[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 26th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
180/12:36:32
153 6
4 8
3 8
4
N/A -0
4 -1
6 210
9
000/00:33:04
306 -5
4 -0
0 209
5
Coasting Arc #1 (Orbit 205)
---------------------------------------
Vector Time (GMT): 2011/175/13:11:12
373
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4598673
20 A = 6755699
36 meter
Y = 19104
68 meter E =
0006638
Z = -4951585
83 I = 51
91300
XDOT = -2408
154460 Wp = 4
95865
YDOT = 6950
748910 meter/sec RA = 122
68673 deg
ZDOT = -2203
466374 TA = 243
62597
MA = 243
69413
Ha = 207
462 n
mi
Hp = 204
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15087510
50 X = 4622171
66
Y = 62679
39 feet Y = 70661
80 meter
Z = -16245360
33 Z = -4929188
41
XDOT = -7900
769225 XDOT = -2474
996066
YDOT = 22804
294324 feet/sec YDOT = 6923
445987 meter/sec
ZDOT = -7229
220386 ZDOT = -2215
326729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4974638
30 X = -1516269
75
Y = -14346955
45 feet Y = -4372952
02 meter
Z = -16154456
88 Z = -4923878
46
XDOT = 23072
971412 XDOT = 7032
641686
YDOT = 217
407399 feet/sec YDOT = 66
265775 meter/sec
ZDOT = -7277
653036 ZDOT = -2218
228646
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
56927780
00016717 00000-0 10270-3 0 9006
2 25544 51
6397 123
5053 0011771 285
6244 74
3614 15
62159488 2062
Satellite: ISS
Catalog Number: 25544
Epoch time: 11175
56927780 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 123
5053 deg
Eccentricity:
0011771
Arg of perigee: 285
6244 deg
Mean anomaly: 74
3614 deg
Mean motion: 15
62159488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 206
Checksum: 312
Coasting Arc #2 (Orbit 221)
---------------------------------------
Vector Time (GMT): 2011/176/13:11:12
373
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1933118
88 A = 6756358
39 meter
Y = -4376425
89 meter E =
0008760
Z = 4777613
89 I = 51
93082
XDOT = 5041
996071 Wp = 328
90925
YDOT = -5138
410201 meter/sec RA = 117
62425 deg
ZDOT = -2661
681345 TA = 147
25341
MA = 147
19909
Ha = 207
720 n
mi
Hp = 204
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6342253
53 X = -1907245
97
Y = -14358352
64 feet Y = -4397899
15 meter
Z = 15674586
25 Z = 4768285
07
XDOT = 16541
981861 XDOT = 5112
010009
YDOT = -16858
301186 feet/sec YDOT = -5081
635723 meter/sec
ZDOT = -8732
550345 ZDOT = -2637
017901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11224665
42 X = -3421278
02
Y = 11026011
48 feet Y = 3360728
30 meter
Z = 15636914
07 Z = 4766131
41
XDOT = -20771
881881 XDOT = -6331
269597
YDOT = -8880
031918 feet/sec YDOT = -2706
633729 meter/sec
ZDOT = -8632
215582 ZDOT = -2631
099309
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
59281923
00016717 00000-0 10270-3 0 9013
2 25544 51
6397 118
3412 0011807 289
3677 70
6203 15
62162644 2223
Satellite: ISS
Catalog Number: 25544
Epoch time: 11176
59281923 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 118
3412 deg
Eccentricity:
0011807
Arg of perigee: 289
3677 deg
Mean anomaly: 70
6203 deg
Mean motion: 15
62162644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 222
Checksum: 300
Coasting Arc #3 (Orbit 236)
---------------------------------------
Vector Time (GMT): 2011/177/13:11:12
373
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1414220
51 A = 6765075
37 meter
Y = 6435877
56 meter E =
0012707
Z = -1493878
40 I = 51
97345
