Date:
April 26th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5812 51 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 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
115/10:23:36
611 -3
2 3
3 3
3
N/A -0
2 0
0 189
2
000/00:00:33
221 0
8 0
0 170
5
118/10:39:49
743 11
7 11
7 11
7
N/A 0
8 -0
0 189
0
000/00:01:59
486 1
0 -0
0 177
3
Coasting Arc #1 (Orbit 213)
---------------------------------------
Vector Time (GMT): 2007/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465395
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2079217
35 A = 6709504
11 meter
Y = -4755720
17 meter E =
0023184
Z = -4271971
85 I = 51
76829
XDOT = 6817
531400 Wp = 88
36163
YDOT = 201
542800 meter/sec RA = 25
96236 deg
ZDOT = -3558
406235 TA = 145
63773
MA = 145
48757
Ha = 187
685 n
mi
Hp = 170
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6821579
24 X = -2005131
22
Y = -15602756
47 feet Y = -4778556
67 meter
Z = -14015655
68 Z = -4281892
99
XDOT = 22367
229003 XDOT = 6832
057105
YDOT = 661
229658 feet/sec YDOT = 277
861666 meter/sec
ZDOT = -11674
561138 ZDOT = -3525
251400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13715025
86 X = -4180339
88
Y = -10040577
05 feet Y = -3060367
88 meter
Z = -14053591
53 Z = -4283534
70
XDOT = 18946
768527 XDOT = 5774
975047
YDOT = -9787
394479 feet/sec YDOT = -2983
197837 meter/sec
ZDOT = -11549
654790 ZDOT = -3520
334780
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 07113
52216523
00020000 00000-0 20000-3 0 9007
2 25544 51
6360 26
3298 0015288 99
6686 260
6207 15
79169192 2141
Satellite: ISS
Catalog Number: 25544
Epoch time: 07113
52216523 = yrday
fracday
Element set: 900
Inclination: 51
6360 deg
RA of node: 26
3298 deg
Eccentricity:
0015288
Arg of perigee: 99
6686 deg
Mean anomaly: 260
6207 deg
Mean motion: 15
79169192 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 214
Checksum: 290
Coasting Arc #2 (Orbit 229)
---------------------------------------
Vector Time (GMT): 2007/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465395
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6425053
58 A = 6716501
50 meter
Y = -1133909
56 meter E =
0029128
Z = 1544210
84 I = 51
76503
XDOT = -514
874439 Wp = 110
28915
YDOT = -5074
820072 meter/sec RA = 20
75644 deg
ZDOT = -5791
224468 TA = 52
65980
MA = 52
39478
Ha = 187
673 n
mi
Hp = 170
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21079572
11 X = -6419397
99
Y = -3720175
74 feet Y = -1205726
55 meter
Z = 5066308
51 Z = 1513011
71
XDOT = -1689
220599 XDOT = -429
956158
YDOT = -16649
672152 feet/sec YDOT = -5080
102670 meter/sec
ZDOT = -19000
080277 ZDOT = -5793
519643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19953941
70 X = -6081961
43
Y = 7823463
52 feet Y = 2384591
68 meter
Z = 4948654
23 Z = 1508349
81
XDOT = -9456
550939 XDOT = -2882
356726
YDOT = -11930
441780 feet/sec YDOT = -3636
398655 meter/sec
ZDOT = -19009
330709 ZDOT = -5794
044000
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 07114
53466560
00020000 00000-0 20000-3 0 9018
2 25544 51
6357 21
0893 0015242 103
9587 256
3275 15
79177338 2305
Satellite: ISS
Catalog Number: 25544
Epoch time: 07114
53466560 = yrday
fracday
Element set: 901
Inclination: 51
6357 deg
RA of node: 21
0893 deg
Eccentricity:
0015242
Arg of perigee: 103
9587 deg
Mean anomaly: 256
3275 deg
Mean motion: 15
79177338 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 230
Checksum: 285
Coasting Arc #3 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2007/115/10:23:53
221
Vector Time (MET): N/A
Weight (LBS) : 465220
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 920005
21 A = 6707985
