Date:
March 22nd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3691)
---------------------------------------
Vector Time (GMT): 2007/080/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5078019
00 A = 6718673
86 meter
Y = -3588262
34 meter E =
0017773
Z = 2513828
46 I = 51
55323
XDOT = 4737
243984 Wp = 22
26706
YDOT = -2989
157431 meter/sec RA = 196
52415 deg
ZDOT = 5306
666694 TA = 6
32567
MA = 6
30326
Ha = 186
968 n
mi
Hp = 177
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16660167
31 X = -5049728
89
Y = -11772514
24 feet Y = -3644889
23 meter
Z = 8247468
70 Z = 2489228
34
XDOT = 15542
139054 XDOT = 4744
538164
YDOT = -9806
946952 feet/sec YDOT = -2936
141744 meter/sec
ZDOT = 17410
323800 ZDOT = 5329
698245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7866895
91 X = -2397829
87
Y = -18862413
49 feet Y = -5749263
63 meter
Z = 8154465
80 Z = 2485481
18
XDOT = 16919
923596 XDOT = 5157
192712
YDOT = 501
438642 feet/sec YDOT = 152
838498 meter/sec
ZDOT = 17496
487258 ZDOT = 5332
929316
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 07080
47505533
00020000 00000-0 20000-3 0 9006
2 25544 51
6328 197
1762 0014683 332
5761 27
4627 15
77805905 36924
Satellite: ISS
Catalog Number: 25544
Epoch time: 07080
47505533 = yrday
fracday
Element set: 900
Inclination: 51
6328 deg
RA of node: 197
1762 deg
Eccentricity:
0014683
Arg of perigee: 332
5761 deg
Mean anomaly: 27
4627 deg
Mean motion: 15
77805905 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3692
Checksum: 302
Coasting Arc #2 (Orbit 3706)
---------------------------------------
Vector Time (GMT): 2007/081/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5038198
94 A = 6714654
51 meter
Y = 2134939
99 meter E =
0011611
Z = -3883195
53 I = 51
56827
XDOT = -4947
416303 Wp = 3
35760
YDOT = -4286
214893 meter/sec RA = 191
30655 deg
ZDOT = 4074
453009 TA = 309
01294
MA = 309
11627
Ha = 187
069 n
mi
Hp = 177
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16529524
09 X = -5042833
75
Y = 7004396
30 feet Y = 2078573
95 meter
Z = -12740142
83 Z = -3907682
55
XDOT = -16231
680784 XDOT = -4918
912570
YDOT = -14062
384819 feet/sec YDOT = -4341
380126 meter/sec
ZDOT = 13367
627983 ZDOT = 4050
487777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17706285
93 X = -5396875
95
Y = -2535251
76 feet Y = -772744
74 meter
Z = -12831909
84 Z = -3911166
12
XDOT = -6846
624522 XDOT = -2086
851154
YDOT = -19184
587935 feet/sec YDOT = -5847
462403 meter/sec
ZDOT = 13276
908989 ZDOT = 4046
801860
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 07081
42510303
00020000 00000-0 20000-3 0 9014
2 25544 51
6331 192
2699 0014798 336
6269 23
4220 15
77810411 37078
Satellite: ISS
Catalog Number: 25544
Epoch time: 07081
42510303 = yrday
fracday
Element set: 901
Inclination: 51
6331 deg
RA of node: 192
2699 deg
Eccentricity:
0014798
Arg of perigee: 336
6269 deg
Mean anomaly: 23
4220 deg
Mean motion: 15
77810411 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3707
Checksum: 274
Coasting Arc #3 (Orbit 3722)
---------------------------------------
Vector Time (GMT): 2007/082/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3317774
66 A = 6712904
77 meter
Y = 3860299
04 meter E =
0017626
Z = -4389444
99 I = 51
59076
XDOT = -6666
110869 Wp = 12
17533
YDOT = 1930
188353 meter/sec RA = 186
18795 deg
ZDOT = -3326
575072 TA = 224
27583
MA = 224
41697
Ha = 187
308 n
mi
Hp = 176
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10885087
48 X = 3295684
83
Y = 12665023
09 feet Y = 3897276
67 meter
Z = -14401066
24 Z = -4373380
93