XDOT = -5024
636282 Wp = 332
50602
YDOT = 246
546555 meter/sec RA = 112
60535 deg
ZDOT = 5810
308275 TA = 11
19326
MA = 11
16502
Ha = 208
034 n
mi
Hp = 204
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4639831
07 X = -1478825
62
Y = 21115083
85 feet Y = 6419701
88 meter
Z = -4901175
86 Z = -1500904
69
XDOT = -16485
027171 XDOT = -5055
245241
YDOT = 808
879773 feet/sec YDOT = 190
186029 meter/sec
ZDOT = 19062
691192 ZDOT = 5785
824233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21345553
17 X = 6506124
61
Y = -3385092
40 feet Y = -1031776
16 meter
Z = -4929993
18 Z = -1502661
92
XDOT = 6544
789834 XDOT = 1994
851941
YDOT = 13611
312657 feet/sec YDOT = 4148
728098 meter/sec
ZDOT = 18963
292880 ZDOT = 5780
011670
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
55237705
00016717 00000-0 10270-3 0 9020
2 25544 51
6399 113
4986 0011900 293
1058 66
8845 15
62174586 2370
Satellite: ISS
Catalog Number: 25544
Epoch time: 11177
55237705 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 113
4986 deg
Eccentricity:
0011900
Arg of perigee: 293
1058 deg
Mean anomaly: 66
8845 deg
Mean motion: 15
62174586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 237
Checksum: 324
Coasting Arc #4 (Orbit 252)
---------------------------------------
Vector Time (GMT): 2011/178/13:11:12
373
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3809146
04 A = 6762734
62 meter
Y = -4855882
72 meter E =
0007122
Z = -2763373
70 I = 51
97764
XDOT = 2645
049777 Wp = 293
20987
YDOT = 5023
886549 meter/sec RA = 107
61832 deg
ZDOT = -5168
831980 TA = 278
03881
MA = 278
11961
Ha = 208
231 n
mi
Hp = 204
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12497198
30 X = 3876586
34
Y = -15931373
76 feet Y = -4812909
01 meter
Z = -9066186
69 Z = -2744705
83
XDOT = 8677
984832 XDOT = 2613
784393
YDOT = 16482
567419 feet/sec YDOT = 5053
291132 meter/sec
ZDOT = -16958
110170 ZDOT = -5156
057437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19504325
70 X = -5944918
47
Y = -5562597
19 feet Y = -1695479
62 meter
Z = -8990170
61 Z = -2740204
00
XDOT = 11508
469701 XDOT = 3507
781565
YDOT = -12957
732685 feet/sec YDOT = -3949
516922 meter/sec
ZDOT = -16906
491373 ZDOT = -5153
098571
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
57589309
00016717 00000-0 10270-3 0 9034
2 25544 51
6411 108
3340 0011887 296
8690 63
1251 15
62206560 2535
Satellite: ISS
Catalog Number: 25544
Epoch time: 11178
57589309 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 108
3340 deg
Eccentricity:
0011887
Arg of perigee: 296
8690 deg
Mean anomaly: 63
1251 deg
Mean motion: 15
62206560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 253
Checksum: 303
Coasting Arc #5 (Orbit 268)
---------------------------------------
Vector Time (GMT): 2011/179/13:11:12
373
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4270213
36 A = 6754255
71 meter
Y = 359755
20 meter E =
0008010
Z = 5226116
15 I = 51
95772
XDOT = 764
160386 Wp = 298
46995
YDOT = -7552
276387 meter/sec RA = 102
58172 deg
ZDOT = 1149
322515 TA = 140
60143
MA = 140
54315
Ha = 208
498 n
mi
Hp = 203
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14009886
35 X = -4299306
33
Y = 1180299
20 feet Y = 311839
47 meter
Z = 17146050
37 Z = 5205300
88
XDOT = 2507
087880 XDOT = 842
971411
YDOT = -24777
809670 feet/sec YDOT = -7543
290631 meter/sec
ZDOT = 3770
743159 ZDOT = 1153
