Date:
April 8th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 30138 95 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 1203)
---------------------------------------
Vector Time (GMT): 2010/095/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3354647
87 A = 6731156
37 meter
Y = -5823708
75 meter E =
0011836
Z = -331079
73 I = 51
36721
XDOT = 4026
284793 Wp = 70
42727
YDOT = -2650
354022 meter/sec RA = 242
31304 deg
ZDOT = 6001
718816 TA = 285
96152
MA = 286
09189
Ha = 191
230 n
mi
Hp = 181
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11006062
57 X = -3287668
47
Y = -19106655
99 feet Y = -5860847
92 meter
Z = -1086219
58 Z = -347213
80
XDOT = 13209
595778 XDOT = 4026
467108
YDOT = -8695
387212 feet/sec YDOT = -2605
328625 meter/sec
ZDOT = 19690
678530 ZDOT = 6021
278918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21755725
25 X = -6631145
06
Y = -3569642
77 feet Y = -1088027
12 meter
Z = -1150503
62 Z = -350673
50
XDOT = 1289
779958 XDOT = 393
124931
YDOT = -14054
440934 feet/sec YDOT = -4283
793597 meter/sec
ZDOT = 19768
300289 ZDOT = 6025
377928
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
60551176
00016717 00000-0 10270-3 0 9003
2 25544 51
6465 243
2084 0005633 143
1622 216
9929 15
74337367 12049
Satellite: ISS
Catalog Number: 25544
Epoch time: 10095
60551176 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 243
2084 deg
Eccentricity:
0005633
Arg of perigee: 143
1622 deg
Mean anomaly: 216
9929 deg
Mean motion: 15
74337367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1204
Checksum: 296
Coasting Arc #2 (Orbit 1219)
---------------------------------------
Vector Time (GMT): 2010/096/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3416098
32 A = 6718953
58 meter
Y = 2456957
43 meter E =
0018477
Z = -5253487
20 I = 51
34172
XDOT = -4296
227656 Wp = 103
34196
YDOT = -6373
321848 meter/sec RA = 237
16015 deg
ZDOT = -191
810050 TA = 164
85496
MA = 164
79957
Ha = 191
004 n
mi
Hp = 181
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11207671
66 X = -3417798
22
Y = 8060883
95 feet Y = 2418746
96 meter
Z = -17235850
40 Z = -5270086
70
XDOT = -14095
235092 XDOT = -4223
708951
YDOT = -20909
848583 feet/sec YDOT = -6420
959351 meter/sec
ZDOT = -629
298064 ZDOT = -212
504712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -548260
32 X = -167109
75
Y = 13711826
89 feet Y = 4179364
84 meter
Z = -17301719
77 Z = -5273564
18
XDOT = -24144
463934 XDOT = -7359
232607
YDOT = -1843
827786 feet/sec YDOT = -561
998709 meter/sec
ZDOT = -711
731981 ZDOT = -216
935908
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
62109985
00016717 00000-0 10270-3 0 9014
2 25544 51
6464 237
9911 0005499 147
4467 212
7037 15
74408647 12203
Satellite: ISS
Catalog Number: 25544
Epoch time: 10096
62109985 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 237
9911 deg
Eccentricity:
0005499
Arg of perigee: 147
4467 deg
Mean anomaly: 212
7037 deg
Mean motion: 15
74408647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1220
Checksum: 321
Coasting Arc #3 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2010/097/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4132377
31 A = 6730882
39 meter
Y = 5301492
59 meter E =
0017678
Z = -9374
78 I = 51
39926
XDOT = -3791
526287 Wp = 139
87097
YDOT = 2955
888609 meter/sec RA = 232
00071 deg
ZDOT = -6022
203994 TA = 40
23128
MA = 40
10058
Ha = 190
888 n
mi
Hp = 181
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13557668
32 X = 4072833
48
Y = 17393348
38 feet Y = 5347370
36 meter
Z = -30757
16 Z = 10555
34
XDOT = -12439
390704 XDOT = -3795
043185
YDOT = 9697
797274 feet/sec YDOT = 2913
469614 meter/sec
