
YDOT = -4102
345084 feet/sec YDOT = -1324
226821 meter/sec
ZDOT = 12041
447135 ZDOT = 3638
158886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10508336
55 X = 3202940
98
Y = 13873459
44 feet Y = 4228630
44 meter
Z = -13941113
72 Z = -4249251
46
XDOT = -9173
874773 XDOT = -2796
197031
YDOT = 18861
779369 feet/sec YDOT = 5749
070352 meter/sec
ZDOT = 11907
608238 ZDOT = 3629
438991
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 13156
50946760
00016717 00000-0 10270-3 0 9055
2 25544 51
6461 166
2539 0010641 34
4697 325
7142 15
50643162 32891
Satellite: ISS
Catalog Number: 25544
Epoch time: 13156
50946760 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 166
2539 deg
Eccentricity:
0010641
Arg of perigee: 34
4697 deg
Mean anomaly: 325
7142 deg
Mean motion: 15
50643162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 310
Coasting Arc #7 (Orbit 3304)
---------------------------------------
Vector Time (GMT): 2013/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3418855
16 A = 6793042
76 meter
Y = -4438828
90 meter E =
0020384
Z = 3833867
05 I = 51
75856
XDOT = 6308
814440 Wp = 60
95861
YDOT = 1229
957818 meter/sec RA = 160
23806 deg
ZDOT = -4175
403385 TA = 73
06842
MA = 72
84507
Ha = 229
806 n
mi
Hp = 217
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11216716
41 X = 3449612
88
Y = -14563086
93 feet Y = -4400425
60 meter
Z = 12578303
98 Z = 3850549
92
XDOT = 20698
210106 XDOT = 6314
875133
YDOT = 4035
294679 feet/sec YDOT = 1300
541359 meter/sec
ZDOT = -13698
830003 ZDOT = -4144
740466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10991410
62 X = -3350181
96
Y = -14673600
11 feet Y = -4472513
31 meter
Z = 12648569
54 Z = 3855283
99
XDOT = 8454
576952 XDOT = 2576
955055
YDOT = -18105
398771 feet/sec YDOT = -5518
525546 meter/sec
ZDOT = -13570
870299 ZDOT = -4136
401267
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 13157
54059854
00016717 00000-0 10270-3 0 9060
2 25544 51
6447 161
1393 0010672 37
9889 322
2013 15
50698991 33050
Satellite: ISS
Catalog Number: 25544
Epoch time: 13157
54059854 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 161
1393 deg
Eccentricity:
0010672
Arg of perigee: 37
9889 deg
Mean anomaly: 322
2013 deg
Mean motion: 15
50698991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3305
Checksum: 324
Coasting Arc #8 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2013/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3578881
68 A = 6794303
27 meter
Y = 4634875
25 meter E =
0014413
Z = -3448168
61 I = 51
79106
XDOT = -5998
496671 Wp = 57
53397
YDOT = -1225
618726 meter/sec RA = 155
28881 deg
ZDOT = 4600
022390 TA = 262
24350
MA = 262
40717
Ha = 229
941 n
mi
Hp = 216
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11741737
79 X = -3613693
41
Y = 15206283
62 feet Y = 4594659
76 meter
Z = -11312889
14 Z = -3465638
62
XDOT = -19680
107189 XDOT = -6006
691614
YDOT = -4021
058812 feet/sec YDOT = -1292
744139 meter/sec
ZDOT = 15091
936976 ZDOT = 4570
861845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11728431
12 X = 3574825
81
Y = 15161557
63 feet Y = 4621242
77 meter
Z = -11386483
31 Z = -3470600
11
XDOT = -7821
200507 XDOT = -2383
901915
YDOT = 17240
226188 feet/sec YDOT = 5254
820942 meter/sec
ZDOT = 14970
239640 ZDOT = 4562
929042
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 13158
50727636
00016717 00000-0 10270-3 0 9078
2 25544 51
6447 156
3461 0010729 41
6005 318
5960 15
50673195 33202
Satellite: ISS
Catalog Number: 25544