224880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6666867
04 X = 2032061
07
Y = 12494572
84 feet Y = 3808345
80 meter
Z = 17061523
92 Z = 5200352
49
XDOT = -22828
571791 XDOT = -6958
148682
YDOT = 7032
478793 feet/sec YDOT = 2143
499536 meter/sec
ZDOT = 3786
961909 ZDOT = 1154
265990
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
59939551
00016717 00000-0 10270-3 0 9046
2 25544 51
6410 103
1690 0011922 300
3931 59
6047 15
62245886 2698
Satellite: ISS
Catalog Number: 25544
Epoch time: 11179
59939551 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 103
1690 deg
Eccentricity:
0011922
Arg of perigee: 300
3931 deg
Mean anomaly: 59
6047 deg
Mean motion: 15
62245886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 269
Checksum: 308
Coasting Arc #6 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2011/180/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3921842
37 A = 6764930
33 meter
Y = -3311110
64 meter E =
0001303
Z = -4407467
97 I = 51
97175
XDOT = 1790
242216 Wp = 354
86494
YDOT = 6645
468922 meter/sec RA = 97
63742 deg
ZDOT = -3398
078276 TA = 240
93229
MA = 240
94534
Ha = 210
949 n
mi
Hp = 209
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12866936
91 X = 3979986
94
Y = -10863223
89 feet Y = -3266928
28 meter
Z = -14460196
75 Z = -4388275
15
XDOT = 5873
498084 XDOT = 1732
305409
YDOT = 21802
719561 feet/sec YDOT = 6665
165201 meter/sec
ZDOT = -11148
550774 ZDOT = -3389
520787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14600464
14 X = -4450221
47
Y = -8523302
95 feet Y = -2597902
74 meter
Z = -14382097
99 Z = -4383663
47
XDOT = 17893
296888 XDOT = 5453
876891
YDOT = -11889
996933 feet/sec YDOT = -3624
071065 meter/sec
ZDOT = -11114
145986 ZDOT = -3387
591696
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
55897609
00016717 00000-0 10270-3 0 9052
2 25544 51
6383 98
3283 0008743 257
7522 102
2655 15
59715322 2848
Satellite: ISS
Catalog Number: 25544
Epoch time: 11180
55897609 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 98
3283 deg
Eccentricity:
0008743
Arg of perigee: 257
7522 deg
Mean anomaly: 102
2655 deg
Mean motion: 15
59715322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 324
Coasting Arc #7 (Orbit 299)
---------------------------------------
Vector Time (GMT): 2011/181/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4128211
82 A = 6761107
08 meter
Y = -710316
37 meter E =
0006281
Z = 5312509
75 I = 51
96218
XDOT = 712
611298 Wp = 266
37233
YDOT = -7626
006957 meter/sec RA = 92
60580 deg
ZDOT = -466
754373 TA = 188
05203
MA = 188
06212
Ha = 210
676 n
mi
Hp = 209
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13544002
05 X = -4145769
07
Y = -2330434
28 feet Y = -756579
73 meter
Z = 17429493
91 Z = 5292412
30
XDOT = 2337
963576 XDOT = 800
101204
YDOT = -25019
707863 feet/sec YDOT = -7617
548832 meter/sec
ZDOT = -1531
346368 ZDOT = -463
081491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2651034
69 X = 808035
37
Y = 13589694
48 feet Y = 4142138
88 meter
Z = 17347921
85 Z = 5287646
58
XDOT = -23240
426345 XDOT = -7083
681950
YDOT = 6465
336738 feet/sec YDOT = 1970
634638 meter/sec
ZDOT = -1516
029732 ZDOT = -462
085862
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
58412502
00016717 00000-0 10270-3 0 9062
2 25544 51
6383 93
1742 0008907 261
6250 98
3895 15
59748676 3003
Satellite: ISS
Catalog Number: 25544
Epoch time: 11181