ZDOT = -19757
887118 ZDOT = -6040
631757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22051597
72 X = 6721326
98
Y = -254084
63 feet Y = -77444
99 meter
Z = 48616
30 Z = 14818
25
XDOT = 234
677956 XDOT = 71
529841
YDOT = 14070
840265 feet/sec YDOT = 4288
792113 meter/sec
ZDOT = -19831
005931 ZDOT = -6044
490608
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
63664920
00016717 00000-0 10270-3 0 9022
2 25544 51
6458 232
7732 0005536 151
0390 209
1081 15
74456503 12368
Satellite: ISS
Catalog Number: 25544
Epoch time: 10097
63664920 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 232
7732 deg
Eccentricity:
0005536
Arg of perigee: 151
0390 deg
Mean anomaly: 209
1081 deg
Mean motion: 15
74456503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 294
Coasting Arc #4 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2010/098/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3213645
20 A = 6718485
59 meter
Y = -2696938
36 meter E =
0006424
Z = 5243464
43 I = 51
37869
XDOT = 5145
846587 Wp = 133
91717
YDOT = 5732
541217 meter/sec RA = 226
84178 deg
ZDOT = -209
560823 TA = 318
05290
MA = 318
10208
Ha = 190
501 n
mi
Hp = 181
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10543455
39 X = 3218092
36
Y = -8848222
96 feet Y = -2660976
32 meter
Z = 17202967
31 Z = 5259087
17
XDOT = 16882
698777 XDOT = 5082
379835
YDOT = 18807
549924 feet/sec YDOT = 5789
730262 meter/sec
ZDOT = -687
535509 ZDOT = -184
716926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -951355
20 X = -289973
06
Y = -13653350
61 feet Y = -4161541
27 meter
Z = 17264950
78 Z = 5262357
00
XDOT = 24158
461117 XDOT = 7363
498949
YDOT = -2410
141857 feet/sec YDOT = -734
611238 meter/sec
ZDOT = -588
608619 ZDOT = -179
407907
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
65215683
00016717 00000-0 10270-3 0 9034
2 25544 51
6464 227
5544 0005300 154
9169 205
2253 15
74565781 12528
Satellite: ISS
Catalog Number: 25544
Epoch time: 10098
65215683 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 227
5544 deg
Eccentricity:
0005300
Arg of perigee: 154
9169 deg
Mean anomaly: 205
2253 deg
Mean motion: 15
74565781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 306
Coasting Arc #5 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2010/099/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4808195
71 A = 6730492
63 meter
Y = -4689766
01 meter E =
0012337
Z = 381350
91 I = 51
44064
XDOT = 3606
653275 Wp = 72
44901
YDOT = -3196
849243 meter/sec RA = 221
69159 deg
ZDOT = 6004
126630 TA = 291
70813
MA = 291
83943
Ha = 190
498 n
mi
Hp = 181
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15774920
32 X = -4757249
08
Y = -15386371
42 feet Y = -4743249
23 meter
Z = 1251151
27 Z = 358116
86
XDOT = 11832
851953 XDOT = 3612
966117
YDOT = -10488
350534 feet/sec YDOT = -3156
481799 meter/sec
ZDOT = 19698
578182 ZDOT = 6021
663226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21677408
24 X = -6607274
03
Y = 3987658
89 feet Y = 1215438
43 meter
Z = 1158647
64 Z = 353155
80
XDOT = -1497
082719 XDOT = -456
310813
YDOT = -14042
307353 feet/sec YDOT = -4280
095281 meter/sec
ZDOT = 19768
149564 ZDOT = 6025
331987
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
66762824
00016717 00000-0 10270-3 0 9041
2 25544 51
6463 222
3363 0005149 156
8646 203
2750 15
74573146 12682
Satellite: ISS
Catalog Number: 25544
Epoch time: 10099
66762824 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 222
3363 deg
Eccentricity:
0005149
Arg of perigee: 156
8646 deg
Mean anomaly: 203
2750 deg
Mean motion: 15
74573146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 317
