[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6727 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 969)
---------------------------------------
Vector Time (GMT): 2011/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4223680
35 A = 6770927
57 meter
Y = -5225843
99 meter E =
0022241
Z = -779153
99 I = 51
36816
XDOT = 3331
144510 Wp = 55
60190
YDOT = -3557
452475 meter/sec RA = 236
37126 deg
ZDOT = 5935
695173 TA = 295
91879
MA = 296
14784
Ha = 215
698 n
mi
Hp = 200
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13857219
01 X = -4161145
15
Y = -17145157
46 feet Y = -5272726
08 meter
Z = -2556279
50 Z = -799520
36
XDOT = 10928
951805 XDOT = 3341
843322
YDOT = -11671
432003 feet/sec YDOT = -3520
141982 meter/sec
ZDOT = 19474
065527 ZDOT = 5951
903282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -493789
71 X = -150507
11
Y = 22029666
00 feet Y = 6714642
20 meter
Z = -2638843
57 Z = -804319
52
XDOT = -14184
096515 XDOT = -4323
312618
YDOT = 1971
966926 feet/sec YDOT = 601
055519 meter/sec
ZDOT = 19540
084925 ZDOT = 5955
817885
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 11224
50155384
00016717 00000-0 10270-3 0 9008
2 25544 51
6380 237
3103 0012640 68
2428 292
0072 15
60383971 9708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11224
50155384 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 237
3103 deg
Eccentricity:
0012640
Arg of perigee: 68
2428 deg
Mean anomaly: 292
0072 deg
Mean motion: 15
60383971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 280
Coasting Arc #2 (Orbit 985)
---------------------------------------
Vector Time (GMT): 2011/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1752585
18 A = 6767798
23 meter
Y = 5876253
75 meter E =
0016244
Z = -2880271
13 I = 51
37365
XDOT = -5738
871200 Wp = 83
35682
YDOT = -742
233229 meter/sec RA = 231
34894 deg
ZDOT = -5028
857594 TA = 129
61300
MA = 129
46949
Ha = 215
828 n
mi
Hp = 200
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5749951
37 X = 1700736
97
Y = 19279047
73 feet Y = 5895562
37 meter
Z = -9449708
43 Z = -2871883
15
XDOT = -18828
317586 XDOT = -5705
716258
YDOT = -2435
148390 feet/sec YDOT = -806
223337 meter/sec
ZDOT = -16498
876622 ZDOT = -5056
655756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7688871
77 X = 2343568
11
Y = -18608164
72 feet Y = -5671768
61 meter
Z = -9415841
36 Z = -2869948
45
XDOT = 11614
069113 XDOT = 3539
968266
YDOT = 13166
972610 feet/sec YDOT = 4013
293251 meter/sec
ZDOT = -16611
837636 ZDOT = -5063
288112
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 11225
52627991
00016717 00000-0 10270-3 0 9010
2 25544 51
6368 232
1520 0012654 71
4925 288
7605 15
60345038 9866
Satellite: ISS
Catalog Number: 25544
Epoch time: 11225
52627991 = yrday
fracday
Element set: 901
Inclination: 51
6368 deg
RA of node: 232
1520 deg
Eccentricity:
0012654
Arg of perigee: 71
4925 deg
Mean anomaly: 288
7605 deg
Mean motion: 15
60345038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 986
Checksum: 310
Coasting Arc #3 (Orbit 1001)
---------------------------------------
Vector Time (GMT): 2011/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1628181
99 A = 6760218
98 meter
Y = -4154123
27 meter E =
0016465
Z = 5064352
35 I = 51
36750
XDOT = 6069
602570 Wp = 88
97727
YDOT = 4418
762974 meter/sec RA = 226
28805 deg
ZDOT = 1668
801118 TA = 344
87112
MA = 344
92030
Ha = 215
772 n
mi
Hp = 200
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5341804
44 X = 1649912
10
Y = -13629013
35 feet Y = -4135794
42 meter
Z = 16615329
24 Z = 5072314
67
XDOT = 19913
394259 XDOT = 6011
633464
YDOT = 14497
253853 feet/sec YDOT = 4486
312861 meter/sec
ZDOT = 5475