XDOT = -21870
442485 XDOT = -6671
039141
YDOT = 6332
638952 feet/sec YDOT = 1855
616565 meter/sec
ZDOT = -10913
960210 ZDOT = -3358
971101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3101151
77 X = 945231
06
Y = 16462765
67 feet Y = 5017850
98 meter
Z = -14340113
41 Z = -4370866
57
XDOT = -20832
637467 XDOT = -6349
787900
YDOT = -5729
976778 feet/sec YDOT = -1746
496922 meter/sec
ZDOT = -11035
508139 ZDOT = -3363
622881
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 07082
43846299
00020000 00000-0 20000-3 0 9023
2 25544 51
6330 187
0356 0014864 340
5563 19
5033 15
77855890 37230
Satellite: ISS
Catalog Number: 25544
Epoch time: 07082
43846299 = yrday
fracday
Element set: 902
Inclination: 51
6330 deg
RA of node: 187
0356 deg
Eccentricity:
0014864
Arg of perigee: 340
5563 deg
Mean anomaly: 19
5033 deg
Mean motion: 15
77855890 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3723
Checksum: 305
Coasting Arc #4 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2007/083/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6375009
37 A = 6719773
37 meter
Y = -1257025
48 meter E =
0012179
Z = 1725966
47 I = 51
64304
XDOT = 2450
774729 Wp = 46
98804
YDOT = 4554
639395 meter/sec RA = 180
97998 deg
ZDOT = -5701
593574 TA = 113
90180
MA = 113
77416
Ha = 187
404 n
mi
Hp = 176
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20915385
08 X = 6380207
39
Y = -4124099
35 feet Y = -1185707
50 meter
Z = 5662619
65 Z = 1756948
82
XDOT = 8040
599503 XDOT = 2427
359203
YDOT = 14943
042635 feet/sec YDOT = 4581
914405 meter/sec
ZDOT = -18706
015662 ZDOT = -5689
744613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20238088
47 X = 6168569
37
Y = 6599255
23 feet Y = 2011452
99 meter
Z = 5778961
44 Z = 1761427
45
XDOT = 291
345731 XDOT = 88
802179
YDOT = 15541
818266 feet/sec YDOT = 4737
146208 meter/sec
ZDOT = -18660
812416 ZDOT = -5687
815624
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 07083
45179909
00020000 00000-0 20000-3 0 9034
2 25544 51
6328 181
8003 0014859 344
5254 15
5455 15
77890770 37390
Satellite: ISS
Catalog Number: 25544
Epoch time: 07083
45179909 = yrday
fracday
Element set: 903
Inclination: 51
6328 deg
RA of node: 181
8003 deg
Eccentricity:
0014859
Arg of perigee: 344
5254 deg
Mean anomaly: 15
5455 deg
Mean motion: 15
77890770 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3739
Checksum: 316
Coasting Arc #5 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2007/084/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -852986
71 A = 6708926
38 meter
Y = -4098271
20 meter E =
0013618
Z = 5242120
46 I = 51
63665
XDOT = 7632
048219 Wp = 358
21039
YDOT = -957
739306 meter/sec RA = 175
83530 deg
ZDOT = 506
528392 TA = 87
06028
MA = 86
90445
Ha = 187
513 n
mi
Hp = 176
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2798512
83 X = -832560
96
Y = -13445771
65 feet Y = -4107695
58 meter
Z = 17198557
95 Z = 5238026
28
XDOT = 25039
528276 XDOT = 7639
729961
YDOT = -3142
189323 feet/sec YDOT = -872
350525 meter/sec
ZDOT = 1661
838555 ZDOT = 543
623286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3813733
26 X = 1162425
90
Y = -13214580
71 feet Y = -4027804
20 meter
Z = 17182582
46 Z = 5237251
13
XDOT = 22572
908598 XDOT = 6880
222541
YDOT = 8799
360436 feet/sec YDOT = 2682
045061 meter/sec
ZDOT = 1801
228188 ZDOT = 549
014352
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 07084
46511009
00020000 00000-0 20000-3 0 9048
2 25544 51
6337 176
5653 0015026 348
3479 11
7336 15
77961436 37552
Satellite: ISS
Catalog Number: 25544
Epoch time: 07084