Coasting Arc #6 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2010/100/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3121289
97 A = 6718436
20 meter
Y = 2873474
10 meter E =
0017483
Z = -5224113
86 I = 51
42343
XDOT = -5798
640827 Wp = 110
75522
YDOT = -4999
981236 meter/sec RA = 216
52738 deg
ZDOT = 710
183813 TA = 166
05363
MA = 166
00528
Ha = 190
263 n
mi
Hp = 181
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10240452
65 X = -3127811
91
Y = 9427408
48 feet Y = 2838533
12 meter
Z = -17139481
18 Z = -5239293
14
XDOT = -19024
412161 XDOT = -5745
749113
YDOT = -16404
137915 feet/sec YDOT = -5064
529301 meter/sec
ZDOT = 2329
999386 ZDOT = 682
142899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2069415
57 X = 630757
87
Y = 13689143
27 feet Y = 4172450
87 meter
Z = -17199697
44 Z = -5242467
78
XDOT = -23283
533545 XDOT = -7096
821025
YDOT = 6324
261919 feet/sec YDOT = 1927
635033 meter/sec
ZDOT = 2218
371473 ZDOT = 676
159625
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
61959407
00016717 00000-0 10270-3 0 9055
2 25544 51
6457 217
4438 0005012 161
1423 198
9927 15
74638457 12834
Satellite: ISS
Catalog Number: 25544
Epoch time: 10100
61959407 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 217
4438 deg
Eccentricity:
0005012
Arg of perigee: 161
1423 deg
Mean anomaly: 198
9927 deg
Mean motion: 15
74638457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 313
Coasting Arc #7 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2010/101/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5295696
05 A = 6729864
87 meter
Y = 4046951
50 meter E =
0015018
Z = -875250
87 I = 51
48732
XDOT = -3552
431988 Wp = 148
64541
YDOT = 3375
267860 meter/sec RA = 211
38831 deg
ZDOT = -5945
678082 TA = 40
93313
MA = 40
82047
Ha = 190
142 n
mi
Hp = 181
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17374330
87 X = 5254300
55
Y = 13277399
94 feet Y = 4105939
60 meter
Z = -2871557
97 Z = -849625
17
XDOT = -11654
960591 XDOT = -3561
027680
YDOT = 11073
713453 feet/sec YDOT = 3335
493907 meter/sec
ZDOT = -19506
817855 ZDOT = -5962
957008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20649454
62 X = 6293953
77
Y = -7234096
03 feet Y = -2204952
47 meter
Z = -2769556
98 Z = -844160
97
XDOT = 2382
887556 XDOT = 726
304127
YDOT = 14220
500565 feet/sec YDOT = 4334
408572 meter/sec
ZDOT = -19575
360819 ZDOT = -5966
569978
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
63498721
00016717 00000-0 10270-3 0 9066
2 25544 51
6454 212
2247 0004998 163
5255 196
6063 15
74704047 12995
Satellite: ISS
Catalog Number: 25544
Epoch time: 10101
63498721 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 212
2247 deg
Eccentricity:
0004998
Arg of perigee: 163
5255 deg
Mean anomaly: 196
6063 deg
Mean motion: 15
74704047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 315
Coasting Arc #8 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2010/102/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3093104
19 A = 6718317
59 meter
Y = -3031067
92 meter E =
0004893
Z = 5132136
20 I = 51
47664
XDOT = 6299
690444 Wp = 119
04587
YDOT = 4246
874949 meter/sec RA = 206
21709 deg
ZDOT = -1289
970768 TA = 343
30064
MA = 343
31674
Ha = 189
726 n
mi
Hp = 182
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10147979
64 X = 3101837
06
Y = -9944448
56 feet Y = -2996429
75 meter
Z = 16837717
20 Z = 5147184
08
XDOT = 20668
275734 XDOT = 6257
999413
YDOT = 13933
316763 feet/sec YDOT = 4317
088628 meter/sec
ZDOT = -4232
187560 ZDOT = -1259
468233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3024402
24 X = -921837
80
Y = -13809881
91 feet Y = -4209252
01 meter
Z = 16897408
71 Z = 5150330
18
XDOT = 21835
709570 XDOT = 6655