069286 ZDOT = 1698
145684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12550529
19 X = -3825401
30
Y = 7462398
60 feet Y = 2274539
09 meter
Z = 16647848
79 Z = 5074264
31
XDOT = -6102
105030 XDOT = -1859
921613
YDOT = -22774
928483 feet/sec YDOT = -6941
798202 meter/sec
ZDOT = 5594
189299 ZDOT = 1705
108898
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 11226
55099979
00016717 00000-0 10270-3 0 9024
2 25544 51
6361 226
9946 0012673 74
8196 285
4360 15
60359071 10024
Satellite: ISS
Catalog Number: 25544
Epoch time: 11226
55099979 = yrday
fracday
Element set: 902
Inclination: 51
6361 deg
RA of node: 226
9946 deg
Eccentricity:
0012673
Arg of perigee: 74
8196 deg
Mean anomaly: 285
4360 deg
Mean motion: 15
60359071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1002
Checksum: 322
Coasting Arc #4 (Orbit 1016)
---------------------------------------
Vector Time (GMT): 2011/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4671422
27 A = 6761378
12 meter
Y = 1008030
66 meter E =
0023479
Z = -4803824
22 I = 51
39342
XDOT = -3899
746936 Wp = 92
60936
YDOT = -6092
737507 meter/sec RA = 221
20547 deg
ZDOT = 2523
403387 TA = 202
26768
MA = 202
36980
Ha = 215
828 n
mi
Hp = 200
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15326188
54 X = -4659011
47
Y = 3307187
22 feet Y = 955861
26 meter
Z = -15760578
14 Z = -4826487
37
XDOT = -12794
445329 XDOT = -3843
584893
YDOT = -19989
296284 feet/sec YDOT = -6136
032787 meter/sec
ZDOT = 8278
882502 ZDOT = 2504
595368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14126243
13 X = 4305678
91
Y = 6585222
50 feet Y = 2007175
82 meter
Z = -15852743
16 Z = -4831916
11
XDOT = -1391
558279 XDOT = -424
146964
YDOT = 22655
819766 feet/sec YDOT = 6905
493865 meter/sec
ZDOT = 8202
641053 ZDOT = 2500
164993
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 11227
51166874
00016717 00000-0 10270-3 0 9031
2 25544 51
6364 222
1602 0012627 77
9508 282
3062 15
60347214 10171
Satellite: ISS
Catalog Number: 25544
Epoch time: 11227
51166874 = yrday
fracday
Element set: 903
Inclination: 51
6364 deg
RA of node: 222
1602 deg
Eccentricity:
0012627
Arg of perigee: 77
9508 deg
Mean anomaly: 282
3062 deg
Mean motion: 15
60347214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1017
Checksum: 286
Coasting Arc #5 (Orbit 1032)
---------------------------------------
Vector Time (GMT): 2011/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5997202
99 A = 6769167
07 meter
Y = 2290921
47 meter E =
0025779
Z = 2118614
09 I = 51
44330
XDOT = -87
367602 Wp = 96
32709
YDOT = 5365
159116 meter/sec RA = 216
15697 deg
ZDOT = -5499
503286 TA = 60
04770
MA = 59
79200
Ha = 215
728 n
mi
Hp = 200
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19675862
84 X = 5960848
08
Y = 7516146
57 feet Y = 2357782
65 meter
Z = 6950833
63 Z = 2147659
61
XDOT = -286
639113 XDOT = -120
640245
YDOT = 17602
228072 feet/sec YDOT = 5363
995919 meter/sec
ZDOT = -18042
989784 ZDOT = -5500
008686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11387053
76 X = -3470773
98
Y = -17672370
75 feet Y = -5386538
60 meter
Z = 7068836
18 Z = 2154581
27
XDOT = 9264
155701 XDOT = 2823
714658
YDOT = -13257
838533 feet/sec YDOT = -4040
989185 meter/sec
ZDOT = -18045
228610 ZDOT = -5500
185680
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 11228
53637589
00016717 00000-0 10270-3 0 9041
2 25544 51
6362 217
0019 0012643 81
1272 279
1315 15
60405605 10339
Satellite: ISS
Catalog Number: 25544
Epoch time: 11228
53637589 = yrday
fracday
Element set: 904
Inclination: 51
6362 deg
RA of node: 217
0019 deg
Eccentricity:
0012643
Arg of perigee: 81
1272 deg
Mean anomaly: 279
1315 deg
