Date:
May 15th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7211 82 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 2290)
---------------------------------------
Vector Time (GMT): 2008/133/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5073551
13 A = 6723550
93 meter
Y = -3734860
60 meter E =
0011154
Z = 2341638
10 I = 51
54281
XDOT = 4652
733845 Wp = 97
51522
YDOT = -2920
881851 meter/sec RA = 199
18881 deg
ZDOT = 5398
865785 TA = 288
90263
MA = 289
02351
Ha = 187
081 n
mi
Hp = 180
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16645508
97 X = -5042785
52
Y = -12253479
64 feet Y = -3791424
09 meter
Z = 7682539
71 Z = 2317065
25
XDOT = 15264
874821 XDOT = 4658
823072
YDOT = -9582
945704 feet/sec YDOT = -2868
818639 meter/sec
ZDOT = 17712
814255 ZDOT = 5421
483375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18526587
25 X = -5646903
80
Y = 9243038
66 feet Y = 2817278
18 meter
Z = 7587749
97 Z = 2312746
19
XDOT = -918
443428 XDOT = -279
941557
YDOT = -16516
284725 feet/sec YDOT = -5034
163584 meter/sec
ZDOT = 17799
381212 ZDOT = 5425
251393
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 08133
59461143
00020000 00000-0 20000-3 0 9007
2 25544 51
6382 199
8566 0005975 202
9754 157
1144 15
76217597 22913
Satellite: ISS
Catalog Number: 25544
Epoch time: 08133
59461143 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 199
8566 deg
Eccentricity:
0005975
Arg of perigee: 202
9754 deg
Mean anomaly: 157
1144 deg
Mean motion: 15
76217597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2291
Checksum: 312
Coasting Arc #2 (Orbit 2305)
---------------------------------------
Vector Time (GMT): 2008/134/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4558540
57 A = 6717522
36 meter
Y = 2400187
40 meter E =
0010236
Z = -4320892
61 I = 51
55159
XDOT = -5468
366082 Wp = 145
99717
YDOT = -4179
145586 meter/sec RA = 193
98424 deg
ZDOT = 3443
251268 TA = 158
86488
MA = 158
82256
Ha = 186
838 n
mi
Hp = 180
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14955841
76 X = -4564050
85
Y = 7874630
57 feet Y = 2349180
61 meter
Z = -14176156
86 Z = -4343051
34
XDOT = -17940
833601 XDOT = -5437
954553
YDOT = -13711
107567 feet/sec YDOT = -4240
126129 meter/sec
ZDOT = 11296
756130 ZDOT = 3416
759492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 494543
44 X = 150736
84
Y = 16823469
10 feet Y = 5127793
38 meter
Z = -14261021
95 Z = -4346759
49
XDOT = -19027
008169 XDOT = -5799
432090
YDOT = 10061
005403 feet/sec YDOT = 3066
594447 meter/sec
ZDOT = 11194
538315 ZDOT = 3412
095278
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 08134
54559705
00020000 00000-0 20000-3 0 9016
2 25544 51
6385 194
9563 0005886 206
6957 153
3905 15
76262127 23065
Satellite: ISS
Catalog Number: 25544
Epoch time: 08134
54559705 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 194
9563 deg
Eccentricity:
0005886
Arg of perigee: 206
6957 deg
Mean anomaly: 153
3905 deg
Mean motion: 15
76262127 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2306
Checksum: 313
Coasting Arc #3 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2008/135/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4388581
65 A = 6720076
52 meter
Y = 3583738
38 meter E =
0004892
Z = -3611596
25 I = 51
58957
XDOT = -5755
528144 Wp = 150
35701
YDOT = 2627
011378 meter/sec RA = 188
87708 deg
ZDOT = -4393
705026 TA = 72
95477
MA = 72
90117
Ha = 186
738 n
mi
Hp = 181
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14398233
76 X = 4365726
18
Y = 11757671
86 feet Y = 3632686
40 meter
Z = -11849069
08 Z = -3590331
70