524277
YDOT = -9806
265844 feet/sec YDOT = -2988
949829 meter/sec
ZDOT = -4110
789592 ZDOT = -1252
968668
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
65033861
00016717 00000-0 10270-3 0 9070
2 25544 51
6462 207
0052 0004803 169
2706 190
8561 15
74803233 13154
Satellite: ISS
Catalog Number: 25544
Epoch time: 10102
65033861 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 207
0052 deg
Eccentricity:
0004803
Arg of perigee: 169
2706 deg
Mean anomaly: 190
8561 deg
Mean motion: 15
74803233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 278
Coasting Arc #9 (Orbit 1330)
---------------------------------------
Vector Time (GMT): 2010/103/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5651246
73 A = 6729084
16 meter
Y = -3367983
21 meter E =
0013240
Z = 1395969
97 I = 51
53986
XDOT = 3574
237964 Wp = 79
76230
YDOT = -3569
814423 meter/sec RA = 201
09047 deg
ZDOT = 5812
465179 TA = 295
60969
MA = 295
74644
Ha = 189
761 n
mi
Hp = 182
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18540835
72 X = -5619946
77
Y = -11049813
67 feet Y = -3431003
71 meter
Z = 4579953
96 Z = 1368592
13
XDOT = 11726
502508 XDOT = 3585
654360
YDOT = -11711
989576 feet/sec YDOT = -3529
780929 meter/sec
ZDOT = 19069
767647 ZDOT = 5829
857022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19098542
40 X = -5821235
72
Y = 10104095
81 feet Y = 3079728
40 meter
Z = 4471003
87 Z = 1362761
98
XDOT = -3219
285407 XDOT = -981
238192
YDOT = -14619
647552 feet/sec YDOT = -4456
068574 meter/sec
ZDOT = 19138
758808 ZDOT = 5833
493685
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
66565451
00016717 00000-0 10270-3 0 9088
2 25544 51
6456 201
7856 0004619 169
3765 190
7497 15
74804350 13317
Satellite: ISS
Catalog Number: 25544
Epoch time: 10103
66565451 = yrday
fracday
Element set: 908
Inclination: 51
6456 deg
RA of node: 201
7856 deg
Eccentricity:
0004619
Arg of perigee: 169
3765 deg
Mean anomaly: 190
7497 deg
Mean motion: 15
74804350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1331
Checksum: 319
Coasting Arc #10 (Orbit 1345)
---------------------------------------
Vector Time (GMT): 2010/104/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3177583
11 A = 6718812
66 meter
Y = 3212913
46 meter E =
0015339
Z = -4985806
94 I = 51
53451
XDOT = -6576
272556 Wp = 120
62084
YDOT = -3481
283501 meter/sec RA = 195
91238 deg
ZDOT = 1944
596557 TA = 168
23724
MA = 168
20136
Ha = 189
514 n
mi
Hp = 181
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10425141
45 X = -3189053
78
Y = 10541054
67 feet Y = 3177315
44 meter
Z = -16357634
32 Z = -5001271
92
XDOT = -21575
697363 XDOT = -6546
302102
YDOT = -11421
533797 feet/sec YDOT = -3554
655619 meter/sec
ZDOT = 6379
909963 ZDOT = 1912
721500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3870771
96 X = 1179811
29
Y = 14240913
91 feet Y = 4340630
56 meter
Z = -16418986
08 Z = -5004506
96
XDOT = -19744
077441 XDOT = -6017
994804
YDOT = 12588
265243 feet/sec YDOT = 3836
903246 meter/sec
ZDOT = 6253
073679 ZDOT = 1905
936857
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
61747416
00016717 00000-0 10270-3 0 9098
2 25544 51
6454 196
8918 0004508 173
6245 186
4977 15
74875715 13460
Satellite: ISS
Catalog Number: 25544
Epoch time: 10104
61747416 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 196
8918 deg
Eccentricity:
0004508
Arg of perigee: 173
6245 deg
Mean anomaly: 186
4977 deg
Mean motion: 15
74875715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1346
Checksum: 342
Coasting Arc #11 (Orbit 1361)
---------------------------------------
Vector Time (GMT): 2010/105/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5802014
