Date:
January 14th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
013/09:05:18
953 -3
7 4
5 4
5
N/A -2
2 -0
4 194
1
000/00:10:33
906 -1
4 0
2 186
7
Coasting Arc #1 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2011/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4906253
54 A = 6726974
90 meter
Y = -1094455
34 meter E =
0014134
Z = -4484488
88 I = 51
34359
XDOT = -1330
696853 Wp = 116
99184
YDOT = -6889
559109 meter/sec RA = 238
10386 deg
ZDOT = 3138
559294 TA = 184
52597
MA = 184
53877
Ha = 193
445 n
mi
Hp = 184
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16096632
34 X = -4871865
82
Y = -3590732
73 feet Y = -1149127
51 meter
Z = -14712890
04 Z = -4508239
81
XDOT = -4365
803323 XDOT = -1268
804040
YDOT = -22603
540385 feet/sec YDOT = -6904
093873 meter/sec
ZDOT = 10297
110546 ZDOT = 3132
244782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2342177
42 X = -713895
68
Y = -16238445
55 feet Y = -4949478
20 meter
Z = -14808482
65 Z = -4513625
51
XDOT = 18362
732080 XDOT = 5596
960738
YDOT = -12012
018487 feet/sec YDOT = -3661
263235 meter/sec
ZDOT = 10271
814291 ZDOT = 3130
848996
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 11012
51038392
00016717 00000-0 10270-3 0 9003
2 25544 51
6447 238
9974 0004403 131
2087 228
9456 15
72728776 16403
Satellite: ISS
Catalog Number: 25544
Epoch time: 11012
51038392 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 238
9974 deg
Eccentricity:
0004403
Arg of perigee: 131
2087 deg
Mean anomaly: 228
9456 deg
Mean motion: 15
72728776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1640
Checksum: 310
Coasting Arc #2 (Orbit 1653)
---------------------------------------
Vector Time (GMT): 2011/013/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700472
88 A = 6726509
88 meter
Y = 3334600
57 meter E =
0014835
Z = -5192225
11 I = 51
34870
XDOT = -5125
090011 Wp = 101
77370
YDOT = -5647
411646 meter/sec RA = 233
59430 deg
ZDOT = -966
690325 TA = 158
99060
MA = 158
92959
Ha = 194
123 n
mi
Hp = 186
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8859819
15 X = -2712337
58
Y = 10940290
59 feet Y = 3304336
26 meter
Z = -17034859
30 Z = -5205372
53
XDOT = -16814
599774 XDOT = -5056
862708
YDOT = -18528
253433 feet/sec YDOT = -5704
341951 meter/sec
ZDOT = -3171
556183 ZDOT = -991
422495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7152578
16 X = -2180105
82
Y = -12050679
49 feet Y = -3673047
11 meter
Z = -17087847
56 Z = -5208375
94
XDOT = 22378
879652 XDOT = 6821
082518
YDOT = -8669
115982 feet/sec YDOT = -2642
346551 meter/sec
ZDOT = -3271
026221 ZDOT = -997
008792
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 11013
39996313
00016717 00000-0 10270-3 0 9017
2 25544 51
6448 234
4373 0004903 178
3889 181
7290 15
71868881 16543
Satellite: ISS
Catalog Number: 25544
Epoch time: 11013
39996313 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 234
4373 deg
Eccentricity:
0004903
Arg of perigee: 178
3889 deg
Mean anomaly: 181
7290 deg
Mean motion: 15
71868881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1654
Checksum: 334
Coasting Arc #3 (Orbit 1669)
---------------------------------------
Vector Time (GMT): 2011/014/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5176926
84 A = 6737293
65 meter
Y = 4022597
11 meter E =
0016817
Z = 1508920
01 I = 51
40358
XDOT = -1972
443413 Wp = 133
50509
YDOT = 4711
982473 meter/sec RA = 228
43389 deg
ZDOT = -5765
673490 TA = 29
81761
MA = 29
72189
Ha = 194
064 n
mi
Hp = 186
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16984668
11 X = 5124230
63
Y = 13197497
07 feet Y = 4080193
86 meter
Z = 4950524
98 Z = 1533941
69
XDOT = -6471
271039 XDOT = -1996
978673
YDOT = 15459
260081 feet/sec YDOT = 4689
788707 meter/sec
ZDOT = -18916
251609 ZDOT = -5775
314771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18129241
66 X = -5525792
86
Y = 11531546
16 feet Y = 3514815
27 meter
Z = 5051199
