Date:
January 29th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2010/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5107058
56 A = 6726096
16 meter
Y = -3826021
85 meter E =
0006893
Z = -2118160
03 I = 51
38806
XDOT = 1569
678208 Wp = 278
44464
YDOT = -5150
994293 meter/sec RA = 232
21169 deg
ZDOT = 5505
342339 TA = 57
77890
MA = 57
71210
Ha = 187
110 n
mi
Hp = 183
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16755441
48 X = -5053606
31
Y = -12552565
11 feet Y = -3882832
91 meter
Z = -6949343
91 Z = -2142840
20
XDOT = 5149
862886 XDOT = 1600
417443
YDOT = -16899
587575 feet/sec YDOT = -5133
269925 meter/sec
ZDOT = 18062
146783 ZDOT = 5513
041814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 371956
09 X = 113372
22
Y = -20899828
23 feet Y = -6370267
64 meter
Z = -7047263
26 Z = -2148005
84
XDOT = 15123
745436 XDOT = 4609
717609
YDOT = -5847
035787 feet/sec YDOT = -1782
176508 meter/sec
ZDOT = 18092
489334 ZDOT = 5514
590749
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 10027
50424258
00016717 00000-0 10270-3 0 9007
2 25544 51
6415 233
1416 0011617 251
3303 108
6600 15
75430769 1310
Satellite: ISS
Catalog Number: 25544
Epoch time: 10027
50424258 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 233
1416 deg
Eccentricity:
0011617
Arg of perigee: 251
3303 deg
Mean anomaly: 108
6600 deg
Mean motion: 15
75430769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 131
Checksum: 261
Coasting Arc #2 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2010/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1476064
97 A = 6717157
21 meter
Y = 4258294
06 meter E =
0001603
Z = -4982236
30 I = 51
37615
XDOT = -6086
065429 Wp = 80
04017
YDOT = -4324
150706 meter/sec RA = 227
08177 deg
ZDOT = -1892
982412 TA = 171
62518
MA = 171
62250
Ha = 186
663 n
mi
Hp = 183
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4842732
85 X = -1499370
10
Y = 13970781
05 feet Y = 4241658
00 meter
Z = -16345919
61 Z = -4989463
04
XDOT = -19967
406263 XDOT = -6028
064158
YDOT = -14186
846148 feet/sec YDOT = -4391
884210 meter/sec
ZDOT = -6210
572217 ZDOT = -1922
407274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14024052
82 X = -4274531
30
Y = 4585663
93 feet Y = 1397710
37 meter
Z = -16374416
06 Z = -4990922
01
XDOT = -275
748558 XDOT = -84
048161
YDOT = -23434
000135 feet/sec YDOT = -7142
683241 meter/sec
ZDOT = -6327
330611 ZDOT = -1928
570370
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 10028
51914029
00016717 00000-0 10270-3 0 9010
2 25544 51
6401 227
9183 0011528 255
1192 104
8696 15
75462722 1470
Satellite: ISS
Catalog Number: 25544
Epoch time: 10028
51914029 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 227
9183 deg
Eccentricity:
0011528
Arg of perigee: 255
1192 deg
Mean anomaly: 104
8696 deg
Mean motion: 15
75462722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 294
Coasting Arc #3 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2010/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5499024
67 A = 6727196
11 meter
Y = 3684443
22 meter E =
0009361
Z = 1165154
85 I = 51
43278
XDOT = -1856
853462 Wp = 178
00582
YDOT = 4626
570453 meter/sec RA = 221
89113 deg
ZDOT = -5874
362042 TA = 349
18394
MA = 349
20405
Ha = 186
109 n
mi
Hp = 183
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18041419
51 X = 5451755
94
Y = 12088068
30 feet Y = 3745672
20 meter
Z = 3822686
51 Z = 1191753
72
XDOT = -6092
038916 XDOT = -1879
914892
YDOT = 15179
036920 feet/sec YDOT = 4605
677478 meter/sec
ZDOT = -19272
841345 ZDOT = -5883
438051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1514436
90 X = 461600
