[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 30th 2013
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ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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 3180)
---------------------------------------
Vector Time (GMT): 2013/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1045441
37 A = 6787739
69 meter
Y = -4105015
52 meter E =
0010027
Z = 5299667
44 I = 51
50050
XDOT = 7294
635647 Wp = 24
05188
YDOT = 2329
501071 meter/sec RA = 199
93777 deg
ZDOT = 374
124193 TA = 62
42412
MA = 62
32230
Ha = 229
115 n
mi
Hp = 218
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3429925
76 X = 1065522
49
Y = -13467898
68 feet Y = -4093212
98 meter
Z = 17387360
36 Z = 5304794
46
XDOT = 23932
531650 XDOT = 7266
227115
YDOT = 7642
720049 feet/sec YDOT = 2410
915408 meter/sec
ZDOT = 1227
441579 ZDOT = 409
492110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11004741
62 X = -3354245
25
Y = -8442857
93 feet Y = -2573383
10 meter
Z = 17409273
33 Z = 5306346
51
XDOT = 15978
165675 XDOT = 4870
144898
YDOT = -18050
601519 feet/sec YDOT = -5501
823343 meter/sec
ZDOT = 1374
802769 ZDOT = 419
039884
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 13149
54908605
00016717 00000-0 10270-3 0 9002
2 25544 51
6460 200
7661 0010127 8
6926 351
4398 15
50583599 31814
Satellite: ISS
Catalog Number: 25544
Epoch time: 13149
54908605 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 200
7661 deg
Eccentricity:
0010127
Arg of perigee: 8
6926 deg
Mean anomaly: 351
4398 deg
Mean motion: 15
50583599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3181
Checksum: 310
Coasting Arc #2 (Orbit 3195)
---------------------------------------
Vector Time (GMT): 2013/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1325946
30 A = 6787752
23 meter
Y = 4021050
15 meter E =
0019556
Z = -5319858
38 I = 51
52990
XDOT = -7340
734788 Wp = 60
91508
YDOT = -2143
057826 meter/sec RA = 194
96662 deg
ZDOT = 219
696094 TA = 211
12893
MA = 211
24493
Ha = 229
319 n
mi
Hp = 218
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4350217
53 X = -1344969
57
Y = 13192421
75 feet Y = 4006116
65 meter
Z = -17453603
59 Z = -5326345
59
XDOT = -24083
775551 XDOT = -7317
292296
YDOT = -7031
029612 feet/sec YDOT = -2225
015495 meter/sec
ZDOT = 720
787711 ZDOT = 184
092216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10539854
57 X = 3212547
67
Y = 8995127
90 feet Y = 2741714
99 meter
Z = -17481184
24 Z = -5328264
96
XDOT = -15109
377687 XDOT = -4605
338319
YDOT = 18753
471490 feet/sec YDOT = 5716
058110 meter/sec
ZDOT = 572
399412 ZDOT = 174
467341
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 13150
51582855
00016717 00000-0 10270-3 0 9017
2 25544 51
6464 195
9724 0010216 12
4288 347
7112 15
50568613 31964
Satellite: ISS
Catalog Number: 25544
Epoch time: 13150
51582855 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 195
9724 deg
Eccentricity:
0010216
Arg of perigee: 12
4288 deg
Mean anomaly: 347
7112 deg
Mean motion: 15
50568613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3196
Checksum: 305
Coasting Arc #3 (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 = 1672547
95 A = 6787782
54 meter
Y = -3945065
55 meter E =
0012793
Z = 5260655
26 I = 51
56004
XDOT = 7358
524587 Wp = 27
17019
YDOT = 1977
735484 meter/sec RA = 189
99729 deg
ZDOT = -844
439040 TA = 70
98334
MA = 70
84479
Ha = 229
312 n
mi
Hp = 218
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5487362
02 X = 1690983
31