Mean motion: 15
60405605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1033
Checksum: 284
Coasting Arc #6 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2011/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4891663
11 A = 6770065
08 meter
Y = -4400471
19 meter E =
0025944
Z = 1552534
65 I = 51
47158
XDOT = 4309
137964 Wp = 73
77255
YDOT = -2738
526798 meter/sec RA = 211
14497 deg
ZDOT = 5742
581750 TA = 303
29865
MA = 303
54687
Ha = 215
707 n
mi
Hp = 200
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16048763
49 X = -4849634
45
Y = -14437241
42 feet Y = -4454937
71 meter
Z = 5093617
62 Z = 1528873
51
XDOT = 14137
591746 XDOT = 4311
544403
YDOT = -8984
667974 feet/sec YDOT = -2690
325753 meter/sec
ZDOT = 18840
491306 ZDOT = 5763
521179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4791183
05 X = 1460352
59
Y = 21071558
29 feet Y = 6422610
97 meter
Z = 4997568
02 Z = 1523258
73
XDOT = -15100
586408 XDOT = -4602
658737
YDOT = -1112
573701 feet/sec YDOT = -339
112464 meter/sec
ZDOT = 18925
714991 ZDOT = 5768
557929
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 11229
56107574
00016717 00000-0 10270-3 0 9052
2 25544 51
6362 211
8457 0012560 86
1859 274
0732 15
60439065 10492
Satellite: ISS
Catalog Number: 25544
Epoch time: 11229
56107574 = yrday
fracday
Element set: 905
Inclination: 51
6362 deg
RA of node: 211
8457 deg
Eccentricity:
0012560
Arg of perigee: 86
1859 deg
Mean anomaly: 274
0732 deg
Mean motion: 15
60439065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 308
Coasting Arc #7 (Orbit 1063)
---------------------------------------
Vector Time (GMT): 2011/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1582088
67 A = 6762504
35 meter
Y = 4788563
72 meter E =
0022072
Z = -4526068
26 I = 51
47237
XDOT = -6965
947942 Wp = 80
72484
YDOT = -643
009943 meter/sec RA = 206
10775 deg
ZDOT = -3124
796334 TA = 157
90100
MA = 157
80570
Ha = 215
811 n
mi
Hp = 200
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5190579
64 X = 1550411
03
Y = 15710510
89 feet Y = 4806078
36 meter
Z = -14849305
33 Z = -4518459
63
XDOT = -22854
159915 XDOT = -6943
060417
YDOT = -2109
612673 feet/sec YDOT = -720
779537 meter/sec
ZDOT = -10251
956477 ZDOT = -3158
580940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4486898
48 X = 1367606
66
Y = -15954407
12 feet Y = -4862903
29 meter
Z = -14818528
05 Z = -4516687
35
XDOT = 16479
818546 XDOT = 5023
048693
YDOT = 14255
145758 feet/sec YDOT = 4344
968427 meter/sec
ZDOT = -10389
299630 ZDOT = -3166
658527
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 11230
52172927
00016717 00000-0 10270-3 0 9065
2 25544 51
6363 207
0096 0012649 88
6777 271
5828 15
60390418 10646
Satellite: ISS
Catalog Number: 25544
Epoch time: 11230
52172927 = yrday
fracday
Element set: 906
Inclination: 51
6363 deg
RA of node: 207
0096 deg
Eccentricity:
0012649
Arg of perigee: 88
6777 deg
Mean anomaly: 271
5828 deg
Mean motion: 15
60390418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1064
Checksum: 315
Coasting Arc #8 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2011/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2557035
09 A = 6759433
41 meter
Y = -3453612
63 meter E =
0015611
Z = 5204446
40 I = 51
49011
XDOT = 6782
917053 Wp = 84
94804
YDOT = 3478
300421 meter/sec RA = 201
03420 deg
ZDOT = -1020
422796 TA = 14
83713
MA = 14
79137
Ha = 215
669 n
mi
Hp = 200
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8389222
75 X = 2570181
96
Y = -11330750
10 feet Y = -3424944
71 meter
Z = 17074955
38 Z = 5216900
37
XDOT = 22253
664872 XDOT = 6748
474886
YDOT = 11411
746787 feet/sec YDOT = 3553
958547 meter/sec
ZDOT = -3347
843818 ZDOT = -987
