Date:
March 26th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8234 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 1526)
---------------------------------------
Vector Time (GMT): 2008/085/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2039949
97 A = 6722554
51 meter
Y = 5919205
31 meter E =
0004937
Z = -2444509
86 I = 51
97551
XDOT = -4131
567134 Wp = 37
71823
YDOT = 3643
004934 meter/sec RA = 88
76159 deg
ZDOT = 5382
961347 TA = 294
78487
MA = 294
83623
Ha = 185
948 n
mi
Hp = 180
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6692749
25 X = 1985483
94
Y = 19419964
92 feet Y = 5941712
52 meter
Z = -8020045
46 Z = -2434732
36
XDOT = -13555
010281 XDOT = -4198
146326
YDOT = 11952
115926 feet/sec YDOT = 3596
431433 meter/sec
ZDOT = 17660
634341 ZDOT = 5362
728146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20338523
98 X = -6199182
11
Y = -2980439
29 feet Y = -908437
89 meter
Z = -7981884
69 Z = -2432878
45
XDOT = -4522
340498 XDOT = -1378
409384
YDOT = -16145
809539 feet/sec YDOT = -4921
242748 meter/sec
ZDOT = 17583
446058 ZDOT = 5359
434358
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 08085
17230508
00020000 00000-0 20000-3 0 9006
2 25544 51
6386 89
4983 0001037 281
6790 78
4258 15
76475578 15270
Satellite: ISS
Catalog Number: 25544
Epoch time: 08085
17230508 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 89
4983 deg
Eccentricity:
0001037
Arg of perigee: 281
6790 deg
Mean anomaly: 78
4258 deg
Mean motion: 15
76475578 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1527
Checksum: 318
Coasting Arc #2 (Orbit 1542)
---------------------------------------
Vector Time (GMT): 2008/086/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3680944
06 A = 6714119
18 meter
Y = -2520440
26 meter E =
0012272
Z = -5028726
05 I = 51
94596
XDOT = 2278
743029 Wp = 73
53532
YDOT = 7102
712173 meter/sec RA = 83
66667 deg
ZDOT = -1892
319177 TA = 178
27027
MA = 178
26602
Ha = 185
862 n
mi
Hp = 180
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12076588
13 X = 3733283
23
Y = -8269160
97 feet Y = -2478985
38 meter
Z = -16498445
06 Z = -5010716
69
XDOT = 7476
191040 XDOT = 2208
342637
YDOT = 23302
861459 feet/sec YDOT = 7127
800681 meter/sec
ZDOT = -6208
396249 ZDOT = -1881
420241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1973510
98 X = 601526
15
Y = 14580584
63 feet Y = 4444162
20 meter
Z = -16429653
05 Z = -5007758
25
XDOT = -23143
703437 XDOT = -7054
200808
YDOT = -3813
781175 feet/sec YDOT = -1162
440502 meter/sec
ZDOT = -6165
812730 ZDOT = -1879
339720
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 08086
18652290
00020000 00000-0 20000-3 0 9015
2 25544 51
6391 84
2706 0001085 283
5422 76
5621 15
76512736 15437
Satellite: ISS
Catalog Number: 25544
Epoch time: 08086
18652290 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 84
2706 deg
Eccentricity:
0001085
Arg of perigee: 283
5422 deg
Mean anomaly: 76
5621 deg
Mean motion: 15
76512736 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1543
Checksum: 284
Coasting Arc #3 (Orbit 1558)
---------------------------------------
Vector Time (GMT): 2008/087/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1942619
84 A = 6724676
77 meter
Y = -6380348
03 meter E =
0012627
Z = 809426
38 I = 51
97762
XDOT = 4360
240765 Wp = 128
15931
YDOT = -2095
520295 meter/sec RA = 78
51138 deg
ZDOT = -5998
417047 TA = 43
04362
MA = 42
94492
Ha = 185
861 n
mi
Hp = 180
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6373424
66 X = -1875061
48
Y = -20932900
35 feet Y = -6401693
76 meter