58412502 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 93
1742 deg
Eccentricity:
0008907
Arg of perigee: 261
6250 deg
Mean anomaly: 98
3895 deg
Mean motion: 15
59748676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 300
Checksum: 319
Coasting Arc #8 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2011/182/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3232516
13 A = 6766690
18 meter
Y = 4496460
13 meter E =
0003584
Z = -3888167
20 I = 51
98164
XDOT = -2993
381999 Wp = 228
27994
YDOT = 5731
648778 meter/sec RA = 87
58004 deg
ZDOT = 4134
965513 TA = 84
88486
MA = 84
84396
Ha = 210
221 n
mi
Hp = 209
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10605367
87 X = 3200883
34
Y = 14752165
77 feet Y = 4532431
93 meter
Z = -12756454
05 Z = -3872539
86
XDOT = -9820
807084 XDOT = -3077
338557
YDOT = 18804
621974 feet/sec YDOT = 5697
704774 meter/sec
ZDOT = 13566
159818 ZDOT = 4120
220989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9753830
34 X = 2972967
49
Y = -15380896
80 feet Y = -4688097
35 meter
Z = -12693232
45 Z = -3868897
25
XDOT = 20012
700756 XDOT = 6099
871190
YDOT = 1532
192678 feet/sec YDOT = 467
012328 meter/sec
ZDOT = 13505
973091 ZDOT = 4116
620598
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
54519406
00016717 00000-0 10270-3 0 9071
2 25544 51
6388 88
3421 0008872 265
6331 94
3811 15
59734546 3154
Satellite: ISS
Catalog Number: 25544
Epoch time: 11182
54519406 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 88
3421 deg
Eccentricity:
0008872
Arg of perigee: 265
6331 deg
Mean anomaly: 94
3811 deg
Mean motion: 15
59734546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 319
Coasting Arc #9 (Orbit 330)
---------------------------------------
Vector Time (GMT): 2011/183/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1444818
15 A = 6772911
07 meter
Y = -6568434
92 meter E =
0008483
Z = 750256
55 I = 51
99988
XDOT = 4501
687286 Wp = 167
92461
YDOT = -1674
874642 meter/sec RA = 82
59460 deg
ZDOT = -5990
115407 TA = 3
98748
MA = 3
98072
Ha = 210
031 n
mi
Hp = 209
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4740217
03 X = -1374905
81
Y = -21549983
33 feet Y = -6584200
98 meter
Z = 2461471
61 Z = 743406
46
XDOT = 14769
315242 XDOT = 4549
179863
YDOT = -5494
995546 feet/sec YDOT = -1624
267491 meter/sec
ZDOT = -19652
609602 ZDOT = -5968
131514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18046549
06 X = -5500588
15
Y = 12701493
93 feet Y = 3871415
35 meter
Z = 2434009
13 Z = 741885
98
XDOT = -9888
213007 XDOT = -3013
927324
YDOT = -10297
849279 feet/sec YDOT = -3138
784460 meter/sec
ZDOT = -19563
233452 ZDOT = -5962
873556
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
57032387
00016717 00000-0 10270-3 0 9084
2 25544 51
6388 83
1883 0008862 268
4314 91
5827 15
59712678 3316
Satellite: ISS
Catalog Number: 25544
Epoch time: 11183
57032387 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 83
1883 deg
Eccentricity:
0008862
Arg of perigee: 268
4314 deg
Mean anomaly: 91
5827 deg
Mean motion: 15
59712678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 331
Checksum: 334
Coasting Arc #10 (Orbit 346)
---------------------------------------
Vector Time (GMT): 2011/184/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -833107
70 A = 6769885
37 meter
Y = 6137473
33 meter E =
0005458
Z = 2724421
20 I = 51
98502
XDOT = -4810
534490 Wp = 53
18503