58 Z = 1539605
63
XDOT = -11580
523287 XDOT = -3529
743498
YDOT = -9862
865215 feet/sec YDOT = -3006
201318 meter/sec
ZDOT = -18955
150283 ZDOT = -5777
529806
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 11014
41717912
00016717 00000-0 10270-3 0 9028
2 25544 51
6444 229
2305 0004991 182
3286 177
7853 15
71844963 16702
Satellite: ISS
Catalog Number: 25544
Epoch time: 11014
41717912 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 229
2305 deg
Eccentricity:
0004991
Arg of perigee: 182
3286 deg
Mean anomaly: 177
7853 deg
Mean motion: 15
71844963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1670
Checksum: 314
Coasting Arc #4 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2011/015/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 618374
31 A = 6728183
89 meter
Y = -4678687
94 meter E =
0010116
Z = 4793825
79 I = 51
39455
XDOT = 6458
429902 Wp = 146
28244
YDOT = 3388
715544 meter/sec RA = 223
33129 deg
ZDOT = 2463
450934 TA = 279
48759
MA = 279
60190
Ha = 193
881 n
mi
Hp = 187
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2028787
12 X = 647358
98
Y = -15350026
04 feet Y = -4671611
31 meter
Z = 15727774
91 Z = 4796899
77
XDOT = 21189
074482 XDOT = 6408
089742
YDOT = 11117
833148 feet/sec YDOT = 3460
655890 meter/sec
ZDOT = 8082
188103 ZDOT = 2494
703793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13923705
66 X = 4243945
49
Y = 6743717
09 feet Y = 2055484
97 meter
Z = 15740231
27 Z = 4797622
49
XDOT = -16805
239843 XDOT = -5122
237104
YDOT = 15457
304803 feet/sec YDOT = 4711
386504 meter/sec
ZDOT = 8207
976665 ZDOT = 2501
791288
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 11015
43437779
00016717 00000-0 10270-3 0 9032
2 25544 51
6446 224
0234 0004804 186
9763 173
1333 15
71894847 16867
Satellite: ISS
Catalog Number: 25544
Epoch time: 11015
43437779 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 224
0234 deg
Eccentricity:
0004804
Arg of perigee: 186
9763 deg
Mean anomaly: 173
1333 deg
Mean motion: 15
71894847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 323
Coasting Arc #5 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2011/016/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5873020
52 A = 6734724
12 meter
Y = -1826820
49 meter E =
0003781
Z = -2749295
58 I = 51
43988
XDOT = -628
957988 Wp = 126
35581
YDOT = -5694
709089 meter/sec RA = 218
15310 deg
ZDOT = 5130
220998 TA = 202
18594
MA = 202
20231
Ha = 193
672 n
mi
Hp = 187
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19268440
04 X = -5838800
75
Y = -5993505
56 feet Y = -1892304
51 meter
Z = -9019998
64 Z = -2777743
48
XDOT = -2063
510458 XDOT = -590
153326
YDOT = -18683
428771 feet/sec YDOT = -5701
526091 meter/sec
ZDOT = 16831
433720 ZDOT = 5127
259164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11543884
56 X = 3518576
02
Y = -16488004
19 feet Y = -5025543
68 meter
Z = -9134534
09 Z = -2784205
99
XDOT = 17255
647897 XDOT = 5259
521479
YDOT = 2767
930935 feet/sec YDOT = 843
665349 meter/sec
ZDOT = 16819
598742 ZDOT = 5126
613697
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 11016
38798753
00016717 00000-0 10270-3 0 9040
2 25544 51
6444 219
1415 0004712 192
6512 167
4532 15
71925170 17014
Satellite: ISS
Catalog Number: 25544
Epoch time: 11016
38798753 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 219
1415 deg
Eccentricity:
0004712
Arg of perigee: 192
6512 deg
Mean anomaly: 167
4532 deg
Mean motion: 15
71925170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1701
Checksum: 298
Coasting Arc #6 (Orbit 1716)
---------------------------------------
Vector Time (GMT): 2011/017/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1725522
38 A = 6730729
95 meter
Y = 5039344
16 meter E =
0006038
Z = -4118205
32 I = 51
45043
XDOT = -6671
237830 Wp = 109
04034
YDOT = -776
320860 meter/sec RA = 213
06795 deg
ZDOT = -3751
617293 TA = 122
41256
MA = 122
35413
Ha = 193
506 n
mi
Hp = 187