87 meter
Y = 4364465
84 meter E =
0022389
Z = 4993832
86 I = 51
70515
XDOT = -7466
920931 Wp = 107
50665
YDOT = -592
144841 meter/sec RA = 15
96275 deg
ZDOT = 1879
648931 TA = 324
35199
MA = 324
50131
Ha = 189
158 n
mi
Hp = 170
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3018389
78 X = 846873
67
Y = 14319113
65 feet Y = 4374344
86 meter
Z = 16383966
08 Z = 4998124
68
XDOT = -24497
772082 XDOT = -7468
875493
YDOT = -1942
732418 feet/sec YDOT = -675
655098 meter/sec
ZDOT = 6166
827201 ZDOT = 1843
369972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4962466
84 X = 1512559
89
Y = 13746800
14 feet Y = 4190024
68 meter
Z = 16400653
82 Z = 4998919
28
XDOT = -23552
954032 XDOT = -7178
940389
YDOT = 1255
433668 feet/sec YDOT = 382
656182 meter/sec
ZDOT = 6030
101925 ZDOT = 1837
975067
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 07115
48388301
00020000 00000-0 20000-3 0 9020
2 25544 51
6350 16
1767 0017186 102
6524 257
6564 15
78652104 2458
Satellite: ISS
Catalog Number: 25544
Epoch time: 07115
48388301 = yrday
fracday
Element set: 902
Inclination: 51
6350 deg
RA of node: 16
1767 deg
Eccentricity:
0017186
Arg of perigee: 102
6524 deg
Mean anomaly: 257
6564 deg
Mean motion: 15
78652104 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 245
Checksum: 280
Coasting Arc #4 (Orbit 259)
---------------------------------------
Vector Time (GMT): 2007/116/10:23:53
221
Vector Time (MET): N/A
Weight (LBS) : 465220
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6614692
95 A = 6718985
43 meter
Y = 1158522
15 meter E =
0025354
Z = -125588
91 I = 51
71424
XDOT = -731
389623 Wp = 80
57581
YDOT = 4719
313346 meter/sec RA = 10
78008 deg
ZDOT = 6046
537492 TA = 278
05917
MA = 278
34676
Ha = 189
177 n
mi
Hp = 170
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21701748
51 X = 6601856
65
Y = 3800925
69 feet Y = 1232419
58 meter
Z = -412037
10 Z = -93485
93
XDOT = -2399
572253 XDOT = -813
480271
YDOT = 15483
311501 feet/sec YDOT = 4710
675531 meter/sec
ZDOT = 19837
721429 ZDOT = 6042
785017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22032595
70 X = 6715535
17
Y = 250517
84 feet Y = 76357
84 meter
Z = -290975
04 Z = -88689
19
XDOT = 38
284358 XDOT = 11
669072
YDOT = 14078
659211 feet/sec YDOT = 4291
175328 meter/sec
ZDOT = 19824
151709 ZDOT = 6042
401441
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 07116
43342763
00020000 00000-0 20000-3 0 9039
2 25544 51
6352 11
2660 0017188 105
7762 254
5300 15
78643147 2606
Satellite: ISS
Catalog Number: 25544
Epoch time: 07116
43342763 = yrday
fracday
Element set: 903
Inclination: 51
6352 deg
RA of node: 11
2660 deg
Eccentricity:
0017188
Arg of perigee: 105
7762 deg
Mean anomaly: 254
5300 deg
Mean motion: 15
78643147 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 260
Checksum: 267
Coasting Arc #5 (Orbit 275)
---------------------------------------
Vector Time (GMT): 2007/117/10:23:53
221
Vector Time (MET): N/A
Weight (LBS) : 465220
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2235701
41 A = 6707740
19 meter
Y = -3813395
90 meter E =
0030625
Z = -5072418
85 I = 51
64888
XDOT = 7224
600613 Wp = 106
24115
YDOT = 2027
671407 meter/sec RA = 5
59834 deg
ZDOT = 1659
766237 TA = 179
74520
MA = 179
74364
Ha = 189
039 n
mi
Hp = 170
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7334978
37 X = 2302818
15
Y = -12511141
41 feet Y = -3788019
81 meter
Z = -16641794
14 Z = -5061394
73
XDOT = 23702
757916 XDOT = 7193
327083
YDOT = 6652
465246 feet/sec YDOT = 2108
286094 meter/sec
ZDOT = 5445
427288 ZDOT = 1694
787462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5078707