Y = -12943128
45 feet Y = -3926259
34 meter
Z = 17259367
66 Z = 5268824
88
XDOT = 24142
141034 XDOT = 7339
964284
YDOT = 6488
633478 feet/sec YDOT = 2059
919428 meter/sec
ZDOT = -2770
469291 ZDOT = -808
736848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10041102
46 X = -3060528
03
Y = -9778370
99 feet Y = -2980447
48 meter
Z = 17293964
56 Z = 5271200
40
XDOT = 14236
126279 XDOT = 4339
171290
YDOT = -19324
460977 feet/sec YDOT = -5890
095706 meter/sec
ZDOT = -2621
633839 ZDOT = -799
073994
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
54700594
00016717 00000-0 10270-3 0 9024
2 25544 51
6460 190
8592 0010284 16
6850 343
4638 15
50623881 32127
Satellite: ISS
Catalog Number: 25544
Epoch time: 13151
54700594 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 190
8592 deg
Eccentricity:
0010284
Arg of perigee: 16
6850 deg
Mean anomaly: 343
4638 deg
Mean motion: 15
50623881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 295
Coasting Arc #4 (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 = -1975879
76 A = 6788260
21 meter
Y = 3943391
61 meter E =
0018594
Z = -5173440
55 I = 51
59291
XDOT = -7299
716873 Wp = 67
70503
YDOT = -1786
450526 meter/sec RA = 185
03058 deg
ZDOT = 1437
295857 TA = 216
10214
MA = 216
22782
Ha = 229
489 n
mi
Hp = 217
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6482545
16 X = -1994697
45
Y = 12937636
52 feet Y = 3921191
18 meter
Z = -16973230
15 Z = -5183084
71
XDOT = -23949
202340 XDOT = -7286
179897
YDOT = -5861
058157 feet/sec YDOT = -1868
004965 meter/sec
ZDOT = 4715
537589 ZDOT = 1401
867060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9850637
26 X = 3002474
24
Y = 10534968
59 feet Y = 3211058
43 meter
Z = -17013987
03 Z = -5185863
25
XDOT = -13182
574781 XDOT = -4018
048793
YDOT = 19644
956112 feet/sec YDOT = 5987
782623 meter/sec
ZDOT = 4567
806028 ZDOT = 1392
267277
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
51372434
00016717 00000-0 10270-3 0 9031
2 25544 51
6471 186
0656 0010353 20
0014 340
1541 15
50608215 32272
Satellite: ISS
Catalog Number: 25544
Epoch time: 13152
51372434 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 186
0656 deg
Eccentricity:
0010353
Arg of perigee: 20
0014 deg
Mean anomaly: 340
1541 deg
Mean motion: 15
50608215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 257
Coasting Arc #5 (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 = 2335718
85 A = 6788798
24 meter
Y = -3953632
90 meter E =
0015766
Z = 4996035
34 I = 51
62467
XDOT = 7201
463232 Wp = 36
23940
YDOT = 1636
413599 meter/sec RA = 180
06566 deg
ZDOT = -2056
044527 TA = 73
85321
MA = 73
67973
Ha = 229
476 n
mi
Hp = 217
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7663119
57 X = 2355486
02
Y = -12971236
55 feet Y = -3927403
22 meter
Z = 16391192
08 Z = 5007429
92
XDOT = 23626
847875 XDOT = 7192
617067
YDOT = 5368
811019 feet/sec YDOT = 1716
895574 meter/sec
ZDOT = -6745
552910 ZDOT = -2021
081532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9663010
83 X = -2945285
70
Y = -11490184
45 feet Y = -3502208
22 meter
Z = 16439265
18 Z = 5010688
03
XDOT = 12192
578109 XDOT = 3716
297808
YDOT = -19769
865297 feet/sec YDOT = -6025
854943 meter/sec
ZDOT = -6599
735087 ZDOT = -2011
599255
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
54487633
00016717 00000-0 10270-3 0 9044
2 25544 51
6458 180
9521 0010424 24
3169 335
8472 15
50665764 32432
Satellite: ISS
Catalog Number: 25544
Epoch time: 13153
54487633 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 180
