[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 30th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 66 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
091/21:57:23
851 -1
3 3
1 3
1
N/A -1
1 -0
4 214
2
000/00:06:47
703 2
6 -0
0 207
7
096/19:03:28
240 -0
2 6
6 6
6
N/A -4
7 -0
7 212
5
000/00:14:56
480 4
7 -0
4 212
1
Coasting Arc #1 (Orbit 551)
---------------------------------------
Vector Time (GMT): 2012/088/23:24:12
316
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6082647
36 A = 6769636
20 meter
Y = -559720
89 meter E =
0012383
Z = 2928107
03 I = 51
74617
XDOT = 2889
645918 Wp = 154
01978
YDOT = -5021
616933 meter/sec RA = 163
05074 deg
ZDOT = 5023
930253 TA = 239
37883
MA = 239
50100
Ha = 214
995 n
mi
Hp = 205
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19956192
14 X = -6090160
49
Y = -1836354
64 feet Y = -627782
64 meter
Z = 9606650
36 Z = 2898539
51
XDOT = 9480
465611 XDOT = 2921
178702
YDOT = -16475
121172 feet/sec YDOT = -4989
126509 meter/sec
ZDOT = 16482
710803 ZDOT = 5038
044959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19892025
93 X = 6063089
50
Y = 2871578
27 feet Y = 875257
06 meter
Z = 9485297
94 Z = 2891118
81
XDOT = -10012
686180 XDOT = -3051
866748
YDOT = 14514
866977 feet/sec YDOT = 4424
131454 meter/sec
ZDOT = 16540
950964 ZDOT = 5041
681854
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 12089
03333321
00016717 00000-0 10270-3 0 9005
2 25544 51
6403 163
7962 0015175 210
6159 149
4112 15
59694724 5524
Satellite: ISS
Catalog Number: 25544
Epoch time: 12089
03333321 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 163
7962 deg
Eccentricity:
0015175
Arg of perigee: 210
6159 deg
Mean anomaly: 149
4112 deg
Mean motion: 15
59694724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 552
Checksum: 293
Coasting Arc #2 (Orbit 566)
---------------------------------------
Vector Time (GMT): 2012/089/23:24:12
316
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3394851
62 A = 6762155
45 meter
Y = 2932195
32 meter E =
0010204
Z = -5061030
61 I = 51
75126
XDOT = -6240
444742 Wp = 156
09395
YDOT = 4077
505952 meter/sec RA = 158
02248 deg
ZDOT = -1834
014874 TA = 96
25360
MA = 96
13736
Ha = 214
702 n
mi
Hp = 205
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11137964
62 X = 3386396
25
Y = 9620063
39 feet Y = 2970111
08 meter
Z = -16604431
12 Z = -5044559
28
XDOT = -20473
900073 XDOT = -6276
667201
YDOT = 13377
644199 feet/sec YDOT = 4007
518804 meter/sec
ZDOT = -6017
109167 ZDOT = -1864
418892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10898232
90 X = -3321781
39
Y = -10003196
62 feet Y = -3048974
33 meter
Z = -16536976
30 Z = -5040470
38
XDOT = 20159
251155 XDOT = 6144
539752
YDOT = -11865
600565 feet/sec YDOT = -3616
635052 meter/sec
ZDOT = -6142
184773 ZDOT = -1872
137919
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 12089
99440138
00016717 00000-0 10270-3 0 9016
2 25544 51
6409 158
9643 0015102 214
4645 145
5532 15
59757609 5675
Satellite: ISS
Catalog Number: 25544
Epoch time: 12089
99440138 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 158
9643 deg
Eccentricity:
0015102
Arg of perigee: 214
4645 deg
Mean anomaly: 145
5532 deg
Mean motion: 15
59757609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 567
Checksum: 325
Coasting Arc #3 (Orbit 582)
---------------------------------------
Vector Time (GMT): 2012/090/23:24:12
316
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 375991
49 A = 6762340
00 meter