Z = 2655598
36 Z = 800153
32
XDOT = 14305
251853 XDOT = 4412
488500
YDOT = -6875
066585 feet/sec YDOT = -2046
469582 meter/sec
ZDOT = -19679
845955 ZDOT = -5977
107946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21643955
89 X = 6597077
75
Y = 3246120
75 feet Y = 989417
61 meter
Z = 2619338
67 Z = 798374
43
XDOT = 235
195844 XDOT = 71
687693
YDOT = 14393
797983 feet/sec YDOT = 4387
229625 meter/sec
ZDOT = -19598
344875 ZDOT = -5973
575518
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 08087
20072149
00020000 00000-0 20000-3 0 9029
2 25544 51
6394 79
0425 0000986 284
6709 75
4346 15
76543013 15590
Satellite: ISS
Catalog Number: 25544
Epoch time: 08087
20072149 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 79
0425 deg
Eccentricity:
0000986
Arg of perigee: 284
6709 deg
Mean anomaly: 75
4346 deg
Mean motion: 15
76543013 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1559
Checksum: 301
Coasting Arc #4 (Orbit 1574)
---------------------------------------
Vector Time (GMT): 2008/088/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3983968
53 A = 6712648
48 meter
Y = 1121372
50 meter E =
0001509
Z = 5283721
50 I = 51
93153
XDOT = -2159
985428 Wp = 66
87497
YDOT = -7397
840810 meter/sec RA = 73
38580 deg
ZDOT = -57
997825 TA = 23
67618
MA = 23
66924
Ha = 185
867 n
mi
Hp = 180
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13070762
88 X = -4021879
22
Y = 3679043
63 feet Y = 1076609
57 meter
Z = 17335044
30 Z = 5264275
24
XDOT = -7086
566366 XDOT = -2076
819344
YDOT = -24271
131265 feet/sec YDOT = -7421
529995 meter/sec
ZDOT = -190
281578 ZDOT = -68
288977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2116924
06 X = 645238
45
Y = -13508333
83 feet Y = -4117340
15 meter
Z = 17260576
90 Z = 5261023
84
XDOT = 24038
034861 XDOT = 7326
793026
YDOT = 3469
973003 feet/sec YDOT = 1057
647771 meter/sec
ZDOT = -230
548646 ZDOT = -70
271227
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 08088
21489861
00020000 00000-0 20000-3 0 9035
2 25544 51
6403 73
8142 0001078 294
7385 65
3668 15
76616923 15758
Satellite: ISS
Catalog Number: 25544
Epoch time: 08088
21489861 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 73
8142 deg
Eccentricity:
0001078
Arg of perigee: 294
7385 deg
Mean anomaly: 65
3668 deg
Mean motion: 15
76616923 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1575
Checksum: 315
Coasting Arc #5 (Orbit 1590)
---------------------------------------
Vector Time (GMT): 2008/089/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1782442
49 A = 6724399
20 meter
Y = 6411308
02 meter E =
0013361
Z = 918760
13 I = 51
96170
XDOT = -4841
645530 Wp = 50
82596
YDOT = 482
507898 meter/sec RA = 68
26216 deg
ZDOT = 5976
829477 TA = 319
17434
MA = 319
27436
Ha = 185
826 n
mi
Hp = 180
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5847908
42 X = 1706154
60
Y = 21034475
14 feet Y = 6430813
77 meter
Z = 3014304
90 Z = 927233
89
XDOT = -15884
663812 XDOT = -4875
715505
YDOT = 1583
031163 feet/sec YDOT = 428
175394 meter/sec
ZDOT = 19609
020595 ZDOT = 5953
226021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21613281
53 X = -6587728
21
Y = -3051569
52 feet Y = -930118
39 meter
Z = 3047490
15 Z = 928875
00
XDOT = 4711
979300 XDOT = 1436
211291
YDOT = -13721
637884 feet/sec YDOT = -4182
355227 meter/sec
ZDOT = 19518
534096 ZDOT = 5949
249193
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 08089
22905813
00020000 00000-0 20000-3 0 9048
2 25544 51
6405 68
5864 0000985 304
0602 56
0469 15
76608276 15911
Satellite: ISS
Catalog Number: 25544
