Date:
April 1st 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 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 1123)
---------------------------------------
Vector Time (GMT): 2010/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1754294
47 A = 6729397
52 meter
Y = 6049098
48 meter E =
0011326
Z = -2365235
86 I = 51
31582
XDOT = -4377
241116 Wp = 128
69434
YDOT = -3358
961477 meter/sec RA = 268
67369 deg
ZDOT = -5368
217381 TA = 78
07314
MA = 77
94617
Ha = 191
830 n
mi
Hp = 181
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5755559
27 X = -1810316
19
Y = 19846123
64 feet Y = 6029167
49 meter
Z = -7759960
15 Z = -2373894
87
XDOT = -14361
027282 XDOT = -4313
277222
YDOT = -11020
214818 feet/sec YDOT = -3407
553195 meter/sec
ZDOT = -17612
261749 ZDOT = -5389
326550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2898957
08 X = -883602
12
Y = 20446493
82 feet Y = 6232091
31 meter
Z = -7794164
87 Z = -2375661
45
XDOT = -14158
244642 XDOT = -4315
432967
YDOT = -8722
941205 feet/sec YDOT = -2658
752479 meter/sec
ZDOT = -17696
195751 ZDOT = -5393
800465
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 10090
52707935
00016717 00000-0 10270-3 0 9005
2 25544 51
6409 269
2906 0005744 123
6812 236
4899 15
74112285 11249
Satellite: ISS
Catalog Number: 25544
Epoch time: 10090
52707935 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 269
2906 deg
Eccentricity:
0005744
Arg of perigee: 123
6812 deg
Mean anomaly: 236
4899 deg
Mean motion: 15
74112285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1124
Checksum: 308
Coasting Arc #2 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2010/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4056873
76 A = 6722310
40 meter
Y = 2639735
55 meter E =
0011484
Z = 4655192
06 I = 51
29353
XDOT = -1418
113690 Wp = 90
04998
YDOT = 7056
219030 meter/sec RA = 263
47038 deg
ZDOT = -2759
546609 TA = 27
28756
MA = 27
22728
Ha = 191
696 n
mi
Hp = 181
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13309953
28 X = 4004439
95
Y = 8660549
71 feet Y = 2684809
02 meter
Z = 15272939
84 Z = 4674773
03
XDOT = -4652
603971 XDOT = -1483
506690
YDOT = 23150
324902 feet/sec YDOT = 7039
995050 meter/sec
ZDOT = -9053
630608 ZDOT = -2766
595114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14408189
84 X = 4391616
26
Y = 6494621
99 feet Y = 1979560
78 meter
Z = 15350785
64 Z = 4678919
46
XDOT = -461
258551 XDOT = -140
591606
YDOT = 22533
369644 feet/sec YDOT = 6868
171067 meter/sec
ZDOT = -9081
409768 ZDOT = -2768
013697
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 10091
54283822
00016717 00000-0 10270-3 0 9013
2 25544 51
6406 264
0727 0005780 129
0945 231
0733 15
74111235 11407
Satellite: ISS
Catalog Number: 25544
Epoch time: 10091
54283822 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 264
0727 deg
Eccentricity:
0005780
Arg of perigee: 129
0945 deg
Mean anomaly: 231
0733 deg
Mean motion: 15
74111235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 274
Coasting Arc #3 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2010/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 729433
20 A = 6729032
97 meter
Y = -6214904
17 meter E =
0017687
Z = 2459814
17 I = 51
32174
XDOT = 4892
292760 Wp = 91
27492
YDOT = 2688
055013 meter/sec RA = 258
35239 deg
ZDOT = 5307
561018 TA = 296
67045
MA = 296
85145
Ha = 191
675 n
mi
Hp = 181
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2393153
53 X = 786925
73
Y = -20390105
55 feet Y = -6206425
68 meter
Z = 8070256
47 Z = 2463497
64
XDOT = 16050
829264 XDOT = 4836
087463
YDOT = 8819
078126 feet/sec YDOT = 2742
449455 meter/sec
ZDOT = 17413