Y = -4579042
62 meter E =
0009428
Z = 4962841
89 I = 51
78039
XDOT = 7157
718211 Wp = 207
34522
YDOT = -1742
203921 meter/sec RA = 152
97301 deg
ZDOT = -2159
552020 TA = 263
58251
MA = 263
68989
Ha = 214
344 n
mi
Hp = 205
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1233567
89 X = 403059
03
Y = -15023105
72 feet Y = -4574686
41 meter
Z = 16282289
67 Z = 4964734
46
XDOT = 23483
327463 XDOT = 7187
158496
YDOT = -5715
892129 feet/sec YDOT = -1661
997415 meter/sec
ZDOT = -7085
144423 ZDOT = -2124
708630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1397189
06 X = -425863
23
Y = 15000040
08 feet Y = 4572012
22 meter
Z = 16290334
94 Z = 4965294
09
XDOT = -22528
529673 XDOT = -6866
695844
YDOT = 5405
761228 feet/sec YDOT = 1647
676022 meter/sec
ZDOT = -6941
962467 ZDOT = -2115
910160
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 12091
01951930
00016717 00000-0 10270-3 0 9020
2 25544 51
6408 153
8105 0015107 218
8895 141
1175 15
59805404 5831
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
01951930 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 153
8105 deg
Eccentricity:
0015107
Arg of perigee: 218
8895 deg
Mean anomaly: 141
1175 deg
Mean motion: 15
59805404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 583
Checksum: 295
Coasting Arc #4 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2012/091/22:00:47
703
Vector Time (MET): N/A
Weight (LBS) : 925057
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5917869
43 A = 6774516
96 meter
Y = 3271043
87 meter E =
0000814
Z = 420624
38 I = 51
84091
XDOT = -1970
140039 Wp = 244
38623
YDOT = -4336
325576 meter/sec RA = 148
26708 deg
ZDOT = 6012
342087 TA = 120
14260
MA = 120
13453
Ha = 214
155 n
mi
Hp = 207
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19415582
12 X = -5956050
36
Y = 10731771
22 feet Y = 3204653
14 meter
Z = 1380001
26 Z = 391782
81
XDOT = -6463
714039 XDOT = -1950
710409
YDOT = -14226
789947 feet/sec YDOT = -4358
247843 meter/sec
ZDOT = 19725
531783 ZDOT = 6002
818778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21975501
94 X = 6698132
99
Y = -3086491
75 feet Y = -940762
68 meter
Z = 1261359
99 Z = 384462
52
XDOT = 843
223772 XDOT = 257
014606
YDOT = 14036
287472 feet/sec YDOT = 4278
260422 meter/sec
ZDOT = 19686
683036 ZDOT = 6000
500989
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 12091
98057351
00016717 00000-0 10270-3 0 9031
2 25544 51
6412 148
9776 0013608 230
2806 129
7150 15
59214615 5988
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
98057351 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 148
9776 deg
Eccentricity:
0013608
Arg of perigee: 230
2806 deg
Mean anomaly: 129
7150 deg
Mean motion: 15
59214615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 598
Checksum: 313
Coasting Arc #5 (Orbit 612)
---------------------------------------
Vector Time (GMT): 2012/092/22:00:47
703
Vector Time (MET): N/A
Weight (LBS) : 925057
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5714224
16 A = 6769263
03 meter
Y = -807571
79 meter E =
0009722
Z = -3525547
77 I = 51
84987
XDOT = -1957
096896 Wp = 218
24086
YDOT = 5891
939075 meter/sec RA = 143
27857 deg
ZDOT = -4522
515090 TA = 3
28269
MA = 3
27631
Ha = 213
963 n
mi
Hp = 207
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18747454
58 X = 5739956
11
Y = -2649513
76 feet Y = -743528
23 meter
Z = -11566757
79 Z = -3497725
92
XDOT = -6420
921575 XDOT = -2000
867058
YDOT = 19330
508775 feet/sec YDOT = 5869