YDOT = -2962
249503 meter/sec RA = 77
61879 deg
ZDOT = 5198
246120 TA = 337
54918
MA = 337
57305
Ha = 210
301 n
mi
Hp = 209
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2733292
99 X = -914910
68
Y = 20136067
37 feet Y = 6127699
24 meter
Z = 8938389
77 Z = 2720176
24
XDOT = -15782
593470 XDOT = -4802
304158
YDOT = -9718
666348 feet/sec YDOT = -3015
998561 meter/sec
ZDOT = 17054
613255 ZDOT = 5174
896557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19560255
71 X = 5961965
94
Y = -5535562
38 feet Y = -1687239
41 meter
Z = 8920810
33 Z = 2719062
99
XDOT = -2923
042982 XDOT = -890
943501
YDOT = 17024
001880 feet/sec YDOT = 5188
915773 meter/sec
ZDOT = 16959
939660 ZDOT = 5169
389608
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
59544127
00016717 00000-0 10270-3 0 9098
2 25544 51
6386 78
0332 0008922 274
1949 85
8187 15
59748545 3475
Satellite: ISS
Catalog Number: 25544
Epoch time: 11184
59544127 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 78
0332 deg
Eccentricity:
0008922
Arg of perigee: 274
1949 deg
Mean anomaly: 85
8187 deg
Mean motion: 15
59748545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 347
Checksum: 347
Coasting Arc #11 (Orbit 361)
---------------------------------------
Vector Time (GMT): 2011/185/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3024682
98 A = 6762334
07 meter
Y = -3418419
18 meter E =
0005591
Z = -4993688
63 I = 51
95224
XDOT = 3722
009960 Wp = 34
94807
YDOT = 6372
424418 meter/sec RA = 72
60768 deg
ZDOT = -2104
497588 TA = 214
65402
MA = 214
69046
Ha = 210
385 n
mi
Hp = 209
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9923500
58 X = 3086941
57
Y = -11215286
02 feet Y = -3384246
62 meter
Z = -16383492
87 Z = -4978844
19
XDOT = 12211
318768 XDOT = 3660
698722
YDOT = 20906
904258 feet/sec YDOT = 6413
703644 meter/sec
ZDOT = -6904
519646 ZDOT = -2086
564556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14375134
16 X = -4381540
89
Y = -4426313
62 feet Y = -1349140
39 meter
Z = -16323008
56 Z = -4975253
01
XDOT = 13562
496981 XDOT = 4133
849080
YDOT = -18811
505933 feet/sec YDOT = -5733
747008 meter/sec
ZDOT = -6832
034323 ZDOT = -2082
404062
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
55647815
00016717 00000-0 10270-3 0 9105
2 25544 51
6382 73
2009 0009082 277
7760 82
2364 15
59796874 3620
Satellite: ISS
Catalog Number: 25544
Epoch time: 11185
55647815 = yrday
fracday
Element set: 910
Inclination: 51
6382 deg
RA of node: 73
2009 deg
Eccentricity:
0009082
Arg of perigee: 277
7760 deg
Mean anomaly: 82
2364 deg
Mean motion: 15
59796874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 329
Coasting Arc #12 (Orbit 377)
---------------------------------------
Vector Time (GMT): 2011/186/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4477223
05 A = 6762046
44 meter
Y = -485510
77 meter E =
0006561
Z = 5049297
54 I = 51
94164
XDOT = -1382
754066 Wp = 319
69301
YDOT = -7298
312640 meter/sec RA = 67
56937 deg
ZDOT = -1924
367220 TA = 148
89894
MA = 148
86008
Ha = 210
686 n
mi
Hp = 209
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14689052
00 X = -4495989
38
Y = -1592883
11 feet Y = -535683
25 meter
Z = 16565936
81 Z = 5027501
92
XDOT = -4536
594706 XDOT = -1291
692084
YDOT = -23944
595277 feet/sec YDOT = -7313
266087 meter/sec
ZDOT = -6313
540748 ZDOT = -1930
864083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4966927
