Date:
June 25th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10064 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 2446)
---------------------------------------
Vector Time (GMT): 2010/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6414107
22 A = 6736113
00 meter
Y = 301825
18 meter E =
0013815
Z = 2033671
30 I = 51
55618
XDOT = 1533
124596 Wp = 70
68954
YDOT = 5094
999695 meter/sec RA = 197
25555 deg
ZDOT = -5556
438987 TA = 86
63566
MA = 86
47764
Ha = 195
337 n
mi
Hp = 185
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21043658
85 X = 6400376
18
Y = 990240
09 feet Y = 373474
39 meter
Z = 6672149
94 Z = 2064797
90
XDOT = 5029
936339 XDOT = 1503
029744
YDOT = 16715
878265 feet/sec YDOT = 5111
976801 meter/sec
ZDOT = -18229
786702 ZDOT = -5549
063156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 707184
07 X = 215549
70
Y = -21015318
77 feet Y = -6405469
16 meter
Z = 6796322
94 Z = 2071519
23
XDOT = 15112
028278 XDOT = 4606
146219
YDOT = -5414
016801 feet/sec YDOT = -1650
192321 meter/sec
ZDOT = -18200
304603 ZDOT = -5547
452843
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 10174
53590799
00016717 00000-0 10270-3 0 9007
2 25544 51
6451 198
1208 0009619 359
1397
9747 15
71965813 24475
Satellite: ISS
Catalog Number: 25544
Epoch time: 10174
53590799 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 198
1208 deg
Eccentricity:
0009619
Arg of perigee: 359
1397 deg
Mean anomaly:
9747 deg
Mean motion: 15
71965813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2447
Checksum: 336
Coasting Arc #2 (Orbit 2462)
---------------------------------------
Vector Time (GMT): 2010/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2512446
87 A = 6728988
69 meter
Y = -4247719
37 meter E =
0010364
Z = 4564039
88 I = 51
56034
XDOT = 7031
601987 Wp = 54
22475
YDOT = -926
940924 meter/sec RA = 192
17071 deg
ZDOT = 3009
312985 TA = 5
86893
MA = 5
85679
Ha = 195
537 n
mi
Hp = 185
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8242935
92 X = -2486932
67
Y = -13936087
17 feet Y = -4275673
32 meter
Z = 14973884
12 Z = 4551895
51
XDOT = 23069
560324 XDOT = 7026
825890
YDOT = -3041
144764 feet/sec YDOT = -848
336678 meter/sec
ZDOT = 9873
074097 ZDOT = 3043
460762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13673423
66 X = -4167659
53
Y = 8754891
69 feet Y = 2668490
99 meter
Z = 14925383
78 Z = 4549256
98
XDOT = -3106
948782 XDOT = -946
997989
YDOT = -21909
616511 feet/sec YDOT = -6678
051112 meter/sec
ZDOT = 10009
304499 ZDOT = 3050
836011
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 10175
55306193
00016717 00000-0 10270-3 0 9014
2 25544 51
6443 192
9132 0009660 3
3114 356
8111 15
71958868 24633
Satellite: ISS
Catalog Number: 25544
Epoch time: 10175
55306193 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 192
9132 deg
Eccentricity:
0009660
Arg of perigee: 3
3114 deg
Mean anomaly: 356
8111 deg
Mean motion: 15
71958868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2463
Checksum: 301
Coasting Arc #3 (Orbit 2477)
---------------------------------------
Vector Time (GMT): 2010/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5631696
31 A = 6733409
51 meter
Y = 1851999
57 meter E =
0011768
Z = -3185923
50 I = 51
60626
XDOT = -4143
216381 Wp = 29
26035
YDOT = -4350
725653 meter/sec RA = 187
00042 deg
ZDOT = 4812
306894 TA = 293
58427
MA = 293
70782
Ha = 195
492 n
mi
Hp = 185
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18476693
94 X = -5636510
56
Y = 6076114
07 feet Y = 1788996
33 meter
Z = -10452504
92 Z = -3213293
50
XDOT = -13593
229596 XDOT = -4117
635076
YDOT = -14274
034295 feet/sec YDOT = -4396
915533 meter/sec