9521 deg
Eccentricity:
0010424
Arg of perigee: 24
3169 deg
Mean anomaly: 335
8472 deg
Mean motion: 15
50665764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 310
Coasting Arc #6 (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 = -2627547
22 A = 6789697
73 meter
Y = 4034327
83 meter E =
0016660
Z = -4798726
46 I = 51
65908
XDOT = -7036
106587 Wp = 70
32938
YDOT = -1478
878072 meter/sec RA = 175
10440 deg
ZDOT = 2622
220543 TA = 225
50544
MA = 225
64174
Ha = 229
626 n
mi
Hp = 217
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8620561
75 X = -2649153
47
Y = 13235983
69 feet Y = 4004824
49 meter
Z = -15743853
22 Z = -4811543
18
XDOT = -23084
339196 XDOT = -7031
784697
YDOT = -4851
962180 feet/sec YDOT = -1557
536285 meter/sec
ZDOT = 8603
085771 ZDOT = 2588
049752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9801647
84 X = 2987542
26
Y = 12317826
53 feet Y = 3754473
53 meter
Z = -15797883
17 Z = -4815194
79
XDOT = -11118
107479 XDOT = -3388
799160
YDOT = 19643
743595 feet/sec YDOT = 5987
413048 meter/sec
ZDOT = 8460
544411 ZDOT = 2578
773936
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
51157042
00016717 00000-0 10270-3 0 9051
2 25544 51
6468 176
1588 0010466 27
3460 332
8240 15
50647399 32586
Satellite: ISS
Catalog Number: 25544
Epoch time: 13154
51157042 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 176
1588 deg
Eccentricity:
0010466
Arg of perigee: 27
3460 deg
Mean anomaly: 332
8240 deg
Mean motion: 15
50647399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 311
Coasting Arc #7 (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 = 2963863
79 A = 6790656
74 meter
Y = -4124717
91 meter E =
0018417
Z = 4502006
36 I = 51
69163
XDOT = 6824
534743 Wp = 48
32033
YDOT = 1383
862391 meter/sec RA = 170
14445 deg
ZDOT = -3204
549150 TA = 73
97352
MA = 73
77075
Ha = 229
602 n
mi
Hp = 217
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9723962
58 X = 2987897
18
Y = -13532539
07 feet Y = -4091440
14 meter
Z = 14770362
09 Z = 4516462
75
XDOT = 22390
205851 XDOT = 6824
119917
YDOT = 4540
230941 feet/sec YDOT = 1460
176611 meter/sec
ZDOT = -10513
612696 ZDOT = -3171
396609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9956911
26 X = -3034866
55
Y = -13294444
52 feet Y = -4052146
69 meter
Z = 14831261
62 Z = 4520568
54
XDOT = 10190
137103 XDOT = 3105
953789
YDOT = -19281
127409 feet/sec YDOT = -5876
887634 meter/sec
ZDOT = -10375
299606 ZDOT = -3162
391320
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
54269657
00016717 00000-0 10270-3 0 9062
2 25544 51
6451 171
0446 0010523 31
4016 328
7761 15
50707783 32746
Satellite: ISS
Catalog Number: 25544
Epoch time: 13155
54269657 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 171
0446 deg
Eccentricity:
0010523
Arg of perigee: 31
4016 deg
Mean anomaly: 328
7761 deg
Mean motion: 15
50707783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 302
Coasting Arc #8 (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 = -3210669
81 A = 6791848
78 meter
Y = 4274326
35 meter E =
0014738
Z = -4197053
71 I = 51
72583
XDOT = -6565
504815 Wp = 66
42614
YDOT = -1297
620505 meter/sec RA = 165
18902 deg
ZDOT = 3717
079143 TA = 241
70503
MA = 241
85381
Ha = 229
734 n
mi
Hp = 217
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10533693
61 X = -3237839
20
Y = 14023380
41 feet Y = 4238271
15 meter
Z = -13769861
24 Z = -4212716
60
XDOT = -21540
370129 XDOT = -6568
563386
YDOT = -4257
285122 feet/sec YDOT = -1371
057619 meter/sec