257934 ZDOT = 5331
191349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1213634
33 X = -369915
74
Y = -20488469
64 feet Y = -6244885
55 meter
Z = 8084697
33 Z = 2464215
75
XDOT = 15738
314555 XDOT = 4797
038276
YDOT = 6019
003585 feet/sec YDOT = 1834
592293 meter/sec
ZDOT = 17507
192625 ZDOT = 5336
192312
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 10092
55856998
00016717 00000-0 10270-3 0 9026
2 25544 51
6409 258
8548 0005813 132
9345 227
2307 15
74178780 11565
Satellite: ISS
Catalog Number: 25544
Epoch time: 10092
55856998 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 258
8548 deg
Eccentricity:
0005813
Arg of perigee: 132
9345 deg
Mean anomaly: 227
2307 deg
Mean motion: 15
74178780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 335
Coasting Arc #4 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2010/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4469392
85 A = 6722321
07 meter
Y = -2062031
00 meter E =
0016076
Z = -4594297
41 I = 51
30773
XDOT = 284
908533 Wp = 119
06403
YDOT = -7108
826872 meter/sec RA = 253
14853 deg
ZDOT = 2913
444091 TA = 179
98308
MA = 179
98303
Ha = 191
609 n
mi
Hp = 181
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14663362
37 X = -4423684
30
Y = -6765193
58 feet Y = -2111754
91 meter
Z = -15073154
23 Z = -4615898
76
XDOT = 934
739281 XDOT = 350
226479
YDOT = -23322
922807 feet/sec YDOT = -7105
275597 meter/sec
ZDOT = 9558
543607 ZDOT = 2914
986954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15593372
33 X = -4752859
89
Y = -3877231
00 feet Y = -1181780
01 meter
Z = -15159018
36 Z = -4620468
80
XDOT = -3845
594365 XDOT = -1172
137162
YDOT = -21928
590402 feet/sec YDOT = -6683
834355 meter/sec
ZDOT = 9564
453770 ZDOT = 2915
245509
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 10093
51079532
00016717 00000-0 10270-3 0 9035
2 25544 51
6418 253
9635 0005851 135
7183 224
4449 15
74210294 11711
Satellite: ISS
Catalog Number: 25544
Epoch time: 10093
51079532 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 253
9635 deg
Eccentricity:
0005851
Arg of perigee: 135
7183 deg
Mean anomaly: 224
4449 deg
Mean motion: 15
74210294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 300
Coasting Arc #5 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2010/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 205536
13 A = 6728349
96 meter
Y = 6179091
69 meter E =
0010600
Z = -2650802
20 I = 51
33843
XDOT = -5303
745866 Wp = 132
59784
YDOT = -2042
652122 meter/sec RA = 248
03339 deg
ZDOT = -5192
944863 TA = 77
71101
MA = 77
59235
Ha = 191
418 n
mi
Hp = 181
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 674331
13 X = 149302
27
Y = 20272610
53 feet Y = 6181075
68 meter
Z = -8696857
61 Z = -2649940
34
XDOT = -17400
741031 XDOT = -5255
283966
YDOT = -6701
614572 feet/sec YDOT = -2101
690838 meter/sec
ZDOT = -17037
220678 ZDOT = -5218
592751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4898253
60 X = 1492987
70
Y = 19685107
73 feet Y = 6000020
84 meter
Z = -8693240
93 Z = -2649699
84
XDOT = -16876
128835 XDOT = -5143
844069
YDOT = -3340
299179 feet/sec YDOT = -1018
123190 meter/sec
ZDOT = -17139
166844 ZDOT = -5224
018054
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 10094
52647559
00016717 00000-0 10270-3 0 9048
2 25544 51
6418 248
7457 0005707 138
5593 221
6004 15
74269825 11878
Satellite: ISS
Catalog Number: 25544
Epoch time: 10094
52647559 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 248
7457 deg
Eccentricity:
0005707
Arg of perigee: 138
5593 deg
Mean anomaly: 221
6004 deg
Mean motion: 15
74269825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 330