808494 meter/sec
ZDOT = -14837
647934 ZDOT = -4532
129336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18593065
34 X = -5667166
32
Y = -3926368
64 feet Y = -1196757
16 meter
Z = -11452441
33 Z = -3490704
12
XDOT = 12257
096597 XDOT = 3735
963043
YDOT = -14655
907554 feet/sec YDOT = -4467
120622 meter/sec
ZDOT = -14877
491390 ZDOT = -4534
659376
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 12092
94193853
00016717 00000-0 10270-3 0 9047
2 25544 51
6421 144
1483 0013644 234
1181 125
8708 15
59253676 6134
Satellite: ISS
Catalog Number: 25544
Epoch time: 12092
94193853 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 144
1483 deg
Eccentricity:
0013644
Arg of perigee: 234
1181 deg
Mean anomaly: 125
8708 deg
Mean motion: 15
59253676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 613
Checksum: 305
Coasting Arc #6 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2012/093/22:00:47
703
Vector Time (MET): N/A
Weight (LBS) : 925057
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3735014
90 A = 6762853
65 meter
Y = -2158779
56 meter E =
0012545
Z = 5216891
00 I = 51
85253
XDOT = 4982
074023 Wp = 220
51199
YDOT = -5706
822940 meter/sec RA = 138
25432 deg
ZDOT = 1197
689718 TA = 217
99039
MA = 218
07894
Ha = 213
572 n
mi
Hp = 207
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12253985
89 X = -3735939
75
Y = -7082610
12 feet Y = -2200551
45 meter
Z = 17115784
13 Z = 5198744
53
XDOT = 16345
387215 XDOT = 5039
700512
YDOT = -18723
172376 feet/sec YDOT = -5650
787978 meter/sec
ZDOT = 3929
428209 ZDOT = 1222
032846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9387360
96 X = 2861267
62
Y = 10711788
67 feet Y = 3264953
19 meter
Z = 17041380
24 Z = 5194212
70
XDOT = -20736
765345 XDOT = -6320
566077
YDOT = 11721
552453 feet/sec YDOT = 3572
729188 meter/sec
ZDOT = 4029
763926 ZDOT = 1228
272045
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 12093
96737468
00016717 00000-0 10270-3 0 9057
2 25544 51
6419 138
9963 0013587 237
8407 122
1431 15
59296042 6296
Satellite: ISS
Catalog Number: 25544
Epoch time: 12093
96737468 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 138
9963 deg
Eccentricity:
0013587
Arg of perigee: 237
8407 deg
Mean anomaly: 122
1431 deg
Mean motion: 15
59296042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 337
Coasting Arc #7 (Orbit 643)
---------------------------------------
Vector Time (GMT): 2012/094/22:00:47
703
Vector Time (MET): N/A
Weight (LBS) : 925057
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 717166
67 A = 6764490
64 meter
Y = 4725476
18 meter E =
0010054
Z = -4789974
11 I = 51
88057
XDOT = -6233
631608 Wp = 186
81017
YDOT = 3621
595946 meter/sec RA = 133
21629 deg
ZDOT = 2629
211030 TA = 109
06171
MA = 108
95279
Ha = 213
168 n
mi
Hp = 207
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2352909
01 X = 687540
71
Y = 15503530
77 feet Y = 4733329
76 meter
Z = -15715138
14 Z = -4786562
67
XDOT = -20451
547270 XDOT = -6286
437818
YDOT = 11881
876463 feet/sec YDOT = 3551
592679 meter/sec
ZDOT = 8626
020441 ZDOT = 2598
799696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2453773
27 X = 747910
09
Y = -15501798
14 feet Y = -4724948
07 meter
Z = -15701416
02 Z = -4785791
60
XDOT = 22038
880318 XDOT = 6717
450721
YDOT = -5156
092107 feet/sec YDOT = -1571
576874 meter/sec
ZDOT = 8500
877222 ZDOT = 2591
067377
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 12094
92870205
00016717 00000-0 10270-3 0 9062
2 25544 51
6420 134