ZDOT = 15788
408446 ZDOT = 4792
240448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6950290
55 X = 2118448
56
Y = 18102657
14 feet Y = 5517689
90 meter
Z = -10561699
97 Z = -3219206
15
XDOT = -12281
929722 XDOT = -3743
532179
YDOT = 13847
032063 feet/sec YDOT = 4220
575373 meter/sec
ZDOT = 15708
288338 ZDOT = 4787
886285
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 10176
50663387
00016717 00000-0 10270-3 0 9022
2 25544 51
6450 188
0322 0009722 6
5631 353
5657 15
71986251 24788
Satellite: ISS
Catalog Number: 25544
Epoch time: 10176
50663387 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 188
0322 deg
Eccentricity:
0009722
Arg of perigee: 6
5631 deg
Mean anomaly: 353
5657 deg
Mean motion: 15
71986251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2478
Checksum: 314
Coasting Arc #4 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2010/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4581864
28 A = 6731750
42 meter
Y = 3163866
90 meter E =
0013365
Z = -3798936
12 I = 51
62919
XDOT = -5634
134033 Wp = 34
98627
YDOT = 3127
401486 meter/sec RA = 181
92893 deg
ZDOT = -4187
214194 TA = 190
97400
MA = 191
00318
Ha = 195
664 n
mi
Hp = 185
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15032363
13 X = 4564599
21
Y = 10380140
76 feet Y = 3215008
28 meter
Z = -12463701
18 Z = -3776718
89
XDOT = -18484
691709 XDOT = -5648
345894
YDOT = 10260
503562 feet/sec YDOT = 3064
318629 meter/sec
ZDOT = -13737
579375 ZDOT = -4214
618495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9375213
63 X = 2857565
11
Y = -15748901
55 feet Y = -4800265
19 meter
Z = -12374998
19 Z = -3771899
45
XDOT = 10286
900656 XDOT = 3135
447320
YDOT = 17013
215662 feet/sec YDOT = 5185
628134 meter/sec
ZDOT = -13846
913117 ZDOT = -4220
539118
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 10177
52376846
00016717 00000-0 10270-3 0 9037
2 25544 51
6436 182
8240 0009716 10
0264 350
1090 15
71989308 24946
Satellite: ISS
Catalog Number: 25544
Epoch time: 10177
52376846 = yrday
fracday
Element set: 903
Inclination: 51
6436 deg
RA of node: 182
8240 deg
Eccentricity:
0009716
Arg of perigee: 10
0264 deg
Mean anomaly: 350
1090 deg
Mean motion: 15
71989308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2494
Checksum: 307
Coasting Arc #5 (Orbit 2509)
---------------------------------------
Vector Time (GMT): 2010/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060354
26 A = 6730444
68 meter
Y = -3471705
82 meter E =
0017347
Z = 4091540
93 I = 51
65529
XDOT = 6136
556636 Wp = 46
00152
YDOT = 2667
014582 meter/sec RA = 176
75759 deg
ZDOT = -3804
999959 TA = 83
16847
MA = 82
97113
Ha = 195
668 n
mi
Hp = 185
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13321372
23 X = 4078997
99
Y = -11390110
95 feet Y = -3426197
06 meter
Z = 13423690
71 Z = 4111310
53
XDOT = 20133
059830 XDOT = 6124
761301
YDOT = 8750
047841 feet/sec YDOT = 2735
571995 meter/sec
ZDOT = -12483
595667 ZDOT = -3775
217039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12439583
06 X = -3791584
92
Y = -12260777
68 feet Y = -3737085
04 meter
Z = 13502561
31 Z = 4115580
69
XDOT = 6165
003907 XDOT = 1879
093191
YDOT = -19950
206810 feet/sec YDOT = -6080
823036 meter/sec
ZDOT = -12364
686013 ZDOT = -3768
756297
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 10178
54089248
00016717 00000-0 10270-3 0 9048
2 25544 51
6432 177
6159 0009824 13
2841 346
8578 15
72029736 25102
Satellite: ISS
Catalog Number: 25544
Epoch time: 10178
54089248 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 177
6159 deg
Eccentricity:
0009824
Arg of perigee: 13
2841 deg
Mean anomaly: 346
8578 deg
Mean motion: 15
