[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 22nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 9 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
180/12:35:33
768 7
7 12
1 12
1
N/A -2
0 -0
3 211
0
000/00:08:37
536 -9
1 -0
2 208
6
Coasting Arc #1 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2011/171/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5861771
20 A = 6763013
33 meter
Y = -1759017
94 meter E =
0008066
Z = -2868537
73 I = 51
86130
XDOT = -781
309110 Wp = 254
08292
YDOT = 5704
546559 meter/sec RA = 141
70217 deg
ZDOT = -5085
016529 TA = 318
57371
MA = 318
63484
Ha = 206
703 n
mi
Hp = 204
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19231532
82 X = 5894939
88
Y = -5771056
25 feet Y = -1693282
25 meter
Z = -9411213
03 Z = -2839981
25
XDOT = -2563
350097 XDOT = -820
338597
YDOT = 18715
703935 feet/sec YDOT = 5695
591884 meter/sec
ZDOT = -16683
125095 ZDOT = -5088
906184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18771983
22 X = -5721700
49
Y = 7275879
41 feet Y = 2217688
04 meter
Z = -9295273
00 Z = -2833199
21
XDOT = 1508
834385 XDOT = 459
892721
YDOT = -17482
042762 feet/sec YDOT = -5328
526634 meter/sec
ZDOT = -16699
128835 ZDOT = -5089
894469
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 11171
79484141
00016717 00000-0 10270-3 0 9006
2 25544 51
6421 142
5487 0011855 269
8246 90
1552 15
62032328 1475
Satellite: ISS
Catalog Number: 25544
Epoch time: 11171
79484141 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 142
5487 deg
Eccentricity:
0011855
Arg of perigee: 269
8246 deg
Mean anomaly: 90
1552 deg
Mean motion: 15
62032328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 295
Coasting Arc #2 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2011/172/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3685556
91 A = 6754734
67 meter
Y = -2173688
61 meter E =
0008581
Z = 5234164
56 I = 51
85708
XDOT = 4922
953710 Wp = 261
81575
YDOT = -5792
019409 meter/sec RA = 136
65805 deg
ZDOT = 1061
351545 TA = 178
05918
MA = 178
05585
Ha = 206
633 n
mi
Hp = 204
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12091722
14 X = -3686402
76
Y = -7131524
31 feet Y = -2214908
05 meter
Z = 17172455
89 Z = 5216258
00
XDOT = 16151
422932 XDOT = 4982
199499
YDOT = -19002
688349 feet/sec YDOT = -5736
636803 meter/sec
ZDOT = 3482
124491 ZDOT = 1085
410295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12823247
66 X = 3908525
89
Y = 5926225
01 feet Y = 1806313
38 meter
Z = 17099877
23 Z = 5212042
58
XDOT = -13797
976525 XDOT = -4205
623245
YDOT = 19529
105465 feet/sec YDOT = 5952
471346 meter/sec
ZDOT = 3579
981374 ZDOT = 1091
178323
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 11172
81844260
00016717 00000-0 10270-3 0 9013
2 25544 51
6422 137
3842 0011685 274
2140 85
7681 15
62065290 1632
Satellite: ISS
Catalog Number: 25544
Epoch time: 11172
81844260 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 137
3842 deg
Eccentricity:
0011685
Arg of perigee: 274
2140 deg
Mean anomaly: 85
7681 deg
Mean motion: 15
62065290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 289
Coasting Arc #3 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2011/173/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -218845
87 A = 6758542
33 meter
Y = 5256296
05 meter E =
0004194
Z = -4240148
76 I = 51
89071
XDOT = -6205
978087 Wp = 253
03289
YDOT = 2684
985873 meter/sec RA = 131