Epoch time: 08089
22905813 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 68
5864 deg
Eccentricity:
0000985
Arg of perigee: 304
0602 deg
Mean anomaly: 56
0469 deg
Mean motion: 15
76608276 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1591
Checksum: 301
Coasting Arc #6 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2008/090/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4507052
24 A = 6713903
33 meter
Y = 257360
60 meter E =
0011972
Z = -4980366
93 I = 51
91461
XDOT = 1847
905742 Wp = 103
27392
YDOT = 7185
511543 meter/sec RA = 63
10297 deg
ZDOT = 2044
997903 TA = 186
44909
MA = 186
46451
Ha = 185
745 n
mi
Hp = 180
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14786916
79 X = 4528033
05
Y = 844358
91 feet Y = 307878
29 meter
Z = -16339786
51 Z = -4958420
79
XDOT = 6062
682879 XDOT = 1757
484701
YDOT = 23574
512937 feet/sec YDOT = 7205
670330 meter/sec
ZDOT = 6709
310706 ZDOT = 2053
755294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6484552
17 X = -1976491
50
Y = 13418693
95 feet Y = 4090017
92 meter
Z = -16255574
71 Z = -4954699
17
XDOT = -23104
301727 XDOT = -7042
191166
YDOT = -3001
328358 feet/sec YDOT = -914
804884 meter/sec
ZDOT = 6743
662558 ZDOT = 2055
468348
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 08090
17981247
00020000 00000-0 20000-3 0 9050
2 25544 51
6404 63
6857 0000969 307
5530 52
5546 15
76668380 16064
Satellite: ISS
Catalog Number: 25544
Epoch time: 08090
17981247 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 63
6857 deg
Eccentricity:
0000969
Arg of perigee: 307
5530 deg
Mean anomaly: 52
5546 deg
Mean motion: 15
76668380 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1606
Checksum: 306
Coasting Arc #7 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2008/091/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1360484
33 A = 6721598
88 meter
Y = -6041248
28 meter E =
0004028
Z = -2613050
63 I = 51
92571
XDOT = 5516
769657 Wp = 126
29303
YDOT = 1034
830011 meter/sec RA = 58
00605 deg
ZDOT = -5272
706389 TA = 83
30159
MA = 83
25576
Ha = 185
727 n
mi
Hp = 179
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4463531
26 X = -1280135
39
Y = -19820368
37 feet Y = -6056012
79 meter
Z = -8573000
75 Z = -2619464
53
XDOT = 18099
637981 XDOT = 5530
401699
YDOT = 3395
111586 feet/sec YDOT = 1096
597796 meter/sec
ZDOT = -17298
905475 ZDOT = -5245
873005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20055997
56 X = 6113068
06
Y = 3177054
49 feet Y = 968366
21 meter
Z = -8598240
64 Z = -2620743
75
XDOT = -9612
655809 XDOT = -2929
937491
YDOT = 14214
462227 feet/sec YDOT = 4332
568087 meter/sec
ZDOT = -17195
860643 ZDOT = -5241
298324
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 08091
19393105
00020000 00000-0 20000-3 0 9064
2 25544 51
6398 58
4570 0000987 306
8854 53
2220 15
76667737 16221
Satellite: ISS
Catalog Number: 25544
Epoch time: 08091
19393105 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 58
4570 deg
Eccentricity:
0000987
Arg of perigee: 306
8854 deg
Mean anomaly: 53
2220 deg
Mean motion: 15
76667737 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1622
Checksum: 307
Coasting Arc #8 (Orbit 1637)
---------------------------------------
Vector Time (GMT): 2008/092/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5127726
42 A = 6717272
51 meter
Y = -1470666
60 meter E =
0010224
Z = 4076333
73 I = 51
89539
XDOT = -1188
527128 Wp = 71
40257
YDOT = -6568
114721 meter/sec RA = 52
82093 deg
ZDOT = -3853
722464 TA = 58
09835
MA = 57
99892
Ha = 185
774 n
mi
Hp = 179