XDOT = -18882
966352 XDOT = -5763
132037
YDOT = 8618
803735 feet/sec YDOT = 2562
607463 meter/sec
ZDOT = -14415
042736 ZDOT = -4421
683952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16801483
00 X = 5121092
02
Y = -8074684
68 feet Y = -2461163
89 meter
Z = -11766990
15 Z = -3586578
60
XDOT = -804
900129 XDOT = -245
333559
YDOT = 19455
756208 feet/sec YDOT = 5930
114492 meter/sec
ZDOT = -14522
248236 ZDOT = -4426
381262
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 08135
55996861
00020000 00000-0 20000-3 0 9027
2 25544 51
6393 189
7293 0005829 210
3157 149
7671 15
76282829 23225
Satellite: ISS
Catalog Number: 25544
Epoch time: 08135
55996861 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 189
7293 deg
Eccentricity:
0005829
Arg of perigee: 210
3157 deg
Mean anomaly: 149
7671 deg
Mean motion: 15
76282829 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2322
Checksum: 324
Coasting Arc #4 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2008/136/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5426134
95 A = 6720861
38 meter
Y = -2238872
41 meter E =
0010717
Z = 3259693
20 I = 51
62103
XDOT = 4526
373688 Wp = 118
42786
YDOT = 4054
595340 meter/sec RA = 183
67051 deg
ZDOT = -4743
105393 TA = 23
30648
MA = 23
25793
Ha = 186
359 n
mi
Hp = 181
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17802280
03 X = 5434931
89
Y = -7345381
92 feet Y = -2178145
25 meter
Z = 10694531
50 Z = 3286074
95
XDOT = 14850
307374 XDOT = 4503
739592
YDOT = 13302
478150 feet/sec YDOT = 4105
085535 meter/sec
ZDOT = -15561
369401 ZDOT = -4721
170759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 586437
28 X = 178746
08
Y = -19192677
06 feet Y = -5849927
97 meter
Z = 10795649
69 Z = 3290514
03
XDOT = 16863
415460 XDOT = 5139
969032
YDOT = -8202
465595 feet/sec YDOT = -2500
111513 meter/sec
ZDOT = -15476
661522 ZDOT = -4717
286432
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 08136
57432518
00020000 00000-0 20000-3 0 9035
2 25544 51
6383 184
5025 0005724 215
1280 144
9508 15
76319219 23381
Satellite: ISS
Catalog Number: 25544
Epoch time: 08136
57432518 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 184
5025 deg
Eccentricity:
0005724
Arg of perigee: 215
1280 deg
Mean anomaly: 144
9508 deg
Mean motion: 15
76319219 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2338
Checksum: 288
Coasting Arc #5 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2008/137/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3430816
91 A = 6716569
48 meter
Y = -3531592
73 meter E =
0009126
Z = 4568545
72 I = 51
63505
XDOT = 6624
574548 Wp = 151
58198
YDOT = -2541
455764 meter/sec RA = 178
56442 deg
ZDOT = 2999
884714 TA = 268
58625
MA = 268
69080
Ha = 186
396 n
mi
Hp = 181
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11255960
99 X = -3413264
63
Y = -11586590
33 feet Y = -3569860
25 meter
Z = 14988667
06 Z = 4551920
94
XDOT = 21734
168465 XDOT = 6637
928011
YDOT = -8338
109461 feet/sec YDOT = -2467
301515 meter/sec
ZDOT = 9842
141450 ZDOT = 3032
099700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15123001
23 X = -4609490
78
Y = 5844875
94 feet Y = 1781518
19 meter
Z = 14924413
98 Z = 4548961
38
XDOT = 1324
681218 XDOT = 403
762835
YDOT = -22105
929610 feet/sec YDOT = -6737
887345 meter/sec
ZDOT = 9965
648204 ZDOT = 3037
529573
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 08137
58866925
00020000 00000-0 20000-3 0 9041
2 25544 51
6378 179
2749 0005624 217
8268 142
2501 15
76317638 23548
Satellite: ISS
Catalog Number: 25544
Epoch time: 08137
58866925 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 179