72029736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2510
Checksum: 324
Coasting Arc #6 (Orbit 2525)
---------------------------------------
Vector Time (GMT): 2010/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5959537
53 A = 6734422
31 meter
Y = -1360987
47 meter E =
0019970
Z = 2795820
36 I = 51
69868
XDOT = 3461
753697 Wp = 54
33340
YDOT = -4597
779035 meter/sec RA = 171
68912 deg
ZDOT = 5126
829874 TA = 337
67192
MA = 337
75874
Ha = 195
825 n
mi
Hp = 184
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19552288
48 X = -5957457
19
Y = -4465181
98 feet Y = -1427619
43 meter
Z = 9172638
99 Z = 2766874
14
XDOT = 11357
459636 XDOT = 3488
004744
YDOT = -15084
576885 feet/sec YDOT = -4558
921764 meter/sec
ZDOT = 16820
307987 ZDOT = 5143
709802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2495321
47 X = -760573
98
Y = 19952694
76 feet Y = 6081581
36 meter
Z = 9057068
15 Z = 2760594
37
XDOT = -14672
689645 XDOT = -4472
235804
YDOT = -9521
916966 feet/sec YDOT = -2902
280291 meter/sec
ZDOT = 16887
638400 ZDOT = 5147
352184
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 10179
55800688
00016717 00000-0 10270-3 0 9050
2 25544 51
6432 172
4089 0009730 16
9062 343
2423 15
72050993 25264
Satellite: ISS
Catalog Number: 25544
Epoch time: 10179
55800688 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 172
4089 deg
Eccentricity:
0009730
Arg of perigee: 16
9062 deg
Mean anomaly: 343
2423 deg
Mean motion: 15
72050993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2526
Checksum: 308
Coasting Arc #7 (Orbit 2540)
---------------------------------------
Vector Time (GMT): 2010/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1893246
56 A = 6727855
82 meter
Y = 4341400
55 meter E =
0015693
Z = -4788623
44 I = 51
70622
XDOT = -7241
179458 Wp = 69
27178
YDOT = -345
539425 meter/sec RA = 166
53022 deg
ZDOT = 2561
805835 TA = 225
78454
MA = 225
91354
Ha = 195
942 n
mi
Hp = 184
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6211438
84 X = -1918390
25
Y = 14243440
12 feet Y = 4320089
30 meter
Z = -15710706
82 Z = -4797881
09
XDOT = -23757
150453 XDOT = -7249
222001
YDOT = -1133
659530 feet/sec YDOT = -426
559980 meter/sec
ZDOT = 8404
874787 ZDOT = 2526
609099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14858434
72 X = 4528850
90
Y = 4418531
76 feet Y = 1346768
48 meter
Z = -15747614
49 Z = -4799872
90
XDOT = 1968
343661 XDOT = 599
951148
YDOT = 22692
966838 feet/sec YDOT = 6916
816292 meter/sec
ZDOT = 8264
346882 ZDOT = 2518
972930
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 10180
51154399
00016717 00000-0 10270-3 0 9060
2 25544 51
6432 167
5264 0009909 20
5526 339
6033 15
72013842 25413
Satellite: ISS
Catalog Number: 25544
Epoch time: 10180
51154399 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 167
5264 deg
Eccentricity:
0009909
Arg of perigee: 20
5526 deg
Mean anomaly: 339
6033 deg
Mean motion: 15
72013842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2541
Checksum: 297
Coasting Arc #8 (Orbit 2556)
---------------------------------------
Vector Time (GMT): 2010/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6481148
59 A = 6736523
08 meter
Y = -779804
06 meter E =
0009386
Z = -1678424
33 I = 51
76509
XDOT = -869
529532 Wp = 72
71952
YDOT = 5052
808298 meter/sec RA = 161
45112 deg
ZDOT = -5728
727797 TA = 125
76356
MA = 125
67626
Ha = 196
013 n
mi
Hp = 184
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21263610
85 X = 6497540
17
Y = -2558412
27 feet Y = -707236
11 meter
Z = -5506641
52 Z = -1646899
63
XDOT = -2852
787178 XDOT = -898
137585
YDOT = 16577
455046 feet/sec YDOT = 5042
925532 meter/sec
ZDOT = -18795
