Date:
December 26th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 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
363/07:06:12
689 -11
9 12
1 12
1
N/A -1
0 -0
0 186
4
000/00:02:25
377 2
1 0
0 183
6
Coasting Arc #1 (Orbit 33)
---------------------------------------
Vector Time (GMT): 2007/355/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5243242
50 A = 6721102
48 meter
Y = -4187416
28 meter E =
0013117
Z = 235099
36 I = 51
46339
XDOT = 3168
850619 Wp = 41
73060
YDOT = -3619
428028 meter/sec RA = 217
01286 deg
ZDOT = 6023
686885 TA = 320
83505
MA = 320
92991
Ha = 183
932 n
mi
Hp = 178
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17202239
18 X = -5197170
57
Y = -13738242
39 feet Y = -4245791
63 meter
Z = 771323
35 Z = 209738
55
XDOT = 10396
491531 XDOT = 3179
825694
YDOT = -11874
763872 feet/sec YDOT = -3583
931750 meter/sec
ZDOT = 19762
752246 ZDOT = 6039
107462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11715846
70 X = 3570990
08
Y = -18642309
73 feet Y = -5682176
01 meter
Z = 674166
33 Z = 205485
90
XDOT = 11596
721771 XDOT = 3534
680796
YDOT = 8029
544393 feet/sec YDOT = 2447
405131 meter/sec
ZDOT = 19821
164842 ZDOT = 6041
491044
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 07355
58377551
00020000 00000-0 20000-3 0 9000
2 25544 51
6384 217
6331 0001379 332
9350 27
1743 15
77897012 345
Satellite: ISS
Catalog Number: 25544
Epoch time: 07355
58377551 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 217
6331 deg
Eccentricity:
0001379
Arg of perigee: 332
9350 deg
Mean anomaly: 27
1743 deg
Mean motion: 15
77897012 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 34
Checksum: 287
Coasting Arc #2 (Orbit 48)
---------------------------------------
Vector Time (GMT): 2007/356/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3774448
06 A = 6709896
95 meter
Y = 2371946
89 meter E =
0012722
Z = -5026274
26 I = 51
44864
XDOT = -5520
001158 Wp = 98
24067
YDOT = -5070
200354 meter/sec RA = 211
81678 deg
ZDOT = 1754
513857 TA = 188
69282
MA = 188
71488
Ha = 183
906 n
mi
Hp = 177
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12383359
76 X = -3776274
04
Y = 7781978
00 feet Y = 2329729
61 meter
Z = -16490401
12 Z = -5044614
70
XDOT = -18110
240019 XDOT = -5471
418336
YDOT = -16634
515597 feet/sec YDOT = -5131
656826 meter/sec
ZDOT = 5756
279059 ZDOT = 1727
814486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9308521
97 X = -2837237
50
Y = -11178320
33 feet Y = -3407152
04 meter
Z = -16560093
08 Z = -5047516
37
XDOT = 13328
891406 XDOT = 4062
646100
YDOT = -19465
750497 feet/sec YDOT = -5933
160752 meter/sec
ZDOT = 5653
910454 ZDOT = 1723
311907
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 07356
53376220
00020000 00000-0 20000-3 0 9019
2 25544 51
6370 212
7252 0001418 335
7297 24
3801 15
77932736 496
Satellite: ISS
Catalog Number: 25544
Epoch time: 07356
53376220 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 212
7252 deg
Eccentricity:
0001418
Arg of perigee: 335
7297 deg
Mean anomaly: 24
3801 deg
Mean motion: 15
77932736 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 49
Checksum: 277
Coasting Arc #3 (Orbit 64)
---------------------------------------
Vector Time (GMT): 2007/357/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4138602
91 A = 6717704
50 meter
Y = 4523948