93 X = 1547990
18
Y = -13634605
51 feet Y = -4155827
76 meter
Z = -16600727
02 Z = -5059901
60
XDOT = 23484
449130 XDOT = 7158
060095
YDOT = 1956
134823 feet/sec YDOT = 596
229894 meter/sec
ZDOT = 5577
582719 ZDOT = 1700
047213
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 07117
44624886
00020000 00000-0 20000-3 0 9041
2 25544 51
6360 6
0276 0017114 109
7059 250
5955 15
78689672 2764
Satellite: ISS
Catalog Number: 25544
Epoch time: 07117
44624886 = yrday
fracday
Element set: 904
Inclination: 51
6360 deg
RA of node: 6
0276 deg
Eccentricity:
0017114
Arg of perigee: 109
7059 deg
Mean anomaly: 250
5955 deg
Mean motion: 15
78689672 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 276
Checksum: 307
Coasting Arc #6 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2007/118/10:23:53
221
Vector Time (MET): N/A
Weight (LBS) : 465220
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5584216
25 A = 6714974
54 meter
Y = -2344825
50 meter E =
0021580
Z = -2905865
05 I = 51
64568
XDOT = 4267
000626 Wp = 113
04413
YDOT = -3957
188569 meter/sec RA =
46539 deg
ZDOT = -5044
549551 TA = 100
43434
MA = 100
19107
Ha = 188
870 n
mi
Hp = 170
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18320919
47 X = -5543464
77
Y = -7692997
05 feet Y = -2407043
51 meter
Z = -9533677
98 Z = -2932894
36
XDOT = 13999
345886 XDOT = 4335
439036
YDOT = -12982
902129 feet/sec YDOT = -3909
089968 meter/sec
ZDOT = -16550
359419 ZDOT = -5023
654036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19417494
28 X = -5918452
26
Y = -3980233
07 feet Y = -1213175
04 meter
Z = -9635765
17 Z = -2936981
23
XDOT = 10996
759988 XDOT = 3351
812444
YDOT = -14067
087807 feet/sec YDOT = -4287
648364 meter/sec
ZDOT = -16472
129558 ZDOT = -5020
705089
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 07118
45904465
00020000 00000-0 20000-3 0 9058
2 25544 51
6365
7892 0017026 113
7731 246
5222 15
78729275 2922
Satellite: ISS
Catalog Number: 25544
Epoch time: 07118
45904465 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node:
7892 deg
Eccentricity:
0017026
Arg of perigee: 113
7731 deg
Mean anomaly: 246
5222 deg
Mean motion: 15
78729275 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 292
Checksum: 292
Coasting Arc #7 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2007/118/10:40:49
486
Vector Time (MET): N/A
Weight (LBS) : 464587
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1211322
27 A = 6713279
39 meter
Y = -4104276
09 meter E =
0022111
Z = -5191531
38 I = 51
61839
XDOT = 7563
574844 Wp = 110
48529
YDOT = 887
812366 meter/sec RA =
37151 deg
ZDOT = 1058
939629 TA = 169
65656
MA = 169
61100
Ha = 189
035 n
mi
Hp = 177
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3974154
44 X = 1282346
56
Y = -13465472
74 feet Y = -4090333
34 meter
Z = -17032583
26 Z = -5185474
17
XDOT = 24814
878098 XDOT = 7547
940880
YDOT = 2912
770229 feet/sec YDOT = 972
305095 meter/sec
ZDOT = 3474
211381 ZDOT = 1095
645758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 322839
26 X = 98401
41
Y = -14063021
90 feet Y = -4286409
08 meter
Z = -17010259
90 Z = -5184727
22
XDOT = 23646
289142 XDOT = 7207
388930
YDOT = -3842
586277 feet/sec YDOT = -1171
220297 meter/sec
ZDOT = 3612
572092 ZDOT = 1101
111974
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 07118
45904645
00020000 00000-0 20000-3 0 9069
2 25544 51
6365
7896 0008596 132
1026 228
0871 15
76541422 2929
Satellite: ISS
Catalog Number: 25544
Epoch time: 07118
45904645 = yrday
fracday
Element set: 906
Inclination: 51
6365 deg
RA of node:
7896 deg
Eccentricity:
0008596
Arg of perigee: 132
1026 deg
Mean anomaly: 228
0871 deg