555370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13146013
80 X = -4006905
01
Y = 4920513
54 feet Y = 1499772
53 meter
Z = 17125709
48 Z = 5219916
25
XDOT = -11992
603592 XDOT = -3655
345575
YDOT = -20807
691186 feet/sec YDOT = -6342
184274 meter/sec
ZDOT = -3214
312930 ZDOT = -979
722581
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 11231
54641741
00016717 00000-0 10270-3 0 9074
2 25544 51
6363 201
8528 0012529 92
0333 268
2258 15
60407503 10804
Satellite: ISS
Catalog Number: 25544
Epoch time: 11231
54641741 = yrday
fracday
Element set: 907
Inclination: 51
6363 deg
RA of node: 201
8528 deg
Eccentricity:
0012529
Arg of perigee: 92
0333 deg
Mean anomaly: 268
2258 deg
Mean motion: 15
60407503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 282
Coasting Arc #9 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2011/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5782636
79 A = 6766261
06 meter
Y = 1111308
86 meter E =
0017381
Z = -3349174
71 I = 51
54184
XDOT = -3627
117085 Wp = 93
91081
YDOT = -4888
508032 meter/sec RA = 195
97703 deg
ZDOT = 4660
158420 TA = 226
93853
MA = 227
08418
Ha = 215
732 n
mi
Hp = 200
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18971905
47 X = -5778364
30
Y = 3646026
44 feet Y = 1046667
76 meter
Z = -10988106
01 Z = -3377256
20
XDOT = -11899
990437 XDOT = -3594
821312
YDOT = -16038
412178 feet/sec YDOT = -4928
888075 meter/sec
ZDOT = 15289
233663 ZDOT = 4642
616472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17926328
74 X = 5463945
00
Y = 7024956
67 feet Y = 2141206
79 meter
Z = -11102337
66 Z = -3383992
52
XDOT = 2074
055104 XDOT = 632
171996
YDOT = 18657
074377 feet/sec YDOT = 5686
676270 meter/sec
ZDOT = 15218
059413 ZDOT = 4638
464509
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 11232
50705621
00016717 00000-0 10270-3 0 9080
2 25544 51
6364 197
0183 0012576 95
2476 265
0115 15
60403212 10959
Satellite: ISS
Catalog Number: 25544
Epoch time: 11232
50705621 = yrday
fracday
Element set: 908
Inclination: 51
6364 deg
RA of node: 197
0183 deg
Eccentricity:
0012576
Arg of perigee: 95
2476 deg
Mean anomaly: 265
0115 deg
Mean motion: 15
60403212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 283
Coasting Arc #10 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2011/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6598669
78 A = 6771046
96 meter
Y = 1469649
03 meter E =
0022975
Z = -236716
32 I = 51
58800
XDOT = -1227
821230 Wp = 117
36348
YDOT = 4618
119327 meter/sec RA = 190
96492 deg
ZDOT = -6012
313850 TA = 65
19620
MA = 64
95739
Ha = 215
688 n
mi
Hp = 200
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21649179
07 X = 6582895
37
Y = 4821683
17 feet Y = 1543351
19 meter
Z = -776628
36 Z = -204698
51
XDOT = -4028
284876 XDOT = -1250
164154
YDOT = 15151
310127 feet/sec YDOT = 4604
264207 meter/sec
ZDOT = -19725
439140 ZDOT = -6018
332794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15989577
45 X = -4873623
21
Y = -15377068
49 feet Y = -4686930
48 meter
Z = -646461
34 Z = -197041
42
XDOT = 10095
326645 XDOT = 3077
055562
YDOT = -9742
913080 feet/sec YDOT = -2969
639907 meter/sec
ZDOT = -19750
070798 ZDOT = -6019
821579
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 11233
53173089
00016717 00000-0 10270-3 0 9092
2 25544 51
6370 191
8604 0012490 98
9415 261
3155 15
60433792 11112
Satellite: ISS
Catalog Number: 25544
Epoch time: 11233
53173089 = yrday
fracday
Element set: 909
Inclination: 51
6370 deg
RA of node: 191
8604 deg
Eccentricity:
0012490
Arg of perigee: 98
9415 deg
Mean anomaly: 261
3155 deg
Mean motion: 15
60433792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 298
