[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 4th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15876 77 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
096/19:03:33
347 -0
2 6
6 6
6
N/A -4
7 -0
7 212
5
000/00:15:02
694 4
6 -0
4 212
1
Coasting Arc #1 (Orbit 621)
---------------------------------------
Vector Time (GMT): 2012/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3929095
88 A = 6763363
78 meter
Y = 1984320
33 meter E =
0005318
Z = -5135563
16 I = 51
84317
XDOT = -4917
671904 Wp = 157
52641
YDOT = 5680
677507 meter/sec RA = 140
34852 deg
ZDOT = -1572
778317 TA = 97
40048
MA = 97
34005
Ha = 213
864 n
mi
Hp = 207
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12890734
50 X = 3931562
06
Y = 6510237
29 feet Y = 2028271
21 meter
Z = -16848960
51 Z = -5116470
10
XDOT = -16134
094172 XDOT = -4973
188733
YDOT = 18637
393397 feet/sec YDOT = 5625
374499 meter/sec
ZDOT = -5160
033848 ZDOT = -1596
803399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13956978
35 X = 4254087
00
Y = 4048384
53 feet Y = 1233947
60 meter
Z = -16770659
91 Z = -5111697
14
XDOT = -12165
386158 XDOT = -3708
009701
YDOT = 20227
550259 feet/sec YDOT = 6165
357319 meter/sec
ZDOT = -5259
057532 ZDOT = -1602
960736
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
51877811
00016717 00000-0 10270-3 0 9000
2 25544 51
6412 141
2521 0013647 235
4593 124
5275 15
59234905 6228
Satellite: ISS
Catalog Number: 25544
Epoch time: 12093
51877811 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 141
2521 deg
Eccentricity:
0013647
Arg of perigee: 235
4593 deg
Mean anomaly: 124
5275 deg
Mean motion: 15
59234905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 622
Checksum: 292
Coasting Arc #2 (Orbit 637)
---------------------------------------
Vector Time (GMT): 2012/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -935563
25 A = 6763913
56 meter
Y = -4529167
85 meter E =
0007132
Z = 4939985
52 I = 51
86822
XDOT = 6304
127387 Wp = 241
45403
YDOT = -3750
851012 meter/sec RA = 135
31066 deg
ZDOT = -2250
790997 TA = 230
41011
MA = 230
47311
Ha = 213
402 n
mi
Hp = 207
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3069433
22 X = -908844
90
Y = -14859474
58 feet Y = -4539479
95 meter
Z = 16207301
58 Z = 4935506
02
XDOT = 20682
832633 XDOT = 6356
535422
YDOT = -12305
941639 feet/sec YDOT = -3680
061584 meter/sec
ZDOT = -7384
484899 ZDOT = -2220
038218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6047290
10 X = -1843214
02
Y = -13937101
19 feet Y = -4248028
44 meter
Z = 16189179
19 Z = 4934461
82
XDOT = 16863
874110 XDOT = 5140
108829
YDOT = -15725
898013 feet/sec YDOT = -4793
253714 meter/sec
ZDOT = -7257
935195 ZDOT = -2212
218647
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
54421336
00016717 00000-0 10270-3 0 9012
2 25544 51
6407 136
1009 0013558 239
6188 120
3627 15
59311984 6388
Satellite: ISS
Catalog Number: 25544
Epoch time: 12094
54421336 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 136
1009 deg
Eccentricity:
0013558
Arg of perigee: 239
6188 deg
Mean anomaly: 120
3627 deg
Mean motion: 15
59311984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 638
Checksum: 304
Coasting Arc #3 (Orbit 652)
---------------------------------------
Vector Time (GMT): 2012/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2134408
96 A = 6770962
08 meter
Y = 5818668
14 meter E =
0008600
Z = -2724750
86 I = 51
91369
XDOT = -5642