73 X = 1513919
57
Y = 14019970
14 feet Y = 4273286
90 meter
Z = 16477434
69 Z = 5022322
09
XDOT = -18614
936825 XDOT = -5673
832744
YDOT = 14059
057453 feet/sec YDOT = 4285
200712 meter/sec
ZDOT = -6339
519575 ZDOT = -1932
285567
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
58157443
00016717 00000-0 10270-3 0 9113
2 25544 51
6384 68
0461 0009164 281
4288 78
5838 15
59827976 3783
Satellite: ISS
Catalog Number: 25544
Epoch time: 11186
58157443 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 68
0461 deg
Eccentricity:
0009164
Arg of perigee: 281
4288 deg
Mean anomaly: 78
5838 deg
Mean motion: 15
59827976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 378
Checksum: 350
Coasting Arc #13 (Orbit 392)
---------------------------------------
Vector Time (GMT): 2011/187/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4616128
33 A = 6769454
55 meter
Y = 4036570
82 meter E =
0006698
Z = -2857159
95 I = 51
95288
XDOT = -1645
746637 Wp = 313
79201
YDOT = 5496
198840 meter/sec RA = 62
55387 deg
ZDOT = 5103
157901 TA = 13
77564
MA = 13
75737
Ha = 210
996 n
mi
Hp = 209
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15144777
99 X = 4584526
92
Y = 13243342
60 feet Y = 4088014
74 meter
Z = -9373884
36 Z = -2834811
48
XDOT = -5399
431223 XDOT = -1731
873776
YDOT = 18032
148426 feet/sec YDOT = 5477
313077 meter/sec
ZDOT = 16742
644031 ZDOT = 5094
954261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5021839
39 X = 1530656
65
Y = -19524877
89 feet Y = -5951182
78 meter
Z = -9283340
14 Z = -2829562
07
XDOT = 17161
021510 XDOT = 5230
679356
YDOT = -3535
215036 feet/sec YDOT = -1077
533543 meter/sec
ZDOT = 16709
008845 ZDOT = 5092
905896
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 11187
54259386
00016717 00000-0 10270-3 0 9120
2 25544 51
6375 63
2127 0009253 285
2414 74
7718 15
59805751 3930
Satellite: ISS
Catalog Number: 25544
Epoch time: 11187
54259386 = yrday
fracday
Element set: 912
Inclination: 51
6375 deg
RA of node: 63
2127 deg
Eccentricity:
0009253
Arg of perigee: 285
2414 deg
Mean anomaly: 74
7718 deg
Mean motion: 15
59805751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 393
Checksum: 324
Coasting Arc #14 (Orbit 408)
---------------------------------------
Vector Time (GMT): 2011/188/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3199124
13 A = 6772730
72 meter
Y = -5933571
17 meter E =
0005602
Z = -614698
26 I = 51
94893
XDOT = 4441
899930 Wp = 198
02822
YDOT = -1771
913406 meter/sec RA = 57
57545 deg
ZDOT = -6004
021884 TA = 348
59390
MA = 348
60659
Ha = 211
071 n
mi
Hp = 209
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10495814
06 X = -3129549
95
Y = -19467097
01 feet Y = -5968956
66 meter
Z = -2016726
59 Z = -630071
02
XDOT = 14573
162499 XDOT = 4490
549879
YDOT = -5813
364192 feet/sec YDOT = -1721
968814 meter/sec
ZDOT = -19698
234529 ZDOT = -5982
325307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12387312
09 X = -3775652
72
Y = 18314752
76 feet Y = 5582336
64 meter
Z = -2078820
70 Z = -633624
55
XDOT = -10627
856164 XDOT = -3239
370559
YDOT = -9417
445287 feet/sec YDOT = -2870
437323 meter/sec
ZDOT = -19610
005417 ZDOT = -5977
129651
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 11188
56767109
00016717 00000-0 10270-3 0 9131
2 25544 51
6375 58
0584 0009183 288
1643 71
8513 15
59796303 4098
Satellite: ISS
Catalog Number: 25544