37
Y = 21644919
18 feet Y = 6597371
37 meter
Z = 3928243
86 Z = 1197328
73
XDOT = -14074
777454 XDOT = -4289
992168
YDOT = 4484
499345 feet/sec YDOT = 1366
875400 meter/sec
ZDOT = -19308
650789 ZDOT = -5885
276761
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 10029
53401911
00016717 00000-0 10270-3 0 9025
2 25544 51
6406 222
6950 0011593 260
1981 99
7874 15
75532203 1633
Satellite: ISS
Catalog Number: 25544
Epoch time: 10029
53401911 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 222
6950 deg
Eccentricity:
0011593
Arg of perigee: 260
1981 deg
Mean anomaly: 99
7874 deg
Mean motion: 15
75532203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 292
Coasting Arc #4 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2010/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1820035
12 A = 6716128
41 meter
Y = -3832433
11 meter E =
0009050
Z = 5214044
94 I = 51
41699
XDOT = 6476
041809 Wp = 251
10315
YDOT = 4092
605213 meter/sec RA = 216
74561 deg
ZDOT = 745
765660 TA = 191
76634
MA = 191
78750
Ha = 186
006 n
mi
Hp = 183
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5971243
83 X = 1837426
75
Y = -12573599
45 feet Y = -3811983
34 meter
Z = 17106446
65 Z = 5222928
49
XDOT = 21246
856330 XDOT = 6426
173589
YDOT = 13427
182456 feet/sec YDOT = 4164
745294 meter/sec
ZDOT = 2446
737731 ZDOT = 777
104238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13474800
07 X = 4107119
06
Y = -3313576
12 feet Y = -1009978
00 meter
Z = 17141518
29 Z = 5224734
77
XDOT = 2617
462563 XDOT = 797
802589
YDOT = 23975
759483 feet/sec YDOT = 7307
811490 meter/sec
ZDOT = 2571
117260 ZDOT = 783
676541
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 10030
54888454
00016717 00000-0 10270-3 0 9030
2 25544 51
6396 217
4702 0011413 263
0266 96
9600 15
75466346 1794
Satellite: ISS
Catalog Number: 25544
Epoch time: 10030
54888454 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 217
4702 deg
Eccentricity:
0011413
Arg of perigee: 263
0266 deg
Mean anomaly: 96
9600 deg
Mean motion: 15
75466346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 179
Checksum: 308
Coasting Arc #5 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2010/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5776295
11 A = 6727795
02 meter
Y = -3436667
87 meter E =
0008503
Z = -121560
20 I = 51
48189
XDOT = 2357
716598 Wp = 338
38059
YDOT = -4180
384402 meter/sec RA = 211
57580 deg
ZDOT = 6025
528590 TA = 20
29509
MA = 20
26131
Ha = 185
686 n
mi
Hp = 183
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18951099
44 X = -5736845
88
Y = -11275157
06 feet Y = -3501041
25 meter
Z = -398819
56 Z = -149524
74
XDOT = 7735
290676 XDOT = 2375
017157
YDOT = -13715
171922 feet/sec YDOT = -4153
922292 meter/sec
ZDOT = 19768
794587 ZDOT = 6037
024034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3477938
05 X = -1060075
52
Y = -21773296
23 feet Y = -6636500
69 meter
Z = -509815
63 Z = -155391
80
XDOT = 13824
555171 XDOT = 4213
724416
YDOT = -2679
741706 feet/sec YDOT = -816
785272 meter/sec
ZDOT = 19814
203663 ZDOT = 6039
369276
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 10031
50030061
00016717 00000-0 10270-3 0 9041
2 25544 51
6394 212
5720 0011498 266
3753 93
6096 15
75536328 1946
Satellite: ISS
Catalog Number: 25544
Epoch time: 10031
50030061 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 212
5720 deg
Eccentricity:
0011498
Arg of perigee: 266
3753 deg
Mean anomaly: 93
6096 deg
Mean motion: 15
75536328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 291
Coasting Arc #6 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2010/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2328199