1661 0013583 241
9300 118
0482 15
59325968 6442
Satellite: ISS
Catalog Number: 25544
Epoch time: 12094
92870205 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 134
1661 deg
Eccentricity:
0013583
Arg of perigee: 241
9300 deg
Mean anomaly: 118
0482 deg
Mean motion: 15
59325968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 644
Checksum: 298
Coasting Arc #8 (Orbit 659)
---------------------------------------
Vector Time (GMT): 2012/095/22:00:47
703
Vector Time (MET): N/A
Weight (LBS) : 925057
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2242936
33 A = 6771727
37 meter
Y = -5908523
01 meter E =
0009406
Z = 2415430
69 I = 51
92461
XDOT = 5469
557494 Wp = 173
90276
YDOT = -123
552379 meter/sec RA = 128
20961 deg
ZDOT = -5388
387622 TA = 339
12779
MA = 339
16617
Ha = 212
881 n
mi
Hp = 208
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7358715
00 X = 2297106
28
Y = -19384918
03 feet Y = -5883137
92 meter
Z = 7924641
38 Z = 2426459
14
XDOT = 17944
742434 XDOT = 5496
708217
YDOT = -405
355574 feet/sec YDOT = -62
237287 meter/sec
ZDOT = -17678
437080 ZDOT = -5361
750724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12653837
99 X = -3856889
82
Y = 16403662
58 feet Y = 4999836
36 meter
Z = 7970314
45 Z = 2429351
84
XDOT = -16187
093242 XDOT = -4933
826020
YDOT = -3961
650488 feet/sec YDOT = -1207
511069 meter/sec
ZDOT = -17569
008408 ZDOT = -5355
033763
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 12095
95409859
00016717 00000-0 10270-3 0 9070
2 25544 51
6416 129
0145 0013471 245
4081 114
5671 15
59331098 6608
Satellite: ISS
Catalog Number: 25544
Epoch time: 12095
95409859 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 129
0145 deg
Eccentricity:
0013471
Arg of perigee: 245
4081 deg
Mean anomaly: 114
5671 deg
Mean motion: 15
59331098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 312
Coasting Arc #9 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2012/096/19:10:56
480
Vector Time (MET): N/A
Weight (LBS) : 924393
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4634166
54 A = 6767680
56 meter
Y = -34795
71 meter E =
0005438
Z = 4936572
06 I = 51
91423
XDOT = 2476
395489 Wp = 222
32955
YDOT = -6894
779131 meter/sec RA = 123
83348 deg
ZDOT = 2273
630242 TA = 205
53485
MA = 205
56172
Ha = 212
549 n
mi
Hp = 212
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15203958
47 X = -4657413
97
Y = -114159
16 feet Y = -86747
19 meter
Z = 16196102
56 Z = 4914002
86
XDOT = 8124
657117 XDOT = 2542
265383
YDOT = -22620
666441 feet/sec YDOT = -6866
717960 meter/sec
ZDOT = 7459
416805 ZDOT = 2285
821417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7880933
15 X = 2402108
42
Y = 13117119
70 feet Y = 3998098
09 meter
Z = 16103390
55 Z = 4908313
44
XDOT = -22558
452179 XDOT = -6875
816224
YDOT = 4323
744309 feet/sec YDOT = 1317
877265 meter/sec
ZDOT = 7509
938241 ZDOT = 2289
029176
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 12096
85135786
00016717 00000-0 10270-3 0 9086
2 25544 51
6413 124
5067 0009304 266
8307 93
1783 15
58054686 6741
Satellite: ISS
Catalog Number: 25544
Epoch time: 12096
85135786 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 124
5067 deg
Eccentricity:
0009304
Arg of perigee: 266
8307 deg
Mean anomaly: 93
1783 deg
Mean motion: 15
58054686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 331
Coasting Arc #10 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2012/097/19:10:56
480
Vector Time (MET): N/A
Weight (LBS) : 924393