59539 deg
ZDOT = 3644
591392 TA = 54
07147
MA = 54
03256
Ha = 206
887 n
mi
Hp = 204
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -717998
25 X = -257008
78
Y = 17245065
78 feet Y = 5253635
85 meter
Z = -13911249
21 Z = -4241304
05
XDOT = -20360
820497 XDOT = -6253
245523
YDOT = 8809
008771 feet/sec YDOT = 2615
322183 meter/sec
ZDOT = 11957
320840 ZDOT = 3614
328414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1321243
11 X = -402714
90
Y = -17205400
13 feet Y = -5244205
96 meter
Z = -13916148
62 Z = -4241642
10
XDOT = 18049
342750 XDOT = 5501
439670
YDOT = -10969
028237 feet/sec YDOT = -3343
359807 meter/sec
ZDOT = 11834
398674 ZDOT = 3607
124716
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 11173
77805776
00016717 00000-0 10270-3 0 9029
2 25544 51
6413 132
5419 0011860 277
8265 82
1545 15
62100556 1782
Satellite: ISS
Catalog Number: 25544
Epoch time: 11173
77805776 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 132
5419 deg
Eccentricity:
0011860
Arg of perigee: 277
8265 deg
Mean anomaly: 82
1545 deg
Mean motion: 15
62100556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 178
Checksum: 305
Coasting Arc #4 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2011/174/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3680874
15 A = 6766159
93 meter
Y = -5648300
75 meter E =
0006128
Z = 525169
96 I = 51
93527
XDOT = 4234
048648 Wp = 193
52936
YDOT = 2201
633094 meter/sec RA = 126
58873 deg
ZDOT = -6017
041545 TA = 340
80968
MA = 340
83276
Ha = 207
139 n
mi
Hp = 204
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12076358
77 X = 3741209
80
Y = -18531170
45 feet Y = -5606801
68 meter
Z = 1722998
54 Z = 543197
53
XDOT = 13891
235723 XDOT = 4238
344479
YDOT = 7223
205688 feet/sec YDOT = 2249
005475 meter/sec
ZDOT = -19740
949951 ZDOT = -5996
461927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9549382
76 X = -2910651
86
Y = 19944766
00 feet Y = 6079164
68 meter
Z = 1796396
76 Z = 547541
73
XDOT = -13376
488567 XDOT = -4077
153715
YDOT = -4639
665568 feet/sec YDOT = -1414
170065 meter/sec
ZDOT = -19657
518552 ZDOT = -5991
611655
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 11174
80163814
00016717 00000-0 10270-3 0 9035
2 25544 51
6412 127
3784 0011776 281
4120 78
5713 15
62088321 1944
Satellite: ISS
Catalog Number: 25544
Epoch time: 11174
80163814 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 127
3784 deg
Eccentricity:
0011776
Arg of perigee: 281
4120 deg
Mean anomaly: 78
5713 deg
Mean motion: 15
62088321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 293
Coasting Arc #5 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2011/175/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5005501
32 A = 6760922
55 meter
Y = 2842147
62 meter E =
0002868
Z = 3543152
33 I = 51
93407
XDOT = -331
443714 Wp = 14
46759
YDOT = -6206
284487 meter/sec RA = 121
59193 deg
ZDOT = 4512
071121 TA = 27
27726
MA = 27
26220
Ha = 207
629 n
mi
Hp = 204
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16422248
42 X = -5054122
72
Y = 9324631
29 feet Y = 2785900
78 meter
Z = 11624515
51 Z = 3518717
85
XDOT = -1087
413759 XDOT = -283
938021
YDOT = -20361
825745 feet/sec YDOT = -6209
725808 meter/sec
ZDOT = 14803
382944 ZDOT = 4510
575624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14938471
86 X = 4553246
22
Y = -11652454
97 feet Y = -3551668
28 meter
Z = 11525220
36 Z = 3512887
17
XDOT = 3312
