Date:
June 19th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 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 2336)
---------------------------------------
Vector Time (GMT): 2010/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4878316
23 A = 6728829
41 meter
Y = 346915
37 meter E =
0011944
Z = 4625042
99 I = 51
36290
XDOT = 2233
780095 Wp = 11
02061
YDOT = 6787
444209 meter/sec RA = 233
17526 deg
ZDOT = -2852
448863 TA = 107
38014
MA = 107
24948
Ha = 194
288 n
mi
Hp = 187
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16004974
51 X = 4851606
99
Y = 1138173
79 feet Y = 401317
58 meter
Z = 15174025
57 Z = 4648676
81
XDOT = 7328
674852 XDOT = 2171
572192
YDOT = 22268
517745 feet/sec YDOT = 6812
076268 meter/sec
ZDOT = -9358
428028 ZDOT = -2841
747357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2830753
08 X = 862813
54
Y = -15702644
95 feet Y = -4786166
18 meter
Z = 15268250
70 Z = 4653762
81
XDOT = 21784
034265 XDOT = 6639
773644
YDOT = -5171
414121 feet/sec YDOT = -1576
247024 meter/sec
ZDOT = -9315
699196 ZDOT = -2839
425115
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 10167
54274156
00016717 00000-0 10270-3 0 9006
2 25544 51
6466 233
9124 0009538 328
5864 31
4727 15
71880379 23373
Satellite: ISS
Catalog Number: 25544
Epoch time: 10167
54274156 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 233
9124 deg
Eccentricity:
0009538
Arg of perigee: 328
5864 deg
Mean anomaly: 31
4727 deg
Mean motion: 15
71880379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2337
Checksum: 323
Coasting Arc #2 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2010/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3094133
38 A = 6736861
47 meter
Y = -5673230
85 meter E =
0016661
Z = 1864892
02 I = 51
40773
XDOT = 5170
523744 Wp = 31
92583
YDOT = -966
470624 meter/sec RA = 228
07683 deg
ZDOT = 5629
609297 TA = 348
85215
MA = 348
88901
Ha = 194
610 n
mi
Hp = 187
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10151356
23 X = -3039523
56
Y = -18612962
11 feet Y = -5707526
19 meter
Z = 6118412
14 Z = 1849992
76
XDOT = 16963
660576 XDOT = 5153
599288
YDOT = -3170
835382 feet/sec YDOT = -908
746083 meter/sec
ZDOT = 18469
846774 ZDOT = 5654
686288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19450768
60 X = -5928594
27
Y = 8478451
20 feet Y = 2584231
93 meter
Z = 6058945
86 Z = 1846766
70
XDOT = -1028
922863 XDOT = -313
615689
YDOT = -15652
181700 feet/sec YDOT = -4770
784982 meter/sec
ZDOT = 18569
819387 ZDOT = 5660
080949
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 10168
55996638
00016717 00000-0 10270-3 0 9015
2 25544 51
6459 228
7056 0009494 334
1167 25
9519 15
71838440 23538
Satellite: ISS
Catalog Number: 25544
Epoch time: 10168
55996638 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 228
7056 deg
Eccentricity:
0009494
Arg of perigee: 334
1167 deg
Mean anomaly: 25
9519 deg
Mean motion: 15
71838440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 337
Coasting Arc #3 (Orbit 2367)
---------------------------------------
Vector Time (GMT): 2010/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3914105
09 A = 6726826
50 meter
Y = 1944182
76 meter E =
0011980
Z = -5121231
68 I = 51
39513
XDOT = -4730
506597 Wp = 58
43618
YDOT = -5904
754994 meter/sec RA = 222
91219 deg
ZDOT = 1382
389335 TA = 224
81237
MA = 224
90919
Ha = 194
696 n
mi
Hp = 187
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12841552
13 X = -3910676
46
Y = 6378552
36 feet Y = 1900432
65 meter
Z = -16801941
21 Z = -5140237
79
XDOT = -15520
034768 XDOT = -4670
842348
YDOT = -19372
555756 feet/sec YDOT = -5957
320895 meter/sec
ZDOT = 4535
398081 ZDOT = 1359