038703 ZDOT = -5733
020707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5378646
44 X = -1639411
44
Y = -20763601
32 feet Y = -6328745
68 meter
Z = -5380775
36 Z = -1640060
33
XDOT = 15280
359216 XDOT = 4657
453489
YDOT = 896
332965 feet/sec YDOT = 273
202288 meter/sec
ZDOT = -18812
115914 ZDOT = -5733
932930
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 10181
52863935
00016717 00000-0 10270-3 0 9076
2 25544 51
6434 162
3181 0010009 24
4787 335
6848 15
72061958 25579
Satellite: ISS
Catalog Number: 25544
Epoch time: 10181
52863935 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 162
3181 deg
Eccentricity:
0010009
Arg of perigee: 24
4787 deg
Mean anomaly: 335
6848 deg
Mean motion: 15
72061958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2557
Checksum: 319
Coasting Arc #9 (Orbit 2572)
---------------------------------------
Vector Time (GMT): 2010/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -382831
22 A = 6726073
97 meter
Y = -4280605
63 meter E =
0013608
Z = 5169117
67 I = 51
75821
XDOT = 7295
284527 Wp = 35
72252
YDOT = -2146
340547 meter/sec RA = 156
31396 deg
ZDOT = -1224
663240 TA = 66
02829
MA = 65
88587
Ha = 196
049 n
mi
Hp = 184
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1256007
94 X = -360046
61
Y = -14043981
72 feet Y = -4284759
91 meter
Z = 16959047
47 Z = 5167312
71
XDOT = 23934
660521 XDOT = 7324
692218
YDOT = -7041
799694 feet/sec YDOT = -2064
595746 meter/sec
ZDOT = -4017
924017 ZDOT = -1189
151980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13679269
11 X = -4169441
23
Y = 3454684
60 feet Y = 1052987
87 meter
Z = 16951785
17 Z = 5166904
12
XDOT = -10316
078921 XDOT = -3144
340855
YDOT = -21627
512223 feet/sec YDOT = -6592
065725 meter/sec
ZDOT = -3876
144445 ZDOT = -1181
448827
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 10182
54572435
00016717 00000-0 10270-3 0 9082
2 25544 51
6433 157
1104 0009959 27
5368 332
6320 15
72067014 25735
Satellite: ISS
Catalog Number: 25544
Epoch time: 10182
54572435 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 157
1104 deg
Eccentricity:
0009959
Arg of perigee: 27
5368 deg
Mean anomaly: 332
6320 deg
Mean motion: 15
72067014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2573
Checksum: 301
Coasting Arc #10 (Orbit 2588)
---------------------------------------
Vector Time (GMT): 2010/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6040094
07 A = 6737486
71 meter
Y = 2925073
71 meter E =
0022604
Z = 437995
40 I = 51
82431
XDOT = -1716
150141 Wp = 42
13075
YDOT = -4471
819270 meter/sec RA = 151
21888 deg
ZDOT = 6035
927298 TA = 322
62135
MA = 322
77839
Ha = 196
042 n
mi
Hp = 184
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19816581
60 X = -6074481
55
Y = 9596698
53 feet Y = 2857337
46 meter
Z = 1436992
80 Z = 408569
67
XDOT = -5630
413850 XDOT = -1695
339096
YDOT = -14671
323063 feet/sec YDOT = -4490
894604 meter/sec
ZDOT = 19802
911082 ZDOT = 6027
640354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12781972
15 X = 3895945
11
Y = 17937071
86 feet Y = 5467219
50 meter
Z = 1319514
46 Z = 402188
01
XDOT = -12192
658530 XDOT = -3716
322320
YDOT = 7191
567831 feet/sec YDOT = 2191
989875 meter/sec
ZDOT = 19769
760084 ZDOT = 6025
822873
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 10183
56279777
00016717 00000-0 10270-3 0 9099
2 25544 51
6434 151
9031 0009895 32
1512 328
0252 15
72115231 25894
Satellite: ISS
Catalog Number: 25544
Epoch time: 10183
56279777 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 151
9031 deg
Eccentricity:
0009895
Arg of perigee: 32
1512 deg
Mean anomaly: 328
0252 deg
Mean motion: 15