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5661162
65 X = 1689048
40
Y = 16533281
36 feet Y = 5058436
55 meter
Z = -13511172
29 Z = -4109910
86
XDOT = -21887
263221 XDOT = -6643
836672
YDOT = -2546
984449 feet/sec YDOT = -850
769008 meter/sec
ZDOT = -12308
455685 ZDOT = -3783
959163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17485164
99 X = -5329478
29
Y = 752781
52 feet Y = 229447
81 meter
Z = -13477843
19 Z = -4108046
61
XDOT = 8758
501989 XDOT = 2669
591406
YDOT = -18888
374621 feet/sec YDOT = -5757
176584 meter/sec
ZDOT = -12438
709013 ZDOT = -3791
318507
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 11017
40515624
00016717 00000-0 10270-3 0 9059
2 25544 51
6438 213
9340 0004731 198
5742 161
5248 15
71938933 17174
Satellite: ISS
Catalog Number: 25544
Epoch time: 11017
40515624 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 213
9340 deg
Eccentricity:
0004731
Arg of perigee: 198
5742 deg
Mean anomaly: 161
5248 deg
Mean motion: 15
71938933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1717
Checksum: 307
Coasting Arc #7 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2011/018/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5553001
55 A = 6731579
78 meter
Y = -454386
23 meter E =
0010014
Z = 3767254
37 I = 51
48035
XDOT = 3310
473049 Wp = 105
67899
YDOT = 5538
580224 meter/sec RA = 207
88455 deg
ZDOT = -4205
077293 TA = 28
60240
MA = 28
54750
Ha = 193
136 n
mi
Hp = 187
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18218509
03 X = 5539369
65
Y = -1490768
46 feet Y = -392365
86 meter
Z = 12359758
43 Z = 3794197
09
XDOT = 10861
132050 XDOT = 3268
720608
YDOT = 18171
194962 feet/sec YDOT = 5575
366954 meter/sec
ZDOT = -13796
185346 ZDOT = -4189
096164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3475502
53 X = -1059333
17
Y = 17870715
17 feet Y = 5446993
98 meter
Z = 12468300
28 Z = 3800337
93
XDOT = -19150
890995 XDOT = -5837
191575
YDOT = 5871
136991 feet/sec YDOT = 1789
522555 meter/sec
ZDOT = -13731
889126 ZDOT = -4185
479805
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 11018
42230881
00016717 00000-0 10270-3 0 9062
2 25544 51
6437 208
7265 0004546 202
4870 157
6093 15
72007349 17333
Satellite: ISS
Catalog Number: 25544
Epoch time: 11018
42230881 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 208
7265 deg
Eccentricity:
0004546
Arg of perigee: 202
4870 deg
Mean anomaly: 157
6093 deg
Mean motion: 15
72007349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1733
Checksum: 299
Coasting Arc #8 (Orbit 1748)
---------------------------------------
Vector Time (GMT): 2011/019/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3968333
32 A = 6733610
93 meter
Y = -4410322
52 meter E =
0011353
Z = 3179061
22 I = 51
51332
XDOT = 5766
589271 Wp = 106
42161
YDOT = -1715
831364 meter/sec RA = 202
80416 deg
ZDOT = 4800
592671 TA = 290
69175
MA = 290
81342
Ha = 193
200 n
mi
Hp = 187
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13019466
26 X = -3934164
21
Y = -14469562
06 feet Y = -4454508
06 meter
Z = 10429990
87 Z = 3159866
16
XDOT = 18919
256139 XDOT = 5762
027664
YDOT = -5629
367991 feet/sec YDOT = -1651
371838 meter/sec
ZDOT = 15749
975956 ZDOT = 4828
594758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17317441
87 X = 5278356
28
Y = -8977023
20 feet Y = -2736196
67 meter
Z = 10352714
57 Z = 3155507
40
XDOT = 7
661376 XDOT = 2
335187
YDOT = 18374
456977 feet/sec YDOT = 5600
534487 meter/sec
ZDOT = 15862
818212 ZDOT = 4834
986991
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 11019
43944691
00016717 00000-0 10270-3 0 9076
2 25544 51
6429 203
5179 0004527 207
1190 152
9736 15
71981944 17497
Satellite: ISS
Catalog Number: 25544
Epoch time: 11019
43944691 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 203
5179 deg
Eccentricity:
0004527
Arg of perigee: 207
1190 deg
Mean anomaly: 152
9736 deg
Mean motion: 15
