[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 9th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10440 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 ET - UTC (sec) : 66 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 1167)
---------------------------------------
Vector Time (GMT): 2012/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2214384
03 A = 6778036
55 meter
Y = 5186391
59 meter E =
0004935
Z = 3763641
18 I = 51
44232
XDOT = -6391
142810 Wp = 10
73524
YDOT = 338
182488 meter/sec RA = 325
25883 deg
ZDOT = -4220
681258 TA = 124
03917
MA = 123
99230
Ha = 217
285 n
mi
Hp = 214
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7265039
48 X = -2290498
00
Y = 17015720
44 feet Y = 5161203
11 meter
Z = 12347904
12 Z = 3752699
11
XDOT = -20968
316306 XDOT = -6373
945930
YDOT = 1109
522599 feet/sec YDOT = 266
809252 meter/sec
ZDOT = -13847
379455 ZDOT = -4251
687924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6821617
74 X = 2079229
09
Y = 17230845
51 feet Y = 5251961
71 meter
Z = 12302429
49 Z = 3749780
51
XDOT = -12745
162185 XDOT = -3884
725434
YDOT = 15036
718546 feet/sec YDOT = 4583
191813 meter/sec
ZDOT = -13974
791867 ZDOT = -4259
516561
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 12128
54011934
00016717 00000-0 10270-3 0 9008
2 25544 51
6387 325
6536 0011194 288
8185 71
1754 15
55961381 11683
Satellite: ISS
Catalog Number: 25544
Epoch time: 12128
54011934 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 325
6536 deg
Eccentricity:
0011194
Arg of perigee: 288
8185 deg
Mean anomaly: 71
1754 deg
Mean motion: 15
55961381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1168
Checksum: 315
Coasting Arc #2 (Orbit 1182)
---------------------------------------
Vector Time (GMT): 2012/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3964087
29 A = 6782667
19 meter
Y = -5184078
28 meter E =
0011416
Z = -1820028
88 I = 51
43212
XDOT = 4901
390623 Wp = 329
98794
YDOT = 1767
668549 meter/sec RA = 320
25266 deg
ZDOT = 5634
854070 TA = 9
91673
MA = 9
89422
Ha = 217
541 n
mi
Hp = 214
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13005535
74 X = 4030603
49
Y = -17008130
86 feet Y = -5139377
33 meter
Z = -5971223
36 Z = -1800610
16
XDOT = 16080
677898 XDOT = 4853
886706
YDOT = 5799
437498 feet/sec YDOT = 1822
212817 meter/sec
ZDOT = 18487
054037 ZDOT = 5658
549888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3144674
02 X = -958496
64
Y = -21201038
31 feet Y = -6462076
48 meter
Z = -5890923
83 Z = -1795553
58
XDOT = 13729
585568 XDOT = 4184
777681
YDOT = -7205
459620 feet/sec YDOT = -2196
224092 meter/sec
ZDOT = 18584
223304 ZDOT = 5664
471263
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 12129
50352481
00016717 00000-0 10270-3 0 9011
2 25544 51
6375 320
8357 0011044 292
0610 67
9371 15
55950829 11832
Satellite: ISS
Catalog Number: 25544
Epoch time: 12129
50352481 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 320
8357 deg
Eccentricity:
0011044
Arg of perigee: 292
0610 deg
Mean anomaly: 67
9371 deg
Mean motion: 15
55950829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1183
Checksum: 297
Coasting Arc #3 (Orbit 1198)
---------------------------------------
Vector Time (GMT): 2012/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5062439
73 A = 6783761
20 meter
Y = 4487403
25 meter E =
0004162
Z = -471405
40 I = 51
41401
XDOT = -2867
422936 Wp = 218
15266
YDOT = -3864
655091 meter/sec RA = 315
25861 deg
ZDOT = -5970
042225 TA = 326
94942
MA = 326
97542
Ha = 217
784 n
mi
Hp = 213
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16609054
24 X = -5109952
53
Y = 14722451
60 feet Y = 4430526
30 meter