2749 deg
Eccentricity:
0005624
Arg of perigee: 217
8268 deg
Mean anomaly: 142
2501 deg
Mean motion: 15
76317638 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2354
Checksum: 321
Coasting Arc #6 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2008/138/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6054552
78 A = 6723775
83 meter
Y = 2217810
97 meter E =
0001310
Z = -1904049
88 I = 51
69027
XDOT = -3273
625602 Wp = 29
80080
YDOT = -4101
440196 meter/sec RA = 173
37289 deg
ZDOT = 5635
034152 TA = 309
04238
MA = 309
05403
Ha = 186
119 n
mi
Hp = 181
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19864018
31 X = -6069652
99
Y = 7276282
70 feet Y = 2150021
23 meter
Z = -6246882
82 Z = -1933499
96
XDOT = -10740
241477 XDOT = -3254
893852
YDOT = -13456
168621 feet/sec YDOT = -4137
943498 meter/sec
ZDOT = 18487
644856 ZDOT = 5619
175721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -780761
40 X = -237976
07
Y = 21106640
42 feet Y = 6433304
00 meter
Z = -6359811
33 Z = -1938470
49
XDOT = -15023
321943 XDOT = -4579
108528
YDOT = 4993
751501 feet/sec YDOT = 1522
095457 meter/sec
ZDOT = 18426
274881 ZDOT = 5616
328584
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 08138
53960340
00020000 00000-0 20000-3 0 9054
2 25544 51
6386 174
3748 0005668 221
3869 138
6866 15
76377469 23694
Satellite: ISS
Catalog Number: 25544
Epoch time: 08138
53960340 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 174
3748 deg
Eccentricity:
0005668
Arg of perigee: 221
3869 deg
Mean anomaly: 138
6866 deg
Mean motion: 15
76377469 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2369
Checksum: 340
Coasting Arc #7 (Orbit 2384)
---------------------------------------
Vector Time (GMT): 2008/139/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2240112
29 A = 6713999
81 meter
Y = 3690604
59 meter E =
0009888
Z = -5150004
93 I = 51
68505
XDOT = -7151
851523 Wp = 98
30982
YDOT = 2534
853694 meter/sec RA = 168
25156 deg
ZDOT = -1297
844341 TA = 159
30192
MA = 159
26184
Ha = 185
973 n
mi
Hp = 181
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7349449
76 X = 2223695
18
Y = 12108282
78 feet Y = 3715563
57 meter
Z = -16896341
63 Z = -5139161
72
XDOT = -23464
079799 XDOT = -7173
360288
YDOT = 8316
449127 feet/sec YDOT = 2454
757477 meter/sec
ZDOT = -4258
019492 ZDOT = -1332
640724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13985014
90 X = 4262632
54
Y = -2542371
59 feet Y = -774914
86 meter
Z = -16854286
97 Z = -5137186
67
XDOT = -944
649228 XDOT = -287
929085
YDOT = 23839
713806 feet/sec YDOT = 7266
344768 meter/sec
ZDOT = -4391
472550 ZDOT = -1338
520833
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 08139
55391982
00020000 00000-0 20000-3 0 9068
2 25544 51
6379 169
1472 0005653 226
8615 133
2077 15
76350361 23850
Satellite: ISS
Catalog Number: 25544
Epoch time: 08139
55391982 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 169
1472 deg
Eccentricity:
0005653
Arg of perigee: 226
8615 deg
Mean anomaly: 133
2077 deg
Mean motion: 15
76350361 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2385
Checksum: 310
Coasting Arc #8 (Orbit 2400)
---------------------------------------
Vector Time (GMT): 2008/140/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6337235
08 A = 6725367
68 meter
Y = -2201529
31 meter E =
0013239
Z = 333469
49 I = 51
75069
XDOT = 1854
938751 Wp = 155
81875
YDOT = 4413
577324 meter/sec RA = 163
08867 deg
ZDOT = -6041
102344 TA = 20
55680
MA = 20
50358
Ha = 185
776 n
mi
Hp = 181
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20791453