71981944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1749
Checksum: 327
Coasting Arc #9 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2011/020/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4332361
15 A = 6728707
45 meter
Y = 2420695
66 meter E =
0010453
Z = -4553844
08 I = 51
52561
XDOT = -5599
408864 Wp = 136
09071
YDOT = -4308
645626 meter/sec RA = 197
62714 deg
ZDOT = 3033
475412 TA = 164
18637
MA = 164
15371
Ha = 192
971 n
mi
Hp = 187
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14213783
31 X = -4336986
76
Y = 7941914
91 feet Y = 2372223
02 meter
Z = -14940433
33 Z = -4574901
13
XDOT = -18370
763989 XDOT = -5565
548249
YDOT = -14135
976464 feet/sec YDOT = -4371
072468 meter/sec
ZDOT = 9952
347153 ZDOT = 3006
356267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4362105
64 X = -1329569
80
Y = -15605583
38 feet Y = -4756581
81 meter
Z = -15025311
93 Z = -4579715
07
XDOT = 16967
835397 XDOT = 5171
796229
YDOT = -14230
191720 feet/sec YDOT = -4337
362436 meter/sec
ZDOT = 9843
123147 ZDOT = 3000
183935
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 11020
39299719
00016717 00000-0 10270-3 0 9088
2 25544 51
6424 198
6347 0004608 211
4704 148
6183 15
72029893 17644
Satellite: ISS
Catalog Number: 25544
Epoch time: 11020
39299719 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 198
6347 deg
Eccentricity:
0004608
Arg of perigee: 211
4704 deg
Mean anomaly: 148
6183 deg
Mean motion: 15
72029893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1764
Checksum: 326
Coasting Arc #10 (Orbit 1779)
---------------------------------------
Vector Time (GMT): 2011/021/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5664960
68 A = 6735954
73 meter
Y = 2966908
23 meter E =
0008883
Z = -2100264
51 I = 51
57900
XDOT = -3942
644555 Wp = 170
53682
YDOT = 3619
291171 meter/sec RA = 192
54229 deg
ZDOT = -5533
506216 TA = 32
93332
MA = 32
87801
Ha = 192
918 n
mi
Hp = 187
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18585829
01 X = 5641565
52
Y = 9733950
88 feet Y = 3030126
51 meter
Z = -6890631
59 Z = -2072801
68
XDOT = -12935
185548 XDOT = -3955
943161
YDOT = 11874
314864 feet/sec YDOT = 3575
127981 meter/sec
ZDOT = -18154
547953 ZDOT = -5552
691179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13602836
12 X = -4146144
45
Y = 16020556
51 feet Y = 4883065
62 meter
Z = -6779989
86 Z = -2066540
91
XDOT = -7583
343182 XDOT = -2311
403002
YDOT = -14137
956365 feet/sec YDOT = -4309
249100 meter/sec
ZDOT = -18231
901440 ZDOT = -5557
083559
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 11021
41010301
00016717 00000-0 10270-3 0 9091
2 25544 51
6422 193
4273 0004666 215
9469 144
1379 15
72022717 17808
Satellite: ISS
Catalog Number: 25544
Epoch time: 11021
41010301 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 193
4273 deg
Eccentricity:
0004666
Arg of perigee: 215
9469 deg
Mean anomaly: 144
1379 deg
Mean motion: 15
72022717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1780
Checksum: 283
Coasting Arc #11 (Orbit 1795)
---------------------------------------
Vector Time (GMT): 2011/022/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2421134
12 A = 6726531
01 meter
Y = -3724990
59 meter E =
0001331
Z = 5049439
37 I = 51
57826
XDOT = 7140
781568 Wp = 114
26787
YDOT = 2304
402253 meter/sec RA = 187
38387 deg
ZDOT = -1724
118470 TA = 352
34009
MA = 352
34212
Ha = 192
601 n
mi
Hp = 187
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7943353
40 X = 2438079
12
Y = -12221097
72 feet Y = -3697821
32 meter
Z = 16566402
13 Z = 5061242
03
XDOT = 23427
761050 XDOT = 7122
857819
YDOT = 7560
374846 feet/sec YDOT = 2384
154588 meter/sec
ZDOT = -5656
556661 ZDOT = -1689
473007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10365426
43 X = 3159381
98
Y = 10170077
37 feet Y = 3099839
58 meter
Z = 16614007
15 Z = 5063949
38
XDOT = -11440
917219 XDOT = -3487
191568
YDOT = 20672
279918 feet/sec YDOT = 6300