ZDOT = 12195
141546 ZDOT = 3685
176503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10419270
04 X = 3175793
51
Y = 14043915
51 feet Y = 4280585
45 meter
Z = -13835831
27 Z = -4217161
37
XDOT = -9276
856271 XDOT = -2827
585791
YDOT = 18714
078757 feet/sec YDOT = 5704
051205 meter/sec
ZDOT = 12062
025287 ZDOT = 3676
505308
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
50936611
00016717 00000-0 10270-3 0 9071
2 25544 51
6454 166
2513 0010556 34
5449 325
6386 15
50687046 32894
Satellite: ISS
Catalog Number: 25544
Epoch time: 13156
50936611 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 166
2513 deg
Eccentricity:
0010556
Arg of perigee: 34
5449 deg
Mean anomaly: 325
6386 deg
Mean motion: 15
50687046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 319
Coasting Arc #9 (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 = 3489714
02 A = 6793049
48 meter
Y = -4424642
33 meter E =
0020364
Z = 3786138
03 I = 51
75837
XDOT = 6259
145922 Wp = 61
70685
YDOT = 1293
648683 meter/sec RA = 160
23464 deg
ZDOT = -4230
535512 TA = 73
05320
MA = 72
83007
Ha = 229
696 n
mi
Hp = 217
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11449192
99 X = 3520539
70
Y = -14516543
09 feet Y = -4385446
26 meter
Z = 12421712
70 Z = 3803165
30
XDOT = 20535
255648 XDOT = 6264
765921
YDOT = 4244
254208 feet/sec YDOT = 1363
674341 meter/sec
ZDOT = -13879
709686 ZDOT = -4200
114944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10883253
96 X = -3317215
81
Y = -14885642
22 feet Y = -4537143
75 meter
Z = 12493415
43 Z = 3807993
02
XDOT = 8596
280503 XDOT = 2620
146297
YDOT = -17900
807795 feet/sec YDOT = -5456
166216 meter/sec
ZDOT = -13752
770620 ZDOT = -4191
844485
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
54046586
00016717 00000-0 10270-3 0 9080
2 25544 51
6440 161
1364 0010582 38
0636 322
1261 15
50749141 33051
Satellite: ISS
Catalog Number: 25544
Epoch time: 13157
54046586 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 161
1364 deg
Eccentricity:
0010582
Arg of perigee: 38
0636 deg
Mean anomaly: 322
1261 deg
Mean motion: 15
50749141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3305
Checksum: 285
Coasting Arc #10 (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 = -3663910
82 A = 6794327
08 meter
Y = 4616872
42 meter E =
0014346
Z = -3381793
62 I = 51
79099
XDOT = -5932
876495 Wp = 56
59019
YDOT = -1309
365957 meter/sec RA = 155
28509 deg
ZDOT = 4662
209148 TA = 264
11165
MA = 264
27520
Ha = 229
817 n
mi
Hp = 216
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12020704
81 X = -3698837
36
Y = 15147219
21 feet Y = 4575705
43 meter
Z = -11095123
41 Z = -3399676
97
XDOT = -19464
817897 XDOT = -5940
441925
YDOT = -4295
820069 feet/sec YDOT = -1375
754053 meter/sec
ZDOT = 15295
961773 ZDOT = 4633
368902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11599889
94 X = 3535646
45
Y = 15417558
94 feet Y = 4699271
97 meter
Z = -11170442
57 Z = -3404750
89
XDOT = -8013
654797 XDOT = -2442
561982
YDOT = 16972
618849 feet/sec YDOT = 5173
254225 meter/sec
ZDOT = 15175
613563 ZDOT = 4625
527014
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
50711055
00016717 00000-0 10270-3 0 9098
2 25544 51
6440 156
3430 0010633 41
7273 318
4687 15
50730257 33201
Satellite: ISS
Catalog Number: 25544
Epoch time: 13158
50711055 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 156
3430 deg
Eccentricity:
0010633
Arg of perigee: 41
7273 deg
Mean anomaly: 318
4687 deg
Mean motion: 15
50730257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 283