48 meter E =
0003694
Z = -2745905
79 I = 51
49955
XDOT = -5428
611596 Wp = 110
06741
YDOT = 1849
511853 meter/sec RA = 206
67786 deg
ZDOT = -5141
659249 TA = 101
41693
MA = 101
37543
Ha = 183
901 n
mi
Hp = 177
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13578093
53 X = 4101046
98
Y = 14842350
67 feet Y = 4570019
25 meter
Z = -9008877
26 Z = -2725890
72
XDOT = -17810
405498 XDOT = -5423
912351
YDOT = 6067
952275 feet/sec YDOT = 1788
833349 meter/sec
ZDOT = -16868
960790 ZDOT = -5168
019721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12684248
87 X = -3866159
05
Y = 15657209
97 feet Y = 4772317
60 meter
Z = -8932047
55 Z = -2722488
09
XDOT = -7457
364229 XDOT = -2273
004617
YDOT = -15709
059337 feet/sec YDOT = -4788
121286 meter/sec
ZDOT = -16969
311568 ZDOT = -5172
246166
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 07357
54705487
00020000 00000-0 20000-3 0 9023
2 25544 51
6360 207
4912 0001469 336
9502 23
1597 15
77955805 656
Satellite: ISS
Catalog Number: 25544
Epoch time: 07357
54705487 = yrday
fracday
Element set: 902
Inclination: 51
6360 deg
RA of node: 207
4912 deg
Eccentricity:
0001469
Arg of perigee: 336
9502 deg
Mean anomaly: 23
1597 deg
Mean motion: 15
77955805 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 65
Checksum: 301
Coasting Arc #4 (Orbit 80)
---------------------------------------
Vector Time (GMT): 2007/358/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5560422
58 A = 6714815
24 meter
Y = -925321
18 meter E =
0011482
Z = 3641526
20 I = 51
51752
XDOT = 3715
555624 Wp = 77
18892
YDOT = 5171
445961 meter/sec RA = 201
45197 deg
ZDOT = -4345
420352 TA = 58
92729
MA = 58
81464
Ha = 183
681 n
mi
Hp = 177
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18242856
25 X = 5552666
63
Y = -3035830
64 feet Y = -863185
46 meter
Z = 11947264
44 Z = 3668519
57
XDOT = 12190
143122 XDOT = 3678
560725
YDOT = 16966
686225 feet/sec YDOT = 5212
789415 meter/sec
ZDOT = -14256
628451 ZDOT = -4327
459123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5967971
92 X = 1819037
84
Y = 17433660
37 feet Y = 5313779
68 meter
Z = 12050145
08 Z = 3672884
22
XDOT = -13459
664278 XDOT = -4102
505672
YDOT = 14445
403932 feet/sec YDOT = 4402
959119 meter/sec
ZDOT = -14187
549930 ZDOT = -4324
365219
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 07358
56031904
00020000 00000-0 20000-3 0 9033
2 25544 51
6361 202
2554 0001611 337
1539 22
9555 15
78038112 817
Satellite: ISS
Catalog Number: 25544
Epoch time: 07358
56031904 = yrday
fracday
Element set: 903
Inclination: 51
6361 deg
RA of node: 202
2554 deg
Eccentricity:
0001611
Arg of perigee: 337
1539 deg
Mean anomaly: 22
9555 deg
Mean motion: 15
78038112 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 81
Checksum: 262
Coasting Arc #5 (Orbit 96)
---------------------------------------
Vector Time (GMT): 2007/359/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2124213
83 A = 6711625
34 meter
Y = -4415256
50 meter E =
0007560
Z = 4581627
46 I = 51
53258
XDOT = 7115
470145 Wp = 106
14024
YDOT = -357
121268 meter/sec RA = 196
32536 deg
ZDOT = 2948
769959 TA = 314
59060
MA = 314
65227
Ha = 183
915 n
mi
Hp = 177
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6969205
47 X = -2096940
34
Y = -14485749
66 feet Y = -4438858
98 meter
Z = 15031586
15 Z = 4571373
61
XDOT = 23344