552868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5437899
01 X = 1657471
62
Y = 13170765
67 feet Y = 4014449
38 meter
Z = -16877701
44 Z = -5144323
40
XDOT = -19487
623822 XDOT = -5939
827741
YDOT = 13705
337529 feet/sec YDOT = 4177
386879 meter/sec
ZDOT = 4444
270848 ZDOT = 1354
613754
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 10169
51360419
00016717 00000-0 10270-3 0 9025
2 25544 51
6457 223
8242 0009587 337
4252 22
6487 15
71852711 23684
Satellite: ISS
Catalog Number: 25544
Epoch time: 10169
51360419 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 223
8242 deg
Eccentricity:
0009587
Arg of perigee: 337
4252 deg
Mean anomaly: 22
6487 deg
Mean motion: 15
71852711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 313
Coasting Arc #4 (Orbit 2383)
---------------------------------------
Vector Time (GMT): 2010/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5026445
69 A = 6738024
45 meter
Y = 4454482
02 meter E =
0004428
Z = -551863
94 I = 51
45688
XDOT = -3554
337102 Wp = 79
89246
YDOT = 3274
540964 meter/sec RA = 217
79433 deg
ZDOT = -5982
177545 TA = 106
11763
MA = 106
06888
Ha = 194
878 n
mi
Hp = 186
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16490963
55 X = 4978942
15
Y = 14614442
32 feet Y = 4510425
19 meter
Z = -1810577
24 Z = -527560
32
XDOT = -11661
210966 XDOT = -3561
629078
YDOT = 10743
244634 feet/sec YDOT = 3234
754155 meter/sec
ZDOT = -19626
566749 ZDOT = -5999
461877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15504507
81 X = 4725773
98
Y = -15667985
73 feet Y = -4775602
05 meter
Z = -1713608
49 Z = -522307
87
XDOT = 8945
235471 XDOT = 2726
507771
YDOT = 10990
846223 feet/sec YDOT = 3350
009929 meter/sec
ZDOT = -19695
448413 ZDOT = -6003
172676
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 10170
53080979
00016717 00000-0 10270-3 0 9030
2 25544 51
6464 218
6171 0009621 342
3524 17
7303 15
71903262 23849
Satellite: ISS
Catalog Number: 25544
Epoch time: 10170
53080979 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 218
6171 deg
Eccentricity:
0009621
Arg of perigee: 342
3524 deg
Mean anomaly: 17
7303 deg
Mean motion: 15
71903262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2384
Checksum: 293
Coasting Arc #5 (Orbit 2399)
---------------------------------------
Vector Time (GMT): 2010/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2134349
47 A = 6726064
64 meter
Y = -3610347
07 meter E =
0008958
Z = 5258027
55 I = 51
44067
XDOT = 6540
180149 Wp =
80802
YDOT = 4058
606833 meter/sec RA = 212
65774 deg
ZDOT = 140
794491 TA = 87
90311
MA = 87
80052
Ha = 194
923 n
mi
Hp = 186
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7002458
88 X = 2149019
71
Y = -11844970
71 feet Y = -3586398
14 meter
Z = 17250746
56 Z = 5268431
45
XDOT = 21457
283952 XDOT = 6493
626030
YDOT = 13315
639216 feet/sec YDOT = 4131
482711 meter/sec
ZDOT = 461
924182 ZDOT = 172
454286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11572801
94 X = -3527390
03
Y = -7346864
69 feet Y = -2239324
36 meter
Z = 17292190
51 Z = 5270659
67
XDOT = 13587
948465 XDOT = 4141
606692
YDOT = -20087
175636 feet/sec YDOT = -6122
571134 meter/sec
ZDOT = 588
231084 ZDOT = 179
292834
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 10171
54800635
00016717 00000-0 10270-3 0 9042
2 25544 51
6458 213
4103 0009602 346
1752 13
9146 15
71910562 24007
Satellite: ISS
Catalog Number: 25544
Epoch time: 10171
54800635 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 213
4103 deg
Eccentricity:
0009602
Arg of perigee: 346
1752 deg
Mean anomaly: 13
9146 deg
Mean motion: 15
71910562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2400