69 X = 6359761
96
Y = -7222865
18 feet Y = -2130536
81 meter
Z = 1094060
00 Z = 364310
83
XDOT = 6085
757057 XDOT = 1834
794740
YDOT = 14480
240565 feet/sec YDOT = 4434
208453 meter/sec
ZDOT = -19819
889581 ZDOT = -6032
139236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 436276
19 X = 132976
98
Y = -21999798
45 feet Y = -6705538
57 meter
Z = 1212363
98 Z = 369528
54
XDOT = 14126
988236 XDOT = 4305
906014
YDOT = -821
921097 feet/sec YDOT = -250
521550 meter/sec
ZDOT = -19784
986297 ZDOT = -6030
463823
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 08140
56822285
00020000 00000-0 20000-3 0 9077
2 25544 51
6365 163
9193 0005509 230
3851 129
6828 15
76377158 24014
Satellite: ISS
Catalog Number: 25544
Epoch time: 08140
56822285 = yrday
fracday
Element set: 907
Inclination: 51
6365 deg
RA of node: 163
9193 deg
Eccentricity:
0005509
Arg of perigee: 230
3851 deg
Mean anomaly: 129
6828 deg
Mean motion: 15
76377158 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2401
Checksum: 303
Coasting Arc #9 (Orbit 2416)
---------------------------------------
Vector Time (GMT): 2008/141/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -998547
67 A = 6713339
08 meter
Y = -4063907
17 meter E =
0002923
Z = 5250993
77 I = 51
73732
XDOT = 7272
058089 Wp = 223
78873
YDOT = -2485
051613 meter/sec RA = 157
94096 deg
ZDOT = -542
627101 TA = 231
34477
MA = 231
37092
Ha = 185
581 n
mi
Hp = 181
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3276075
03 X = -978539
04
Y = -13333028
76 feet Y = -4074962
39 meter
Z = 17227669
85 Z = 5246190
75
XDOT = 23858
458296 XDOT = 7301
941879
YDOT = -8153
056474 feet/sec YDOT = -2403
564133 meter/sec
ZDOT = -1780
272640 ZDOT = -507
226572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13698564
11 X = -4175322
34
Y = -1225433
85 feet Y = -373512
24 meter
Z = 17208793
83 Z = 5245240
36
XDOT = 110
314526 XDOT = 33
623868
YDOT = -24222
576225 feet/sec YDOT = -7383
041233 meter/sec
ZDOT = -1644
457299 ZDOT = -501
230585
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 08141
58251144
00020000 00000-0 20000-3 0 9081
2 25544 51
6358 158
6911 0005518 235
6015 124
4629 15
76403892 24179
Satellite: ISS
Catalog Number: 25544
Epoch time: 08141
58251144 = yrday
fracday
Element set: 908
Inclination: 51
6358 deg
RA of node: 158
6911 deg
Eccentricity:
0005518
Arg of perigee: 235
6015 deg
Mean anomaly: 124
4629 deg
Mean motion: 15
76403892 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2417
Checksum: 292
Coasting Arc #10 (Orbit 2432)
---------------------------------------
Vector Time (GMT): 2008/142/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6259966
27 A = 6724503
27 meter
Y = 2083794
86 meter E =
0008309
Z = 1279154
86 I = 51
80212
XDOT = -447
859891 Wp = 58
82644
YDOT = -4965
167057 meter/sec RA = 152
81351 deg
ZDOT = 5873
019214 TA = 315
18961
MA = 315
25669
Ha = 185
307 n
mi
Hp = 181
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20537947
07 X = -6289016
33
Y = 6836597
31 feet Y = 2013629
71 meter
Z = 4196702
30 Z = 1248673
26
XDOT = -1469
356598 XDOT = -420
835814
YDOT = -16289
918165 feet/sec YDOT = -4970
025119 meter/sec
ZDOT = 19268
435743 ZDOT = 5870
908330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 24310
74 X = 7409
91
Y = 21668267
22 feet Y = 6604487
85 meter
Z = 4079736
21 Z = 1243503
60
XDOT = -14379
976967 XDOT = -4383
016980
YDOT = -3625
188372 feet/sec YDOT = -1104
957416 meter/sec
ZDOT = 19259
819815 ZDOT = 5870
393080
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 08142
59678504
00020000 00000-0 20000-3 0 9097
