Date:
September 7th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5651 05 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2345)
---------------------------------------
Vector Time (GMT): 2007/248/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5194499
17 A = 6717507
77 meter
Y = 956910
01 meter E =
0005766
Z = -4149619
82 I = 51
87131
XDOT = 1799
165716 Wp = 30
47351
YDOT = 6482
028042 meter/sec RA = 48
50954 deg
ZDOT = 3754
089474 TA = 277
77299
MA = 277
83845
Ha = 187
104 n
mi
Hp = 180
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17042320
10 X = 5203570
77
Y = 3139468
54 feet Y = 1015048
72 meter
Z = -13614238
26 Z = -4124363
03
XDOT = 5902
774659 XDOT = 1708
312422
YDOT = 21266
496201 feet/sec YDOT = 6501
639186 meter/sec
ZDOT = 12316
566515 ZDOT = 3762
609354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17365137
33 X = -5292893
86
Y = -1163305
60 feet Y = -354575
55 meter
Z = -13518252
32 Z = -4120363
31
XDOT = -8309
675208 XDOT = -2532
789003
YDOT = -19194
460336 feet/sec YDOT = -5850
471510 meter/sec
ZDOT = 12349
664032 ZDOT = 3764
177597
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 07248
57300578
00020000 00000-0 20000-3 0 9005
2 25544 51
6353 49
0584 0008755 329
9888 30
0774 15
76553076 23468
Satellite: ISS
Catalog Number: 25544
Epoch time: 07248
57300578 = yrday
fracday
Element set: 900
Inclination: 51
6353 deg
RA of node: 49
0584 deg
Eccentricity:
0008755
Arg of perigee: 329
9888 deg
Mean anomaly: 30
0774 deg
Mean motion: 15
76553076 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2346
Checksum: 315
Coasting Arc #2 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2007/249/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1166858
80 A = 6718119
52 meter
Y = -5339396
03 meter E =
0010235
Z = -3916564
11 I = 51
85387
XDOT = 6336
325568 Wp = 14
30087
YDOT = 1601
797607 meter/sec RA = 43
42108 deg
ZDOT = -4064
016658 TA = 213
48734
MA = 213
55209
Ha = 187
109 n
mi
Hp = 180
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3828276
89 X = -1088040
40
Y = -17517703
50 feet Y = -5352003
69 meter
Z = -12849619
79 Z = -3922041
35
XDOT = 20788
469712 XDOT = 6337
685143
YDOT = 5255
241494 feet/sec YDOT = 1672
661693 meter/sec
ZDOT = -13333
387984 ZDOT = -4033
231776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6023828
99 X = 1836063
08
Y = 16872709
44 feet Y = 5142801
84 meter
Z = -12871034
49 Z = -3923091
31
XDOT = -20142
128220 XDOT = -6139
320681
YDOT = -2909
431960 feet/sec YDOT = -886
794861 meter/sec
ZDOT = -13216
336395 ZDOT = -4028
339333
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 07249
58717619
00020000 00000-0 20000-3 0 9016
2 25544 51
6354 43
8294 0008816 333
8264 26
2453 15
76588956 23623
Satellite: ISS
Catalog Number: 25544
Epoch time: 07249
58717619 = yrday
fracday
Element set: 901
Inclination: 51
6354 deg
RA of node: 43
8294 deg
Eccentricity:
0008816
Arg of perigee: 333
8264 deg
Mean anomaly: 26
2453 deg
Mean motion: 15
76588956 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2362
Checksum: 321
Coasting Arc #3 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2007/250/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5833992
16 A = 6721334
95 meter
Y = -1759516
08 meter E =
0011609
Z = 2835768
86 I = 51
84302
XDOT = -769
187048 Wp = 59
33872
YDOT = -5713
382766 meter/sec RA = 38
23053 deg
ZDOT = -5106
256847 TA = 88
21038
MA = 88
07742
Ha = 187
246 n
mi
Hp = 180
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19140394
22 X = -5827658
85
Y = -5772690