718323 XDOT = 7104
610270
YDOT = -1171
657702 feet/sec YDOT = -277
613288 meter/sec
ZDOT = 9674
442123 ZDOT = 2983
310079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12974322
37 X = 3954573
46
Y = -9553154
19 feet Y = -2911801
40 meter
Z = 14991983
00 Z = 4569556
42
XDOT = 4660
112047 XDOT = 1420
402152
YDOT = 21749
433813 feet/sec YDOT = 6629
227426 meter/sec
ZDOT = 9806
195121 ZDOT = 2988
928273
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 07359
57355986
00020000 00000-0 20000-3 0 9045
2 25544 51
6347 197
0194 0001573 345
6102 14
5018 15
78020278 971
Satellite: ISS
Catalog Number: 25544
Epoch time: 07359
57355986 = yrday
fracday
Element set: 904
Inclination: 51
6347 deg
RA of node: 197
0194 deg
Eccentricity:
0001573
Arg of perigee: 345
6102 deg
Mean anomaly: 14
5018 deg
Mean motion: 15
78020278 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 97
Checksum: 298
Coasting Arc #6 (Orbit 111)
---------------------------------------
Vector Time (GMT): 2007/360/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6581841
62 A = 6719788
67 meter
Y = -234186
76 meter E =
0009826
Z = -1310687
69 I = 51
58886
XDOT = -984
319708 Wp = 31
11827
YDOT = -4920
428610 meter/sec RA = 191
11683 deg
ZDOT = 5849
760075 TA = 314
45781
MA = 314
53814
Ha = 183
749 n
mi
Hp = 177
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21593968
56 X = -6572366
74
Y = -768329
26 feet Y = -307735
47 meter
Z = -4300156
47 Z = -1342638
83
XDOT = -3229
395368 XDOT = -957
642224
YDOT = -16143
138483 feet/sec YDOT = -4931
287542 meter/sec
ZDOT = 19192
126230 ZDOT = 5845
042384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3504913
05 X = -1068297
50
Y = -21296517
65 feet Y = -6491178
58 meter
Z = -4422111
97 Z = -1347859
73
XDOT = 13613
523011 XDOT = 4149
401814
YDOT = -6203
432696 feet/sec YDOT = -1890
806286 meter/sec
ZDOT = 19173
584493 ZDOT = 5844
108554
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 07360
52344556
00020000 00000-0 20000-3 0 9054
2 25544 51
6343 192
1104 0001449 347
3561 12
7568 15
78081330 1128
Satellite: ISS
Catalog Number: 25544
Epoch time: 07360
52344556 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 192
1104 deg
Eccentricity:
0001449
Arg of perigee: 347
3561 deg
Mean anomaly: 12
7568 deg
Mean motion: 15
78081330 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 112
Checksum: 264
Coasting Arc #7 (Orbit 127)
---------------------------------------
Vector Time (GMT): 2007/361/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -514045
59 A = 6708361
55 meter
Y = 4143751
83 meter E =
0015063
Z = -5263292
80 I = 51
57934
XDOT = -7648
572554 Wp = 85
25261
YDOT = -857
007515 meter/sec RA = 185
95805 deg
ZDOT = 73
695884 TA = 185
43943
MA = 185
45581
Ha = 183
803 n
mi
Hp = 177
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1686501
29 X = -534775
71
Y = 13594986
32 feet Y = 4137888
21 meter
Z = -17268021
00 Z = -5265839
85
XDOT = -25093
741975 XDOT = -7638
778905
YDOT = -2811
704446 feet/sec YDOT = -942
483443 meter/sec
ZDOT = 241
784397 ZDOT = 36
563356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13619705
13 X = -4151286
13
Y = 1360722
63 feet Y = 414748
26 meter
Z = -17277284
36 Z = -5266116
27
XDOT = -2530
886470 XDOT = -771
414196
YDOT = -24121
224620 feet/sec YDOT = -7352
149264 meter/sec
ZDOT = 99