Coasting Arc #6 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2010/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4784699
09 A = 6722583
42 meter
Y = 1483433
74 meter E =
0011668
Z = 4472599
48 I = 51
33115
XDOT = 769
311185 Wp = 95
83286
YDOT = 6998
346411 meter/sec RA = 242
82814 deg
ZDOT = -3138
311701 TA = 25
62577
MA = 25
56799
Ha = 191
273 n
mi
Hp = 181
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15697831
67 X = 4746028
44
Y = 4866908
58 feet Y = 1536722
91 meter
Z = 14673882
80 Z = 4495749
53
XDOT = 2523
986829 XDOT = 706
242555
YDOT = 22960
454105 feet/sec YDOT = 7006
596638 meter/sec
ZDOT = -10296
298230 ZDOT = -3134
727664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16304008
26 X = 4969461
72
Y = 1256623
91 feet Y = 383018
97 meter
Z = 14765898
75 Z = 4500645
94
XDOT = 7740
298802 XDOT = 2359
243075
YDOT = 20613
581754 feet/sec YDOT = 6283
019719 meter/sec
ZDOT = -10281
835194 ZDOT = -3133
903367
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 10095
54213063
00016717 00000-0 10270-3 0 9051
2 25544 51
6414 243
5279 0005792 142
9948 217
1616 15
74266160 12033
Satellite: ISS
Catalog Number: 25544
Epoch time: 10095
54213063 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 243
5279 deg
Eccentricity:
0005792
Arg of perigee: 142
9948 deg
Mean anomaly: 217
1616 deg
Mean motion: 15
74266160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 298
Coasting Arc #7 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2010/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1107783
27 A = 6727664
80 meter
Y = -5995082
07 meter E =
0016599
Z = 2834360
38 I = 51
36500
XDOT = 5644
855256 Wp = 99
33876
YDOT = 1362
451415 meter/sec RA = 237
71663 deg
ZDOT = 5060
190806 TA = 293
32415
MA = 293
49873
Ha = 191
161 n
mi
Hp = 181
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3634459
54 X = -1054431
59
Y = -19668904
42 feet Y = -6007171
59 meter
Z = 9299082
60 Z = 2829108
51
XDOT = 18519
866324 XDOT = 5604
619183
YDOT = 4469
984956 feet/sec YDOT = 1425
350678 meter/sec
ZDOT = 16601
675873 ZDOT = 5087
515599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8304404
97 X = -2531182
63
Y = -18207231
51 feet Y = -5549564
16 meter
Z = 9278017
75 Z = 2827939
81
XDOT = 17628
604266 XDOT = 5373
198580
YDOT = 521
347639 feet/sec YDOT = 158
906760 meter/sec
ZDOT = 16710
283783 ZDOT = 5093
294497
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 10096
55775549
00016717 00000-0 10270-3 0 9066
2 25544 51
6424 238
3101 0005708 147
7601 212
3912 15
74364900 12190
Satellite: ISS
Catalog Number: 25544
Epoch time: 10096
55775549 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 238
3101 deg
Eccentricity:
0005708
Arg of perigee: 147
7601 deg
Mean anomaly: 212
3912 deg
Mean motion: 15
74364900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 300
Coasting Arc #8 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2010/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5065196
42 A = 6722836
60 meter
Y = -901772
53 meter E =
0013853
Z = -4341934
41 I = 51
36638
XDOT = -1714
842059 Wp = 125
75178
YDOT = -6686
000061 meter/sec RA = 232
51159 deg
ZDOT = 3388
697324 TA = 178
59437
MA = 178
59047
Ha = 191
051 n
mi
Hp = 181
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16618098
50 X = -5033643
99
Y = -2958571
31 feet Y = -958238
31 meter
Z = -14245191
64 Z = -4366464
30
XDOT = -5626
122240 XDOT = -1656
412127
YDOT = -21935
695739 feet/sec YDOT = -6704
849623 meter/sec
ZDOT = 11117
773373 ZDOT = 3380
508847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16739336
63 X = -5102149
81
Y = 1386256