99 A = 6727733
06 meter
Y = 2733330
63 meter E =
0010749
Z = -2015606
25 I = 51
59503
XDOT = -3717
862990 Wp = 154
57849
YDOT = 3793
069413 meter/sec RA = 190
79900 deg
ZDOT = -5578
800375 TA = 47
91573
MA = 47
82436
Ha = 189
380 n
mi
Hp = 182
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19035482
26 X = 5780810
80
Y = 8967620
19 feet Y = 2798093
60 meter
Z = -6612881
41 Z = -1987471
15
XDOT = -12197
713221 XDOT = -3732
900160
YDOT = 12444
453456 feet/sec YDOT = 3751
409813 meter/sec
ZDOT = -18303
150835 ZDOT = -5596
898713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17174049
75 X = 5234650
36
Y = -12218341
96 feet Y = -3724150
63 meter
Z = -6500933
19 Z = -1981484
44
XDOT = 4018
298852 XDOT = 1224
777490
YDOT = 15388
379904 feet/sec YDOT = 4690
378195 meter/sec
ZDOT = -18374
956973 ZDOT = -5600
686885
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 10105
63271147
00016717 00000-0 10270-3 0 9106
2 25544 51
6458 191
6716 0004438 175
6734 184
4468 15
74960197 13620
Satellite: ISS
Catalog Number: 25544
Epoch time: 10105
63271147 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 191
6716 deg
Eccentricity:
0004438
Arg of perigee: 175
6734 deg
Mean anomaly: 184
4468 deg
Mean motion: 15
74960197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1362
Checksum: 320
Coasting Arc #12 (Orbit 1377)
---------------------------------------
Vector Time (GMT): 2010/106/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3312960
02 A = 6719406
96 meter
Y = -3436440
04 meter E =
0006553
Z = 4723339
54 I = 51
59681
XDOT = 6678
326937 Wp = 96
38706
YDOT = 2776
599857 meter/sec RA = 185
61497 deg
ZDOT = -2661
664454 TA = 19
77496
MA = 19
74956
Ha = 189
004 n
mi
Hp = 182
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10869291
41 X = 3328195
14
Y = -11274409
57 feet Y = -3399307
34 meter
Z = 15496520
81 Z = 4739471
21
XDOT = 21910
521446 XDOT = 6659
712262
YDOT = 9109
579583 feet/sec YDOT = 2851
176787 meter/sec
ZDOT = -8732
494927 ZDOT = -2629
265795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4789724
89 X = -1459908
15
Y = -14843326
92 feet Y = -4524246
05 meter
Z = 15560531
65 Z = 4742850
05
XDOT = 17377
324017 XDOT = 5296
608361
YDOT = -14635
020606 feet/sec YDOT = -4460
754281 meter/sec
ZDOT = -8603
585984 ZDOT = -2622
373008
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 10106
64790836
00016717 00000-0 10270-3 0 9110
2 25544 51
6447 186
4515 0004321 180
6797 179
4362 15
75038545 13781
Satellite: ISS
Catalog Number: 25544
Epoch time: 10106
64790836 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 186
4515 deg
Eccentricity:
0004321
Arg of perigee: 180
6797 deg
Mean anomaly: 179
4362 deg
Mean motion: 15
75038545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1378
Checksum: 325
Coasting Arc #13 (Orbit 1393)
---------------------------------------
Vector Time (GMT): 2010/107/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5802248
89 A = 6726256
76 meter
Y = -2138290
80 meter E =
0013421
Z = 2636829
32 I = 51
64934
XDOT = 3897
485567 Wp = 95
09534
YDOT = -4100
757717 meter/sec RA = 180
51325 deg
ZDOT = 5226
950923 TA = 294
91551
MA = 295
05493
Ha = 189
059 n
mi
Hp = 182
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19036249
65 X = -5790716
34
Y = -7015389
76 feet Y = -2203110
56 meter
Z = 8651014
83 Z = 2608669
53
XDOT = 12787
026139 XDOT = 3917
659320
YDOT = -13453
929517 feet/sec YDOT = -4057
061006 meter/sec
ZDOT = 17148
789118 ZDOT = 5245
934139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15016515
29 X = -4577033
86
Y = 13712213
55 feet Y = 4179482
69 meter
Z = 8538970
66 Z = 2602678
26
XDOT = -5100
453220 XDOT = -1554
618141