Checksum: 273
Coasting Arc #6 (Orbit 2414)
---------------------------------------
Vector Time (GMT): 2010/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6191293
44 A = 6737860
80 meter
Y = -2503634
29 meter E =
0018232
Z = -804895
55 I = 51
50670
XDOT = 1150
223382 Wp = 15
66305
YDOT = -4744
823044 meter/sec RA = 207
51740 deg
ZDOT = 5959
758999 TA = 335
54302
MA = 335
62940
Ha = 195
144 n
mi
Hp = 186
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20312642
51 X = -6158927
13
Y = -8214023
25 feet Y = -2572687
93 meter
Z = -2640733
42 Z = -834894
83
XDOT = 3773
698761 XDOT = 1174
243726
YDOT = -15567
004736 feet/sec YDOT = -4731
827138 meter/sec
ZDOT = 19553
015088 ZDOT = 5965
404469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8636915
14 X = -2632531
74
Y = 20120410
95 feet Y = 6132701
26 meter
Z = -2760408
76 Z = -841372
59
XDOT = -14019
231194 XDOT = -4273
061668
YDOT = -3353
160228 feet/sec YDOT = -1022
043237 meter/sec
ZDOT = 19575
471773 ZDOT = 5966
603796
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 10172
50162099
00016717 00000-0 10270-3 0 9055
2 25544 51
6461 208
5289 0009758 350
1579 9
9391 15
71898076 24153
Satellite: ISS
Catalog Number: 25544
Epoch time: 10172
50162099 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 208
5289 deg
Eccentricity:
0009758
Arg of perigee: 350
1579 deg
Mean anomaly: 9
9391 deg
Mean motion: 15
71898076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2415
Checksum: 332
Coasting Arc #7 (Orbit 2430)
---------------------------------------
Vector Time (GMT): 2010/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 185031
20 A = 6727015
44 meter
Y = 4436386
82 meter E =
0017518
Z = -5067034
40 I = 51
49791
XDOT = -7333
037381 Wp = 44
33450
YDOT = -1597
590708 meter/sec RA = 202
41017 deg
ZDOT = -1657
670170 TA = 209
61841
MA = 209
71773
Ha = 195
281 n
mi
Hp = 186
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 607057
75 X = 160023
88
Y = 14555074
87 feet Y = 4438316
99 meter
Z = -16624128
62 Z = -5066195
50
XDOT = -24058
521590 XDOT = -7306
575102
YDOT = -5241
439332 feet/sec YDOT = -1679
444860 meter/sec
ZDOT = -5438
550426 ZDOT = -1693
230326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14557052
18 X = 4436989
51
Y = -651119
68 feet Y = -198461
28 meter
Z = -16620729
55 Z = -5065998
37
XDOT = -5378
418806 XDOT = -1639
342052
YDOT = 22944
797336 feet/sec YDOT = 6993
574228 meter/sec
ZDOT = -5580
407282 ZDOT = -1700
908140
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 10173
51880069
00016717 00000-0 10270-3 0 9062
2 25544 51
6464 203
3220 0009660 354
0077 6
0968 15
71916090 24315
Satellite: ISS
Catalog Number: 25544
Epoch time: 10173
51880069 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 203
3220 deg
Eccentricity:
0009660
Arg of perigee: 354
0077 deg
Mean anomaly: 6
0968 deg
Mean motion: 15
71916090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2431
Checksum: 291
Coasting Arc #8 (Orbit 2446)
---------------------------------------
Vector Time (GMT): 2010/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6405833
19 A = 6736091
93 meter
Y = 273485
81 meter E =
0013847
Z = 2063870
19 I = 51
55587
XDOT = 1579
061598 Wp = 69
57278
YDOT = 5096
785729 meter/sec RA = 197
24983 deg
ZDOT = -5541
739940 TA = 87
39675
MA = 87
23825
Ha = 195
393 n
mi
Hp = 185
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21016513
10 X = 6392272
97
Y = 897263
17 feet Y = 345043
44 meter
Z = 6771227
67 Z = 2094957
00
XDOT = 5180
648289 XDOT = 1548
871955
YDOT = 16721
737956 feet/sec YDOT = 5114
275997 meter/sec
ZDOT = -18181
561482 ZDOT = -5534
141176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 614592