55 feet Y = -1824719
68 meter
Z = 9303703
61 Z = 2807443
09
XDOT = -2523
579555 XDOT = -680
437055
YDOT = -18744
694113 feet/sec YDOT = -5721
487990 meter/sec
ZDOT = -16752
811179 ZDOT = -5109
777972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19836390
50 X = 6046131
82
Y = 2861711
88 feet Y = 872249
78 meter
Z = 9195964
60 Z = 2802930
01
XDOT = 5391
932513 XDOT = 1643
461030
YDOT = 16730
291548 feet/sec YDOT = 5099
392864 meter/sec
ZDOT = -16766
845379 ZDOT = -5110
534472
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 07250
60132756
00020000 00000-0 20000-3 0 9025
2 25544 51
6357 38
6002 0008807 337
8983 22
1801 15
76611725 23787
Satellite: ISS
Catalog Number: 25544
Epoch time: 07250
60132756 = yrday
fracday
Element set: 902
Inclination: 51
6357 deg
RA of node: 38
6002 deg
Eccentricity:
0008807
Arg of perigee: 337
8983 deg
Mean anomaly: 22
1801 deg
Mean motion: 15
76611725 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2378
Checksum: 284
Coasting Arc #4 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2007/251/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 85692
88 A = 6714204
41 meter
Y = 4625198
05 meter E =
0005664
Z = 4862146
29 I = 51
79743
XDOT = -6960
565207 Wp = 29
26830
YDOT = -2335
764076 meter/sec RA = 33
12940 deg
ZDOT = 2348
314805 TA = 37
94203
MA = 37
90214
Ha = 187
311 n
mi
Hp = 179
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 281144
60 X = 10347
77
Y = 15174534
29 feet Y = 4625735
14 meter
Z = 15951923
53 Z = 4862379
48
XDOT = -22836
500022 XDOT = -6945
336546
YDOT = -7663
267965 feet/sec YDOT = -2413
515854 meter/sec
ZDOT = 7704
444899 ZDOT = 2314
537908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2697766
09 X = -822279
10
Y = -14933922
93 feet Y = -4551859
71 meter
Z = 15953350
79 Z = 4862581
32
XDOT = 22742
582192 XDOT = 6931
939052
YDOT = 3971
739234 feet/sec YDOT = 1210
586119 meter/sec
ZDOT = 7575
941306 ZDOT = 2309
146910
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 07251
61545728
00020000 00000-0 20000-3 0 9035
2 25544 51
6368 33
3709 0008950 341
4413 18
6423 15
76688343 23941
Satellite: ISS
Catalog Number: 25544
Epoch time: 07251
61545728 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 33
3709 deg
Eccentricity:
0008950
Arg of perigee: 341
4413 deg
Mean anomaly: 18
6423 deg
Mean motion: 15
76688343 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2394
Checksum: 298
Coasting Arc #5 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2007/252/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6217209
82 A = 6724006
15 meter
Y = 2234044
06 meter E =
0016663
Z = -1196243
20 I = 51
80567
XDOT = -637
759787 Wp = 11
79322
YDOT = 4919
651840 meter/sec RA = 27
95531 deg
ZDOT = 5903
392529 TA = 335
10331
MA = 335
18360
Ha = 187
582 n
mi
Hp = 179
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20397670
02 X = 6197577
39
Y = 7329540
87 feet Y = 2303458
59 meter
Z = -3924682
42 Z = -1166088
17
XDOT = -2092
387752 XDOT = -721
401913
YDOT = 16140
590025 feet/sec YDOT = 4912
052639 meter/sec
ZDOT = 19368
085724 ZDOT = 5900
090954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21413336
22 X = -6526784
88
Y = -3484771
21 feet Y = -1062158
27 meter
Z = -3809940
29 Z = -1161269
80
XDOT = -1031
838132 XDOT = -314
504262
YDOT = -14709
803292 feet/sec YDOT = -4483
548043 meter/sec
ZDOT = 19356
130680 ZDOT = 5899
748631
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 07252
56618834
00020000 00000-0 20000-3 0 9040
2 25544 51
6372 28
4691 0009128 345
9423 14
1486 15
76668363 24096