75 A = 6715673
12 meter
Y = 3502054
71 meter E =
0003730
Z = -5239137
39 I = 51
46810
XDOT = -6708
704640 Wp = 103
96210
YDOT = -3752
363284 meter/sec RA = 206
41421 deg
ZDOT = 472
415415 TA = 170
53897
MA = 170
53194
Ha = 185
378 n
mi
Hp = 183
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7638450
63 X = -2341737
21
Y = 11489680
79 feet Y = 3475943
60 meter
Z = -17188770
96 Z = -5250480
43
XDOT = -22010
185827 XDOT = -6668
541293
YDOT = -12310
903163 feet/sec YDOT = -3827
159420 meter/sec
ZDOT = 1549
919341 ZDOT = 439
923036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13621914
62 X = -4151959
58
Y = 1805263
66 feet Y = 550244
36 meter
Z = -17233601
05 Z = -5252801
60
XDOT = -4943
420286 XDOT = -1506
754503
YDOT = -23717
674290 feet/sec YDOT = -7229
147124 meter/sec
ZDOT = 1420
946895 ZDOT = 433
104614
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 10032
51512941
00016717 00000-0 10270-3 0 9056
2 25544 51
6398 207
3483 0011324 270
0626 89
9240 15
75573859 2105
Satellite: ISS
Catalog Number: 25544
Epoch time: 10032
51512941 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 207
3483 deg
Eccentricity:
0011324
Arg of perigee: 270
0626 deg
Mean anomaly: 89
9240 deg
Mean motion: 15
75573859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 295
Coasting Arc #7 (Orbit 225)
---------------------------------------
Vector Time (GMT): 2010/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5886797
45 A = 6727154
57 meter
Y = 3102623
05 meter E =
0008506
Z = -951361
40 I = 51
53541
XDOT = -3009
763603 Wp = 216
94293
YDOT = 3885
348962 meter/sec RA = 201
26978 deg
ZDOT = -5931
959551 TA = 333
47073
MA = 333
51424
Ha = 185
594 n
mi
Hp = 183
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19313639
92 X = 5856287
29
Y = 10179209
47 feet Y = 3168282
09 meter
Z = -3121264
45 Z = -922838
15
XDOT = -9874
552503 XDOT = -3024
170801
YDOT = 12747
207880 feet/sec YDOT = 3851
611292 meter/sec
ZDOT = -19461
809550 ZDOT = -5946
615763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5297302
14 X = 1614617
69
Y = 21195884
97 feet Y = 6460505
74 meter
Z = -3008044
97 Z = -916852
11
XDOT = -14462
163124 XDOT = -4408
067320
YDOT = 834
243639 feet/sec YDOT = 254
277461 meter/sec
ZDOT = -19519
760456 ZDOT = -5949
622987
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 10033
52993873
00016717 00000-0 10270-3 0 9066
2 25544 51
6403 202
1243 0011399 275
3691 84
6172 15
75637575 2260
Satellite: ISS
Catalog Number: 25544
Epoch time: 10033
52993873 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 202
1243 deg
Eccentricity:
0011399
Arg of perigee: 275
3691 deg
Mean anomaly: 84
6172 deg
Mean motion: 15
75637575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 226
Checksum: 310
Coasting Arc #8 (Orbit 241)
---------------------------------------
Vector Time (GMT): 2010/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2946911
78 A = 6716521
88 meter
Y = -3322863
82 meter E =
0008290
Z = 5045550
31 I = 51
52754
XDOT = 6714
521994 Wp = 303
32696
YDOT = 3352
351330 meter/sec RA = 196
09081 deg
ZDOT = -1711
464097 TA = 163
18537
MA = 163
15787
Ha = 185
828 n
mi
Hp = 183
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9668345
72 X = 2959339
65
Y = -10901784
20 feet Y = -3289840
13 meter
Z = 16553642
74 Z = 5059896
41
XDOT = 22029
271635 XDOT = 6684
850214
YDOT = 10998
527987 feet/sec YDOT = 3427
271160 meter/sec
ZDOT = -5615
039689 ZDOT = -1678
917636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14501677
92 X = 4420111
43
Y = -381003
76 feet Y = -116129
95 meter
Z = 16610390
41 Z = 5062847