75 X = 187327
87
Y = -20986337
14 feet Y = -6396635
56 meter
Z = 6895241
63 Z = 2101669
65
XDOT = 15117
974294 XDOT = 4607
958565
YDOT = -5557
754703 feet/sec YDOT = -1694
003633 meter/sec
ZDOT = -18151
190039 ZDOT = -5532
482724
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
53597089
00016717 00000-0 10270-3 0 9073
2 25544 51
6449 198
1146 0009786 358
6279 1
4855 15
71954129 24475
Satellite: ISS
Catalog Number: 25544
Epoch time: 10174
53597089 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 198
1146 deg
Eccentricity:
0009786
Arg of perigee: 358
6279 deg
Mean anomaly: 1
4855 deg
Mean motion: 15
71954129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2447
Checksum: 352
Coasting Arc #9 (Orbit 2462)
---------------------------------------
Vector Time (GMT): 2010/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2555554
04 A = 6729099
50 meter
Y = -4241750
71 meter E =
0010508
Z = 4545648
65 I = 51
56046
XDOT = 7011
276855 Wp = 53
48241
YDOT = -961
535776 meter/sec RA = 192
16547 deg
ZDOT = 3045
766448 TA = 6
21184
MA = 6
19882
Ha = 195
597 n
mi
Hp = 185
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8384363
63 X = -2530014
03
Y = -13916504
96 feet Y = -4270186
56 meter
Z = 14913545
43 Z = 4533294
92
XDOT = 23002
876821 XDOT = 7006
712030
YDOT = -3154
644934 feet/sec YDOT = -883
157644 meter/sec
ZDOT = 9992
672072 ZDOT = 3079
815991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13649524
63 X = -4160375
11
Y = 8895293
29 feet Y = 2711285
40 meter
Z = 14864209
89 Z = 4530611
18
XDOT = -3208
085788 XDOT = -977
824548
YDOT = -21840
519894 feet/sec YDOT = -6656
990464 meter/sec
ZDOT = 10128
510169 ZDOT = 3087
169899
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
55313289
00016717 00000-0 10270-3 0 9085
2 25544 51
6441 192
9070 0009826 2
8002 357
3213 15
71945848 24639
Satellite: ISS
Catalog Number: 25544
Epoch time: 10175
55313289 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 192
9070 deg
Eccentricity:
0009826
Arg of perigee: 2
8002 deg
Mean anomaly: 357
3213 deg
Mean motion: 15
71945848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2463
Checksum: 308
Coasting Arc #10 (Orbit 2477)
---------------------------------------
Vector Time (GMT): 2010/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5602904
51 A = 6733359
60 meter
Y = 1882273
14 meter E =
0011804
Z = -3218723
92 I = 51
60581
XDOT = -4193
949148 Wp = 29
08219
YDOT = -4333
688239 meter/sec RA = 186
99497 deg
ZDOT = 4783
648744 TA = 293
31363
MA = 293
43781
Ha = 195
555 n
mi
Hp = 185
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18382232
64 X = -5607900
08
Y = 6175436
81 feet Y = 1819590
86 meter
Z = -10560117
85 Z = -3245954
49
XDOT = -13759
675681 XDOT = -4168
415372
YDOT = -14218
137267 feet/sec YDOT = -4380
445703 meter/sec
ZDOT = 15694
385643 ZDOT = 4763
335726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7044943
71 X = 2147298
84
Y = 18002916
30 feet Y = 5487288
89 meter
Z = -10668756
17 Z = -3251836
88
XDOT = -12225
432237 XDOT = -3726
311746
YDOT = 14003
151693 feet/sec YDOT = 4268
160636 meter/sec
ZDOT = 15613
281818 ZDOT = 4758
928298
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
50671287
00016717 00000-0 10270-3 0 9097
2 25544 51
6448 188
0261 0009891 6
0406 354
0873 15
71971636 24786
Satellite: ISS
Catalog Number: 25544
Epoch time: 10176
50671287 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 188
0261 deg
Eccentricity:
0009891
Arg of perigee: 6
0406 deg
Mean anomaly: 354
0873 deg
Mean motion: 15
71971636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2478
Checksum: 327