608984 XDOT = 1009
683218
YDOT = 18876
473315 feet/sec YDOT = 5753
549066 meter/sec
ZDOT = 14797
578696 ZDOT = 4510
301987
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 11175
82520593
00016717 00000-0 10270-3 0 9040
2 25544 51
6402 122
2124 0011952 285
8112 74
1727 15
62116329 2106
Satellite: ISS
Catalog Number: 25544
Epoch time: 11175
82520593 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 122
2124 deg
Eccentricity:
0011952
Arg of perigee: 285
8112 deg
Mean anomaly: 74
1727 deg
Mean motion: 15
62116329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 270
Coasting Arc #6 (Orbit 224)
---------------------------------------
Vector Time (GMT): 2011/176/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3776527
72 A = 6754091
02 meter
Y = 1762749
20 meter E =
0005553
Z = -5318189
24 I = 51
92532
XDOT = -3363
414816 Wp = 42
51751
YDOT = 6902
844760 meter/sec RA = 116
54168 deg
ZDOT = -96
484264 TA = 226
54487
MA = 226
59108
Ha = 207
804 n
mi
Hp = 204
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12390182
80 X = 3782370
46
Y = 5783297
89 feet Y = 1805014
00 meter
Z = -17448127
44 Z = -5299828
42
XDOT = -11034
825513 XDOT = -3439
885077
YDOT = 22647
128479 feet/sec YDOT = 6864
805455 meter/sec
ZDOT = -316
549421 ZDOT = -113
008588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13274920
03 X = -4046195
63
Y = -3651313
94 feet Y = -1112920
49 meter
Z = -17373678
95 Z = -5295497
34
XDOT = 6896
228577 XDOT = 2101
970470
YDOT = -23183
817849 feet/sec YDOT = -7066
427680 meter/sec
ZDOT = -383
929361 ZDOT = -117
021669
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 11176
78479058
00016717 00000-0 10270-3 0 9056
2 25544 51
6390 117
3699 0011852 289
0937 70
8936 15
62151751 2253
Satellite: ISS
Catalog Number: 25544
Epoch time: 11176
78479058 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 117
3699 deg
Eccentricity:
0011852
Arg of perigee: 289
0937 deg
Mean anomaly: 70
8936 deg
Mean motion: 15
62151751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 225
Checksum: 333
Coasting Arc #7 (Orbit 240)
---------------------------------------
Vector Time (GMT): 2011/177/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -864452
63 A = 6760285
46 meter
Y = -5620680
56 meter E =
0005655
Z = 3659890
20 I = 51
95997
XDOT = 5129
434598 Wp = 7
38258
YDOT = -3651
649638 meter/sec RA = 111
49127 deg
ZDOT = -4390
254773 TA = 129
21232
MA = 129
16210
Ha = 207
986 n
mi
Hp = 204
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2836130
66 X = -819315
96
Y = -18440553
01 feet Y = -5630095
57 meter
Z = 12007513
79 Z = 3655799
48
XDOT = 16828
853667 XDOT = 5191
213913
YDOT = -11980
477816 feet/sec YDOT = -3593
943101 meter/sec
ZDOT = -14403
723008 ZDOT = -4365
186416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6201710
02 X = 1890281
22
Y = 17607631
28 feet Y = 5366806
02 meter
Z = 11991168
97 Z = 3654908
30
XDOT = -13179
821339 XDOT = -4017
209544
YDOT = 14395
891716 feet/sec YDOT = 4387
867795 meter/sec
ZDOT = -14301
793085 ZDOT = -4359
186532
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 11177
80833587
00016717 00000-0 10270-3 0 9062
2 25544 51
6399 112
2055 0012071 292
8239 67
1643 15
62188525 2414
Satellite: ISS
Catalog Number: 25544
Epoch time: 11177
80833587 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 112
2055 deg
Eccentricity:
0012071
Arg of perigee: 292
8239 deg
Mean anomaly: 67
1643 deg
Mean motion: 15