72115231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2589
Checksum: 307
Coasting Arc #11 (Orbit 2603)
---------------------------------------
Vector Time (GMT): 2010/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2502077
28 A = 6725570
75 meter
Y = 3336428
16 meter E =
0022452
Z = -5294470
07 I = 51
81049
XDOT = -6290
917469 Wp = 67
54318
YDOT = 4405
283856 meter/sec RA = 146
10803 deg
ZDOT = -189
146307 TA = 200
61631
MA = 200
70705
Ha = 196
182 n
mi
Hp = 184
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8208914
97 X = 2490302
23
Y = 10946286
62 feet Y = 3364342
63 meter
Z = -17370308
63 Z = -5282343
27
XDOT = -20639
493010 XDOT = -6338
791763
YDOT = 14453
031022 feet/sec YDOT = 4334
667404 meter/sec
ZDOT = -620
558749 ZDOT = -219
823245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9224940
93 X = 2811762
00
Y = -10187717
18 feet Y = -3105216
20 meter
Z = -17321835
38 Z = -5279695
42
XDOT = 17268
204132 XDOT = 5263
348620
YDOT = 16942
978891 feet/sec YDOT = 5164
219966 meter/sec
ZDOT = -743
026803 ZDOT = -226
474570
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 10184
51629655
00016717 00000-0 10270-3 0 9101
2 25544 51
6440 147
0204 0010013 34
7073 325
4741 15
72091620 26040
Satellite: ISS
Catalog Number: 25544
Epoch time: 10184
51629655 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 147
0204 deg
Eccentricity:
0010013
Arg of perigee: 34
7073 deg
Mean anomaly: 325
4741 deg
Mean motion: 15
72091620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2604
Checksum: 265
Coasting Arc #12 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2010/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4808940
58 A = 6737260
96 meter
Y = -4655520
52 meter E =
0017001
Z = 752736
67 I = 51
87497
XDOT = 3818
024988 Wp = 90
79339
YDOT = 2956
710767 meter/sec RA = 140
99224 deg
ZDOT = -5989
643249 TA = 81
03928
MA = 80
84688
Ha = 196
204 n
mi
Hp = 183
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15777364
11 X = 4856985
39
Y = -15274017
46 feet Y = -4601475
53 meter
Z = 2469608
50 Z = 776214
65
XDOT = 12526
328700 XDOT = 3813
775310
YDOT = 9700
494642 feet/sec YDOT = 2999
383124 meter/sec
ZDOT = -19651
060529 ZDOT = -5971
105290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18134535
01 X = -5527406
27
Y = -12364779
00 feet Y = -3768784
64 meter
Z = 2563332
58 Z = 781303
77
XDOT = 6054
432758 XDOT = 1845
391105
YDOT = -13013
830723 feet/sec YDOT = -3966
615604 meter/sec
ZDOT = -19576
983596 ZDOT = -5967
064600
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 10185
53335028
00016717 00000-0 10270-3 0 9113
2 25544 51
6443 141
8124 0010058 38
1366 322
0507 15
72121648 26203
Satellite: ISS
Catalog Number: 25544
Epoch time: 10185
53335028 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 141
8124 deg
Eccentricity:
0010058
Arg of perigee: 38
1366 deg
Mean anomaly: 322
0507 deg
Mean motion: 15
72121648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 270
Coasting Arc #13 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2010/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4028433
82 A = 6726134
09 meter
Y = -1680862
83 meter E =
0011479
Z = 5107312
82 I = 51
86105
XDOT = 4499
536319 Wp = 66
60307
YDOT = -6060
402554 meter/sec RA = 135
90850 deg
ZDOT = 1556
236153 TA = 8
53012
MA = 8
51062
Ha = 196
259 n
mi
Hp = 183
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13216646
38 X = -4034149
13
Y = -5514641
83 feet Y = -1725943
78 meter
Z = 16756275
66 Z = 5087728
57
XDOT = 14762
258263 XDOT = 4559
410500
YDOT = -19883
210479 feet/sec YDOT = -6009
751475 meter/sec
ZDOT = 5105
761658 ZDOT = 1578
239610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2476647