Coasting Arc #11 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2010/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4625116
06 A = 6731897
49 meter
Y = 3139450
30 meter E =
0013327
Z = -3766850
11 I = 51
62939
XDOT = -5588
105921 Wp = 34
26333
YDOT = 3159
187147 meter/sec RA = 181
92368 deg
ZDOT = -4224
777557 TA = 191
19759
MA = 191
22727
Ha = 195
729 n
mi
Hp = 185
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15174265
27 X = 4607964
93
Y = 10300033
80 feet Y = 3191075
98 meter
Z = -12358432
12 Z = -3744422
49
XDOT = -18333
680843 XDOT = -5602
494161
YDOT = 10364
787228 feet/sec YDOT = 3096
618026 meter/sec
ZDOT = -13860
818757 ZDOT = -4251
958678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9286090
60 X = 2830400
42
Y = -15884669
75 feet Y = -4841647
34 meter
Z = -12268889
74 Z = -3739557
59
XDOT = 10371
189540 XDOT = 3161
138572
YDOT = 16861
516703 feet/sec YDOT = 5139
390291 meter/sec
ZDOT = -13969
261448 ZDOT = -4257
830889
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
52385662
00016717 00000-0 10270-3 0 9101
2 25544 51
6435 182
8179 0009883 9
5297 350
6050 15
71974568 24943
Satellite: ISS
Catalog Number: 25544
Epoch time: 10177
52385662 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 182
8179 deg
Eccentricity:
0009883
Arg of perigee: 9
5297 deg
Mean anomaly: 350
6050 deg
Mean motion: 15
71974568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2494
Checksum: 338
Coasting Arc #12 (Orbit 2509)
---------------------------------------
Vector Time (GMT): 2010/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4008277
03 A = 6730376
97 meter
Y = -3494465
66 meter E =
0017407
Z = 4123443
47 I = 51
65474
XDOT = 6181
110144 Wp = 44
93212
YDOT = 2628
033928 meter/sec RA = 176
75254 deg
ZDOT = -3759
583460 TA = 83
68607
MA = 83
48783
Ha = 195
737 n
mi
Hp = 185
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13150515
20 X = 4027024
17
Y = -11464782
34 feet Y = -3449538
69 meter
Z = 13528357
83 Z = 4142960
32
XDOT = 20279
232755 XDOT = 6169
526763
YDOT = 8622
158557 feet/sec YDOT = 2697
090741 meter/sec
ZDOT = -12334
591405 ZDOT = -3729
583594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12499903
43 X = -3809970
57
Y = -12083747
71 feet Y = -3683126
30 meter
Z = 13606219
36 Z = 4147175
66
XDOT = 6038
518917 XDOT = 1840
540566
YDOT = -20080
094327 feet/sec YDOT = -6120
412751 meter/sec
ZDOT = -12214
816252 ZDOT = -3723
075994
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
54099038
00016717 00000-0 10270-3 0 9114
2 25544 51
6430 177
6099 0009993 12
8070 347
3344 15
72013835 25109
Satellite: ISS
Catalog Number: 25544
Epoch time: 10178
54099038 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 177
6099 deg
Eccentricity:
0009993
Arg of perigee: 12
8070 deg
Mean anomaly: 347
3344 deg
Mean motion: 15
72013835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2510
Checksum: 307
Coasting Arc #13 (Orbit 2525)
---------------------------------------
Vector Time (GMT): 2010/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5991430
53 A = 6734582
09 meter
Y = -1317626
94 meter E =
0020184
Z = 2748026
88 I = 51
69890
XDOT = 3388
416437 Wp = 53
46824
YDOT = -4614
522392 meter/sec RA = 171
68382 deg
ZDOT = 5160
799928 TA = 337
92682
MA = 338
01361
Ha = 195
894 n
mi
Hp = 184
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19656924
31 X = -5989600
52
Y = -4322923
03 feet Y = -1384616
94 meter
Z = 9015836
23 Z = 2718925
12
XDOT = 11116
851828 XDOT = 3414
695144
YDOT = -15139
509160 feet/sec YDOT = -4576
485073 meter/sec
ZDOT = 16931
758293 ZDOT = 5177
323652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2343469
99 X = -714289
65
Y = 20041759
08 feet Y = 6108728
17 meter