Epoch time: 13158
50727636 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 156
3461 deg
Eccentricity:
0010729
Arg of perigee: 41
6005 deg
Mean anomaly: 318
5960 deg
Mean motion: 15
50673195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 304
Coasting Arc #9 (Orbit 3335)
---------------------------------------
Vector Time (GMT): 2013/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3762205
02 A = 6795491
38 meter
Y = -4818422
27 meter E =
0021410
Z = 2957464
11 I = 51
82230
XDOT = 5649
587545 Wp = 74
13346
YDOT = 1314
920253 meter/sec RA = 150
34068 deg
ZDOT = -5008
691741 TA = 72
22483
MA = 71
99132
Ha = 229
910 n
mi
Hp = 216
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12343192
31 X = 3801439
36
Y = -15808472
02 feet Y = -4776131
97 meter
Z = 9702966
23 Z = 2975835
32
XDOT = 18535
392207 XDOT = 5658
794991
YDOT = 4314
042825 feet/sec YDOT = 1378
149700 meter/sec
ZDOT = -16432
715686 ZDOT = -4981
223777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12426832
35 X = -3787698
50
Y = -15694840
75 feet Y = -4783787
46 meter
Z = 9780365
49 Z = 2981055
40
XDOT = 7483
477860 XDOT = 2280
964052
YDOT = -16166
726414 feet/sec YDOT = -4927
618211 meter/sec
ZDOT = -16318
088734 ZDOT = -4973
753446
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 13159
53838880
00016717 00000-0 10270-3 0 9087
2 25544 51
6441 151
2312 0010728 44
5372 315
6639 15
50725990 33362
Satellite: ISS
Catalog Number: 25544
Epoch time: 13159
53838880 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 151
2312 deg
Eccentricity:
0010728
Arg of perigee: 44
5372 deg
Mean anomaly: 315
6639 deg
Mean motion: 15
50725990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3336
Checksum: 313
Coasting Arc #10 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2013/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3833634
74 A = 6796603
52 meter
Y = 5024522
67 meter E =
0016073
Z = -2493661
36 I = 51
85204
XDOT = -5312
810011 Wp = 49
47049
YDOT = -1423
241592 meter/sec RA = 145
39706 deg
ZDOT = 5332
658373 TA = 282
70860
MA = 282
88822
Ha = 230
019 n
mi
Hp = 216
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12577541
79 X = -3877421
52
Y = 16484654
42 feet Y = 4981408
08 meter
Z = -8181303
67 Z = -2512390
53
XDOT = -17430
479038 XDOT = -5322
404889
YDOT = -4669
427796 feet/sec YDOT = -1482
707207 meter/sec
ZDOT = 17495
598335 ZDOT = 5306
825576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13300490
75 X = 4053989
58
Y = 15866237
12 feet Y = 4836029
07 meter
Z = -8260241
16 Z = -2517721
51
XDOT = -7279
268476 XDOT = -2218
721031
YDOT = 15099
181086 feet/sec YDOT = 4602
230395 meter/sec
ZDOT = 17387
806175 ZDOT = 5299
803322
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 13160
50504919
00016717 00000-0 10270-3 0 9090
2 25544 51
6440 146
4379 0010792 48
7348 311
4731 15
50709205 33515
Satellite: ISS
Catalog Number: 25544
Epoch time: 13160
50504919 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 146
4379 deg
Eccentricity:
0010792
Arg of perigee: 48
7348 deg
Mean anomaly: 311
4731 deg
Mean motion: 15
50709205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 299
Coasting Arc #11 (Orbit 3366)
---------------------------------------
Vector Time (GMT): 2013/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3923886
80 A = 6797568
93 meter
Y = -5199948
21 meter E =
0021313
Z = 1926336
56 I = 51
88054
XDOT = 4947
920656 Wp = 86
44377
YDOT = 1631
922069 meter/sec RA = 140
45468 deg