00
XDOT = 6886
658392 XDOT = 2099
053478
YDOT = 22604
326775 feet/sec YDOT = 6889
798801 meter/sec
ZDOT = -5485
849009 ZDOT = -1672
086778
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 10034
54473350
00016717 00000-0 10270-3 0 9073
2 25544 51
6401 196
8999 0011235 278
0055 81
9834 15
75582036 2422
Satellite: ISS
Catalog Number: 25544
Epoch time: 10034
54473350 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 196
8999 deg
Eccentricity:
0011235
Arg of perigee: 278
0055 deg
Mean anomaly: 81
9834 deg
Mean motion: 15
75582036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 242
Checksum: 309
Coasting Arc #9 (Orbit 257)
---------------------------------------
Vector Time (GMT): 2010/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5781942
31 A = 6725698
84 meter
Y = -2759754
33 meter E =
0007734
Z = 2029407
50 I = 51
58940
XDOT = 3754
655199 Wp = 15
70054
YDOT = -3771
535183 meter/sec RA = 190
96954 deg
ZDOT = 5570
858754 TA = 6
96645
MA = 6
95571
Ha = 186
145 n
mi
Hp = 183
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18969627
00 X = -5760510
88
Y = -9054312
11 feet Y = -2824291
60 meter
Z = 6658161
09 Z = 2001371
29
XDOT = 12318
422568 XDOT = 3769
488278
YDOT = -12373
803095 feet/sec YDOT = -3729
465454 meter/sec
ZDOT = 18277
095648 ZDOT = 5589
134647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6611982
98 X = -2015332
41
Y = -19989462
04 feet Y = -6092788
03 meter
Z = 6546870
56 Z = 1995486
15
XDOT = 15924
504334 XDOT = 4853
788921
YDOT = 739
711892 feet/sec YDOT = 225
464185 meter/sec
ZDOT = 18349
413553 ZDOT = 5592
901251
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 10035
55950595
00016717 00000-0 10270-3 0 9087
2 25544 51
6410 191
6758 0011312 281
7253 78
2641 15
75668690 2588
Satellite: ISS
Catalog Number: 25544
Epoch time: 10035
55950595 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 191
6758 deg
Eccentricity:
0011312
Arg of perigee: 281
7253 deg
Mean anomaly: 78
2641 deg
Mean motion: 15
75668690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 258
Checksum: 319
Coasting Arc #10 (Orbit 272)
---------------------------------------
Vector Time (GMT): 2010/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3595483
51 A = 6718050
77 meter
Y = 3309243
36 meter E =
0000892
Z = -4609813
22 I = 51
59439
XDOT = -6478
775953 Wp = 232
55005
YDOT = -2977
920807 meter/sec RA = 185
77844 deg
ZDOT = 2914
529910 TA = 66
32494
MA = 66
31558
Ha = 186
390 n
mi
Hp = 183
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11796205
74 X = -3609827
49
Y = 10857097
64 feet Y = 3268956
40 meter
Z = -15124059
11 Z = -4627314
63
XDOT = -21255
826619 XDOT = -6459
152867
YDOT = -9770
081389 feet/sec YDOT = -3050
260646 meter/sec
ZDOT = 9562
106003 ZDOT = 2883
104059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15952417
56 X = -4862296
87
Y = -668738
60 feet Y = -203831
53 meter
Z = -15193332
93 Z = -4630927
88
XDOT = -8117
133941 XDOT = -2474
102425
YDOT = -20848
916533 feet/sec YDOT = -6354
749759 meter/sec
ZDOT = 9437
354271 ZDOT = 2876
505582
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 10036
51084067
00016717 00000-0 10270-3 0 9097
2 25544 51
6415 186
7791 0011257 285
8416 74
1507 15
75678261 2737
Satellite: ISS
Catalog Number: 25544
Epoch time: 10036
51084067 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 186
7791 deg
Eccentricity:
0011257
Arg of perigee: 285
8416 deg
Mean anomaly: 74
1507 deg
Mean motion: 15
75678261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 273
Checksum: 318
Coasting Arc #11 (Orbit 288)
---------------------------------------