Coasting Arc #11 (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 = 3860356
35 A = 6795526
74 meter
Y = -4794469
13 meter E =
0021313
Z = 2868717
23 I = 51
82233
XDOT = 5564
474732 Wp = 75
24161
YDOT = 1422
267656 meter/sec RA = 150
33669 deg
ZDOT = -5074
135049 TA = 72
25373
MA = 72
02123
Ha = 229
777 n
mi
Hp = 216
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12665211
13 X = 3899746
67
Y = -15729885
58 feet Y = -4751080
35 meter
Z = 9411801
92 Z = 2887565
64
XDOT = 18256
150696 XDOT = 5572
806030
YDOT = 4666
232467 feet/sec YDOT = 1484
540428 meter/sec
ZDOT = -16647
424703 ZDOT = -5047
082672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12273396
15 X = -3740931
15
Y = -15990619
19 feet Y = -4873940
73 meter
Z = 9491192
44 Z = 2892915
46
XDOT = 7737
745850 XDOT = 2358
464935
YDOT = -15824
117539 feet/sec YDOT = -4823
191026 meter/sec
ZDOT = -16534
548429 ZDOT = -5039
730361
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
53818346
00016717 00000-0 10270-3 0 9105
2 25544 51
6433 151
2277 0010627 44
6507 315
5498 15
50788747 33363
Satellite: ISS
Catalog Number: 25544
Epoch time: 13159
53818346 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 151
2277 deg
Eccentricity:
0010627
Arg of perigee: 44
6507 deg
Mean anomaly: 315
5498 deg
Mean motion: 15
50788747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3336
Checksum: 322
Coasting Arc #12 (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 = -3945122
09 A = 6796632
32 meter
Y = 4992958
42 meter E =
0016246
Z = -2379410
19 I = 51
85211
XDOT = -5207
796597 Wp = 48
58179
YDOT = -1558
438317 meter/sec RA = 145
39281 deg
ZDOT = 5398
745215 TA = 284
97225
MA = 285
15203
Ha = 229
868 n
mi
Hp = 216
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12943313
93 X = -3989102
63
Y = 16381097
18 feet Y = 4948596
01 meter
Z = -7806463
88 Z = -2398681
44
XDOT = -17085
946842 XDOT = -5216
208515
YDOT = -5112
986604 feet/sec YDOT = -1616
723001 meter/sec
ZDOT = 17712
418684 ZDOT = 5373
425420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13118016
45 X = 3998371
42
Y = 16202253
37 feet Y = 4938446
83 meter
Z = -7887663
07 Z = -2404159
70
XDOT = -7611
291124 XDOT = -2319
921535
YDOT = 14679
596568 feet/sec YDOT = 4474
341034 meter/sec
ZDOT = 17606
788344 ZDOT = 5366
549087
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
50480278
00016717 00000-0 10270-3 0 9114
2 25544 51
6433 146
4341 0010679 48
9287 311
2785 15
50780167 33517
Satellite: ISS
Catalog Number: 25544
Epoch time: 13160
50480278 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 146
4341 deg
Eccentricity:
0010679
Arg of perigee: 48
9287 deg
Mean anomaly: 311
2785 deg
Mean motion: 15
50780167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 305
Coasting Arc #13 (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 = 4046738
41 A = 6797573
78 meter
Y = -5156719
89 meter E =
0021038
Z = 1783532
71 I = 51
88060
XDOT = 4820
015867 Wp = 87
80517
YDOT = 1798
216394 meter/sec RA = 140
45020 deg
ZDOT = -5678
592817 TA = 72
70034
MA = 72
47028
Ha = 229
847 n
mi
Hp = 216
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13276700
81 X = 4095437
26
Y = -16918372
33 feet Y = -5111194
67 meter
Z = 5851485
28 Z = 1803309
00
XDOT = 15813
700351 XDOT = 4827
134704
YDOT = 5899
660085 feet/sec YDOT = 1852
157465 meter/sec
ZDOT = -18630
553863 ZDOT = -5655
160017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13850125
86 X = -4221518
36
Y = -16422355
73 feet Y = -5005534