Z = -1546605
65 Z = -496113
71
XDOT = -9407
555564 XDOT = -2794
993121
YDOT = -12679
314602 feet/sec YDOT = -3896
314882 meter/sec
ZDOT = -19586
752708 ZDOT = -5983
796557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -591193
67 X = -180195
83
Y = 22179629
63 feet Y = 6760351
11 meter
Z = -1648566
78 Z = -502483
15
XDOT = -13987
916043 XDOT = -4263
516810
YDOT = -1838
586481 feet/sec YDOT = -560
401159 meter/sec
ZDOT = -19642
872732 ZDOT = -5987
147609
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 12130
53114152
00016717 00000-0 10270-3 0 9028
2 25544 51
6378 315
6984 0011093 296
9698 63
0322 15
56007787 11993
Satellite: ISS
Catalog Number: 25544
Epoch time: 12130
53114152 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 315
6984 deg
Eccentricity:
0011093
Arg of perigee: 296
9698 deg
Mean anomaly: 63
0322 deg
Mean motion: 15
56007787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1199
Checksum: 315
Coasting Arc #4 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2012/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5409590
89 A = 6780734
71 meter
Y = -3071314
61 meter E =
0008834
Z = 2683466
55 I = 51
38237
XDOT = 637
104688 Wp = 24
22471
YDOT = 5636
342559 meter/sec RA = 310
25775 deg
ZDOT = 5168
497612 TA = 6
23635
MA = 6
22536
Ha = 217
815 n
mi
Hp = 213
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17748001
62 X = 5430497
18
Y = -10076491
51 feet Y = -3010704
53 meter
Z = 8804024
10 Z = 2709796
75
XDOT = 2090
238477 XDOT = 548
923111
YDOT = 18491
937529 feet/sec YDOT = 5642
973611 meter/sec
ZDOT = 16957
013164 ZDOT = 5171
378891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4390581
36 X = 1338249
20
Y = -19882859
54 feet Y = -6060295
59 meter
Z = 8912506
65 Z = 2716532
03
XDOT = 13601
331856 XDOT = 4145
685950
YDOT = 10606
829616 feet/sec YDOT = 3232
961667 meter/sec
ZDOT = 16968
290972 ZDOT = 5171
935088
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 12131
55874467
00016717 00000-0 10270-3 0 9034
2 25544 51
6371 310
5593 0010988 299
5275 60
4782 15
56007554 12150
Satellite: ISS
Catalog Number: 25544
Epoch time: 12131
55874467 = yrday
fracday
Element set: 903
Inclination: 51
6371 deg
RA of node: 310
5593 deg
Eccentricity:
0010988
Arg of perigee: 299
5275 deg
Mean anomaly: 60
4782 deg
Mean motion: 15
56007554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 318
Coasting Arc #5 (Orbit 1229)
---------------------------------------
Vector Time (GMT): 2012/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5059918
50 A = 6775548
89 meter
Y = 1097009
79 meter E =
0009291
Z = -4375551
82 I = 51
34675
XDOT = 1459
506508 Wp = 356
51761
YDOT = -6731
526823 meter/sec RA = 305
24078 deg
ZDOT = -3365
982253 TA = 239
22743
MA = 239
31894
Ha = 218
108 n
mi
Hp = 213
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16600782
47 X = -5050553
92
Y = 3599113
47 feet Y = 1040479
27 meter
Z = -14355484
97 Z = -4400109
93
XDOT = 4788
407178 XDOT = 1551
022556
YDOT = -22085
061755 feet/sec YDOT = -6714
693825 meter/sec
ZDOT = -11043
248861 ZDOT = -3358
670124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8150577
74 X = -2484296
10
Y = 14805319
53 feet Y = 4512661
39 meter
Z = -14456491
32 Z = -4406338
55
XDOT = -12363
148798 XDOT = -3768
287753
YDOT = -17589
376814 feet/sec YDOT = -5361
242053 meter/sec
ZDOT = -11012
546474 ZDOT = -3356
624165
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 12132
52210990
00016717 00000-0 10270-3 0 9048
2 25544 51
6374 305
7432 0010874 304
1714 55
8408 15
56035283 12306
Satellite: ISS
Catalog Number: 25544
Epoch time: 12132
52210990 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 305
7432 deg