46511009 = yrday
fracday
Element set: 904
Inclination: 51
6337 deg
RA of node: 176
5653 deg
Eccentricity:
0015026
Arg of perigee: 348
3479 deg
Mean anomaly: 11
7336 deg
Mean motion: 15
77961436 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3755
Checksum: 302
Coasting Arc #6 (Orbit 3770)
---------------------------------------
Vector Time (GMT): 2007/085/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6636040
83 A = 6720640
42 meter
Y = 392971
03 meter E =
0024704
Z = 870521
63 I = 51
70518
XDOT = 499
927101 Wp = 21
90482
YDOT = -4862
986457 meter/sec RA = 170
67604 deg
ZDOT = 5974
806006 TA = 347
61799
MA = 347
67859
Ha = 187
725 n
mi
Hp = 175
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21771787
49 X = -6644170
67
Y = 1289275
02 feet Y = 318717
65 meter
Z = 2856042
08 Z = 838264
35
XDOT = 1640
180779 XDOT = 525
244353
YDOT = -15954
679978 feet/sec YDOT = -4857
254407 meter/sec
ZDOT = 19602
381910 ZDOT = 5977
296144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19958080
15 X = -6083222
83
Y = -8833237
98 feet Y = -2692370
94 meter
Z = 2734754
16 Z = 833553
07
XDOT = 8024
646237 XDOT = 2445
912173
YDOT = -12026
244657 feet/sec YDOT = -3665
599372 meter/sec
ZDOT = 19611
065049 ZDOT = 5977
452627
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 07085
47839940
00020000 00000-0 20000-3 0 9058
2 25544 51
6342 171
3307 0015082 352
9266 7
1684 15
77962957 37716
Satellite: ISS
Catalog Number: 25544
Epoch time: 07085
47839940 = yrday
fracday
Element set: 905
Inclination: 51
6342 deg
RA of node: 171
3307 deg
Eccentricity:
0015082
Arg of perigee: 352
9266 deg
Mean anomaly: 7
1684 deg
Mean motion: 15
77962957 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3771
Checksum: 316
Coasting Arc #7 (Orbit 3785)
---------------------------------------
Vector Time (GMT): 2007/086/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1689198
18 A = 6710565
05 meter
Y = 4364447
50 meter E =
0015562
Z = -4814105
35 I = 51
70029
XDOT = -7296
989918 Wp = 43
09987
YDOT = -122
343183 meter/sec RA = 165
48790 deg
ZDOT = 2465
294741 TA = 250
88283
MA = 251
05139
Ha = 187
734 n
mi
Hp = 175
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5541988
78 X = -1714490
79
Y = 14319053
48 feet Y = 4345416
42 meter
Z = -15794308
88 Z = -4822372
88
XDOT = -23940
255637 XDOT = -7307
055321
YDOT = -401
388396 feet/sec YDOT = -203
998434 meter/sec
ZDOT = 8088
237338 ZDOT = 2429
822021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11229173
02 X = -3422651
94
Y = 10425478
13 feet Y = 3177685
74 meter
Z = -15824797
14 Z = -4823398
17
XDOT = -20568
930709 XDOT = -6269
410080
YDOT = -10158
623029 feet/sec YDOT = -3096
348299 meter/sec
ZDOT = 7954
766886 ZDOT = 2424
612947
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 07086
42833508
00020000 00000-0 20000-3 0 9069
2 25544 51
6344 166
4241 0015068 356
5333 3
5726 15
78029266 37860
Satellite: ISS
Catalog Number: 25544
Epoch time: 07086
42833508 = yrday
fracday
Element set: 906
Inclination: 51
6344 deg
RA of node: 166
4241 deg
Eccentricity:
0015068
Arg of perigee: 356
5333 deg
Mean anomaly: 3
5726 deg
Mean motion: 15
78029266 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3786
Checksum: 301
Coasting Arc #8 (Orbit 3801)
---------------------------------------
Vector Time (GMT): 2007/087/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5811094
56 A = 6716015
86 meter
Y = 700755
94 meter E =
0015434
Z = -3312915
01 I = 51
74638
XDOT = -3302
607312 Wp = 18
27177
YDOT = 5114
357461 meter/sec RA = 160
37224 deg
ZDOT = -4702
728684 TA = 200