Vector Time (GMT): 2010/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5466100
02 A = 6723365
12 meter
Y = 2467702
88 meter E =
0006776
Z = -3036610
83 I = 51
64238
XDOT = -4486
120483 Wp = 291
20532
YDOT = 3851
962663 meter/sec RA = 180
67504 deg
ZDOT = -4933
805811 TA = 283
96908
MA = 284
04442
Ha = 186
761 n
mi
Hp = 183
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17933399
02 X = 5452850
57
Y = 8096138
06 feet Y = 2528754
06 meter
Z = -9962633
96 Z = -3010089
01
XDOT = -14718
243054 XDOT = -4504
893211
YDOT = 12637
672779 feet/sec YDOT = 3801
691397 meter/sec
ZDOT = -16187
026939 ZDOT = -4955
644540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7236140
27 X = 2205575
56
Y = 18354275
41 feet Y = 5594383
15 meter
Z = -9857341
19 Z = -3004517
59
XDOT = -17954
059845 XDOT = -5472
397441
YDOT = -1681
440309 feet/sec YDOT = -512
503006 meter/sec
ZDOT = -16273
491329 ZDOT = -4960
160157
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 10037
52557872
00016717 00000-0 10270-3 0 9100
2 25544 51
6414 181
5548 0011297 290
2627 69
7323 15
75716051 2890
Satellite: ISS
Catalog Number: 25544
Epoch time: 10037
52557872 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 181
5548 deg
Eccentricity:
0011297
Arg of perigee: 290
2627 deg
Mean anomaly: 69
7323 deg
Mean motion: 15
75716051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 289
Checksum: 314
Coasting Arc #12 (Orbit 304)
---------------------------------------
Vector Time (GMT): 2010/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213975
86 A = 6720465
92 meter
Y = -3456208
62 meter E =
0006671
Z = 3936715
98 I = 51
66318
XDOT = 5982
113974 Wp = 4
95227
YDOT = 2712
052593 meter/sec RA = 175
47708 deg
ZDOT = -4015
375498 TA = 126
75870
MA = 126
69744
Ha = 186
991 n
mi
Hp = 183
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13825380
13 X = 4233187
09
Y = -11339267
13 feet Y = -3408978
20 meter
Z = 12915734
85 Z = 3957233
63
XDOT = 19626
358184 XDOT = 5970
848342
YDOT = 8897
810345 feet/sec YDOT = 2778
885316 meter/sec
ZDOT = -13173
804127 ZDOT = -3986
342150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17783414
74 X = 5420384
81
Y = 1168253
23 feet Y = 356083
58 meter
Z = 12996986
80 Z = 3961481
58
XDOT = 8332
924458 XDOT = 2539
875375
YDOT = 18687
302601 feet/sec YDOT = 5695
889833 meter/sec
ZDOT = -13058
526783 ZDOT = -3980
238963
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 10038
54029917
00016717 00000-0 10270-3 0 9118
2 25544 51
6414 176
3304 0011237 293
9186 66
0801 15
75716236 3051
Satellite: ISS
Catalog Number: 25544
Epoch time: 10038
54029917 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 176
3304 deg
Eccentricity:
0011237
Arg of perigee: 293
9186 deg
Mean anomaly: 66
0801 deg
Mean motion: 15
75716236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 305
Checksum: 293
Coasting Arc #13 (Orbit 320)
---------------------------------------
Vector Time (GMT): 2010/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4929134
25 A = 6720418
63 meter
Y = -2316433
82 meter E =
0003473
Z = 3933840
68 I = 51
69468
XDOT = 5135
301707 Wp = 16
56185
YDOT = -4095
231344 meter/sec RA = 170
38292 deg
ZDOT = 4025
506766 TA = 31
69740
MA = 31
67649
Ha = 187
266 n
mi
Hp = 183
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16171700
28 X = -4921974
61
Y = -7599848
48 feet Y = -2371514
46 meter
Z = 12906301
46 Z = 3909912
75
XDOT = 16848
102713 XDOT = 5161
158880
YDOT = -13435
798373 feet/sec YDOT = -4037
660967 meter/sec
ZDOT = 13207
043197 ZDOT = 4050
516146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6906668
22 X = -2105152
47
Y = -16553647
31 feet Y = -5045551