62188525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 241
Checksum: 310
Coasting Arc #8 (Orbit 256)
---------------------------------------
Vector Time (GMT): 2011/178/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2199588
54 A = 6766023
59 meter
Y = 6377386
85 meter E =
0013717
Z = 381554
84 I = 51
98785
XDOT = -4370
753141 Wp = 355
95491
YDOT = -1867
281069 meter/sec RA = 106
49574 deg
ZDOT = 6040
039858 TA = 8
15515
MA = 8
13288
Ha = 208
300 n
mi
Hp = 204
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7216497
83 X = -2272591
76
Y = 20923185
20 feet Y = 6352381
47 meter
Z = 1251820
34 Z = 370692
97
XDOT = -14339
741276 XDOT = -4378
889433
YDOT = -6126
250225 feet/sec YDOT = -1916
203987 meter/sec
ZDOT = 19816
403735 ZDOT = 6018
786648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2935647
18 X = 894785
26
Y = -21939660
29 feet Y = -6687208
46 meter
Z = 1207417
03 Z = 368020
71
XDOT = 13785
551286 XDOT = 4201
836032
YDOT = 2925
455005 feet/sec YDOT = 891
678686 meter/sec
ZDOT = 19730
213210 ZDOT = 6013
768986
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 11178
83187284
00016717 00000-0 10270-3 0 9073
2 25544 51
6388 107
0395 0011897 296
4949 63
4988 15
62162729 2570
Satellite: ISS
Catalog Number: 25544
Epoch time: 11178
83187284 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 107
0395 deg
Eccentricity:
0011897
Arg of perigee: 296
4949 deg
Mean anomaly: 63
4988 deg
Mean motion: 15
62162729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 257
Checksum: 357
Coasting Arc #9 (Orbit 271)
---------------------------------------
Vector Time (GMT): 2011/179/18:26:47
554
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4035107
09 A = 6758595
79 meter
Y = -3465981
04 meter E =
0008999
Z = -4172701
84 I = 51
97077
XDOT = 1677
111220 Wp = 341
49818
YDOT = 6483
853744 meter/sec RA = 101
49446 deg
ZDOT = -3753
362092 TA = 250
08900
MA = 250
18598
Ha = 208
472 n
mi
Hp = 204
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13238540
32 X = 4093834
65
Y = -11371328
88 feet Y = -3420528
90 meter
Z = -13689966
67 Z = -4152957
31
XDOT = 5502
333399 XDOT = 1622
715983
YDOT = 21272
486036 feet/sec YDOT = 6502
304764 meter/sec
ZDOT = -12314
180092 ZDOT = -3745
345645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10564915
68 X = -3220186
30
Y = 13969315
85 feet Y = 4257847
47 meter
Z = -13609630
00 Z = -4148215
23
XDOT = -8999
378542 XDOT = -2743
010580
YDOT = -18805
748207 feet/sec YDOT = -5731
992054 meter/sec
ZDOT = -12281
957981 ZDOT = -3743
540793
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 11179
79142666
00016717 00000-0 10270-3 0 9085
2 25544 51
6386 102
1980 0011772 300
3586 59
6406 15
62202584 2721
Satellite: ISS
Catalog Number: 25544
Epoch time: 11179
79142666 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 102
1980 deg
Eccentricity:
0011772
Arg of perigee: 300
3586 deg
Mean anomaly: 59
6406 deg
Mean motion: 15
62202584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 272
Checksum: 310
Coasting Arc #10 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2011/180/12:39:52
536
Vector Time (MET): N/A
Weight (LBS) : 882681
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1152124
99 A = 6772648
84 meter
Y = -6658155
84 meter E =
0011453
Z = -325147
70 I = 52
00262
XDOT = 4614
981119 Wp = 178
59378
YDOT = 1092
832780 meter/sec RA = 97
66289 deg
ZDOT = -6041
241742 TA = 4
90296
MA = 4
