Date:
June 27th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4305 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 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 1198)
---------------------------------------
Vector Time (GMT): 2007/175/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4758912
20 A = 6712522
71 meter
Y = -2275777
43 meter E =
0013690
Z = 4149951
58 I = 51
91603
XDOT = -62
200323 Wp = 42
54665
YDOT = -6734
134167 meter/sec RA = 63
61904 deg
ZDOT = -3747
222355 TA = 85
68263
MA = 85
52621
Ha = 184
824 n
mi
Hp = 176
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15613228
99 X = -4753270
24
Y = -7466461
38 feet Y = -2328963
35 meter
Z = 13615326
72 Z = 4126846
02
XDOT = -204
069302 XDOT = 31
309792
YDOT = -22093
616035 feet/sec YDOT = -6734
306305 meter/sec
ZDOT = -12294
036597 ZDOT = -3747
298431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16769002
71 X = 5111192
03
Y = -4549658
75 feet Y = -1386735
99 meter
Z = 13527721
18 Z = 4123249
42
XDOT = 14157
480324 XDOT = 4315
200003
YDOT = 15456
695476 feet/sec YDOT = 4711
200781 meter/sec
ZDOT = -12295
060433 ZDOT = -3747
534420
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 07175
89841288
00020000 00000-0 20000-3 0 9007
2 25544 51
6335 64
0573 0007460 353
9129 6
1945 15
78306467 11991
Satellite: ISS
Catalog Number: 25544
Epoch time: 07175
89841288 = yrday
fracday
Element set: 900
Inclination: 51
6335 deg
RA of node: 64
0573 deg
Eccentricity:
0007460
Arg of perigee: 353
9129 deg
Mean anomaly: 6
1945 deg
Mean motion: 15
78306467 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1199
Checksum: 310
Coasting Arc #2 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2007/176/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -792326
57 A = 6711761
75 meter
Y = 5111676
60 meter E =
0010021
Z = 4266337
79 I = 51
90136
XDOT = -5645
480493 Wp = 63
11441
YDOT = -3857
440755 meter/sec RA = 58
51948 deg
ZDOT = 3571
372579 TA = 350
83914
MA = 350
85740
Ha = 184
804 n
mi
Hp = 176
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2599496
63 X = -870152
43
Y = 16770592
51 feet Y = 5102380
47 meter
Z = 13997171
24 Z = 4262300
49
XDOT = -18521
917627 XDOT = -5619
275630
YDOT = -12655
645523 feet/sec YDOT = -3920
425788 meter/sec
ZDOT = 11717
101637 ZDOT = 3544
009637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9135758
25 X = -2784579
12
Y = -14316414
87 feet Y = -4363643
25 meter
Z = 13982458
47 Z = 4261853
34
XDOT = 21257
176866 XDOT = 6479
187509
YDOT = -2216
350759 feet/sec YDOT = -675
543711 meter/sec
ZDOT = 11613
229454 ZDOT = 3539
712338
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 07176
91144561
00020000 00000-0 20000-3 0 9012
2 25544 51
6345 58
8205 0007538 356
7427 3
3688 15
78388488 12158
Satellite: ISS
Catalog Number: 25544
Epoch time: 07176
91144561 = yrday
fracday
Element set: 901
Inclination: 51
6345 deg
RA of node: 58
8205 deg
Eccentricity:
0007538
Arg of perigee: 356
7427 deg
Mean anomaly: 3
3688 deg
Mean motion: 15
78388488 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1215
Checksum: 312
Coasting Arc #3 (Orbit 1229)
---------------------------------------
Vector Time (GMT): 2007/177/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4908961
12 A = 6718404
68 meter
Y = 4195534
81 meter E =
0014360
Z = -1826299
40 I = 51
90738
XDOT = -1992
887529 Wp = 18
47621
YDOT = 4800
300413 meter/sec RA = 53
32814 deg
ZDOT = 5696
348887 TA = 321
29386
MA = 321
39668
Ha = 185
050 n
mi
Hp = 176
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16105515
48 X = 4870553
07