70 meter
Z = 12811280
15 Z = 3904878
19
XDOT = 20239
271248 XDOT = 6168
929877
YDOT = 1847
364147 feet/sec YDOT = 563
076592 meter/sec
ZDOT = 13306
101299 ZDOT = 4055
699676
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 10039
55499831
00016717 00000-0 10270-3 0 9127
2 25544 51
6426 171
1060 0011357 297
9316 62
0698 15
75796964 3212
Satellite: ISS
Catalog Number: 25544
Epoch time: 10039
55499831 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 171
1060 deg
Eccentricity:
0011357
Arg of perigee: 297
9316 deg
Mean anomaly: 62
0698 deg
Mean motion: 15
75796964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 321
Checksum: 323
Coasting Arc #14 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2010/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4696540
19 A = 6723019
61 meter
Y = 3719704
80 meter E =
0009089
Z = -3036967
29 I = 51
73349
XDOT = -5288
228813 Wp = 324
82512
YDOT = -2638
016422 meter/sec RA = 165
18941 deg
ZDOT = 4946
949913 TA =
01431
MA =
01428
Ha = 187
461 n
mi
Hp = 183
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15408596
43 X = -4723032
87
Y = 12203755
89 feet Y = 3667037
30 meter
Z = -9963803
45 Z = -3059846
70
XDOT = -17349
832063 XDOT = -5282
367792
YDOT = -8654
909522 feet/sec YDOT = -2697
119963 meter/sec
ZDOT = 16230
150634 ZDOT = 4921
274478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19586102
67 X = -5969844
09
Y = -962671
43 feet Y = -293422
25 meter
Z = -10054438
19 Z = -3064592
76
XDOT = -7464
059094 XDOT = -2275
045212
YDOT = -16587
165508 feet/sec YDOT = -5055
768047 meter/sec
ZDOT = 16128
170330 ZDOT = 4915
866316
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 10040
50626436
00016717 00000-0 10270-3 0 9138
2 25544 51
6430 166
2088 0011432 302
5525 57
4535 15
75778672 3361
Satellite: ISS
Catalog Number: 25544
Epoch time: 10040
50626436 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 166
2088 deg
Eccentricity:
0011432
Arg of perigee: 302
5525 deg
Mean anomaly: 57
4535 deg
Mean motion: 15
75778672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 293
Coasting Arc #15 (Orbit 351)
---------------------------------------
Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4258736
04 A = 6717741
38 meter
Y = 2348584
77 meter E =
0010379
Z = -4639668
32 I = 51
74519
XDOT = -5593
416196 Wp = 4
66170
YDOT = 4438
570909 meter/sec RA = 160
09431 deg
ZDOT = -2877
688970 TA = 236
86332
MA = 236
96296
Ha = 187
724 n
mi
Hp = 182
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13972231
11 X = 4254695
26
Y = 7705330
61 feet Y = 2396186
02 meter
Z = -15222008
92 Z = -4618989
72
XDOT = -18351
103004 XDOT = -5628
654478
YDOT = 14562
240515 feet/sec YDOT = 4375
825071 meter/sec
ZDOT = -9441
236778 ZDOT = -2904
946467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5737066
40 X = 1748657
84
Y = 14972499
66 feet Y = 4563617
90 meter
Z = -15139856
03 Z = -4614628
12
XDOT = -22279
834722 XDOT = -6790
893623
YDOT = -1151
272194 feet/sec YDOT = -350
907765 meter/sec
ZDOT = -9549
227496 ZDOT = -2910
604541
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 10041
52092902
00016717 00000-0 10270-3 0 9147
2 25544 51
6435 160
9847 0011437 306
2527 53
7580 15
75815917 3529
Satellite: ISS
Catalog Number: 25544
Epoch time: 10041
52092902 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 160
9847 deg
Eccentricity:
0011437
Arg of perigee: 306
2527 deg
Mean anomaly: 53
7580 deg
Mean motion: 15
75815917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 352
Checksum: 300
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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