2 25544 51
6358 153
4638 0005637 239
1227 120
9384 15
76465542 24331
Satellite: ISS
Catalog Number: 25544
Epoch time: 08142
59678504 = yrday
fracday
Element set: 909
Inclination: 51
6358 deg
RA of node: 153
4638 deg
Eccentricity:
0005637
Arg of perigee: 239
1227 deg
Mean anomaly: 120
9384 deg
Mean motion: 15
76465542 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2433
Checksum: 310
Coasting Arc #11 (Orbit 2447)
---------------------------------------
Vector Time (GMT): 2008/143/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -178012
24 A = 6715013
15 meter
Y = 4639991
85 meter E =
0008945
Z = -4858670
52 I = 51
79488
XDOT = -6981
059651 Wp = 131
65709
YDOT = 2216
118357 meter/sec RA = 147
63932 deg
ZDOT = 2369
109782 TA = 161
41629
MA = 161
38360
Ha = 185
120 n
mi
Hp = 181
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -584029
66 X = -206281
33
Y = 15223070
36 feet Y = 4637843
96 meter
Z = -15940520
07 Z = -4859603
20
XDOT = -22903
739011 XDOT = -7016
830617
YDOT = 7270
729519 feet/sec YDOT = 2137
851756 meter/sec
ZDOT = 7772
669887 ZDOT = 2335
108893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14383984
71 X = 4384238
54
Y = 5008434
84 feet Y = 1526570
94 meter
Z = -15943641
56 Z = -4859621
95
XDOT = 465
429772 XDOT = 141
862995
YDOT = 23022
795453 feet/sec YDOT = 7017
348054 meter/sec
ZDOT = 7642
169803 ZDOT = 2329
333356
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 08143
54765723
00020000 00000-0 20000-3 0 9105
2 25544 51
6354 148
5621 0005503 244
7980 115
2614 15
76419144 24480
Satellite: ISS
Catalog Number: 25544
Epoch time: 08143
54765723 = yrday
fracday
Element set: 910
Inclination: 51
6354 deg
RA of node: 148
5621 deg
Eccentricity:
0005503
Arg of perigee: 244
7980 deg
Mean anomaly: 115
2614 deg
Mean motion: 15
76419144 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2448
Checksum: 287
Coasting Arc #12 (Orbit 2463)
---------------------------------------
Vector Time (GMT): 2008/144/12:51:32
855
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5859082
87 A = 6721816
97 meter
Y = -1706521
90 meter E =
0004453
Z = -2811363
23 I = 51
84197
XDOT = -802
045569 Wp = 192
92332
YDOT = 5691
854572 meter/sec RA = 142
53946 deg
ZDOT = -5129
224568 TA = 19
22629
MA = 19
20949
Ha = 185
003 n
mi
Hp = 181
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19222712
82 X = 5891387
19
Y = -5598825
14 feet Y = -1640821
20 meter
Z = -9223632
65 Z = -2782821
41
XDOT = -2631
383099 XDOT = -840
716149
YDOT = 18674
063558 feet/sec YDOT = 5682
670275 meter/sec
ZDOT = -16828
164593 ZDOT = -5133
213919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 55710
63 X = 16980
60
Y = -20071517
88 feet Y = -6117798
65 meter
Z = -9114054
91 Z = -2777963
94
XDOT = 15740
576826 XDOT = 4797
727816
YDOT = 7687
645328 feet/sec YDOT = 2343
194296 meter/sec
ZDOT = -16842
938189 ZDOT = -5133
727560
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 08144
56190601
00020000 00000-0 20000-3 0 9116
2 25544 51
6352 143
3336 0005422 248
8352 111
2233 15
76460678 24641
Satellite: ISS
Catalog Number: 25544
Epoch time: 08144
56190601 = yrday
fracday
Element set: 911
Inclination: 51
6352 deg
RA of node: 143
3336 deg
Eccentricity:
0005422
Arg of perigee: 248
8352 deg
Mean anomaly: 111
2233 deg
Mean motion: 15
76460678 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2464
Checksum: 269
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 normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! 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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