Coasting Arc #11 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2011/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4578997
73 A = 6765364
89 meter
Y = -3379152
88 meter E =
0024318
Z = 3641195
03 I = 51
59932
XDOT = 5627
438748 Wp = 99
07469
YDOT = -2891
536410 meter/sec RA = 185
95282 deg
ZDOT = 4364
776037 TA = 304
37488
MA = 304
60464
Ha = 215
644 n
mi
Hp = 200
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15022958
43 X = -4558559
18
Y = -11086459
58 feet Y = -3430243
82 meter
Z = 11946177
91 Z = 3619000
02
XDOT = 18462
725551 XDOT = 5638
151114
YDOT = -9486
668012 feet/sec YDOT = -2828
547146 meter/sec
ZDOT = 14320
131354 ZDOT = 4392
139864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7426829
90 X = 2263697
75
Y = 17192649
03 feet Y = 5240319
42 meter
Z = 11856013
23 Z = 3613712
83
XDOT = -19397
303597 XDOT = -5912
298136
YDOT = -1637
925358 feet/sec YDOT = -499
239649 meter/sec
ZDOT = 14431
528263 ZDOT = 4398
729815
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 11234
55639728
00016717 00000-0 10270-3 0 9104
2 25544 51
6373 186
7042 0012428 103
4125 256
8417 15
60472310 11271
Satellite: ISS
Catalog Number: 25544
Epoch time: 11234
55639728 = yrday
fracday
Element set: 910
Inclination: 51
6373 deg
RA of node: 186
7042 deg
Eccentricity:
0012428
Arg of perigee: 103
4125 deg
Mean anomaly: 256
8417 deg
Mean motion: 15
60472310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 289
Coasting Arc #12 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2011/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 514448
87 A = 6759143
03 meter
Y = 4201766
69 meter E =
0026702
Z = -5292147
02 I = 51
60862
XDOT = -7636
225496 Wp = 95
44208
YDOT = 290
051288 meter/sec RA = 180
89610 deg
ZDOT = -516
745351 TA = 169
64743
MA = 169
59233
Ha = 215
578 n
mi
Hp = 200
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1687824
38 X = 493133
66
Y = 13785323
79 feet Y = 4207400
53 meter
Z = -17362687
08 Z = -5289699
52
XDOT = -25053
233253 XDOT = -7636
391136
YDOT = 951
611838 feet/sec YDOT = 204
657441 meter/sec
ZDOT = -1695
358762 ZDOT = -553
842108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5195558
95 X = 1583606
37
Y = -12893054
55 feet Y = -3929803
03 meter
Z = -17352870
58 Z = -5289154
95
XDOT = 21353
030493 XDOT = 6508
403694
YDOT = 11068
775233 feet/sec YDOT = 3373
762691 meter/sec
ZDOT = -1846
276514 ZDOT = -562
745081
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 11235
51701756
00016717 00000-0 10270-3 0 9113
2 25544 51
6374 181
8683 0012371 106
2573 253
9945 15
60444043 11427
Satellite: ISS
Catalog Number: 25544
Epoch time: 11235
51701756 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 181
8683 deg
Eccentricity:
0012371
Arg of perigee: 106
2573 deg
Mean anomaly: 253
9945 deg
Mean motion: 15
60444043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 294
Coasting Arc #13 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2011/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3765136
72 A = 6763117
17 meter
Y = -3648040
81 meter E =
0021087
Z = 4253597
33 I = 51
65316
XDOT = 6373
414697 Wp = 93
79439
YDOT = 2380
326725 meter/sec RA = 175
83486 deg
ZDOT = -3586
169574 TA = 32
75248
MA = 32
62192
Ha = 215
449 n
mi
Hp = 200
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12352810
75 X = 3784987
09
Y = -11968637
82 feet Y = -3605825
87 meter
Z = 13955371
83 Z = 4271936
22
XDOT = 20910
153206 XDOT = 6363
744435
YDOT = 7809
470881 feet/sec YDOT = 2451
544163 meter/sec
ZDOT = -11765
648208 ZDOT = -3555
231414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16481866
98 X = -5023673
05
Y = 4700729
28 feet Y = 1432782
28 meter
Z = 14030104