Y = 13764877
98 feet Y = 4250215
17 meter
Z = -5991795
92 Z = -1802544
00
XDOT = -6538
344910 XDOT = -2074
089071
YDOT = 15749
017102 feet/sec YDOT = 4777
559704 meter/sec
ZDOT = 18688
808684 ZDOT = 5686
471067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21196836
34 X = -6460795
72
Y = 791956
76 feet Y = 241388
42 meter
Z = -5901529
18 Z = -1798786
10
XDOT = -5712
797081 XDOT = -1741
260550
YDOT = -14543
360439 feet/sec YDOT = -4432
816262 meter/sec
ZDOT = 18651
971838 ZDOT = 5685
121016
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 07177
86115374
00020000 00000-0 20000-3 0 9028
2 25544 51
6348 53
9119 0007775
3322 359
7847 15
78350967 12303
Satellite: ISS
Catalog Number: 25544
Epoch time: 07177
86115374 = yrday
fracday
Element set: 902
Inclination: 51
6348 deg
RA of node: 53
9119 deg
Eccentricity:
0007775
Arg of perigee:
3322 deg
Mean anomaly: 359
7847 deg
Mean motion: 15
78350967 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1230
Checksum: 303
Coasting Arc #4 (Orbit 1245)
---------------------------------------
Vector Time (GMT): 2007/178/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2759185
03 A = 6707655
15 meter
Y = -3123411
15 meter E =
0017685
Z = -5269552
22 I = 51
85339
XDOT = 5372
199260 Wp = 60
86717
YDOT = 5493
977079 meter/sec RA = 48
19732 deg
ZDOT = -436
168205 TA = 204
95759
MA = 205
04320
Ha = 185
004 n
mi
Hp = 176
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9052444
34 X = 2819505
03
Y = -10247411
92 feet Y = -3092218
02 meter
Z = -17288557
14 Z = -5256002
18
XDOT = 17625
325655 XDOT = 5312
484363
YDOT = 18024
859182 feet/sec YDOT = 5553
718235 meter/sec
ZDOT = -1430
998048 ZDOT = -410
213839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 438030
81 X = 133511
79
Y = 13730329
46 feet Y = 4185004
42 meter
Z = -17237650
34 Z = -5254035
82
XDOT = -24198
218555 XDOT = -7375
617016
YDOT = -930
917533 feet/sec YDOT = -283
743664 meter/sec
ZDOT = -1332
280410 ZDOT = -406
079069
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 07178
87416032
00020000 00000-0 20000-3 0 9036
2 25544 51
6349 48
6757 0007718 3
8561 356
2663 15
78397728 12464
Satellite: ISS
Catalog Number: 25544
Epoch time: 07178
87416032 = yrday
fracday
Element set: 903
Inclination: 51
6349 deg
RA of node: 48
6757 deg
Eccentricity:
0007718
Arg of perigee: 3
8561 deg
Mean anomaly: 356
2663 deg
Mean motion: 15
78397728 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1246
Checksum: 322
Coasting Arc #5 (Orbit 1261)
---------------------------------------
Vector Time (GMT): 2007/179/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4208168
37 A = 6719061
54 meter
Y = -5120971
27 meter E =
0006865
Z = -1107667
35 I = 51
87148
XDOT = 4349
757251 Wp = 88
84552
YDOT = -2299
773952 meter/sec RA = 43
05114 deg
ZDOT = -5924
178958 TA = 103
24977
MA = 103
17319
Ha = 185
055 n
mi
Hp = 176
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13806326
67 X = -4145211
31
Y = -16801086
84 feet Y = -5167677
11 meter
Z = -3634079
22 Z = -1127958
86
XDOT = 14270
857123 XDOT = 4403
928966
YDOT = -7545
190132 feet/sec YDOT = -2250
828305 meter/sec
ZDOT = -19436
282672 ZDOT = -5902
916763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21611636
80 X = 6587226
90
Y = 2293639
35 feet Y = 699101
27 meter
Z = -3711344
78 Z = -1131217
89
XDOT = -4780
981474 XDOT = -1457
243153
YDOT = 13890
531339 feet/sec YDOT = 4233
833952 meter/sec
ZDOT = -19356
120346 ZDOT = -5899
745481
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 07179
88715276
00020000 00000-0 20000-3 0 9041
2 25544 51
6344 43