57656
MA = 200
63879
Ha = 187
881 n
mi
Hp = 175
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19065270
85 X = 5818920
01
Y = 2299068
03 feet Y = 765782
46 meter
Z = -10869143
75 Z = -3284666
17
XDOT = -10835
325828 XDOT = -3336
706681
YDOT = 16779
387995 feet/sec YDOT = 5077
235004 meter/sec
ZDOT = -15428
899881 ZDOT = -4718
855540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16310455
65 X = 4971426
88
Y = 10248931
92 feet Y = 3123874
45 meter
Z = -10762759
08 Z = -3280488
97
XDOT = -16139
641577 XDOT = -4919
362753
YDOT = 9390
205189 feet/sec YDOT = 2862
134542 meter/sec
ZDOT = -15488
853431 ZDOT = -4721
002526
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 07087
44157736
00020000 00000-0 20000-3 0 9075
2 25544 51
6347 161
1886 0015088
3741 359
7433 15
78040064 38028
Satellite: ISS
Catalog Number: 25544
Epoch time: 07087
44157736 = yrday
fracday
Element set: 907
Inclination: 51
6347 deg
RA of node: 161
1886 deg
Eccentricity:
0015088
Arg of perigee:
3741 deg
Mean anomaly: 359
7433 deg
Mean motion: 15
78040064 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3802
Checksum: 295
Coasting Arc #9 (Orbit 3817)
---------------------------------------
Vector Time (GMT): 2007/088/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3901297
10 A = 6716364
33 meter
Y = -4501719
52 meter E =
0020065
Z = 3106419
85 I = 51
77453
XDOT = 5740
777593 Wp = 45
60758
YDOT = 1581
987802 meter/sec RA = 155
16409 deg
ZDOT = -4884
098400 TA = 98
33569
MA = 98
10814
Ha = 187
996 n
mi
Hp = 174
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12799531
16 X = 3936255
81
Y = -14769420
99 feet Y = -4457897
37 meter
Z = 10191666
17 Z = 3125457
27
XDOT = 18834
572155 XDOT = 5746
386640
YDOT = 5190
248694 feet/sec YDOT = 1646
215449 meter/sec
ZDOT = -16023
944883 ZDOT = -4856
196581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17691960
63 X = 5392509
60
Y = -8216214
44 feet Y = -2504302
16 meter
Z = 10262660
62 Z = 3128058
96
XDOT = 14511
184946 XDOT = 4423
009172
YDOT = 11228
617510 feet/sec YDOT = 3422
482617 meter/sec
ZDOT = -15918
733100 ZDOT = -4852
029849
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 07088
45479628
00020000 00000-0 20000-3 0 9085
2 25544 51
6346 155
9536 0015175 4
7295 355
4011 15
78067354 38182
Satellite: ISS
Catalog Number: 25544
Epoch time: 07088
45479628 = yrday
fracday
Element set: 908
Inclination: 51
6346 deg
RA of node: 155
9536 deg
Eccentricity:
0015175
Arg of perigee: 4
7295 deg
Mean anomaly: 355
4011 deg
Mean motion: 15
78067354 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3818
Checksum: 319
Coasting Arc #10 (Orbit 3833)
---------------------------------------
Vector Time (GMT): 2007/089/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4028343
92 A = 6709932
55 meter
Y = -2141481
38 meter E =
0013817
Z = 4910007
33 I = 51
77929
XDOT = 5369
484941 Wp = 33
51034
YDOT = -5088
404291 meter/sec RA = 150
04927 deg
ZDOT = 2194
429910 TA = 35
31264
MA = 35
22119
Ha = 188
119 n
mi
Hp = 174
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13216351
43 X = -4027949
82
Y = -7025857
54 feet Y = -2186525
99 meter
Z = 16108947
94 Z = 4890438
99
XDOT = 17616
420410 XDOT = 5415
325119
YDOT = -16694
239801 feet/sec YDOT = -5028
103227 meter/sec
ZDOT = 7199
573194 ZDOT = 2220
626307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9438003
94 X = -2876703
60
Y = -11719018
11 feet Y = -3571956
72 meter
Z = 16035009
18 Z = 4887470
80
XDOT = 21894
039099 XDOT = 6673
303117
YDOT = -7685
441932 feet/sec YDOT = -2342
522701 meter/sec
ZDOT = 7297