52 Z = 4276375
86
XDOT = -14407
224751 XDOT = -4391
322104
YDOT = -15638
665802 feet/sec YDOT = -4766
665336 meter/sec
ZDOT = -11639
855297 ZDOT = -3547
827894
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 11236
54167102
00016717 00000-0 10270-3 0 9129
2 25544 51
6378 176
7114 0012371 109
8794 250
3696 15
60468245 11588
Satellite: ISS
Catalog Number: 25544
Epoch time: 11236
54167102 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 176
7114 deg
Eccentricity:
0012371
Arg of perigee: 109
8794 deg
Mean anomaly: 250
3696 deg
Mean motion: 15
60468245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1158
Checksum: 311
Coasting Arc #14 (Orbit 1172)
---------------------------------------
Vector Time (GMT): 2011/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6387500
18 A = 6770362
69 meter
Y = 1939830
79 meter E =
0017200
Z = -1134457
12 I = 51
70744
XDOT = -2345
437403 Wp = 82
24043
YDOT = -4327
458523 meter/sec RA = 170
81788 deg
ZDOT = 5884
776323 TA = 265
43406
MA = 265
63055
Ha = 215
456 n
mi
Hp = 200
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20956365
42 X = -6403206
13
Y = 6364274
24 feet Y = 1868314
06 meter
Z = -3721972
18 Z = -1165525
14
XDOT = -7695
004602 XDOT = -2325
459248
YDOT = -14197
698565 feet/sec YDOT = -4353
575023 meter/sec
ZDOT = 19307
008933 ZDOT = 5873
430859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21514906
09 X = 6557743
38
Y = 3978007
43 feet Y = 1212496
66 meter
Z = -3848452
69 Z = -1173008
38
XDOT = 695
731564 XDOT = 212
058981
YDOT = 14629
818109 feet/sec YDOT = 4459
168560 meter/sec
ZDOT = 19260
985996 ZDOT = 5870
748532
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 11237
50227693
00016717 00000-0 10270-3 0 9139
2 25544 51
6377 171
8765 0012322 113
3129 246
9325 15
60469122 11735
Satellite: ISS
Catalog Number: 25544
Epoch time: 11237
50227693 = yrday
fracday
Element set: 913
Inclination: 51
6377 deg
RA of node: 171
8765 deg
Eccentricity:
0012322
Arg of perigee: 113
3129 deg
Mean anomaly: 246
9325 deg
Mean motion: 15
60469122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1173
Checksum: 298
Coasting Arc #15 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2011/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6213412
92 A = 6768030
30 meter
Y = 564219
31 meter E =
0017368
Z = -2622658
32 I = 51
73074
XDOT = -2647
846978 Wp = 120
57695
YDOT = 4936
948882 meter/sec RA = 165
82150 deg
ZDOT = -5245
378803 TA = 88
99969
MA = 88
80071
Ha = 215
461 n
mi
Hp = 200
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20385213
00 X = 6219382
05
Y = 1851113
22 feet Y = 633734
85 meter
Z = -8604522
04 Z = -2592459
71
XDOT = -8687
162000 XDOT = -2677
375551
YDOT = 16197
338852 feet/sec YDOT = 4907
173911 meter/sec
ZDOT = -17209
248041 ZDOT = -5258
313516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17482522
76 X = -5328672
94
Y = -10744505
89 feet Y = -3274925
40 meter
Z = -8481646
05 Z = -2585205
72
XDOT = 14106
188904 XDOT = 4299
566378
YDOT = -9416
162904 feet/sec YDOT = -2870
046453 meter/sec
ZDOT = -17262
046094 ZDOT = -5261
471649
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 11238
52691625
00016717 00000-0 10270-3 0 9143
2 25544 51
6391 166
7185 0012320 117
0048 243
2367 15
60492358 11899
Satellite: ISS
Catalog Number: 25544
Epoch time: 11238
52691625 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 166
7185 deg
Eccentricity:
0012320
Arg of perigee: 117
0048 deg
Mean anomaly: 243
2367 deg
Mean motion: 15
60492358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1189
Checksum: 306
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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