910919 meter/sec
ZDOT = -5516
946417 ZDOT = -1681
565268
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 11022
42719144
00016717 00000-0 10270-3 0 9106
2 25544 51
6425 188
2184 0004598 220
3401 139
7420 15
72071535 17960
Satellite: ISS
Catalog Number: 25544
Epoch time: 11022
42719144 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 188
2184 deg
Eccentricity:
0004598
Arg of perigee: 220
3401 deg
Mean anomaly: 139
7420 deg
Mean motion: 15
72071535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1796
Checksum: 290
Coasting Arc #12 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2011/023/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6600093
41 A = 6737263
31 meter
Y = -979137
85 meter E =
0009102
Z = 904153
68 I = 51
64405
XDOT = 1509
515396 Wp = 59
73597
YDOT = -4648
357907 meter/sec RA = 182
28258 deg
ZDOT = 5945
352990 TA = 310
12390
MA = 310
20362
Ha = 192
485 n
mi
Hp = 187
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21653849
78 X = -6593046
09
Y = -3212394
53 feet Y = -1052904
68 meter
Z = 2966383
47 Z = 872108
28
XDOT = 4952
478334 XDOT = 1532
501227
YDOT = -15250
518068 feet/sec YDOT = -4631
349075 meter/sec
ZDOT = 19505
751279 ZDOT = 5952
741878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7206325
81 X = 2196488
11
Y = -20688816
39 feet Y = -6305951
24 meter
Z = 2837228
29 Z = 864787
18
XDOT = 12568
403646 XDOT = 3830
849431
YDOT = 7075
653854 feet/sec YDOT = 2156
659295 meter/sec
ZDOT = 19535
575989 ZDOT = 5954
443561
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 11023
44426353
00016717 00000-0 10270-3 0 9117
2 25544 51
6416 183
0092 0004580 224
2981 135
7815 15
72101148 18125
Satellite: ISS
Catalog Number: 25544
Epoch time: 11023
44426353 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 183
0092 deg
Eccentricity:
0004580
Arg of perigee: 224
2981 deg
Mean anomaly: 135
7815 deg
Mean motion: 15
72101148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 276
Coasting Arc #13 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2011/024/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -187341
26 A = 6725479
12 meter
Y = 4186587
87 meter E =
0012243
Z = -5270361
98 I = 51
63438
XDOT = -7680
643997 Wp = 107
90684
YDOT = 103
366308 meter/sec RA = 177
14942 deg
ZDOT = 352
104747 TA = 165
45887
MA = 165
42362
Ha = 192
330 n
mi
Hp = 187
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -614636
68 X = -208540
55
Y = 13735524
52 feet Y = 4184374
39 meter
Z = -17291213
85 Z = -5271323
55
XDOT = -25198
963244 XDOT = -7682
939446
YDOT = 339
128307 feet/sec YDOT = 17
463874 meter/sec
ZDOT = 1155
199301 ZDOT = 314
787283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13447993
00 X = -4098948
27
Y = -2838751
75 feet Y = -865251
53 meter
Z = -17295128
26 Z = -5271555
09
XDOT = 3743
399713 XDOT = 1140
988232
YDOT = -23915
581004 feet/sec YDOT = -7289
469090 meter/sec
ZDOT = 1004
772550 ZDOT = 306
254673
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 11024
39775366
00016717 00000-0 10270-3 0 9124
2 25544 51
6408 178
1257 0004494 227
2921 132
7863 15
72126254 18276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11024
39775366 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 178
1257 deg
Eccentricity:
0004494
Arg of perigee: 227
2921 deg
Mean anomaly: 132
7863 deg
Mean motion: 15
72126254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 314
Coasting Arc #14 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2011/025/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6623309
68 A = 6737307
45 meter
Y = -1156162
70 meter E =
0012632
Z = 287177
19 I = 51
70576
XDOT = 1079
310453 Wp = 151
87786
YDOT = 4660
217930 meter/sec RA = 172
03093 deg
ZDOT = -6034
592542 TA = 25
00528
MA = 24
94414
Ha = 192
049 n
mi
Hp = 187
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21730018
63 X = 6634350
81
Y = -3793184
73 feet Y = -1082035
13 meter
Z = 942182
39 Z = 319379