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2997456
64 A = 6766280
77 meter
Y = 3065875
68 meter E =
0005277
Z = -5238864
10 I = 51
92614
XDOT = -4394
294248 Wp = 111
30930
YDOT = 6189
765351 meter/sec RA = 118
81141 deg
ZDOT = 1107
155147 TA = 169
26041
MA = 169
24914
Ha = 212
069 n
mi
Hp = 211
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9834175
34 X = 2988400
17
Y = 10058647
24 feet Y = 3099343
88 meter
Z = -17187874
33 Z = -5224324
74
XDOT = -14416
975879 XDOT = -4468
561239
YDOT = 20307
629104 feet/sec YDOT = 6140
210507 meter/sec
ZDOT = 3632
398775 ZDOT = 1085
626521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3164841
28 X = 964643
62
Y = -13780927
11 feet Y = -4200426
58 meter
Z = -17128346
11 Z = -5220719
89
XDOT = 23878
411149 XDOT = 7278
139718
YDOT = 1075
490195 feet/sec YDOT = 327
809412 meter/sec
ZDOT = 3543
549033 ZDOT = 1080
073745
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 12097
81345759
00016717 00000-0 10270-3 0 9097
2 25544 51
6415 119
6814 0009237 271
0788 88
9308 15
58070845 6890
Satellite: ISS
Catalog Number: 25544
Epoch time: 12097
81345759 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 119
6814 deg
Eccentricity:
0009237
Arg of perigee: 271
0788 deg
Mean anomaly: 88
9308 deg
Mean motion: 15
58070845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 351
Coasting Arc #11 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2012/098/19:10:56
480
Vector Time (MET): N/A
Weight (LBS) : 924393
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -898402
78 A = 6771459
39 meter
Y = -5479183
57 meter E =
0003170
Z = 3876359
65 I = 51
95706
XDOT = 5221
155219 Wp = 39
25103
YDOT = -3793
874536 meter/sec RA = 113
80153 deg
ZDOT = -4148
275184 TA = 94
12468
MA = 94
08845
Ha = 212
701 n
mi
Hp = 212
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2947515
68 X = -855897
44
Y = -17976324
03 feet Y = -5488992
08 meter
Z = 12717715
38 Z = 3872098
88
XDOT = 17129
774340 XDOT = 5283
342738
YDOT = -12447
094934 feet/sec YDOT = -3735
140983 meter/sec
ZDOT = -13609
826718 ZDOT = -4122
759289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13343278
16 X = -4067031
18
Y = 12418875
33 feet Y = 3785273
20 meter
Z = 12700583
55 Z = 3871137
87
XDOT = -18960
565638 XDOT = -5779
180406
YDOT = -6546
581815 feet/sec YDOT = -1995
398137 meter/sec
ZDOT = -13504
740664 ZDOT = -4116
244954
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 12098
83967779
00016717 00000-0 10270-3 0 9104
2 25544 51
6411 114
5350 0009186 274
9075 85
1031 15
58088229 7055
Satellite: ISS
Catalog Number: 25544
Epoch time: 12098
83967779 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 114
5350 deg
Eccentricity:
0009186
Arg of perigee: 274
9075 deg
Mean anomaly: 85
1031 deg
Mean motion: 15
58088229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 323
Coasting Arc #12 (Orbit 719)
---------------------------------------
Vector Time (GMT): 2012/099/19:10:56
480
Vector Time (MET): N/A
Weight (LBS) : 924393
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1185344
74 A = 6777028
21 meter
Y = 6544952
27 meter E =
0009266
Z = -1266004
92 I = 51
98821
XDOT = -4934
512052 Wp = 336
74480
YDOT = 243
942016 meter/sec RA = 108
82111 deg
ZDOT = 5874
956205 TA = 9
52689
MA = 9
50933
Ha = 213
084 n
mi
Hp = 211
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3888926
32 X = -1252293
57
Y = 21472940
50 feet Y = 6531322
61 meter
Z = -4153559
46 Z = -1271926
32
XDOT = -16189
344001 XDOT = -4965