4389 0007682 8
1365 351
9924 15
78420879 12627
Satellite: ISS
Catalog Number: 25544
Epoch time: 07179
88715276 = yrday
fracday
Element set: 904
Inclination: 51
6344 deg
RA of node: 43
4389 deg
Eccentricity:
0007682
Arg of perigee: 8
1365 deg
Mean anomaly: 351
9924 deg
Mean motion: 15
78420879 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1262
Checksum: 320
Coasting Arc #6 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2007/180/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4754132
91 A = 6710180
99 meter
Y = 927009
46 meter E =
0014434
Z = 4641469
76 I = 51
82011
XDOT = -3976
348362 Wp = 38
07392
YDOT = -5948
932602 meter/sec RA = 37
86322 deg
ZDOT = -2868
879545 TA = 80
26364
MA = 80
10065
Ha = 185
226 n
mi
Hp = 175
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15597548
92 X = -4786692
84
Y = 3041369
63 feet Y = 873662
96 meter
Z = 15227919
17 Z = 4618295
41
XDOT = -13045
762343 XDOT = -3895
594565
YDOT = -19517
495413 feet/sec YDOT = -5992
946183 meter/sec
ZDOT = -9412
334465 ZDOT = -2888
001779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8809413
54 X = 2685109
25
Y = -13326148
01 feet Y = -4061809
91 meter
Z = 15140376
36 Z = 4614786
71
XDOT = 22060
336040 XDOT = 6723
990425
YDOT = 3747
249197 feet/sec YDOT = 1142
161555 meter/sec
ZDOT = -9485
265887 ZDOT = -2891
109042
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 07180
90012997
00020000 00000-0 20000-3 0 9057
2 25544 51
6348 38
2016 0007864 11
7395 348
3952 15
78466537 12784
Satellite: ISS
Catalog Number: 25544
Epoch time: 07180
90012997 = yrday
fracday
Element set: 905
Inclination: 51
6348 deg
RA of node: 38
2016 deg
Eccentricity:
0007864
Arg of perigee: 11
7395 deg
Mean anomaly: 348
3952 deg
Mean motion: 15
78466537 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1278
Checksum: 313
Coasting Arc #7 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2007/181/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2456753
00 A = 6713441
18 meter
Y = 5030466
53 meter E =
0015100
Z = 3688068
79 I = 51
80757
XDOT = -6387
395054 Wp = 65
18661
YDOT = -59
746443 meter/sec RA = 32
75410 deg
ZDOT = 4328
865304 TA = 339
23793
MA = 339
29920
Ha = 185
150 n
mi
Hp = 175
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8060213
25 X = 2382403
20
Y = 16504155
29 feet Y = 5057522
78 meter
Z = 12099963
21 Z = 3699824
12
XDOT = -20956
020519 XDOT = -6407
280874
YDOT = -196
018515 feet/sec YDOT = -131
286044 meter/sec
ZDOT = 14202
313991 ZDOT = 4297
787316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17477429
95 X = -5327120
65
Y = -5550055
81 feet Y = -1691657
01 meter
Z = 12144941
83 Z = 3701778
27
XDOT = 14205
757056 XDOT = 4329
914751
YDOT = -13859
996880 feet/sec YDOT = -4224
527049 meter/sec
ZDOT = 14084
771464 ZDOT = 4293
038342
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 07181
91309277
00020000 00000-0 20000-3 0 9060
2 25544 51
6345 32
9644 0007786 15
3477 344
7923 15
78486039 12948
Satellite: ISS
Catalog Number: 25544
Epoch time: 07181
91309277 = yrday
fracday
Element set: 906
Inclination: 51
6345 deg
RA of node: 32
9644 deg
Eccentricity:
0007786
Arg of perigee: 15
3477 deg
Mean anomaly: 344
7923 deg
Mean motion: 15
78486039 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1294
Checksum: 320
Coasting Arc #8 (Orbit 1308)
---------------------------------------
Vector Time (GMT): 2007/182/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6129001
77 A = 6716641
43 meter
Y = 903255
42 meter E =
0012599
Z = -2583724
32 I = 51
79250
XDOT = 1417
924124 Wp = 30
56364
YDOT = 5430
553195 meter/sec RA = 27