60 feet Y = 422531
01 meter
Z = -14342689
03 Z = -4371651
61
XDOT = -11032
568223 XDOT = -3362
726794
YDOT = -18517
565154 feet/sec YDOT = -5644
153859 meter/sec
ZDOT = 11085
007487 ZDOT = 3378
710282
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 10097
50988180
00016717 00000-0 10270-3 0 9070
2 25544 51
6427 233
4188 0005551 150
2735 209
8745 15
74368125 12342
Satellite: ISS
Catalog Number: 25544
Epoch time: 10097
50988180 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 233
4188 deg
Eccentricity:
0005551
Arg of perigee: 150
2735 deg
Mean anomaly: 209
8745 deg
Mean motion: 15
74368125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 316
Coasting Arc #9 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2010/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1850900
08 A = 6726831
70 meter
Y = 5673232
54 meter E =
0009134
Z = -3103248
91 I = 51
39959
XDOT = -5927
935491 Wp = 132
18022
YDOT = -715
806216 meter/sec RA = 227
40322 deg
ZDOT = -4859
418058 TA = 84
00166
MA = 83
89758
Ha = 190
908 n
mi
Hp = 182
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6072506
82 X = 1802398
34
Y = 18612967
65 feet Y = 5693659
06 meter
Z = -10181262
84 Z = -3094375
40
XDOT = -19448
607253 XDOT = -5895
884613
YDOT = -2348
445592 feet/sec YDOT = -781
916966 meter/sec
ZDOT = -15942
972632 ZDOT = -4888
137895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10987214
48 X = 3348902
97
Y = 16227133
74 feet Y = 4946030
36 meter
Z = -10145800
39 Z = -3092439
96
XDOT = -18075
936897 XDOT = -5509
545566
YDOT = 2230
714593 feet/sec YDOT = 679
921808 meter/sec
ZDOT = -16057
120974 ZDOT = -4894
210473
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 10098
52545567
00016717 00000-0 10270-3 0 9082
2 25544 51
6428 228
1998 0005513 154
0476 206
0965 15
74414774 12508
Satellite: ISS
Catalog Number: 25544
Epoch time: 10098
52545567 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 228
1998 deg
Eccentricity:
0005513
Arg of perigee: 154
0476 deg
Mean anomaly: 206
0965 deg
Mean motion: 15
74414774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1250
Checksum: 324
Coasting Arc #10 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2010/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5278110
95 A = 6723357
19 meter
Y = 326066
41 meter E =
0012278
Z = 4140014
19 I = 51
41015
XDOT = 2521
376845 Wp = 101
12373
YDOT = 6273
456031 meter/sec RA = 222
19813 deg
ZDOT = -3701
684695 TA = 26
81575
MA = 26
75233
Ha = 190
701 n
mi
Hp = 182
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17316636
97 X = 5253961
18
Y = 1069771
67 feet Y = 384954
63 meter
Z = 13582723
71 Z = 4165596
45
XDOT = 8272
233745 XDOT = 2469
020579
YDOT = 20582
204827 feet/sec YDOT = 6301
358584 meter/sec
ZDOT = -12144
634826 ZDOT = -3689
563488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16806447
95 X = 5122605
34
Y = -3972566
54 feet Y = -1210838
28 meter
Z = 13684397
43 Z = 4171004
34
XDOT = 13662
183454 XDOT = 4164
233517
YDOT = 16053
795881 feet/sec YDOT = 4893
196984 meter/sec
ZDOT = -12096
235485 ZDOT = -3686
932576
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 10099
54100317
00016717 00000-0 10270-3 0 9096
2 25544 51
6433 222
9818 0005516 156
7821 203
3592 15
74433054 12668
Satellite: ISS
Catalog Number: 25544
Epoch time: 10099
54100317 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 222
9818 deg
Eccentricity:
0005516
Arg of perigee: 156
7821 deg
Mean anomaly: 203
3592 deg
Mean motion: 15
74433054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1266
Checksum: 298
Coasting Arc #11 (Orbit 1281)
---------------------------------------