Eccentricity:
0010874
Arg of perigee: 304
1714 deg
Mean anomaly: 55
8408 deg
Mean motion: 15
56035283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1230
Checksum: 278
Coasting Arc #6 (Orbit 1245)
---------------------------------------
Vector Time (GMT): 2012/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4130537
21 A = 6772161
41 meter
Y = 1226013
97 meter E =
0007559
Z = 5229022
04 I = 51
31778
XDOT = -3188
550510 Wp = 310
91978
YDOT = 6915
100676 meter/sec RA = 300
20309 deg
ZDOT = 903
098563 TA = 130
43590
MA = 130
36995
Ha = 218
332 n
mi
Hp = 213
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13551631
28 X = 4091119
21
Y = 4022355
54 feet Y = 1271983
58 meter
Z = 17155584
12 Z = 5248992
36
XDOT = -10461
123722 XDOT = -3270
026651
YDOT = 22687
338176 feet/sec YDOT = 6878
988736 meter/sec
ZDOT = 2962
921796 ZDOT = 887
411066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11744536
54 X = 3579734
74
Y = -7685963
25 feet Y = -2342681
60 meter
Z = 17237515
82 Z = 5253994
82
XDOT = 10027
906846 XDOT = 3056
506007
YDOT = 21780
234870 feet/sec YDOT = 6638
615588 meter/sec
ZDOT = 2897
799776 ZDOT = 883
249372
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 12133
54968597
00016717 00000-0 10270-3 0 9055
2 25544 51
6369 300
6042 0010897 308
0472 51
9698 15
56000801 12463
Satellite: ISS
Catalog Number: 25544
Epoch time: 12133
54968597 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 300
6042 deg
Eccentricity:
0010897
Arg of perigee: 308
0472 deg
Mean anomaly: 51
9698 deg
Mean motion: 15
56000801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1246
Checksum: 312
Coasting Arc #7 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2012/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2840411
99 A = 6772736
52 meter
Y = -3492148
46 meter E =
0006306
Z = -5063411
61 I = 51
30656
XDOT = 4374
787170 Wp = 49
43997
YDOT = -6056
938727 meter/sec RA = 295
16007 deg
ZDOT = 1728
699372 TA = 237
31610
MA = 237
37693
Ha = 218
390 n
mi
Hp = 213
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9318936
98 X = -2776553
95
Y = -11457179
98 feet Y = -3523554
52 meter
Z = -16612242
82 Z = -5077055
25
XDOT = 14352
976281 XDOT = 4433
794278
YDOT = -19871
846217 feet/sec YDOT = -6007
687268 meter/sec
ZDOT = 5671
585866 ZDOT = 1750
095152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14705355
02 X = -4482192
21
Y = -87209
95 feet Y = -26581
59 meter
Z = -16667966
26 Z = -5080396
12
XDOT = -6374
732911 XDOT = -1943
018591
YDOT = -22577
837776 feet/sec YDOT = -6881
724954 meter/sec
ZDOT = 5760
069690 ZDOT = 1755
669241
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 12134
51302274
00016717 00000-0 10270-3 0 9068
2 25544 51
6376 295
7876 0010814 311
1791 48
8430 15
56063532 12614
Satellite: ISS
Catalog Number: 25544
Epoch time: 12134
51302274 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 295
7876 deg
Eccentricity:
0010814
Arg of perigee: 311
1791 deg
Mean anomaly: 48
8430 deg
Mean motion: 15
56063532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 296
Coasting Arc #8 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2012/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1354769
56 A = 6777230
88 meter
Y = 5378636
97 meter E =
0010024
Z = 3899005
50 I = 51
30879
XDOT = -4984
304656 Wp = 19
12661
YDOT = 4194
091284 meter/sec RA = 290
12541 deg
ZDOT = -4041
564468 TA = 113
41504
MA = 113
30960
Ha = 218
676 n
mi
Hp = 212
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4444782
01 X = 1275583
23
Y = 17646446
74 feet Y = 5393344
01 meter
Z = 12792012
79 Z = 3905394
71
XDOT = -16352
705564 XDOT = -5011
200239
YDOT = 13760
142009 feet/sec YDOT = 4138