54775 deg
ZDOT = 5283
844212 TA = 300
10510
MA = 300
22994
Ha = 185
383 n
mi
Hp = 175
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20108273
51 X = 6130997
00
Y = 2963436
40 feet Y = 971805
06 meter
Z = -8476785
82 Z = -2553945
00
XDOT = 4651
982034 XDOT = 1331
425903
YDOT = 17816
775573 feet/sec YDOT = 5445
924465 meter/sec
ZDOT = 17335
446889 ZDOT = 5290
523439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15795218
22 X = -4814382
51
Y = 12866005
11 feet Y = 3921558
36 meter
Z = -8364060
64 Z = -2549365
68
XDOT = -15279
245200 XDOT = -4657
113937
YDOT = -7518
646586 feet/sec YDOT = -2291
683479 meter/sec
ZDOT = 17361
271629 ZDOT = 5291
715592
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 07182
86273339
00020000 00000-0 20000-3 0 9075
2 25544 51
6340 28
0551 0007939 17
9909 342
1536 15
78468281 13092
Satellite: ISS
Catalog Number: 25544
Epoch time: 07182
86273339 = yrday
fracday
Element set: 907
Inclination: 51
6340 deg
RA of node: 28
0551 deg
Eccentricity:
0007939
Arg of perigee: 17
9909 deg
Mean anomaly: 342
1536 deg
Mean motion: 15
78468281 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1309
Checksum: 309
Coasting Arc #9 (Orbit 1324)
---------------------------------------
Vector Time (GMT): 2007/183/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 170043
02 A = 6707907
96 meter
Y = -4319864
56 meter E =
0019580
Z = -5145281
84 I = 51
73639
XDOT = 7338
444259 Wp = 59
54179
YDOT = 1887
556214 meter/sec RA = 22
41985 deg
ZDOT = -1336
251085 TA = 197
64539
MA = 197
71349
Ha = 185
361 n
mi
Hp = 175
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 557883
91 X = 243330
16
Y = -14172783
99 feet Y = -4317552
30 meter
Z = -16880845
93 Z = -5144278
59
XDOT = 24076
260691 XDOT = 7323
283079
YDOT = 6192
769730 feet/sec YDOT = 1969
534299 meter/sec
ZDOT = -4384
025870 ZDOT = -1300
637979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10184951
99 X = 3104373
37
Y = 9877181
49 feet Y = 3010564
92 meter
Z = -16877500
96 Z = -5144262
29
XDOT = -19883
771212 XDOT = -6060
573465
YDOT = 13209
197991 feet/sec YDOT = 4026
163548 meter/sec
ZDOT = -4249
127014 ZDOT = -1295
133914
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 07183
87566896
00020000 00000-0 20000-3 0 9081
2 25544 51
6333 22
8174 0007931 21
9481 338
2023 15
78487213 13250
Satellite: ISS
Catalog Number: 25544
Epoch time: 07183
87566896 = yrday
fracday
Element set: 908
Inclination: 51
6333 deg
RA of node: 22
8174 deg
Eccentricity:
0007931
Arg of perigee: 21
9481 deg
Mean anomaly: 338
2023 deg
Mean motion: 15
78487213 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1325
Checksum: 303
Coasting Arc #10 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2007/184/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6318163
60 A = 6719213
76 meter
Y = -2257579
76 meter E =
0011322
Z = -358358
75 I = 51
74806
XDOT = 1902
202796 Wp = 95
82237
YDOT = -4391
531188 meter/sec RA = 17
24922 deg
ZDOT = -6035
168754 TA = 88
07203
MA = 87
94237
Ha = 185
438 n
mi
Hp = 175
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20728883
20 X = -6290708
62
Y = -7406757
73 feet Y = -2328079
44 meter
Z = -1175717
67 Z = -388985
55
XDOT = 6240
822820 XDOT = 1980
485421
YDOT = -14407
910722 feet/sec YDOT = -4369
821012 meter/sec
ZDOT = -19800
422421 ZDOT = -6025
738573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19089970
31 X = 5818622
95
Y = -10946837
84 feet Y = -3336596
17 meter
Z = -1291799
42 Z = -393740
46
XDOT = 6032
539743 XDOT = 1838
718114
YDOT = 12794
870460 feet/sec YDOT = 3899
876516 meter/sec