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16823249
41 X = -5130702
03
Y = -4825021
64 feet Y = -1528024
25 meter
Z = 13373798
31 Z = 4051416
26
XDOT = -3899
367218 XDOT = -1096
272573
YDOT = -21548
932811 feet/sec YDOT = -6580
889829 meter/sec
ZDOT = -12643
446404 ZDOT = -3859
271959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10455580
59 X = 3186860
96
Y = -14125690
01 feet Y = -4305510
32 meter
Z = 13278055
29 Z = 4047151
25
XDOT = 20489
571754 XDOT = 6245
221471
YDOT = 3226
388385 feet/sec YDOT = 983
403180 meter/sec
ZDOT = -12665
425071 ZDOT = -3860
421562
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 08092
20802769
00020000 00000-0 20000-3 0 9079
2 25544 51
6403 53
2280 0001089 318
0858 42
0223 15
76729010 16381
Satellite: ISS
Catalog Number: 25544
Epoch time: 08092
20802769 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 53
2280 deg
Eccentricity:
0001089
Arg of perigee: 318
0858 deg
Mean anomaly: 42
0223 deg
Mean motion: 15
76729010 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1638
Checksum: 272
Coasting Arc #9 (Orbit 1653)
---------------------------------------
Vector Time (GMT): 2008/093/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 611994
22 A = 6717311
64 meter
Y = 5350041
52 meter E =
0009972
Z = 4008247
20 I = 51
87706
XDOT = -6228
329591 Wp = 98
64800
YDOT = -2250
239054 meter/sec RA = 47
73324 deg
ZDOT = 3944
740790 TA = 310
72776
MA = 310
81432
Ha = 185
629 n
mi
Hp = 179
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2007855
06 X = 532652
55
Y = 17552629
65 feet Y = 5356441
79 meter
Z = 13150417
33 Z = 4011027
23
XDOT = -20434
152201 XDOT = -6221
866858
YDOT = -7382
674061 feet/sec YDOT = -2319
851437 meter/sec
ZDOT = 12942
062959 ZDOT = 3914
499623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17184944
31 X = -5237971
03
Y = -4063076
35 feet Y = -1238425
67 meter
Z = 13161643
71 Z = 4011669
00
XDOT = 13534
101389 XDOT = 4125
194103
YDOT = -15592
457646 feet/sec YDOT = -4752
581090 meter/sec
ZDOT = 12825
814620 ZDOT = 3909
308296
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 08093
22210311
00020000 00000-0 20000-3 0 9089
2 25544 51
6400 47
9989 0001055 316
0742 44
0339 15
76759426 16549
Satellite: ISS
Catalog Number: 25544
Epoch time: 08093
22210311 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 47
9989 deg
Eccentricity:
0001055
Arg of perigee: 316
0742 deg
Mean anomaly: 44
0339 deg
Mean motion: 15
76759426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1654
Checksum: 280
Coasting Arc #10 (Orbit 1668)
---------------------------------------
Vector Time (GMT): 2008/094/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5690002
10 A = 6721250
00 meter
Y = 2363563
75 meter E =
0005072
Z = -2682981
79 I = 51
86909
XDOT = 106
252954 Wp = 41
40614
YDOT = 5660
957318 meter/sec RA = 42
54509 deg
ZDOT = 5221
640317 TA = 288
09291
MA = 288
14816
Ha = 185
690 n
mi
Hp = 179
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18667985
89 X = 5676182
85
Y = 7754474
24 feet Y = 2427115
13 meter
Z = -8802433
71 Z = -2655373
65
XDOT = 348
598930 XDOT = 17
577692
YDOT = 18572
694614 feet/sec YDOT = 5661
650088 meter/sec
ZDOT = 17131
365871 ZDOT = 5221
940670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13320071
48 X = -4059957
79
Y = 15266266
25 feet Y = 4653157
95 meter
Z = -8696276
09 Z = -2650624
95
XDOT = -16569
341856 XDOT = -5050
335398
YDOT = -4714
914351 feet/sec YDOT = -1437
105894 meter/sec
ZDOT = 17133
111819 ZDOT = 5222
172482
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 08094