203396 meter/sec
ZDOT = -13259
725945 ZDOT = -4065
843426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16572673
61 X = 5051350
92
Y = 7472640
15 feet Y = 2277660
72 meter
Z = 12817757
19 Z = 3906852
39
XDOT = 1306
612211 XDOT = 398
255402
YDOT = 20087
192328 feet/sec YDOT = 6122
576222 meter/sec
ZDOT = -13359
872350 ZDOT = -4072
089092
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 12135
54056899
00016717 00000-0 10270-3 0 9072
2 25544 51
6368 290
6488 0010879 314
9261 45
1009 15
56063916 12777
Satellite: ISS
Catalog Number: 25544
Epoch time: 12135
54056899 = yrday
fracday
Element set: 907
Inclination: 51
6368 deg
RA of node: 290
6488 deg
Eccentricity:
0010879
Arg of perigee: 314
9261 deg
Mean anomaly: 45
1009 deg
Mean motion: 15
56063916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 333
Coasting Arc #9 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2012/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 115389
00 A = 6781947
89 meter
Y = -6478879
03 meter E =
0013722
Z = -1970126
23 I = 51
31681
XDOT = 5044
231042 Wp = 348
12947
YDOT = -1599
420424 meter/sec RA = 285
10955 deg
ZDOT = 5561
512973 TA = 349
99194
MA = 350
01924
Ha = 218
774 n
mi
Hp = 212
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 378572
84 X = 197399
10
Y = -21256164
81 feet Y = -6477130
10 meter
Z = -6463668
74 Z = -1969366
59
XDOT = 16549
314441 XDOT = 5034
724317
YDOT = -5247
442336 feet/sec YDOT = -1543
065967 meter/sec
ZDOT = 18246
433640 ZDOT = 5585
994766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16682548
74 X = -5084840
86
Y = -13179854
27 feet Y = -4017219
58 meter
Z = -6459944
44 Z = -1968991
06
XDOT = 4793
805538 XDOT = 1461
151928
YDOT = -15050
340245 feet/sec YDOT = -4587
343707 meter/sec
ZDOT = 18347
167009 ZDOT = 5592
216504
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 12136
50387982
00016717 00000-0 10270-3 0 9080
2 25544 51
6382 285
8317 0010876 318
8001 41
2331 15
56102670 12925
Satellite: ISS
Catalog Number: 25544
Epoch time: 12136
50387982 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 285
8317 deg
Eccentricity:
0010876
Arg of perigee: 318
8001 deg
Mean anomaly: 41
2331 deg
Mean motion: 15
56102670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 299
Coasting Arc #10 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2012/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1476186
59 A = 6783387
80 meter
Y = 6611039
51 meter E =
0001076
Z = -366188
89 I = 51
31448
XDOT = -4612
611585 Wp = 65
54001
YDOT = -1359
841180 meter/sec RA = 280
10621 deg
ZDOT = -5969
080288 TA = 118
42536
MA = 118
41451
Ha = 218
988 n
mi
Hp = 212
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4843131
87 X = -1548223
98
Y = 21689762
18 feet Y = 6594129
11 meter
Z = -1201407
12 Z = -373535
04
XDOT = -15133
240107 XDOT = -4568
065884
YDOT = -4461
421194 feet/sec YDOT = -1411
173032 meter/sec
ZDOT = -19583
596745 ZDOT = -5991
380301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14647245
90 X = 4464480
55
Y = 16711820
98 feet Y = 5093763
03 meter
Z = -1232199
62 Z = -375574
44
XDOT = -11249
409511 XDOT = -3428
820019
YDOT = 8412
142066 feet/sec YDOT = 2564
020902 meter/sec
ZDOT = -19675
091642 ZDOT = -5996
967932
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 12137
53139663
00016717 00000-0 10270-3 0 9096
2 25544 51
6374 280
6930 0011047 323
0255 37
0136 15
56151668 13085
Satellite: ISS
Catalog Number: 25544
Epoch time: 12137
53139663 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 280
6930 deg
Eccentricity:
0011047
Arg of perigee: 323
0255 deg
Mean anomaly: 37
0136 deg
Mean motion: 15
56151668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 295