412758
YDOT = 800
334699 feet/sec YDOT = 188
588785 meter/sec
ZDOT = 19274
790698 ZDOT = 5850
909135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19903522
54 X = 6066593
67
Y = -8936115
73 feet Y = -2723728
07 meter
Z = -4178349
47 Z = -1273560
92
XDOT = 9217
316942 XDOT = 2809
438204
YDOT = 11553
950507 feet/sec YDOT = 3521
644114 meter/sec
ZDOT = 19175
973953 ZDOT = 5844
836861
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 12099
80173997
00016717 00000-0 10270-3 0 9114
2 25544 51
6419 109
7090 0009274 278
6888 81
3216 15
58130941 7200
Satellite: ISS
Catalog Number: 25544
Epoch time: 12099
80173997 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 109
7090 deg
Eccentricity:
0009274
Arg of perigee: 278
6888 deg
Mean anomaly: 81
3216 deg
Mean motion: 15
58130941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 720
Checksum: 328
Coasting Arc #13 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2012/100/19:10:56
480
Vector Time (MET): N/A
Weight (LBS) : 924393
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2866439
18 A = 6776428
01 meter
Y = -5878596
30 meter E =
0006023
Z = -1759863
76 I = 51
99566
XDOT = 3723
740853 Wp = 228
00608
YDOT = 3526
984054 meter/sec RA = 103
85632 deg
ZDOT = -5707
709058 TA = 331
24828
MA = 331
28147
Ha = 213
282 n
mi
Hp = 211
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9404328
00 X = 2940510
91
Y = -19286733
26 feet Y = -5846127
89 meter
Z = -5773831
24 Z = -1745758
48
XDOT = 12216
997550 XDOT = 3711
751746
YDOT = 11571
469994 feet/sec YDOT = 3568
558035 meter/sec
ZDOT = -18726
079586 ZDOT = -5689
648292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21191554
80 X = -6459185
90
Y = 3465296
10 feet Y = 1056222
25 meter
Z = -5715445
76 Z = -1742067
87
XDOT = 2551
540615 XDOT = 777
709579
YDOT = -15206
805946 feet/sec YDOT = -4635
034452 meter/sec
ZDOT = -18652
126688 ZDOT = -5685
168215
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 12100
82792104
00016717 00000-0 10270-3 0 9127
2 25544 51
6426 104
5623 0009323 281
8377 78
1732 15
58130211 7361
Satellite: ISS
Catalog Number: 25544
Epoch time: 12100
82792104 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 104
5623 deg
Eccentricity:
0009323
Arg of perigee: 281
8377 deg
Mean anomaly: 78
1732 deg
Mean motion: 15
58130211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 282
Coasting Arc #14 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2012/101/19:10:56
480
Vector Time (MET): N/A
Weight (LBS) : 924393
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3901116
95 A = 6770059
61 meter
Y = 3571004
28 meter E =
0000969
Z = 4225670
85 I = 51
98143
XDOT = -1910
876980 Wp = 94
13580
YDOT = -6452
417311 meter/sec RA = 98
87244 deg
ZDOT = 3687
865432 TA = 318
26908
MA = 318
27647
Ha = 213
641 n
mi
Hp = 211
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12798940
13 X = -3961286
22
Y = 11715893
31 feet Y = 3527043
21 meter
Z = 13863749
50 Z = 4206573
05
XDOT = -6269
281431 XDOT = -1856
497680
YDOT = -21169
348132 feet/sec YDOT = -6473
481818 meter/sec
ZDOT = 12099
296037 ZDOT = 3678
714578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17072716
93 X = 5203764
12
Y = 3431407
98 feet Y = 1045893
15 meter
Z = 13785004
57 Z = 4201669
39
XDOT = -13039
785666 XDOT = -3974
526671
YDOT = 16410
567885 feet/sec YDOT = 5001
941091 meter/sec
ZDOT = 12062
176553 ZDOT = 3676
551413
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 12101
85408160
00016717 00000-0 10270-3 0 9138