89175
Ha = 211
000 n
mi
Hp = 208
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3779937
63 X = 1228071
64
Y = -21844343
31 feet Y = -6644847
38 meter
Z = -1066757
56 Z = -319367
50
XDOT = 15141
014169 XDOT = 4631
764964
YDOT = 3585
409384 feet/sec YDOT = 1144
535293 meter/sec
ZDOT = -19820
346921 ZDOT = -6018
781295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22023287
04 X = -6712697
89
Y = 2547219
20 feet Y = 776392
41 meter
Z = -1042946
33 Z = -317890
04
XDOT = -692
572586 XDOT = -211
096124
YDOT = -14044
550293 feet/sec YDOT = -4280
778929 meter/sec
ZDOT = -19729
206734 ZDOT = -6013
462212
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 11180
55912046
00016717 00000-0 10270-3 0 9099
2 25544 51
6419 98
3276 0008095 248
2268 111
8027 15
59870583 2842
Satellite: ISS
Catalog Number: 25544
Epoch time: 11180
55912046 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 98
3276 deg
Eccentricity:
0008095
Arg of perigee: 248
2268 deg
Mean anomaly: 111
8027 deg
Mean motion: 15
59870583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 325
Coasting Arc #11 (Orbit 299)
---------------------------------------
Vector Time (GMT): 2011/181/12:39:52
536
Vector Time (MET): N/A
Weight (LBS) : 882681
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3060209
76 A = 6767060
56 meter
Y = 4827323
31 meter E =
0005329
Z = 3622044
23 I = 51
98738
XDOT = -3218
871488 Wp = 125
80085
YDOT = -5373
981836 meter/sec RA = 92
68013 deg
ZDOT = 4435
080073 TA = 276
99581
MA = 277
05642
Ha = 210
628 n
mi
Hp = 208
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10040058
25 X = -3131557
44
Y = 15837674
91 feet Y = 4792702
57 meter
Z = 11883347
22 Z = 3607005
49
XDOT = -10560
601996 XDOT = -3180
083960
YDOT = -17631
174004 feet/sec YDOT = -5409
761191 meter/sec
ZDOT = 14550
787640 ZDOT = 4419
536123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18138604
64 X = 5528646
69
Y = 4907076
79 feet Y = 1495677
01 meter
Z = 11822025
07 Z = 3603353
24
XDOT = -13277
281575 XDOT = -4046
915424
YDOT = 14114
054775 feet/sec YDOT = 4301
963896 meter/sec
ZDOT = 14487
951804 ZDOT = 4415
927710
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 11181
58414184
00016717 00000-0 10270-3 0 9105
2 25544 51
6422 93
1730 0008014 253
1012 106
9265 15
59900399 3004
Satellite: ISS
Catalog Number: 25544
Epoch time: 11181
58414184 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 93
1730 deg
Eccentricity:
0008014
Arg of perigee: 253
1012 deg
Mean anomaly: 106
9265 deg
Mean motion: 15
59900399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 300
Checksum: 273
Coasting Arc #12 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2011/182/12:39:52
536
Vector Time (MET): N/A
Weight (LBS) : 882681
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4089340
40 A = 6760682
26 meter
Y = -1079456
06 meter E =
0006648
Z = -5280039
79 I = 51
96741
XDOT = 947
759254 Wp = 91
92046
YDOT = 7570
940807 meter/sec RA = 87
65658 deg
ZDOT = -814
877141 TA = 170
33755
MA = 170
32476
Ha = 210
477 n
mi
Hp = 209
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13416471
13 X = 4126756
27
Y = -3541522
52 feet Y = -1033516
40 meter
Z = -17322965
18 Z = -5260083
36
XDOT = 3109
446373 XDOT = 866
987562
YDOT = 24839
044641 feet/sec YDOT = 7581
087757 meter/sec
ZDOT = -2673
481435 ZDOT = -810
467790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7629382
10 X = -2325435
66