425907 ZDOT = 2224
255416
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 07089
46798931
00020000 00000-0 20000-3 0 9099
2 25544 51
6350 150
7176 0015219 8
1942 351
9469 15
78143843 38340
Satellite: ISS
Catalog Number: 25544
Epoch time: 07089
46798931 = yrday
fracday
Element set: 909
Inclination: 51
6350 deg
RA of node: 150
7176 deg
Eccentricity:
0015219
Arg of perigee: 8
1942 deg
Mean anomaly: 351
9469 deg
Mean motion: 15
78143843 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3834
Checksum: 321
Coasting Arc #11 (Orbit 3848)
---------------------------------------
Vector Time (GMT): 2007/090/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5187786
57 A = 6720343
95 meter
Y = 4208556
02 meter E =
0025626
Z = -581406
59 I = 51
83817
XDOT = -3415
959234 Wp = 23
90220
YDOT = -3393
195899 meter/sec RA = 144
87138 deg
ZDOT = 6032
694584 TA = 329
76658
MA = 329
91420
Ha = 188
262 n
mi
Hp = 174
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17020297
13 X = -5231637
33
Y = 13807598
50 feet Y = 4150298
06 meter
Z = -1907501
93 Z = -606715
55
XDOT = -11207
215336 XDOT = -3407
067675
YDOT = -11132
532476 feet/sec YDOT = -3431
344821 meter/sec
ZDOT = 19792
305064 ZDOT = 6016
121875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20980193
28 X = -6394762
91
Y = 6308863
82 feet Y = 1922941
69 meter
Z = -2002144
23 Z = -610253
56
XDOT = -5778
257907 XDOT = -1761
213010
YDOT = -13068
123248 feet/sec YDOT = -3983
163966 meter/sec
ZDOT = 19729
458571 ZDOT = 6013
538972
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 07090
41783878
00020000 00000-0 20000-3 0 9102
2 25544 51
6347 145
8101 0015500 11
8297 348
3229 15
78112127 38497
Satellite: ISS
Catalog Number: 25544
Epoch time: 07090
41783878 = yrday
fracday
Element set: 910
Inclination: 51
6347 deg
RA of node: 145
8101 deg
Eccentricity:
0015500
Arg of perigee: 11
8297 deg
Mean anomaly: 348
3229 deg
Mean motion: 15
78112127 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3849
Checksum: 291
Coasting Arc #12 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2007/091/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1863131
31 A = 6708486
12 meter
Y = 3800537
44 meter E =
0022844
Z = -5218948
29 I = 51
82046
XDOT = -6277
889527 Wp = 55
34091
YDOT = 4349
903740 meter/sec RA = 139
71584 deg
ZDOT = 942
130941 TA = 223
52866
MA = 223
70917
Ha = 188
300 n
mi
Hp = 174
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6112635
52 X = 1845847
33
Y = 12468954
87 feet Y = 3821274
91 meter
Z = -17122533
77 Z = -5209939
55
XDOT = -20596
750418 XDOT = -6330
640883
YDOT = 14271
337730 feet/sec YDOT = 4279
406000 meter/sec
ZDOT = 3090
980776 ZDOT = 911
504510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1243182
56 X = 378922
04
Y = 13873422
64 feet Y = 4228619
22 meter
Z = -17088093
89 Z = -5208451
02
XDOT = -23382
665203 XDOT = -7127
036354
YDOT = 5698
072580 feet/sec YDOT = 1736
772522 meter/sec
ZDOT = 2976
343232 ZDOT = 907
189417
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 07091
43098741
00020000 00000-0 20000-3 0 9114
2 25544 51
6337 140
5746 0015440 15
7004 344
4637 15
78178726 38650
Satellite: ISS
Catalog Number: 25544
Epoch time: 07091
43098741 = yrday
fracday
Element set: 911
Inclination: 51
6337 deg
RA of node: 140
5746 deg
Eccentricity:
0015440
Arg of perigee: 15
7004 deg
Mean anomaly: 344
4637 deg
Mean motion: 15
78178726 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3865
Checksum: 296
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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