03 meter
Z = 5934832
15 Z = 1808936
84
XDOT = 7835
724408 XDOT = 2388
328799
YDOT = -13374
434483 feet/sec YDOT = -4076
527630 meter/sec
ZDOT = -18532
830929 ZDOT = -5648
806867
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
53584844
00016717 00000-0 10270-3 0 9123
2 25544 51
6436 141
3188 0010655 51
4641 308
7464 15
50824265 33670
Satellite: ISS
Catalog Number: 25544
Epoch time: 13161
53584844 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 141
3188 deg
Eccentricity:
0010655
Arg of perigee: 51
4641 deg
Mean anomaly: 308
7464 deg
Mean motion: 15
50824265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3367
Checksum: 307
Coasting Arc #14 (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 = -4039598
14 A = 6798252
65 meter
Y = 5319667
59 meter E =
0019425
Z = -1229920
51 I = 51
90604
XDOT = -4475
031718 Wp = 48
04595
YDOT = -2057
167342 meter/sec RA = 135
51134 deg
ZDOT = 5872
360994 TA = 298
65127
MA = 298
84647
Ha = 229
877 n
mi
Hp = 216
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13253274
73 X = -4092808
96
Y = 17452977
66 feet Y = 5274196
90 meter
Z = -4035172
28 Z = -1249673
03
XDOT = -14681
862593 XDOT = -4480
221754
YDOT = -6749
236687 feet/sec YDOT = -2107
239781 meter/sec
ZDOT = 19266
276228 ZDOT = 5850
608818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14658086
70 X = 4467784
82
Y = 16270130
74 feet Y = 4959135
85 meter
Z = -4118455
50 Z = -1255305
23
XDOT = -8220
668803 XDOT = -2505
659851
YDOT = 12201
431334 feet/sec YDOT = 3718
996271 meter/sec
ZDOT = 19175
603445 ZDOT = 5844
723930
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
50244151
00016717 00000-0 10270-3 0 9136
2 25544 51
6436 136
5251 0010661 56
0064 304
2098 15
50834372 33825
Satellite: ISS
Catalog Number: 25544
Epoch time: 13162
50244151 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 136
5251 deg
Eccentricity:
0010661
Arg of perigee: 56
0064 deg
Mean anomaly: 304
2098 deg
Mean motion: 15
50834372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 275
Coasting Arc #15 (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 = 4050248
49 A = 6798700
96 meter
Y = -5425847
92 meter E =
0019455
Z = 577896
21 I = 51
92983
XDOT = 4113
857765 Wp = 97
86527
YDOT = 2414
341758 meter/sec RA = 130
57352 deg
ZDOT = -5994
327356 TA = 75
93339
MA = 75
71721
Ha = 229
886 n
mi
Hp = 216
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13288216
83 X = 4107813
21
Y = -17801338
33 feet Y = -5380233
70 meter
Z = 1895984
93 Z = 597711
06
XDOT = 13496
908679 XDOT = 4115
673074
YDOT = 7921
068761 feet/sec YDOT = 2460
356399 meter/sec
ZDOT = -19666
428332 ZDOT = -5974
337940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15270957
34 X = -4654587
80
Y = -16122603
14 feet Y = -4914169
44 meter
Z = 1979555
92 Z = 603368
64
XDOT = 8954
297783 XDOT = 2729
269964
YDOT = -10951
311080 feet/sec YDOT = -3337
959617 meter/sec
ZDOT = -19583
165143 ZDOT = -5968
948735
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
53345930
00016717 00000-0 10270-3 0 9148
2 25544 51
6445 131
4100 0010632 58
5004 301
7185 15
50856971 33986
Satellite: ISS
Catalog Number: 25544
Epoch time: 13163
53345930 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 131
4100 deg
Eccentricity:
0010632
Arg of perigee: 58
5004 deg
Mean anomaly: 301
7185 deg
Mean motion: 15
50856971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3398
Checksum: 288
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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