Satellite: ISS
Catalog Number: 25544
Epoch time: 07252
56618834 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 28
4691 deg
Eccentricity:
0009128
Arg of perigee: 345
9423 deg
Mean anomaly: 14
1486 deg
Mean motion: 15
76668363 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2409
Checksum: 308
Coasting Arc #6 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2007/253/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1269557
40 A = 6712384
10 meter
Y = -3974516
30 meter E =
0016462
Z = -5269917
20 I = 51
74119
XDOT = 7182
899805 Wp = 53
87411
YDOT = 2741
738504 meter/sec RA = 22
82339 deg
ZDOT = -328
580857 TA = 212
95737
MA = 213
06010
Ha = 187
588 n
mi
Hp = 179
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4165214
55 X = 1339506
74
Y = -13039751
63 feet Y = -3959928
61 meter
Z = -17289754
60 Z = -5263579
60
XDOT = 23565
944243 XDOT = 7153
303601
YDOT = 8995
205067 feet/sec YDOT = 2821
896247 meter/sec
ZDOT = -1078
021185 ZDOT = -293
758721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1579899
85 X = -481553
47
Y = 13627296
86 feet Y = 4153600
08 meter
Z = -17266164
76 Z = -5262727
02
XDOT = -23897
204572 XDOT = -7283
867954
YDOT = -4005
175327 feet/sec YDOT = -1220
777440 meter/sec
ZDOT = -945
503489 ZDOT = -288
189464
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 07253
58028061
00020000 00000-0 20000-3 0 9051
2 25544 51
6376 23
2406 0009171 349
6355 10
4619 15
76722088 24250
Satellite: ISS
Catalog Number: 25544
Epoch time: 07253
58028061 = yrday
fracday
Element set: 905
Inclination: 51
6376 deg
RA of node: 23
2406 deg
Eccentricity:
0009171
Arg of perigee: 349
6355 deg
Mean anomaly: 10
4619 deg
Mean motion: 15
76722088 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2425
Checksum: 283
Coasting Arc #7 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2007/254/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6203534
77 A = 6724154
43 meter
Y = -2514601
92 meter E =
0005917
Z = -649561
15 I = 51
75408
XDOT = 2334
108158 Wp = 81
03885
YDOT = -4220
005785 meter/sec RA = 17
67843 deg
ZDOT = -6000
257468 TA = 106
02539
MA = 105
96022
Ha = 187
671 n
mi
Hp = 179
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20352804
35 X = -6171799
62
Y = -8250006
28 feet Y = -2583795
95 meter
Z = -2131106
12 Z = -679620
50
XDOT = 7657
835163 XDOT = 2410
271446
YDOT = -13845
163337 feet/sec YDOT = -4193
479059 meter/sec
ZDOT = -19685
884080 ZDOT = -5988
733116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21642300
39 X = 6596573
16
Y = 3661880
64 feet Y = 1116141
22 meter
Z = -2245512
33 Z = -684432
16
XDOT = -4327
545505 XDOT = -1319
035870
YDOT = 13617
929230 feet/sec YDOT = 4150
744829 meter/sec
ZDOT = -19642
635469 ZDOT = -5987
075291
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 07254
59435284
00020000 00000-0 20000-3 0 9063
2 25544 51
6376 18
0113 0009155 353
7187 6
3861 15
76749460 24412
Satellite: ISS
Catalog Number: 25544
Epoch time: 07254
59435284 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 18
0113 deg
Eccentricity:
0009155
Arg of perigee: 353
7187 deg
Mean anomaly: 6
3861 deg
Mean motion: 15
76749460 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2441
Checksum: 297
Coasting Arc #8 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2007/255/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2810271
63 A = 6713229
88 meter
Y = 3446324
88 meter E =
0013168
Z = 5029069
68 I = 51
69034
XDOT = -6878
624772 Wp = 17
77987
YDOT = -2975
312604 meter/sec RA = 12
50599 deg
ZDOT = -1791