81 X = -754882
25
Y = 14197651
92 feet Y = 4327444
30 meter
Z = 16678030
03 Z = 5083463
55
XDOT = -21582
507732 XDOT = -6578
348357
YDOT = -9859
124251 feet/sec YDOT = -3005
061072 meter/sec
ZDOT = 5193
594844 ZDOT = 1583
007709
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 10186
55039196
00016717 00000-0 10270-3 0 9124
2 25544 51
6447 136
6052 0009922 41
3935 318
7977 15
72169628 26365
Satellite: ISS
Catalog Number: 25544
Epoch time: 10186
55039196 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 136
6052 deg
Eccentricity:
0009922
Arg of perigee: 41
3935 deg
Mean anomaly: 318
7977 deg
Mean motion: 15
72169628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 333
Coasting Arc #14 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2010/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2931635
88 A = 6735789
21 meter
Y = 5737191
03 meter E =
0016908
Z = -1948078
03 I = 51
91393
XDOT = -5187
714308 Wp = 43
02489
YDOT = -750
233916 meter/sec RA = 130
77399 deg
ZDOT = 5638
038245 TA = 295
40030
MA = 295
57523
Ha = 196
268 n
mi
Hp = 183
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9618227
96 X = -2986108
87
Y = 18822805
22 feet Y = 5704103
43 meter
Z = -6391332
12 Z = -1962451
46
XDOT = -17020
060066 XDOT = -5206
328135
YDOT = -2461
397363 feet/sec YDOT = -808
350910 meter/sec
ZDOT = 18497
500804 ZDOT = 5612
790935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20546313
94 X = 6262516
49
Y = 4890872
53 feet Y = 1490737
95 meter
Z = -6448703
84 Z = -1965564
93
XDOT = 1988
269454 XDOT = 606
024530
YDOT = 15729
625180 feet/sec YDOT = 4794
389755 meter/sec
ZDOT = 18396
635873 ZDOT = 5607
294614
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 10187
50386081
00016717 00000-0 10270-3 0 9139
2 25544 51
6443 131
7225 0010062 44
9597 315
2379 15
72140972 26515
Satellite: ISS
Catalog Number: 25544
Epoch time: 10187
50386081 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 131
7225 deg
Eccentricity:
0010062
Arg of perigee: 44
9597 deg
Mean anomaly: 315
2379 deg
Mean motion: 15
72140972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 298
Coasting Arc #15 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2010/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4822787
34 A = 6727962
23 meter
Y = -405956
68 meter E =
0020534
Z = -4693333
92 I = 51
90755
XDOT = -2171
477528 Wp = 60
28347
YDOT = 6807
222742 meter/sec RA = 125
71037 deg
ZDOT = -2819
414699 TA = 181
91307
MA = 181
92094
Ha = 196
284 n
mi
Hp = 183
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15822793
10 X = 4849767
80
Y = -1331878
87 feet Y = -351873
78 meter
Z = -15398077
17 Z = -4669839
29
XDOT = -7124
270104 XDOT = -2233
739502
YDOT = 22333
407947 feet/sec YDOT = 6782
592318 meter/sec
ZDOT = -9250
048225 ZDOT = -2830
113891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5293083
72 X = -1613331
92
Y = -15066511
37 feet Y = -4592272
67 meter
Z = -15304213
91 Z = -4664724
40
XDOT = 22294
657227 XDOT = 6795
411523
YDOT = 1609
464268 feet/sec YDOT = 490
564709 meter/sec
ZDOT = -9292
748400 ZDOT = -2832
429712
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 10188
52088251
00016717 00000-0 10270-3 0 9141
2 25544 51
6453 126
5139 0010073 48
8316 311
3713 15
72179669 26677
Satellite: ISS
Catalog Number: 25544
Epoch time: 10188
52088251 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 126
5139 deg
Eccentricity:
0010073
Arg of perigee: 48
8316 deg
Mean anomaly: 311
3713 deg
Mean motion: 15
72179669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 312
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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