Vector Time (GMT): 2010/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2506878
67 A = 6725780
20 meter
Y = -5254205
30 meter E =
0015202
Z = 3361106
45 I = 51
44322
XDOT = 6158
705794 Wp = 109
41103
YDOT = 34
627822 meter/sec RA = 217
09461 deg
ZDOT = 4625
649531 TA = 290
33559
MA = 290
49887
Ha = 190
571 n
mi
Hp = 182
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8224667
55 X = -2464266
52
Y = -17238206
35 feet Y = -5282000
19 meter
Z = 11027252
14 Z = 3349031
95
XDOT = 20205
727671 XDOT = 6135
390304
YDOT = 113
608339 feet/sec YDOT = 103
368123 meter/sec
ZDOT = 15176
015523 ZDOT = 4655
511849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13171187
48 X = -4014577
94
Y = -13870150
78 feet Y = -4227621
96 meter
Z = 10979068
37 Z = 3346420
04
XDOT = 18172
563308 XDOT = 5538
997296
YDOT = -5092
857666 feet/sec YDOT = -1552
303016 meter/sec
ZDOT = 15294
693659 ZDOT = 4661
822627
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 10100
55651999
00016717 00000-0 10270-3 0 9109
2 25544 51
6443 217
7631 0005388 161
4580 198
6781 15
74536899 12821
Satellite: ISS
Catalog Number: 25544
Epoch time: 10100
55651999 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 217
7631 deg
Eccentricity:
0005388
Arg of perigee: 161
4580 deg
Mean anomaly: 198
6781 deg
Mean motion: 15
74536899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1282
Checksum: 334
Coasting Arc #12 (Orbit 1296)
---------------------------------------
Vector Time (GMT): 2010/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5470589
97 A = 6723890
27 meter
Y = 266466
10 meter E =
0010569
Z = -3912538
99 I = 51
46219
XDOT = -3158
854027 Wp = 132
12297
YDOT = -5742
095923 meter/sec RA = 211
89110 deg
ZDOT = 4025
673654 TA = 179
87856
MA = 179
87830
Ha = 190
399 n
mi
Hp = 182
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17948129
83 X = -5454156
59
Y = 874232
62 feet Y = 205382
28 meter
Z = -12836414
01 Z = -3939075
30
XDOT = -10363
694315 XDOT = -3113
966162
YDOT = -18838
897385 feet/sec YDOT = -5777
168801 meter/sec
ZDOT = 13207
590729 ZDOT = 4010
437396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16634497
92 X = -5070194
97
Y = 6593534
97 feet Y = 2009709
46 meter
Z = -12941868
00 Z = -3944681
37
XDOT = -15480
197192 XDOT = -4718
364104
YDOT = -13249
295654 feet/sec YDOT = -4038
385315 meter/sec
ZDOT = 13146
816529 ZDOT = 4007
149678
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 10101
50854564
00016717 00000-0 10270-3 0 9119
2 25544 51
6445 212
8713 0005163 165
0557 195
0760 15
74537004 12978
Satellite: ISS
Catalog Number: 25544
Epoch time: 10101
50854564 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 212
8713 deg
Eccentricity:
0005163
Arg of perigee: 165
0557 deg
Mean anomaly: 195
0760 deg
Mean motion: 15
74537004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1297
Checksum: 291
Coasting Arc #13 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2010/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2967364
92 A = 6724682
05 meter
Y = 4781648
95 meter E =
0007753
Z = -3683429
54 I = 51
49174
XDOT = -6349
462196 Wp = 121
41314
YDOT = 631
704870 meter/sec RA = 206
79182 deg
ZDOT = -4305
687456 TA = 103
00255
MA = 102
91598
Ha = 190
296 n
mi
Hp = 182
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9735449
23 X = 2931568
70
Y = 15687824
65 feet Y = 4814631
35 meter
Z = -12084742
58 Z = -3669101
30
XDOT = -20831
568883 XDOT = -6335
137710
YDOT = 2072
522541 feet/sec YDOT = 560
781153 meter/sec
ZDOT = -14126
271182 ZDOT = -4336
498631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14542318
27 X = 4432498
61
Y = 11436144
29 feet Y = 3485736