Z = 8899645
00 Z = 2712611
80
XDOT = -14696
887374 XDOT = -4479
611272
YDOT = -9287
464939 feet/sec YDOT = -2830
819313 meter/sec
ZDOT = 16997
666531 ZDOT = 5180
888759
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
55811509
00016717 00000-0 10270-3 0 9122
2 25544 51
6430 172
4029 0009899 16
4332 343
7149 15
72035098 25266
Satellite: ISS
Catalog Number: 25544
Epoch time: 10179
55811509 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 172
4029 deg
Eccentricity:
0009899
Arg of perigee: 16
4332 deg
Mean anomaly: 343
7149 deg
Mean motion: 15
72035098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2526
Checksum: 312
Coasting Arc #14 (Orbit 2540)
---------------------------------------
Vector Time (GMT): 2010/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1818385
81 A = 6727799
49 meter
Y = 4344830
25 meter E =
0015920
Z = -4814559
57 I = 51
70568
XDOT = -7266
008003 Wp = 68
78533
YDOT = -286
917242 meter/sec RA = 166
52566 deg
ZDOT = 2497
583948 TA = 225
59922
MA = 225
72966
Ha = 196
017 n
mi
Hp = 184
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5965832
72 X = -1843447
43
Y = 14254692
42 feet Y = 4324356
60 meter
Z = -15795799
10 Z = -4823453
35
XDOT = -23838
608934 XDOT = -7274
392251
YDOT = -941
329533 feet/sec YDOT = -368
217345 meter/sec
ZDOT = 8194
173059 ZDOT = 2462
265777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14840953
39 X = 4523522
59
Y = 4172791
02 feet Y = 1271866
70 meter
Z = -15831253
98 Z = -4825366
21
XDOT = 2150
778136 XDOT = 655
557176
YDOT = 22751
515269 feet/sec YDOT = 6934
661854 meter/sec
ZDOT = 8053
161036 ZDOT = 2454
603484
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
51166247
00016717 00000-0 10270-3 0 9133
2 25544 51
6430 167
5205 0010081 20
0774 340
0783 15
71996560 25413
Satellite: ISS
Catalog Number: 25544
Epoch time: 10180
51166247 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 167
5205 deg
Eccentricity:
0010081
Arg of perigee: 20
0774 deg
Mean anomaly: 340
0783 deg
Mean motion: 15
71996560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2541
Checksum: 280
Coasting Arc #15 (Orbit 2556)
---------------------------------------
Vector Time (GMT): 2010/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6490462
23 A = 6736664
09 meter
Y = -837066
97 meter E =
0009489
Z = -1614054
43 I = 51
76521
XDOT = -774
248804 Wp = 72
78779
YDOT = 5040
979468 meter/sec RA = 161
44574 deg
ZDOT = -5752
710171 TA = 124
96200
MA = 124
87285
Ha = 196
090 n
mi
Hp = 184
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21294167
41 X = 6507180
75
Y = -2746282
72 feet Y = -764393
05 meter
Z = -5295454
18 Z = -1582483
70
XDOT = -2540
186364 XDOT = -802
615165
YDOT = 16538
646549 feet/sec YDOT = 5032
163543 meter/sec
ZDOT = -18873
721034 ZDOT = -5756
539628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5568740
95 X = -1697352
24
Y = -20767567
17 feet Y = -6329954
47 meter
Z = -5169404
93 Z = -1575634
62
XDOT = 15199
813247 XDOT = 4632
903078
YDOT = 605
117869 feet/sec YDOT = 184
439926 meter/sec
ZDOT = -18888
947860 ZDOT = -5757
351308
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
52876935
00016717 00000-0 10270-3 0 9148
2 25544 51
6433 162
3122 0010184 24
0000 336
1634 15
72043915 25573
Satellite: ISS
Catalog Number: 25544
Epoch time: 10181
52876935 = yrday
fracday
Element set: 914
Inclination: 51
6433 deg
RA of node: 162
3122 deg
Eccentricity:
0010184
Arg of perigee: 24
0000 deg
Mean anomaly: 336
1634 deg
Mean motion: 15
72043915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2557
Checksum: 275
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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