Mean motion: 15
76541422 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 292
Checksum: 290
Coasting Arc #8 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2007/119/10:40:49
486
Vector Time (MET): N/A
Weight (LBS) : 464587
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6419843
02 A = 6723528
74 meter
Y = -876535
59 meter E =
0015905
Z = -1775659
90 I = 51
62458
XDOT = 2205
023921 Wp = 138
84299
YDOT = -4705
069930 meter/sec RA = 355
24103 deg
ZDOT = -5690
057966 TA = 60
85953
MA = 60
70043
Ha = 188
898 n
mi
Hp = 177
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21062477
09 X = -6400938
39
Y = -2875772
94 feet Y = -948220
18 meter
Z = -5825655
85 Z = -1806801
95
XDOT = 7234
330451 XDOT = 2285
114418
YDOT = -15436
581135 feet/sec YDOT = -4679
964326 meter/sec
ZDOT = -18668
169181 ZDOT = -5679
151275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20981256
30 X = -6395086
92
Y = 3209871
36 feet Y = 978368
79 meter
Z = -5943053
68 Z = -1811442
76
XDOT = 2890
502163 XDOT = 881
025059
YDOT = -15354
277441 feet/sec YDOT = -4679
983764 meter/sec
ZDOT = -18627
651737 ZDOT = -5677
708250
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 07119
47323305
00020000 00000-0 20000-3 0 9071
2 25544 51
6367 355
5609 0008563 137
1565 223
0268 15
76538697 3084
Satellite: ISS
Catalog Number: 25544
Epoch time: 07119
47323305 = yrday
fracday
Element set: 907
Inclination: 51
6367 deg
RA of node: 355
5609 deg
Eccentricity:
0008563
Arg of perigee: 137
1565 deg
Mean anomaly: 223
0268 deg
Mean motion: 15
76538697 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 308
Checksum: 307
Coasting Arc #9 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2007/120/10:40:49
486
Vector Time (MET): N/A
Weight (LBS) : 464587
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2582555
05 A = 6715515
48 meter
Y = 4151780
17 meter E =
0013280
Z = 4590970
39 I = 51
56946
XDOT = -7043
303849 Wp = 101
74211
YDOT = -1129
192927 meter/sec RA = 350
04381 deg
ZDOT = -2936
436030 TA = 17
35429
MA = 17
30894
Ha = 188
731 n
mi
Hp = 177
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8472949
62 X = -2651091
38
Y = 13621326
01 feet Y = 4122517
34 meter
Z = 15062238
81 Z = 4578257
70
XDOT = -23107
952260 XDOT = -7015
888666
YDOT = -3704
701203 feet/sec YDOT = -1207
801781 meter/sec
ZDOT = -9633
976478 ZDOT = -2970
586376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4072848
43 X = -1241404
20
Y = 15561765
67 feet Y = 4743226
18 meter
Z = 15014852
34 Z = 4576526
99
XDOT = -21967
834195 XDOT = -6695
795863
YDOT = 3684
325772 feet/sec YDOT = 1122
982495 meter/sec
ZDOT = -9762
730394 ZDOT = -2975
680224
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 07120
48739706
00020000 00000-0 20000-3 0 9081
2 25544 51
6363 350
3324 0008327 140
0343 220
1435 15
76637359 3249
Satellite: ISS
Catalog Number: 25544
Epoch time: 07120
48739706 = yrday
fracday
Element set: 908
Inclination: 51
6363 deg
RA of node: 350
3324 deg
Eccentricity:
0008327
Arg of perigee: 140
0343 deg
Mean anomaly: 220
1435 deg
Mean motion: 15
76637359 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 324
Checksum: 272
Coasting Arc #10 (Orbit 339)
---------------------------------------
Vector Time (GMT): 2007/121/10:40:49
486
Vector Time (MET): N/A
Weight (LBS) : 464587
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5748032
96 A = 6719964
13 meter
Y = 1147281
36 meter E =
0018808
Z = 3278145
06 I = 51
55643
XDOT = -3675
147818 Wp = 109
56145
YDOT = 4864
596699 meter/sec RA = 344
93023 deg
ZDOT = 4713
587065 TA = 288
99050
MA = 289
19420
Ha = 188
599 n
mi
Hp = 177