78 meter
Z = -12027609
92 Z = -3666015
50
XDOT = -17984
258660 XDOT = -5481
602040
YDOT = 7920
148991 feet/sec YDOT = 2414
061413 meter/sec
ZDOT = -14248
706726 ZDOT = -4343
005810
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 10102
52401223
00016717 00000-0 10270-3 0 9123
2 25544 51
6450 207
6524 0005187 168
5356 191
5927 15
74578038 13134
Satellite: ISS
Catalog Number: 25544
Epoch time: 10102
52401223 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 207
6524 deg
Eccentricity:
0005187
Arg of perigee: 168
5356 deg
Mean anomaly: 191
5927 deg
Mean motion: 15
74578038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1313
Checksum: 291
Coasting Arc #14 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2010/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5604851
72 A = 6724677
94 meter
Y = -859592
65 meter E =
0013407
Z = 3600263
77 I = 51
51979
XDOT = 3625
332759 Wp = 107
88834
YDOT = 5191
791129 meter/sec RA = 201
59107 deg
ZDOT = -4394
989798 TA = 28
89851
MA = 28
82434
Ha = 190
044 n
mi
Hp = 182
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18388621
14 X = 5596557
63
Y = -2820185
86 feet Y = -796961
98 meter
Z = 11811889
03 Z = 3627472
39
XDOT = 11894
136350 XDOT = 3588
358102
YDOT = 17033
435462 feet/sec YDOT = 5232
124709 meter/sec
ZDOT = -14419
257866 ZDOT = -4377
467902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16124441
14 X = 4914729
66
Y = -9139555
75 feet Y = -2785736
59 meter
Z = 11920003
21 Z = 3633216
98
XDOT = 16578
989297 XDOT = 5053
275938
YDOT = 10495
176441 feet/sec YDOT = 3198
929779 meter/sec
ZDOT = -14349
412877 ZDOT = -4373
701045
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 10103
53945229
00016717 00000-0 10270-3 0 9135
2 25544 51
6449 202
4341 0005081 170
2820 189
8442 15
74613232 13296
Satellite: ISS
Catalog Number: 25544
Epoch time: 10103
53945229 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 202
4341 deg
Eccentricity:
0005081
Arg of perigee: 170
2820 deg
Mean anomaly: 189
8442 deg
Mean motion: 15
74613232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 285
Coasting Arc #15 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2010/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3313673
26 A = 6723366
31 meter
Y = -4280441
73 meter E =
0013264
Z = 3983344
20 I = 51
54456
XDOT = 6483
607655 Wp = 122
78075
YDOT = -1340
554870 meter/sec RA = 196
49475 deg
ZDOT = 3936
527614 TA = 286
40682
MA = 286
55258
Ha = 189
943 n
mi
Hp = 182
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10871631
42 X = -3284912
98
Y = -14043443
99 feet Y = -4317336
17 meter
Z = 13068714
58 Z = 3967316
22
XDOT = 21271
678659 XDOT = 6478
992859
YDOT = -4398
145900 feet/sec YDOT = -1268
076899 meter/sec
ZDOT = 12915
116845 ZDOT = 3968
014335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15377389
45 X = -4687028
31
Y = -8978418
65 feet Y = -2736622
00 meter
Z = 13004840
70 Z = 3963875
45
XDOT = 17395
833853 XDOT = 5302
250158
YDOT = -10826
817389 feet/sec YDOT = -3300
013940 meter/sec
ZDOT = 13040
225414 ZDOT = 3974
660706
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 10104
55486289
00016717 00000-0 10270-3 0 9145
2 25544 51
6451 197
2146 0004985 175
4712 184
6497 15
74693389 13454
Satellite: ISS
Catalog Number: 25544
Epoch time: 10104
55486289 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 197
2146 deg
Eccentricity:
0004985
Arg of perigee: 175
4712 deg
Mean anomaly: 184
6497 deg
Mean motion: 15
74693389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 343
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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