Y = -11710674
20 feet Y = -3569413
49 meter
Z = -17241863
02 Z = -5255319
85
XDOT = 21728
149138 XDOT = 6622
739857
YDOT = -10250
533756 feet/sec YDOT = -3124
362689 meter/sec
ZDOT = -2655
982030 ZDOT = -809
543323
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 11182
54508991
00016717 00000-0 10270-3 0 9113
2 25544 51
6428 88
3409 0008069 257
0793 102
9462 15
59945005 3152
Satellite: ISS
Catalog Number: 25544
Epoch time: 11182
54508991 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 88
3409 deg
Eccentricity:
0008069
Arg of perigee: 257
0793 deg
Mean anomaly: 102
9462 deg
Mean motion: 15
59945005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 319
Coasting Arc #13 (Orbit 330)
---------------------------------------
Vector Time (GMT): 2011/183/12:39:52
536
Vector Time (MET): N/A
Weight (LBS) : 882681
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3972430
76 A = 6763720
63 meter
Y = -3069431
73 meter E =
0002205
Z = 4533854
81 I = 51
97530
XDOT = 1624
244769 Wp = 3
46200
YDOT = -6796
661678 meter/sec RA = 82
62206 deg
ZDOT = -3176
017579 TA = 118
23422
MA = 118
21196
Ha = 210
121 n
mi
Hp = 209
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13032909
32 X = -3959836
80
Y = -10070314
07 feet Y = -3113784
21 meter
Z = 14874851
74 Z = 4514587
15
XDOT = 5328
887036 XDOT = 1715
553881
YDOT = -22298
758787 feet/sec YDOT = -6777
987317 meter/sec
ZDOT = -10420
005179 ZDOT = -3167
906487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5142590
54 X = -1567461
60
Y = 15720643
75 feet Y = 4791652
22 meter
Z = 14796766
12 Z = 4510054
31
XDOT = -21678
124178 XDOT = -6607
492250
YDOT = 2691
767095 feet/sec YDOT = 820
450611 meter/sec
ZDOT = -10386
692331 ZDOT = -3165
863823
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 11183
57009216
00016717 00000-0 10270-3 0 9124
2 25544 51
6426 83
1866 0008159 261
7409 98
2822 15
59967291 3312
Satellite: ISS
Catalog Number: 25544
Epoch time: 11183
57009216 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 83
1866 deg
Eccentricity:
0008159
Arg of perigee: 261
7409 deg
Mean anomaly: 98
2822 deg
Mean motion: 15
59967291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 331
Checksum: 320
Coasting Arc #14 (Orbit 345)
---------------------------------------
Vector Time (GMT): 2011/184/12:39:52
536
Vector Time (MET): N/A
Weight (LBS) : 882681
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2684067
23 A = 6771177
91 meter
Y = 5969760
35 meter E =
0006367
Z = -1717552
94 I = 51
99556
XDOT = -3840
567808 Wp = 327
10401
YDOT = 3375
718306 meter/sec RA = 77
62306 deg
ZDOT = 5726
653852 TA = 14
10523
MA = 14
08746
Ha = 209
659 n
mi
Hp = 209
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8805994
84 X = 2625456
13
Y = 19585827
93 feet Y = 5999447
76 meter
Z = -5635016
22 Z = -1704655
49
XDOT = -12600
288085 XDOT = -3905
848807
YDOT = 11075
191294 feet/sec YDOT = 3332
404903 meter/sec
ZDOT = 18788
234422 ZDOT = 5707
838661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15282946
66 X = 4658242
14
Y = -15105154
73 feet Y = -4604051
16 meter
Z = -5582960
71 Z = -1701686
42
XDOT = 13707
590594 XDOT = 4178
073613
YDOT = 6947
255900 feet/sec YDOT = 2117
523598 meter/sec
ZDOT = 18711
628563 ZDOT = 5703
304386
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 11184
53102372
00016717 00000-0 10270-3 0 9139
2 25544 51
6428 78
3535 0008200 265
1074 94
9146 15
59964974 3469
Satellite: ISS