2 25544 51
6429 99
4149 0009234 286
8871 73
1271 15
58177501 7528
Satellite: ISS
Catalog Number: 25544
Epoch time: 12101
85408160 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 99
4149 deg
Eccentricity:
0009234
Arg of perigee: 286
8871 deg
Mean anomaly: 73
1271 deg
Mean motion: 15
58177501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 310
Coasting Arc #15 (Orbit 766)
---------------------------------------
Vector Time (GMT): 2012/102/19:10:56
480
Vector Time (MET): N/A
Weight (LBS) : 924393
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4183893
12 A = 6765471
62 meter
Y = -240851
27 meter E =
0007326
Z = -5316622
69 I = 51
97063
XDOT = -153
045956 Wp = 55
15869
YDOT = 7655
335518 meter/sec RA = 93
85960 deg
ZDOT = -463
611837 TA = 210
41956
MA = 210
46209
Ha = 213
721 n
mi
Hp = 211
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13726683
45 X = 4212102
45
Y = -790194
47 feet Y = -193906
73 meter
Z = -17442987
84 Z = -5296228
94
XDOT = -502
119278 XDOT = -236
385963
YDOT = 25115
930177 feet/sec YDOT = 7653
158078 meter/sec
ZDOT = -1521
036211 ZDOT = -464
557851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9018257
98 X = -2748765
03
Y = -10518301
08 feet Y = -3205978
17 meter
Z = -17359160
01 Z = -5291071
97
XDOT = 19501
403792 XDOT = 5944
027876
YDOT = -14182
862729 feet/sec YDOT = -4322
936560 meter/sec
ZDOT = -1525
510715 ZDOT = -464
975666
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 12102
81608736
00016717 00000-0 10270-3 0 9147
2 25544 51
6432 94
5897 0009350 290
4357 69
5794 15
58241644 7672
Satellite: ISS
Catalog Number: 25544
Epoch time: 12102
81608736 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 94
5897 deg
Eccentricity:
0009350
Arg of perigee: 290
4357 deg
Mean anomaly: 69
5794 deg
Mean motion: 15
58241644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 767
Checksum: 333
Coasting Arc #16 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2012/103/19:10:56
480
Vector Time (MET): N/A
Weight (LBS) : 924393
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3713162
08 A = 6768072
33 meter
Y = -3208588
35 meter E =
0007523
Z = 4665495
94 I = 51
98112
XDOT = 2152
122718 Wp = 350
73873
YDOT = -6755
866474 meter/sec RA = 88
84204 deg
ZDOT = -2926
788113 TA = 128
26338
MA = 128
19566
Ha = 213
833 n
mi
Hp = 211
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12182290
28 X = -3699670
94
Y = -10526864
65 feet Y = -3250035
69 meter
Z = 15306745
21 Z = 4647490
41
XDOT = 7060
770071 XDOT = 2241
725907
YDOT = -22164
916253 feet/sec YDOT = -6731
299169 meter/sec
ZDOT = -9602
323205 ZDOT = -2916
115415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -646659
76 X = -197101
89
Y = 16157264
54 feet Y = 4924734
23 meter
Z = 15232995
73 Z = 4643017
10
XDOT = -20625
918274 XDOT = -6286
779890
YDOT = 8206
117375 feet/sec YDOT = 2501
224576 meter/sec
ZDOT = -9557
933002 ZDOT = -2913
257979
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 12103
84220681
00016717 00000-0 10270-3 0 9151
2 25544 51
6435 89
4427 0009477 294
3548 65
6617 15
58292082 7833
Satellite: ISS
Catalog Number: 25544
Epoch time: 12103
84220681 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 89
4427 deg
Eccentricity:
0009477
Arg of perigee: 294
3548 deg
Mean anomaly: 65
6617 deg
Mean motion: 15
58292082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 328
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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