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18858375
85 X = 5718851
74
Y = 3764046
47 feet Y = 1211395
84 meter
Z = 10755069
09 Z = 3305998
70
XDOT = -12057
571580 XDOT = -3752
169496
YDOT = 15959
962924 feet/sec YDOT = 4823
068355 meter/sec
ZDOT = 15464
524490 ZDOT = 4695
545895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19022839
53 X = 5798161
49
Y = -2380660
89 feet Y = -725625
44 meter
Z = 10860107
11 Z = 3310160
65
XDOT = -6640
136742 XDOT = -2023
913679
YDOT = 17596
209363 feet/sec YDOT = 5363
324614 meter/sec
ZDOT = 15397
151820 ZDOT = 4693
051875
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 07121
50154277
00020000 00000-0 20000-3 0 9090
2 25544 51
6363 345
1031 0008325 143
6291 216
5441 15
76618802 3401
Satellite: ISS
Catalog Number: 25544
Epoch time: 07121
50154277 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node: 345
1031 deg
Eccentricity:
0008325
Arg of perigee: 143
6291 deg
Mean anomaly: 216
5441 deg
Mean motion: 15
76618802 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 340
Checksum: 263
Coasting Arc #11 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2007/122/10:40:49
486
Vector Time (MET): N/A
Weight (LBS) : 464587
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3761321
53 A = 6719360
66 meter
Y = -4348807
24 meter E =
0011855
Z = -3492179
98 I = 51
52699
XDOT = 6025
774994 Wp = 127
57867
YDOT = 1593
262824 meter/sec RA = 339
71546 deg
ZDOT = 4509
414101 TA = 190
88725
MA = 190
91293
Ha = 188
434 n
mi
Hp = 177
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12340293
74 X = 3826635
71
Y = -14267740
28 feet Y = -4306380
67 meter
Z = -11457283
41 Z = -3473748
66
XDOT = 19769
602999 XDOT = 5985
604665
YDOT = 5227
240237 feet/sec YDOT = 1660
421592 meter/sec
ZDOT = 14794
665687 ZDOT = 4538
590440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6947803
86 X = 2117690
62
Y = -17582761
14 feet Y = -5359225
59 meter
Z = -11388377
30 Z = -3471177
40
XDOT = 19021
938201 XDOT = 5797
886764
YDOT = -2130
222061 feet/sec YDOT = -649
291684 meter/sec
ZDOT = 14904
735992 ZDOT = 4542
963530
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 07122
45228316
00020000 00000-0 20000-3 0 9103
2 25544 51
6361 340
2006 0008157 148
4611 211
7044 15
76662975 3551
Satellite: ISS
Catalog Number: 25544
Epoch time: 07122
45228316 = yrday
fracday
Element set: 910
Inclination: 51
6361 deg
RA of node: 340
2006 deg
Eccentricity:
0008157
Arg of perigee: 148
4611 deg
Mean anomaly: 211
7044 deg
Mean motion: 15
76662975 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 355
Checksum: 266
Coasting Arc #12 (Orbit 370)
---------------------------------------
Vector Time (GMT): 2007/123/10:40:49
486
Vector Time (MET): N/A
Weight (LBS) : 464587
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4700112
95 A = 6715645
49 meter
Y = -1720711
50 meter E =
0013545
Z = -4486809
10 I = 51
48793
XDOT = 4853
073138 Wp = 105
41917
YDOT = -5077
678777 meter/sec RA = 334
59854 deg
ZDOT = -3147
886753 TA = 133
12628
MA = 133
01292
Ha = 188
213 n
mi
Hp = 177
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15420318
06 X = -4658725
81
Y = -5645378
93 feet Y = -1773039
07 meter
Z = -14720502
30 Z = -4509542
32
XDOT = 15922
155964 XDOT = 4924
783971
YDOT = -16659
051106 feet/sec YDOT = -5023
007815 meter/sec
ZDOT = -10327
712444 ZDOT = -3124
136198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16343763
03 X = -4981578
97
Y = 62937
80 feet Y = 19183
44 meter
Z = -14806321
25 Z = -4512966
72
XDOT = 9164
972709 XDOT = 2793
483682
YDOT = -19996
727144 feet/sec YDOT = -6095
002433 meter/sec
ZDOT = -10238
853471 ZDOT = -3120
802538