Coasting Arc #11 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2012/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2619733
70 A = 6780405
53 meter
Y = -5663211
63 meter E =
0013951
Z = 2628832
23 I = 51
30186
XDOT = 3808
172708 Wp = 30
84071
YDOT = 4174
777890 meter/sec RA = 275
09984 deg
ZDOT = 5198
117331 TA = 358
99213
MA = 358
99493
Ha = 218
973 n
mi
Hp = 212
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8594926
82 X = 2670095
68
Y = -18580090
65 feet Y = -5633634
66 meter
Z = 8624777
64 Z = 2641681
09
XDOT = 12494
004946 XDOT = 3735
954750
YDOT = 13696
777853 feet/sec YDOT = 4216
959231 meter/sec
ZDOT = 17054
190720 ZDOT = 5216
442326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10254283
06 X = -3125505
48
Y = -17692365
36 feet Y = -5392632
96 meter
Z = 8678088
04 Z = 2645081
23
XDOT = 17045
417715 XDOT = 5195
443319
YDOT = -1476
739241 feet/sec YDOT = -450
110121 meter/sec
ZDOT = 17129
097352 ZDOT = 5220
948873
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 12138
55889899
00016717 00000-0 10270-3 0 9104
2 25544 51
6389 275
5545 0010917 326
2183 33
8274 15
56176869 13241
Satellite: ISS
Catalog Number: 25544
Epoch time: 12138
55889899 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 275
5545 deg
Eccentricity:
0010917
Arg of perigee: 326
2183 deg
Mean anomaly: 33
8274 deg
Mean motion: 15
56176869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 349
Coasting Arc #12 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2012/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3508418
59 A = 6775227
04 meter
Y = 3818934
40 meter E =
0013074
Z = -4370159
65 I = 51
28301
XDOT = -2690
298436 Wp = 12
75323
YDOT = -6336
231727 meter/sec RA = 270
07696 deg
ZDOT = -3366
614910 TA = 222
92657
MA = 223
02868
Ha = 219
284 n
mi
Hp = 211
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11510559
69 X = -3529632
30
Y = 12529312
34 feet Y = 3779582
73 meter
Z = -14337794
13 Z = -4387255
02
XDOT = -8826
438439 XDOT = -2602
890895
YDOT = -20788
161835 feet/sec YDOT = -6365
827394 meter/sec
ZDOT = -11045
324508 ZDOT = -3379
472549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3933555
12 X = 1198947
60
Y = 16491653
99 feet Y = 5026656
14 meter
Z = -14408382
46 Z = -4391674
97
XDOT = -20912
675372 XDOT = -6374
183453
YDOT = -4737
879205 feet/sec YDOT = -1444
105582 meter/sec
ZDOT = -11097
573867 ZDOT = -3382
540515
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 12139
52217047
00016717 00000-0 10270-3 0 9113
2 25544 51
6391 270
7379 0011070 330
2447 29
8076 15
56168020 13396
Satellite: ISS
Catalog Number: 25544
Epoch time: 12139
52217047 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 270
7379 deg
Eccentricity:
0011070
Arg of perigee: 330
2447 deg
Mean anomaly: 29
8076 deg
Mean motion: 15
56168020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 293
Coasting Arc #13 (Orbit 1354)
---------------------------------------
Vector Time (GMT): 2012/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4095837
20 A = 6771506
38 meter
Y = -1315126
58 meter E =
0008608
Z = 5230258
54 I = 51
27282
XDOT = 1336
137205 Wp = 346
20753
YDOT = 7506
483147 meter/sec RA = 265
03424 deg
ZDOT = 849
648385 TA = 95
68000
MA = 95
58184
Ha = 219
301 n
mi
Hp = 211
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13437786
08 X = 4084830
90
Y = -4314719
76 feet Y = -1269386
33 meter
Z = 17159640
89 Z = 5250129
48
XDOT = 4383
652246 XDOT = 1247
971398
YDOT = 24627
569381 feet/sec YDOT = 7520
931634 meter/sec
ZDOT = 2787
560317 ZDOT = 855
925808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3700932
56 X = 1128044
24
Y = -13515958