ZDOT = -19765
213078 ZDOT = -6024
436946
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 07184
88858991
00020000 00000-0 20000-3 0 9094
2 25544 51
6335 17
5795 0008133 26
4596 333
6983 15
78541016 13418
Satellite: ISS
Catalog Number: 25544
Epoch time: 07184
88858991 = yrday
fracday
Element set: 909
Inclination: 51
6335 deg
RA of node: 17
5795 deg
Eccentricity:
0008133
Arg of perigee: 26
4596 deg
Mean anomaly: 333
6983 deg
Mean motion: 15
78541016 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1341
Checksum: 324
Coasting Arc #11 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2007/185/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3110062
31 A = 6708584
32 meter
Y = 3317287
55 meter E =
0013966
Z = 4927986
92 I = 51
68488
XDOT = -6718
858739 Wp = 40
51136
YDOT = -3141
992410 meter/sec RA = 12
06304 deg
ZDOT = -2111
481459 TA = 69
98723
MA = 69
83691
Ha = 185
477 n
mi
Hp = 174
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10203616
52 X = -3170864
47
Y = 10883489
32 feet Y = 3282168
45 meter
Z = 16167936
10 Z = 4912731
23
XDOT = -22043
499801 XDOT = -6672
968120
YDOT = -10308
374048 feet/sec YDOT = -3216
869589 meter/sec
ZDOT = -6927
432607 ZDOT = -2144
010151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1846424
27 X = -562790
12
Y = -14866276
47 feet Y = -4531241
07 meter
Z = 16110581
28 Z = 4910505
17
XDOT = 20869
206211 XDOT = 6360
934053
YDOT = -10282
063883 feet/sec YDOT = -3133
973072 meter/sec
ZDOT = -7050
803540 ZDOT = -2149
084919
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 07185
90149462
00020000 00000-0 20000-3 0 9106
2 25544 51
6339 12
3416 0008086 28
7206 331
4403 15
78590359 13579
Satellite: ISS
Catalog Number: 25544
Epoch time: 07185
90149462 = yrday
fracday
Element set: 910
Inclination: 51
6339 deg
RA of node: 12
3416 deg
Eccentricity:
0008086
Arg of perigee: 28
7206 deg
Mean anomaly: 331
4403 deg
Mean motion: 15
78590359 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1357
Checksum: 287
Coasting Arc #12 (Orbit 1372)
---------------------------------------
Vector Time (GMT): 2007/186/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5015146
33 A = 6714736
80 meter
Y = 3128208
26 meter E =
0019101
Z = 3162278
99 I = 51
67686
XDOT = -5073
826236 Wp = 66
16911
YDOT = 3231
919399 meter/sec RA = 6
93804 deg
ZDOT = 4834
400861 TA = 330
79372
MA = 330
90039
Ha = 185
515 n
mi
Hp = 174
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16453892
16 X = 4964431
90
Y = 10263150
45 feet Y = 3184006
51 meter
Z = 10374931
08 Z = 3186519
50
XDOT = -16646
411537 XDOT = -5133
073329
YDOT = 10603
410102 feet/sec YDOT = 3174
849189 meter/sec
ZDOT = 15860
895212 ZDOT = 4809
608944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18241678
44 X = -5560063
59
Y = 6433205
03 feet Y = 1960840
89 meter
Z = 10466950
85 Z = 3190326
62
XDOT = 2598
478700 XDOT = 792
016308
YDOT = -18366
400674 feet/sec YDOT = -5598
078925 meter/sec
ZDOT = 15767
463141 ZDOT = 4805
922765
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 07186
91438790
00020000 00000-0 20000-3 0 9114
2 25544 51
6336 7
1038 0008268 33
9891 326
1802 15
78575491 13730
Satellite: ISS
Catalog Number: 25544
Epoch time: 07186
91438790 = yrday
fracday
Element set: 911
Inclination: 51
6336 deg
RA of node: 7
1038 deg
Eccentricity:
0008268
Arg of perigee: 33
9891 deg
Mean anomaly: 326
1802 deg
Mean motion: 15
78575491 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1373
Checksum: 306
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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