970831 ZDOT = 30
471109
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 07361
53663210
00020000 00000-0 20000-3 0 9068
2 25544 51
6341 186
8745 0001415 356
6128 3
5028 15
78128864 1282
Satellite: ISS
Catalog Number: 25544
Epoch time: 07361
53663210 = yrday
fracday
Element set: 906
Inclination: 51
6341 deg
RA of node: 186
8745 deg
Eccentricity:
0001415
Arg of perigee: 356
6128 deg
Mean anomaly: 3
5028 deg
Mean motion: 15
78128864 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 128
Checksum: 282
Coasting Arc #8 (Orbit 143)
---------------------------------------
Vector Time (GMT): 2007/362/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6440520
91 A = 6719365
63 meter
Y = 1238098
64 meter E =
0007358
Z = -1450482
03 I = 51
64692
XDOT = -2181
145999 Wp = 135
51525
YDOT = 4566
769761 meter/sec RA = 180
80310 deg
ZDOT = -5809
602198 TA = 60
46871
MA = 60
39538
Ha = 183
763 n
mi
Hp = 177
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21130317
95 X = 6433243
72
Y = 4062003
41 feet Y = 1310079
65 meter
Z = -4758799
31 Z = -1419211
94
XDOT = -7155
990809 XDOT = -2203
828579
YDOT = 14982
840423 feet/sec YDOT = 4542
252688 meter/sec
ZDOT = -19060
374664 ZDOT = -5820
252720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 935531
80 X = 285150
09
Y = 21522964
50 feet Y = 6560199
58 meter
Z = -4639305
86 Z = -1414060
43
XDOT = -14636
316214 XDOT = -4461
149182
YDOT = -3464
389123 feet/sec YDOT = -1055
945805 meter/sec
ZDOT = -19100
518831 ZDOT = -5821
838140
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 07362
54979012
00020000 00000-0 20000-3 0 9071
2 25544 51
6347 181
6387 0001663 359
8239
2926 15
78203660 1443
Satellite: ISS
Catalog Number: 25544
Epoch time: 07362
54979012 = yrday
fracday
Element set: 907
Inclination: 51
6347 deg
RA of node: 181
6387 deg
Eccentricity:
0001663
Arg of perigee: 359
8239 deg
Mean anomaly:
2926 deg
Mean motion: 15
78203660 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 144
Checksum: 296
Coasting Arc #9 (Orbit 155)
---------------------------------------
Vector Time (GMT): 2007/363/07:07:25
377
Vector Time (MET): N/A
Weight (LBS) : 538460
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1803723
46 A = 6715605
95 meter
Y = 4082183
20 meter E =
0003772
Z = -5021105
22 I = 51
63961
XDOT = -7410
644398 Wp = 78
64807
YDOT = -1029
781638 meter/sec RA = 176
76892 deg
ZDOT = 1826
778024 TA = 208
94901
MA = 208
96994
Ha = 186
415 n
mi
Hp = 183
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5917727
87 X = -1824845
63
Y = 13392989
49 feet Y = 4061895
26 meter
Z = -16473442
31 Z = -5029918
57
XDOT = -24313
137790 XDOT = -7407
452513
YDOT = -3378
548681 feet/sec YDOT = -1112
633979 meter/sec
ZDOT = 5993
366220 ZDOT = 1790
785155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6696
44 X = 2041
07
Y = -14604695
78 feet Y = -4451511
27 meter
Z = -16506628
62 Z = -5031220
40
XDOT = 22612
091053 XDOT = 6892
165353
YDOT = -6601
122535 feet/sec YDOT = -2012
022149 meter/sec
ZDOT = 5855
860424 ZDOT = 1784
866257
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 07363
30964303
00020000 00000-0 20000-3 0 9084
2 25544 51
6390 177
7161 0010122 292
5504 67
4589 15
75946071 1565
Satellite: ISS
Catalog Number: 25544
Epoch time: 07363
30964303 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 177
7161 deg