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 07123
46638684
00020000 00000-0 20000-3 0 9119
2 25544 51
6355 334
9707 0008059 153
0706 207
0878 15
76694377 3712
Satellite: ISS
Catalog Number: 25544
Epoch time: 07123
46638684 = yrday
fracday
Element set: 911
Inclination: 51
6355 deg
RA of node: 334
9707 deg
Eccentricity:
0008059
Arg of perigee: 153
0706 deg
Mean anomaly: 207
0878 deg
Mean motion: 15
76694377 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 371
Checksum: 313
Coasting Arc #13 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2007/124/10:40:49
486
Vector Time (MET): N/A
Weight (LBS) : 464587
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4596185
73 A = 6722881
77 meter
Y = 4496274
95 meter E =
0020829
Z = 1921873
61 I = 51
48716
XDOT = -4711
539774 Wp = 127
99693
YDOT = -2404
140866 meter/sec RA = 329
39033 deg
ZDOT = -5614
704143 TA = 30
53385
MA = 30
41275
Ha = 188
191 n
mi
Hp = 177
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15079349
50 X = -4655458
42
Y = 14751558
24 feet Y = 4444546
24 meter
Z = 6305359
62 Z = 1899401
35
XDOT = -15457
807657 XDOT = -4657
030407
YDOT = -7887
601267 feet/sec YDOT = -2456
522646 meter/sec
ZDOT = -18420
945350 ZDOT = -5637
461063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8685441
04 X = -2647322
43
Y = 19251287
57 feet Y = 5867792
45 meter
Z = 6221242
04 Z = 1896234
57
XDOT = -15770
711987 XDOT = -4806
913014
YDOT = -1103
868171 feet/sec YDOT = -336
459019 meter/sec
ZDOT = -18506
934016 ZDOT = -5640
913488
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 07124
48047105
00020000 00000-0 20000-3 0 9125
2 25544 51
6357 329
7413 0008111 156
0044 204
1500 15
76721975 3879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07124
48047105 = yrday
fracday
Element set: 912
Inclination: 51
6357 deg
RA of node: 329
7413 deg
Eccentricity:
0008111
Arg of perigee: 156
0044 deg
Mean anomaly: 204
1500 deg
Mean motion: 15
76721975 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 387
Checksum: 266
Coasting Arc #14 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2007/125/10:40:49
486
Vector Time (MET): N/A
Weight (LBS) : 464587
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3485748
42 A = 6712743
96 meter
Y = 2541059
75 meter E =
0011459
Z = 5139821
92 I = 51
42869
XDOT = -5571
089972 Wp = 148
25734
YDOT = 5191
083757 meter/sec RA = 324
24791 deg
ZDOT = 1201
004799 TA = 290
18684
MA = 290
31006
Ha = 187
923 n
mi
Hp = 178
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11436182
48 X = 3432106
13
Y = 8336810
21 feet Y = 2579738
86 meter
Z = 16862932
81 Z = 5156625
94
XDOT = -18277
854240 XDOT = -5634
557723
YDOT = 17031
114688 feet/sec YDOT = 5128
429712 meter/sec
ZDOT = 3940
304458 ZDOT = 1173
786406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13662921
46 X = 4164458
46
Y = 3385959
92 feet Y = 1032040
59 meter
Z = 16926518
54 Z = 5159202
85
XDOT = -10182
435102 XDOT = -3103
606219
YDOT = 21722
848204 feet/sec YDOT = 6621
124132 meter/sec
ZDOT = 3838
385376 ZDOT = 1169
939863
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 07125
49453343
00020000 00000-0 20000-3 0 9133
2 25544 51
6351 324
5111 0008002 160
4534 199
6938 15
76744475 4035
Satellite: ISS
Catalog Number: 25544
Epoch time: 07125
49453343 = yrday
fracday
Element set: 913
Inclination: 51
6351 deg
RA of node: 324
5111 deg
Eccentricity:
0008002
Arg of perigee: 160
4534 deg
Mean anomaly: 199
6938 deg
Mean motion: 15
76744475 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 403
Checksum: 280
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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