YDOT = -16360
988579 feet/sec YDOT = -4986
829319 meter/sec
ZDOT = 17224
125462 ZDOT = 5249
913441
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 10107
66306948
00016717 00000-0 10270-3 0 9121
2 25544 51
6441 181
2302 0004148 180
8171 179
2986 15
75046185 13944
Satellite: ISS
Catalog Number: 25544
Epoch time: 10107
66306948 = yrday
fracday
Element set: 912
Inclination: 51
6441 deg
RA of node: 181
2302 deg
Eccentricity:
0004148
Arg of perigee: 180
8171 deg
Mean anomaly: 179
2986 deg
Mean motion: 15
75046185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1394
Checksum: 309
Coasting Arc #14 (Orbit 1408)
---------------------------------------
Vector Time (GMT): 2010/108/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3499107
22 A = 6720652
82 meter
Y = 3744661
36 meter E =
0010934
Z = -4358758
76 I = 51
66263
XDOT = -6552
831545 Wp = 132
38386
YDOT = -2162
451418 meter/sec RA = 175
32418 deg
ZDOT = 3400
844077 TA = 171
93012
MA = 171
91251
Ha = 188
765 n
mi
Hp = 182
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11480010
56 X = -3519546
31
Y = 12285634
39 feet Y = 3705418
13 meter
Z = -14300389
64 Z = -4375807
15
XDOT = -21498
791159 XDOT = -6544
684484
YDOT = -7094
656883 feet/sec YDOT = -2235
683636 meter/sec
ZDOT = 11157
624923 ZDOT = 3369
029759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5927996
28 X = 1806853
27
Y = 15673110
48 feet Y = 4777164
08 meter
Z = -14368057
17 Z = -4379383
82
XDOT = -14809
218393 XDOT = -4513
849766
YDOT = 15719
223286 feet/sec YDOT = 4791
219257 meter/sec
ZDOT = 11031
033979 ZDOT = 3362
259157
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 10108
61474464
00016717 00000-0 10270-3 0 9137
2 25544 51
6450 176
3354 0004087 186
3999 173
7114 15
75121049 14099
Satellite: ISS
Catalog Number: 25544
Epoch time: 10108
61474464 = yrday
fracday
Element set: 913
Inclination: 51
6450 deg
RA of node: 176
3354 deg
Eccentricity:
0004087
Arg of perigee: 186
3999 deg
Mean anomaly: 173
7114 deg
Mean motion: 15
75121049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1409
Checksum: 310
Coasting Arc #15 (Orbit 1424)
---------------------------------------
Vector Time (GMT): 2010/109/14:30:57
852
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5606658
39 A = 6724119
04 meter
Y = 1684213
19 meter E =
0005947
Z = -3306565
23 I = 51
70427
XDOT = -4120
540645 Wp = 138
63168
YDOT = 4484
611682 meter/sec RA = 170
23255 deg
ZDOT = -4711
763692 TA = 80
17060
MA = 80
10346
Ha = 188
643 n
mi
Hp = 182
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18394548
52 X = 5603471
32
Y = 5525633
81 feet Y = 1746892
48 meter
Z = -10848311
13 Z = -3279335
56
XDOT = -13518
834137 XDOT = -4147
493067
YDOT = 14713
292920 feet/sec YDOT = 4438
382827 meter/sec
ZDOT = -15458
542295 ZDOT = -4731
846718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12920527
43 X = 3938176
76
Y = -14293048
85 feet Y = -4356521
29 meter
Z = -10739954
58 Z = -3273538
16
XDOT = 6473
427083 XDOT = 1973
100575
YDOT = 17504
583230 feet/sec YDOT = 5335
396968 meter/sec
ZDOT = -15538
265498 ZDOT = -4736
063324
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 10109
62982856
00016717 00000-0 10270-3 0 9149
2 25544 51
6445 171
1137 0004072 190
0288 170
0795 15
75191142 14256
Satellite: ISS
Catalog Number: 25544
Epoch time: 10109
62982856 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 171
1137 deg
Eccentricity:
0004072
Arg of perigee: 190
0288 deg
Mean anomaly: 170
0795 deg
Mean motion: 15
75191142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1425
Checksum: 299
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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