ZDOT = -5618
683739 TA = 72
42882
MA = 72
19611
Ha = 230
003 n
mi
Hp = 216
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12873644
37 X = 3972384
48
Y = -17060197
55 feet Y = -5155797
95 meter
Z = 6320001
84 Z = 1945515
55
XDOT = 16233
335484 XDOT = 4956
598502
YDOT = 5354
075030 feet/sec YDOT = 1687
302161 meter/sec
ZDOT = -18434
001769 ZDOT = -5594
625825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14071993
00 X = -4289143
47
Y = -16054018
82 feet Y = -4893264
94 meter
Z = 6400857
42 Z = 1950981
34
XDOT = 7414
192419 XDOT = 2259
845849
YDOT = -13879
464814 feet/sec YDOT = -4230
460875 meter/sec
ZDOT = -18333
643873 ZDOT = -5588
094652
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 13161
53614295
00016717 00000-0 10270-3 0 9105
2 25544 51
6443 141
3230 0010769 51
2964 308
9148 15
50748843 33676
Satellite: ISS
Catalog Number: 25544
Epoch time: 13161
53614295 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 141
3230 deg
Eccentricity:
0010769
Arg of perigee: 51
2964 deg
Mean anomaly: 308
9148 deg
Mean motion: 15
50748843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3367
Checksum: 305
Coasting Arc #12 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2013/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3905033
62 A = 6798303
63 meter
Y = 5377576
52 meter E =
0019055
Z = -1403603
63 I = 51
90611
XDOT = -4624
953618 Wp = 48
13572
YDOT = -1855
256455 meter/sec RA = 135
51608 deg
ZDOT = 5822
440741 TA = 296
64181
MA = 296
83685
Ha = 230
056 n
mi
Hp = 216
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12811790
10 X = -3958058
29
Y = 17642967
59 feet Y = 5333611
68 meter
Z = -4604998
79 Z = -1422701
99
XDOT = -15173
732342 XDOT = -4632
147823
YDOT = -6086
799393 feet/sec YDOT = -1907
016615 meter/sec
ZDOT = 19102
495870 ZDOT = 5799
955417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14928219
17 X = 4550121
20
Y = 15868715
60 feet Y = 4836784
51 meter
Z = -4685554
64 Z = -1428157
05
XDOT = -7691
476527 XDOT = -2344
362045
YDOT = 12788
243270 feet/sec YDOT = 3897
856549 meter/sec
ZDOT = 19008
731309 ZDOT = 5793
861303
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 13162
50278527
00016717 00000-0 10270-3 0 9118
2 25544 51
6444 136
5298 0010794 55
7511 304
4661 15
50749494 33823
Satellite: ISS
Catalog Number: 25544
Epoch time: 13162
50278527 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 136
5298 deg
Eccentricity:
0010794
Arg of perigee: 55
7511 deg
Mean anomaly: 304
4661 deg
Mean motion: 15
50749494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 315
Coasting Arc #13 (Orbit 3397)
---------------------------------------
Vector Time (GMT): 2013/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3906327
84 A = 6798838
41 meter
Y = -5504741
22 meter E =
0020008
Z = 783741
72 I = 51
93012
XDOT = 4287
708672 Wp = 96
63109
YDOT = 2175
249474 meter/sec RA = 130
57857 deg
ZDOT = -5964
311347 TA = 74
94456
MA = 74
72324
Ha = 230
070 n
mi
Hp = 216
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12816036
21 X = 3963785
52
Y = -18060174
61 feet Y = -5460737
03 meter
Z = 2571331
10 Z = 802857
15
XDOT = 14067
285669 XDOT = 4292
038832
YDOT = 7136
645256 feet/sec YDOT = 2223
222282 meter/sec
ZDOT = -19567
950614 ZDOT = -5943
471302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15607327
19 X = -4757113
33
Y = -15697475
35 feet Y = -4784590
49 meter
Z = 2651987
99 Z = 808325
94
XDOT = 8309
770108 XDOT = 2532
817929
YDOT = -11622
190238 feet/sec YDOT = -3542