17278067
00020000 00000-0 20000-3 0 9097
2 25544 51
6395 43
0970 0001126 323
9635 36
1454 15
76764773 16693
Satellite: ISS
Catalog Number: 25544
Epoch time: 08094
17278067 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 43
0970 deg
Eccentricity:
0001126
Arg of perigee: 323
9635 deg
Mean anomaly: 36
1454 deg
Mean motion: 15
76764773 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1669
Checksum: 312
Coasting Arc #11 (Orbit 1684)
---------------------------------------
Vector Time (GMT): 2008/095/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 532308
55 A = 6713559
76 meter
Y = -4505137
66 meter E =
0012635
Z = -4960466
86 I = 51
82100
XDOT = 6732
393589 Wp = 69
73423
YDOT = 3090
685782 meter/sec RA = 37
44204 deg
ZDOT = -2084
507278 TA = 180
10944
MA = 180
10971
Ha = 185
652 n
mi
Hp = 179
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1746419
13 X = 606743
19
Y = -14780635
38 feet Y = -4498769
35 meter
Z = -16274497
56 Z = -4957699
70
XDOT = 22087
905476 XDOT = 6707
458851
YDOT = 10140
045216 feet/sec YDOT = 3165
831652 meter/sec
ZDOT = -6838
934640 ZDOT = -2051
862167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13530990
03 X = 4124245
76
Y = 6225715
68 feet Y = 1897598
14 meter
Z = -16264353
84 Z = -4957375
05
XDOT = -15906
813745 XDOT = -4848
396829
YDOT = 17033
344082 feet/sec YDOT = 5191
763276 meter/sec
ZDOT = -6713
382933 ZDOT = -2046
239118
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 08095
18681546
00020000 00000-0 20000-3 0 9101
2 25544 51
6395 37
8674 0001086 329
3802 30
7299 15
76786121 16852
Satellite: ISS
Catalog Number: 25544
Epoch time: 08095
18681546 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 37
8674 deg
Eccentricity:
0001086
Arg of perigee: 329
3802 deg
Mean anomaly: 30
7299 deg
Mean motion: 15
76786121 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1685
Checksum: 315
Coasting Arc #12 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2008/096/04:01:08
440
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5972284
00 A = 6723732
19 meter
Y = -2945007
23 meter E =
0012640
Z = 889173
64 I = 51
83277
XDOT = 1403
120577 Wp = 122
43161
YDOT = -4664
749947 meter/sec RA = 32
27305 deg
ZDOT = -5971
156898 TA = 47
87665
MA = 47
76929
Ha = 185
619 n
mi
Hp = 179
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19594107
60 X = -5943228
06
Y = -9662097
20 feet Y = -3011630
18 meter
Z = 2917236
34 Z = 860230
96
XDOT = 4603
413965 XDOT = 1484
185234
YDOT = -15304
297728 feet/sec YDOT = -4648
606741 meter/sec
ZDOT = -19590
409771 ZDOT = -5964
143165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14870367
47 X = 4532488
00
Y = -16024808
49 feet Y = -4884361
63 meter
Z = 2805909
30 Z = 855241
16
XDOT = 12146
244481 XDOT = 3702
175318
YDOT = 7813
033600 feet/sec YDOT = 2381
412641 meter/sec
ZDOT = -19563
990626 ZDOT = -5963
104343
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 08096
20082769
00020000 00000-0 20000-3 0 9118
2 25544 51
6404 32
6381 0001203 341
2796 18
8324 15
76861275 17016
Satellite: ISS
Catalog Number: 25544
Epoch time: 08096
20082769 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 32
6381 deg
Eccentricity:
0001203
Arg of perigee: 341
2796 deg
Mean anomaly: 18
8324 deg
Mean motion: 15
76861275 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1701
Checksum: 276
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 may contain past, current and future orbital data 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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