Eccentricity:
0010122
Arg of perigee: 292
5504 deg
Mean anomaly: 67
4589 deg
Mean motion: 15
75946071 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 156
Checksum: 291
Coasting Arc #10 (Orbit 171)
---------------------------------------
Vector Time (GMT): 2007/364/07:07:25
377
Vector Time (MET): N/A
Weight (LBS) : 538460
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6290044
27 A = 6724582
52 meter
Y = 847434
28 meter E =
0005055
Z = -2217439
03 I = 51
69879
XDOT = -2577
002032 Wp = 268
69372
YDOT = 4754
292708 meter/sec RA = 171
65550 deg
ZDOT = -5482
459569 TA = 296
15890
MA = 296
21089
Ha = 186
652 n
mi
Hp = 183
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20636628
19 X = 6290872
49
Y = 2780296
21 feet Y = 917777
93 meter
Z = -7275062
42 Z = -2186880
12
XDOT = -8454
731077 XDOT = -2603
341115
YDOT = 15598
073189 feet/sec YDOT = 4725
328368 meter/sec
ZDOT = -17987
072076 ZDOT = -5495
042166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19972487
51 X = -6087614
19
Y = 6032025
72 feet Y = 1838561
44 meter
Z = -7158310
66 Z = -2181853
09
XDOT = 1583
612057 XDOT = 482
684955
YDOT = -16200
397902 feet/sec YDOT = -4937
881280 meter/sec
ZDOT = -18034
573966 ZDOT = -5496
938145
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 07364
32421726
00020000 00000-0 20000-3 0 9095
2 25544 51
6392 172
4907 0010217 295
8361 64
1749 15
75942084 1729
Satellite: ISS
Catalog Number: 25544
Epoch time: 07364
32421726 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 172
4907 deg
Eccentricity:
0010217
Arg of perigee: 295
8361 deg
Mean anomaly: 64
1749 deg
Mean motion: 15
75942084 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 172
Checksum: 296
Coasting Arc #11 (Orbit 187)
---------------------------------------
Vector Time (GMT): 2007/365/07:07:25
377
Vector Time (MET): N/A
Weight (LBS) : 538460
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2671364
28 A = 6717641
48 meter
Y = -4262827
40 meter E =
0008784
Z = 4457013
47 I = 51
70521
XDOT = 6924
032160 Wp = 356
70449
YDOT = 955
119091 meter/sec RA = 166
46574 deg
ZDOT = -3228
202594 TA = 125
62954
MA = 125
54770
Ha = 186
789 n
mi
Hp = 182
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8764318
50 X = 2697182
03
Y = -13985654
19 feet Y = -4232810
69 meter
Z = 14622747
61 Z = 4470053
29
XDOT = 22716
640945 XDOT = 6928
519238
YDOT = 3133
592817 feet/sec YDOT = 1032
572900 meter/sec
ZDOT = -10591
215859 ZDOT = -3194
554772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1829436
36 X = -557612
20
Y = 16359111
45 feet Y = 4986257
17 meter
Z = 14672054
56 Z = 4472042
23
XDOT = -20719
744062 XDOT = -6315
377990
YDOT = 7090
910289 feet/sec YDOT = 2161
309456 meter/sec
ZDOT = -10462
651274 ZDOT = -3189
016108
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 07365
33876588
00020000 00000-0 20000-3 0 9109
2 25544 51
6392 167
2646 0010360 301
1950 58
8199 15
76050657 1888
Satellite: ISS
Catalog Number: 25544
Epoch time: 07365
33876588 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 167
2646 deg
Eccentricity:
0010360
Arg of perigee: 301
1950 deg
Mean anomaly: 58
8199 deg
Mean motion: 15
76050657 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 188
Checksum: 309
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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