443585 meter/sec
ZDOT = -19481
099001 ZDOT = -5937
838976
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 13163
53385997
00016717 00000-0 10270-3 0 9123
2 25544 51
6452 131
4151 0010766 58
2798 301
9401 15
50768372 33985
Satellite: ISS
Catalog Number: 25544
Epoch time: 13163
53385997 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 131
4151 deg
Eccentricity:
0010766
Arg of perigee: 58
2798 deg
Mean anomaly: 301
9401 deg
Mean motion: 15
50768372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3398
Checksum: 322
Coasting Arc #14 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2013/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3810055
94 A = 6799038
90 meter
Y = 5616357
59 meter E =
0022010
Z = -225667
56 I = 51
95011
XDOT = -4017
261362 Wp = 52
90478
YDOT = -2499
634464 meter/sec RA = 125
64371 deg
ZDOT = 6032
152512 TA = 304
67652
MA = 304
88374
Ha = 230
065 n
mi
Hp = 216
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12500183
54 X = -3871479
87
Y = 18426370
05 feet Y = 5573407
72 meter
Z = -740379
12 Z = -244325
00
XDOT = -13179
991345 XDOT = -4018
313816
YDOT = -8200
900473 feet/sec YDOT = -2544
564557 meter/sec
ZDOT = 19790
526615 ZDOT = 6012
634242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16283873
34 X = 4963324
59
Y = 15182171
43 feet Y = 4627525
85 meter
Z = -819147
56 Z = -249676
18
XDOT = -9041
683685 XDOT = -2755
905187
YDOT = 10694
477989 feet/sec YDOT = 3259
676891 meter/sec
ZDOT = 19709
238913 ZDOT = 6007
376021
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 13164
50048356
00016717 00000-0 10270-3 0 9137
2 25544 51
6452 126
6218 0010735 62
4972 297
7269 15
50785629 34138
Satellite: ISS
Catalog Number: 25544
Epoch time: 13164
50048356 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 126
6218 deg
Eccentricity:
0010735
Arg of perigee: 62
4972 deg
Mean anomaly: 297
7269 deg
Mean motion: 15
50785629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 319
Coasting Arc #15 (Orbit 3428)
---------------------------------------
Vector Time (GMT): 2013/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3741602
23 A = 6798975
08 meter
Y = -5659356
96 meter E =
0017731
Z = -417754
46 I = 51
96804
XDOT = 3746
714283 Wp = 102
66562
YDOT = 2904
951902 meter/sec RA = 120
70947 deg
ZDOT = -6014
977204 TA = 81
80956
MA = 81
60849
Ha = 230
092 n
mi
Hp = 216
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12275597
85 X = 3806637
63
Y = -18567444
10 feet Y = -5617152
33 meter
Z = -1370585
50 Z = -399420
70
XDOT = 12292
369696 XDOT = 3743
171086
YDOT = 9530
682093 feet/sec YDOT = 2946
830787 meter/sec
ZDOT = -19734
177177 ZDOT = -5996
784369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16711478
58 X = -5093658
67
Y = -14709623
53 feet Y = -4483493
25 meter
Z = -1293153
81 Z = -394153
28
XDOT = 10065
992557 XDOT = 3068
114531
YDOT = -9774
508101 feet/sec YDOT = -2979
270069 meter/sec
ZDOT = -19658
482559 ZDOT = -5991
905484
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 13165
53153855
00016717 00000-0 10270-3 0 9143
2 25544 51
6461 121
5074 0010716 65
2860 294
9405 15
50791619 34292
Satellite: ISS
Catalog Number: 25544
Epoch time: 13165
53153855 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 121
5074 deg
Eccentricity:
0010716
Arg of perigee: 65
2860 deg
Mean anomaly: 294
9405 deg
Mean motion: 15
50791619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3429
Checksum: 309
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