Epoch time: 11188
56767109 = yrday
fracday
Element set: 913
Inclination: 51
6375 deg
RA of node: 58
0584 deg
Eccentricity:
0009183
Arg of perigee: 288
1643 deg
Mean anomaly: 71
8513 deg
Mean motion: 15
59796303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 409
Checksum: 333
Coasting Arc #15 (Orbit 424)
---------------------------------------
Vector Time (GMT): 2011/189/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 492405
42 A = 6766594
04 meter
Y = 5564357
93 meter E =
0003490
Z = 3814512
16 I = 51
91113
XDOT = -5966
625631 Wp = 52
21647
YDOT = -2362
018997 meter/sec RA = 52
58445 deg
ZDOT = 4215
239552 TA = 353
54957
MA = 353
55406
Ha = 211
349 n
mi
Hp = 208
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1615503
34 X = 411616
97
Y = 18255767
49 feet Y = 5569412
19 meter
Z = 12514803
66 Z = 3816708
60
XDOT = -19575
543410 XDOT = -5960
246394
YDOT = -7749
406158 feet/sec YDOT = -2428
706211 meter/sec
ZDOT = 13829
526088 ZDOT = 4186
269067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15289817
94 X = 4660336
51
Y = -10094024
41 feet Y = -3076658
64 meter
Z = 12523391
98 Z = 3817129
88
XDOT = 1874
413757 XDOT = 571
321313
YDOT = 19853
536588 feet/sec YDOT = 6051
357952 meter/sec
ZDOT = 13711
998243 ZDOT = 4179
417065
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 11189
59273703
00016717 00000-0 10270-3 0 9148
2 25544 51
6370 52
9021 0009313 293
3302 66
6873 15
59825411 4259
Satellite: ISS
Catalog Number: 25544
Epoch time: 11189
59273703 = yrday
fracday
Element set: 914
Inclination: 51
6370 deg
RA of node: 52
9021 deg
Eccentricity:
0009313
Arg of perigee: 293
3302 deg
Mean anomaly: 66
6873 deg
Mean motion: 15
59825411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 425
Checksum: 301
Coasting Arc #16 (Orbit 438)
---------------------------------------
Vector Time (GMT): 2011/190/12:53:04
306
Vector Time (MET): N/A
Weight (LBS) : 897711
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2662206
07 A = 6760778
63 meter
Y = -3253762
12 meter E =
0008253
Z = -5300627
00 I = 51
87174
XDOT = 5468
839127 Wp = 51
25761
YDOT = 5355
470811 meter/sec RA = 47
55219 deg
ZDOT = -536
260076 TA = 213
61903
MA = 213
67142
Ha = 211
461 n
mi
Hp = 208
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8734271
89 X = 2724141
81
Y = -10675072
59 feet Y = -3223644
73 meter
Z = -17390508
54 Z = -5287544
02
XDOT = 17942
385586 XDOT = 5411
151804
YDOT = 17570
442294 feet/sec YDOT = 5416
304219 meter/sec
ZDOT = -1759
383453 ZDOT = -509
831968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13648232
83 X = -4159981
37
Y = -2413041
30 feet Y = -735494
99 meter
Z = -17337169
32 Z = -5284369
21
XDOT = 6235
905862 XDOT = 1900
704107
YDOT = -23292
667752 feet/sec YDOT = -7099
605131 meter/sec
ZDOT = -1652
370441 ZDOT = -503
642511
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 11190
55372618
00016717 00000-0 10270-3 0 9152
2 25544 51
6360 48
0688 0009263 296
4737 63
5468 15
59867172 4394
Satellite: ISS
Catalog Number: 25544
Epoch time: 11190
55372618 = yrday
fracday
Element set: 915
Inclination: 51
6360 deg
RA of node: 48
0688 deg
Eccentricity:
0009263
Arg of perigee: 296
4737 deg
Mean anomaly: 63
5468 deg
Mean motion: 15
59867172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 439
Checksum: 340
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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