Catalog Number: 25544
Epoch time: 11184
53102372 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 78
3535 deg
Eccentricity:
0008200
Arg of perigee: 265
1074 deg
Mean anomaly: 94
9146 deg
Mean motion: 15
59964974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 346
Checksum: 312
Coasting Arc #15 (Orbit 361)
---------------------------------------
Vector Time (GMT): 2011/185/12:39:52
536
Vector Time (MET): N/A
Weight (LBS) : 882681
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -476743
81 A = 6770972
84 meter
Y = -6479580
36 meter E =
0006961
Z = -1889891
15 I = 51
98683
XDOT = 5031
844740 Wp = 213
89123
YDOT = 1280
692995 meter/sec RA = 72
64968 deg
ZDOT = -5655
905743 TA = 346
87206
MA = 346
89017
Ha = 209
477 n
mi
Hp = 209
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1564120
10 X = -395071
88
Y = -21258465
76 feet Y = -6484454
72 meter
Z = -6200430
28 Z = -1892009
54
XDOT = 16508
676968 XDOT = 5044
624641
YDOT = 4201
748670 feet/sec YDOT = 1337
034289 meter/sec
ZDOT = -18556
121204 ZDOT = -5631
430311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19242569
87 X = -5865135
30
Y = 9164607
94 feet Y = 2793372
50 meter
Z = -6208674
57 Z = -1892404
01
XDOT = -1472
514234 XDOT = -448
822339
YDOT = -15605
189355 feet/sec YDOT = -4756
461715 meter/sec
ZDOT = -18456
779300 ZDOT = -5625
626331
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 11185
55600807
00016717 00000-0 10270-3 0 9149
2 25544 51
6425 73
1989 0008355 268
2430 91
7768 15
59935138 3626
Satellite: ISS
Catalog Number: 25544
Epoch time: 11185
55600807 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 73
1989 deg
Eccentricity:
0008355
Arg of perigee: 268
2430 deg
Mean anomaly: 91
7768 deg
Mean motion: 15
59935138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 329
Coasting Arc #16 (Orbit 377)
---------------------------------------
Vector Time (GMT): 2011/186/12:39:52
536
Vector Time (MET): N/A
Weight (LBS) : 882681
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2080112
05 A = 6763314
55 meter
Y = 4471127
57 meter E =
0003099
Z = 4630680
02 I = 51
95120
XDOT = -4699
698150 Wp = 191
44178
YDOT = -5282
441473 meter/sec RA = 67
64686 deg
ZDOT = 2986
696927 TA = 228
93196
MA = 228
95874
Ha = 209
587 n
mi
Hp = 209
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6824514
59 X = -2152449
09
Y = 14669053
72 feet Y = 4447461
57 meter
Z = 15192519
75 Z = 4620399
76
XDOT = -15418
957185 XDOT = -4654
788163
YDOT = -17330
844728 feet/sec YDOT = -5334
745556 meter/sec
ZDOT = 9798
874434 ZDOT = 2963
974724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16197483
42 X = 4936992
95
Y = 819331
57 feet Y = 249732
26 meter
Z = 15150512
18 Z = 4617876
11
XDOT = -10085
168282 XDOT = -3073
959292
YDOT = 19722
869521 feet/sec YDOT = 6011
530630 meter/sec
ZDOT = 9706
878162 ZDOT = 2958
656464
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 11186
58098275
00016717 00000-0 10270-3 0 9154
2 25544 51
6423 68
0431 0008204 273
6542 86
3675 15
59963020 3781
Satellite: ISS
Catalog Number: 25544
Epoch time: 11186
58098275 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 68
0431 deg
Eccentricity:
0008204
Arg of perigee: 273
6542 deg
Mean anomaly: 86
3675 deg
Mean motion: 15
59963020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 378
Checksum: 319
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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