56
XDOT = 3541
044794 XDOT = 1056
433331
YDOT = 15289
428905 feet/sec YDOT = 4672
159609 meter/sec
ZDOT = -19798
531961 ZDOT = -6029
404827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 424425
66 X = 129364
94
Y = 22048590
02 feet Y = 6720410
24 meter
Z = 1072011
43 Z = 326749
08
XDOT = -14060
680920 XDOT = -4285
695544
YDOT = 1245
753495 feet/sec YDOT = 379
705665 meter/sec
ZDOT = -19777
663373 ZDOT = -6028
231796
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 11025
41479173
00016717 00000-0 10270-3 0 9136
2 25544 51
6413 172
9178 0004407 234
2589 125
8163 15
72183628 18430
Satellite: ISS
Catalog Number: 25544
Epoch time: 11025
41479173 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 172
9178 deg
Eccentricity:
0004407
Arg of perigee: 234
2589 deg
Mean anomaly: 125
8163 deg
Mean motion: 15
72183628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 310
Coasting Arc #15 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2011/026/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2026377
25 A = 6725808
27 meter
Y = -3749448
94 meter E =
0004544
Z = 5204158
77 I = 51
69544
XDOT = 7212
481535 Wp = 186
40985
YDOT = -2492
634285 meter/sec RA = 166
92472 deg
ZDOT = 1008
153527 TA = 253
95729
MA = 254
00734
Ha = 192
165 n
mi
Hp = 187
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6648219
31 X = -2009580
13
Y = -12301341
67 feet Y = -3772015
38 meter
Z = 17074011
71 Z = 5194355
43
XDOT = 23662
997163 XDOT = 7234
921230
YDOT = -8177
934007 feet/sec YDOT = -2411
854530 meter/sec
ZDOT = 3307
590311 ZDOT = 1043
245719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13104319
68 X = 3994196
64
Y = -5014520
22 feet Y = -1528425
76 meter
Z = 17034526
57 Z = 5192123
70
XDOT = 4520
939191 XDOT = 1377
982265
YDOT = 23579
719438 feet/sec YDOT = 7187
098485 meter/sec
ZDOT = 3449
097848 ZDOT = 1051
285024
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 11026
43181581
00016717 00000-0 10270-3 0 9143
2 25544 51
6402 167
7084 0004352 235
4261 124
6491 15
72126938 18594
Satellite: ISS
Catalog Number: 25544
Epoch time: 11026
43181581 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 167
7084 deg
Eccentricity:
0004352
Arg of perigee: 235
4261 deg
Mean anomaly: 124
6491 deg
Mean motion: 15
72126938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 301
Coasting Arc #16 (Orbit 1873)
---------------------------------------
Vector Time (GMT): 2011/027/09:10:35
906
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5791963
88 A = 6736335
36 meter
Y = 3111865
56 meter E =
0004512
Z = -1453749
25 I = 51
76108
XDOT = -3438
906495 Wp = 17
21217
YDOT = -3689
756282 meter/sec RA = 161
78615 deg
ZDOT = 5811
718510 TA = 326
83389
MA = 326
86217
Ha = 191
887 n
mi
Hp = 187
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19002506
18 X = -5819268
93
Y = 10209532
69 feet Y = 3046943
74 meter
Z = -4769518
53 Z = -1481952
37
XDOT = -11282
501624 XDOT = -3425
623239
YDOT = -12105
499613 feet/sec YDOT = -3728
138257 meter/sec
ZDOT = 19067
317945 ZDOT = 5795
044598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7880340
18 X = -2401927
69
Y = -20053228
73 feet Y = -6112224
12 meter
Z = -4883273
69 Z = -1488421
82
XDOT = 11911
844470 XDOT = 3630
730195
YDOT = -9300
975921 feet/sec YDOT = -2834
937461 meter/sec
ZDOT = 19000
127825 ZDOT = 5791
238961
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 11027
38525592
00016717 00000-0 10270-3 0 9153
2 25544 51
6401 162
8244 0004437 238
0954 121
9777 15
72200914 18740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11027
38525592 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 162
8244 deg
Eccentricity:
0004437
Arg of perigee: 238
0954 deg
Mean anomaly: 121
9777 deg
Mean motion: 15
72200914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1874
Checksum: 307
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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