88 feet Y = -4119664
27 meter
Z = 17241407
44 Z = 5255180
99
XDOT = 22005
910899 XDOT = 6707
401642
YDOT = 9578
139557 feet/sec YDOT = 2919
416937 meter/sec
ZDOT = 2812
670793 ZDOT = 857
302058
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 12140
54964406
00016717 00000-0 10270-3 0 9126
2 25544 51
6399 265
5988 0011173 333
9787 26
0804 15
56219208 13554
Satellite: ISS
Catalog Number: 25544
Epoch time: 12140
54964406 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 265
5988 deg
Eccentricity:
0011173
Arg of perigee: 333
9787 deg
Mean anomaly: 26
0804 deg
Mean motion: 15
56219208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1355
Checksum: 324
Coasting Arc #14 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2012/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4334643
93 A = 6772320
52 meter
Y = -1333952
29 meter E =
0011272
Z = -5034993
72 I = 51
27963
XDOT = 176
054301 Wp = 50
20658
YDOT = -7443
472782 meter/sec RA = 259
98829 deg
ZDOT = 1830
301647 TA = 237
55522
MA = 237
66427
Ha = 219
460 n
mi
Hp = 211
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14221272
75 X = -4294945
94
Y = -4376483
90 feet Y = -1382202
54 meter
Z = -16519008
28 Z = -5055955
31
XDOT = 577
605973 XDOT = 250
384291
YDOT = -24420
842459 feet/sec YDOT = -7441
088599 meter/sec
ZDOT = 6004
926663 ZDOT = 1831
336793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11238010
72 X = -3425345
67
Y = 9605011
23 feet Y = 2927607
42 meter
Z = -16605020
89 Z = -5061210
37
XDOT = -19662
614642 XDOT = -5993
164943
YDOT = -12671
221631 feet/sec YDOT = -3862
188353 meter/sec
ZDOT = 6009
853903 ZDOT = 1831
803470
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 12141
51288888
00016717 00000-0 10270-3 0 9138
2 25544 51
6401 260
7829 0011136 338
2327 21
8352 15
56236943 13709
Satellite: ISS
Catalog Number: 25544
Epoch time: 12141
51288888 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 260
7829 deg
Eccentricity:
0011136
Arg of perigee: 338
2327 deg
Mean anomaly: 21
8352 deg
Mean motion: 15
56236943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1370
Checksum: 301
Coasting Arc #15 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2012/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4161245
66 A = 6777086
83 meter
Y = 3775203
79 meter E =
0014454
Z = 3792830
85 I = 51
30192
XDOT = -1793
672636 Wp = 33
36094
YDOT = 6181
758151 meter/sec RA = 254
95224 deg
ZDOT = -4165
669125 TA = 100
84009
MA = 100
67738
Ha = 219
721 n
mi
Hp = 211
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13652380
77 X = 4100296
27
Y = 12385839
22 feet Y = 3821396
23 meter
Z = 12443670
78 Z = 3812898
68
XDOT = -5884
752742 XDOT = -1842
428800
YDOT = 20281
358762 feet/sec YDOT = 6161
428024 meter/sec
ZDOT = -13666
893454 ZDOT = -4174
500621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17634336
58 X = 5374945
79
Y = -5174554
43 feet Y = -1577204
19 meter
Z = 12525798
02 Z = 3817863
24
XDOT = 13945
654132 XDOT = 4250
635380
YDOT = 14199
795279 feet/sec YDOT = 4328
097601 meter/sec
ZDOT = -13703
741989 ZDOT = -4176
900558
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 12142
54033599
00016717 00000-0 10270-3 0 9140
2 25544 51
6404 255
6441 0011126 342
2800 17
7965 15
56214005 13861
Satellite: ISS
Catalog Number: 25544
Epoch time: 12142
54033599 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 255
6441 deg
Eccentricity:
0011126
Arg of perigee: 342
2800 deg
Mean anomaly: 17
7965 deg
Mean motion: 15
56214005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1386
Checksum: 285
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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