345004 TA = 89
52906
MA = 89
37818
Ha = 187
839 n
mi
Hp = 178
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9220051
29 X = -2873030
41
Y = 11306840
16 feet Y = 3414548
32 meter
Z = 16499572
43 Z = 5015264
67
XDOT = -22567
666575 XDOT = -6836
141115
YDOT = -9761
524292 feet/sec YDOT = -3051
995874 meter/sec
ZDOT = -5877
116156 ZDOT = -1824
657945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6425173
93 X = 1958393
01
Y = -13163746
57 feet Y = -4012309
96 meter
Z = 16447576
92 Z = 5013221
45
XDOT = 23227
502452 XDOT = 7079
742747
YDOT = 3779
898864 feet/sec YDOT = 1152
113174 meter/sec
ZDOT = -6003
921926 ZDOT = -1829
995403
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 07255
60840363
00020000 00000-0 20000-3 0 9075
2 25544 51
6383 12
7818 0009359 357
6611 2
4508 15
76806601 24577
Satellite: ISS
Catalog Number: 25544
Epoch time: 07255
60840363 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 12
7818 deg
Eccentricity:
0009359
Arg of perigee: 357
6611 deg
Mean anomaly: 2
4508 deg
Mean motion: 15
76806601 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2457
Checksum: 294
Coasting Arc #9 (Orbit 2472)
---------------------------------------
Vector Time (GMT): 2007/256/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5660028
03 A = 6721538
72 meter
Y = 2665427
52 meter E =
0018854
Z = 2424348
64 I = 51
69015
XDOT = -4072
863450 Wp = 46
18493
YDOT = 3751
118982 meter/sec RA = 7
38969 deg
ZDOT = 5371
688281 TA = 341
23348
MA = 341
30290
Ha = 187
820 n
mi
Hp = 178
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18569645
77 X = 5618025
05
Y = 8744840
93 feet Y = 2728486
48 meter
Z = 7953899
74 Z = 2451742
97
XDOT = -13362
412893 XDOT = -4140
601140
YDOT = 12306
820806 feet/sec YDOT = 3705
195575 meter/sec
ZDOT = 17623
649217 ZDOT = 5351
737404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20120427
32 X = -6132706
25
Y = -3847385
98 feet Y = -1172683
25 meter
Z = 8058196
66 Z = 2456138
34
XDOT = 9685
258415 XDOT = 2952
066765
YDOT = -13808
345834 feet/sec YDOT = -4208
783810 meter/sec
ZDOT = 17548
362606 ZDOT = 5348
740922
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 07256
62243463
00020000 00000-0 20000-3 0 9087
2 25544 51
6383 7
5528 0009365 1
8742 358
2456 15
76820032 24733
Satellite: ISS
Catalog Number: 25544
Epoch time: 07256
62243463 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 7
5528 deg
Eccentricity:
0009365
Arg of perigee: 1
8742 deg
Mean anomaly: 358
2456 deg
Mean motion: 15
76820032 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2473
Checksum: 292
Coasting Arc #10 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2007/257/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4235140
50 A = 6716538
17 meter
Y = -3137191
64 meter E =
0010693
Z = -4165953
47 I = 51
64427
XDOT = 5969
145511 Wp = 50
78042
YDOT = 3159
660925 meter/sec RA = 2
18884 deg
ZDOT = 3701
822732 TA = 256
96162
MA = 257
08102
Ha = 187
991 n
mi
Hp = 178
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13894817
91 X = 4290143
91
Y = -10292623
49 feet Y = -3089524
63 meter
Z = -13667826
34 Z = -4145245
17
XDOT = 19583
810732 XDOT = 5915
387124
YDOT = 10366
341619 feet/sec YDOT = 3226
110942 meter/sec
ZDOT = 12145
087703 ZDOT = 3730
690310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10729265
11 X = -3270280
00
Y = 13638891
06 feet Y = 4157134
00 meter
Z = -13589593
84 Z = -4142108
20
XDOT = -20575
378587 XDOT = -6271
375393
YDOT = -4017
785536 feet/sec YDOT = -1224
621031 meter/sec
ZDOT = 12255
029181 ZDOT = 3735
332895
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 07257
57306968
00020000 00000-0 20000-3 0 9093
2 25544 51
6379 2
6513 0009430 5
5329 354
5939 15
76867279 24888
Satellite: ISS
Catalog Number: 25544
Epoch time: 07257
57306968 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 2
6513 deg
Eccentricity:
0009430
Arg of perigee: 5
5329 deg
Mean anomaly: 354
5939 deg
Mean motion: 15
76867279 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2488
Checksum: 333
Coasting Arc #11 (Orbit 2503)
---------------------------------------
Vector Time (GMT): 2007/258/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4618893
37 A = 6717189
16 meter
Y = -2891915
47 meter E =
0014120
Z = -3942995
66 I = 51
61696
XDOT = 5585
606781 Wp = 34
83039
YDOT = -3458
780728 meter/sec RA = 357
08223 deg
ZDOT = -4001
945295 TA = 193
57119
MA = 193
60920
Ha = 188
069 n
mi
Hp = 177
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15153849
64 X = -4567057
67
Y = -9487911
65 feet Y = -2943276
92 meter
Z = -12936337
47 Z = -3965308
44
XDOT = 18325
481564 XDOT = 5643
309196
YDOT = -11347
705802 feet/sec YDOT = -3395
996885 meter/sec
ZDOT = -13129
741783 ZDOT = -3974
669780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17147494
02 X = 5226556
18
Y = 4839006
59 feet Y = 1474929
21 meter
Z = -13021363
90 Z = -3968911
72
XDOT = -14089
102882 XDOT = -4294
358559
YDOT = 14834
376030 feet/sec YDOT = 4521
517814 meter/sec
ZDOT = -13026
621006 ZDOT = -3970
514083
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 07258
58706013
00020000 00000-0 20000-3 0 9102
2 25544 51
6372 357
4215 0009505 9
1245 351
0091 15
76862852 25043
Satellite: ISS
Catalog Number: 25544
Epoch time: 07258
58706013 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 357
4215 deg
Eccentricity:
0009505
Arg of perigee: 9
1245 deg
Mean anomaly: 351
0091 deg
Mean motion: 15
76862852 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2504
Checksum: 277
Coasting Arc #12 (Orbit 2519)
---------------------------------------
Vector Time (GMT): 2007/259/13:32:04
852
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5414663
43 A = 6720764
98 meter
Y = 2929071
45 meter E =
0016964
Z = 2692829
08 I = 51
60081
XDOT = -4491
090119 Wp = 66
38957
YDOT = -3507
897548 meter/sec RA = 351
87351 deg
ZDOT = -5182
562354 TA = 82
85557
MA = 82
66271
Ha = 188
183 n
mi
Hp = 177
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17764643
80 X = -5460095
75
Y = 9609814
46 feet Y = 2868267
68 meter
Z = 8834741
07 Z = 2666413
86
XDOT = -14734
547633 XDOT = -4426
354229
YDOT = -11508
850224 feet/sec YDOT = -3557
757668 meter/sec
ZDOT = -17003
157331 ZDOT = -5204
222981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14124701
50 X = 4305209
02
Y = -14497566
11 feet Y = -4418858
15 meter
Z = 8734823
25 Z = 2662374
13
XDOT = 16353
492380 XDOT = 4984
544477
YDOT = 5573
995808 feet/sec YDOT = 1698
953922 meter/sec
ZDOT = -17085
777108 ZDOT = -5207
744862
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 07259
60102851
00020000 00000-0 20000-3 0 9117
2 25544 51
6375 352
1915 0009760 13
0097 347
1318 15
76930650 25205
Satellite: ISS
Catalog Number: 25544
Epoch time: 07259
60102851 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 352
1915 deg
Eccentricity:
0009760
Arg of perigee: 13
0097 deg
Mean anomaly: 347
1318 deg
Mean motion: 15
76930650 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2520
Checksum: 274
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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