139025 Wp = 245
79663
YDOT = 367
252245 meter/sec RA = 130
29820 deg
ZDOT = 5187
692840 TA = 83
45108
MA = 83
35319
Ha = 213
003 n
mi
Hp = 207
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7002654
07 X = -2186079
62
Y = 19090118
56 feet Y = 5794510
61 meter
Z = -8939471
31 Z = -2735245
96
XDOT = -18510
954807 XDOT = -5671
027037
YDOT = 1204
895817 feet/sec YDOT = 303
997487 meter/sec
ZDOT = 17019
989633 ZDOT = 5160
213355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2684731
53 X = -818306
17
Y = 20136605
08 feet Y = 6137637
23 meter
Z = -8982944
41 Z = -2738001
46
XDOT = -16451
971346 XDOT = -5014
560866
YDOT = 5372
504464 feet/sec YDOT = 1637
539361 meter/sec
ZDOT = 16907
086578 ZDOT = 5153
279989
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
50553638
00016717 00000-0 10270-3 0 9021
2 25544 51
6411 131
2703 0013381 242
6868 117
2925 15
59361518 6534
Satellite: ISS
Catalog Number: 25544
Epoch time: 12095
50553638 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 131
2703 deg
Eccentricity:
0013381
Arg of perigee: 242
6868 deg
Mean anomaly: 117
2925 deg
Mean motion: 15
59361518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 653
Checksum: 299
Coasting Arc #4 (Orbit 668)
---------------------------------------
Vector Time (GMT): 2012/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4271173
47 A = 6774000
91 meter
Y = -5210769
50 meter E =
0014423
Z = -603361
41 I = 51
94228
XDOT = 3334
015733 Wp = 201
12156
YDOT = 3432
274839 meter/sec RA = 125
32050 deg
ZDOT = -6009
245735 TA = 345
38281
MA = 345
42447
Ha = 212
715 n
mi
Hp = 208
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14013036
32 X = 4332054
91
Y = -17095700
46 feet Y = -5162666
27 meter
Z = -1979532
18 Z = -582463
57
XDOT = 10938
371827 XDOT = 3324
579288
YDOT = 11260
744221 feet/sec YDOT = 3469
504333 meter/sec
ZDOT = -19715
373147 ZDOT = -5993
072502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9683945
55 X = 2951666
60
Y = -19879213
15 feet Y = -6059184
17 meter
Z = -1893354
65 Z = -577094
50
XDOT = 11915
540519 XDOT = 3631
856750
YDOT = 7686
197121 feet/sec YDOT = 2342
752882 meter/sec
ZDOT = -19649
151610 ZDOT = -5989
061411
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
53092031
00016717 00000-0 10270-3 0 9031
2 25544 51
6406 126
1180 0013333 246
9087 113
0663 15
59369195 6696
Satellite: ISS
Catalog Number: 25544
Epoch time: 12096
53092031 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 126
1180 deg
Eccentricity:
0013333
Arg of perigee: 246
9087 deg
Mean anomaly: 113
0663 deg
Mean motion: 15
59369195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 669
Checksum: 301
Coasting Arc #5 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2012/096/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4623486
72 A = 6767621
18 meter
Y = -64376
23 meter E =
0005381
Z = 4946164
90 I = 51
91443
XDOT = 2502
009176 Wp = 223
00328
YDOT = -6894
444860 meter/sec RA = 123
83593 deg
ZDOT = 2246
647882 TA = 205
13784
MA = 205
16404
Ha = 212
500 n
mi
Hp = 212
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15168919
68 X = -4646450
76
Y = -211208
09 feet Y = -116206
69 meter
Z = 16227575
12 Z = 4923648
27
XDOT = 8208
691522 XDOT = 2568
004503
YDOT = -22619
569752 feet/sec YDOT = -6866
096563 meter/sec
ZDOT = 7370
892000 ZDOT = 2258
963792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7787818
87 X = 2373727
19
Y = 13133315
15 feet Y = 4003034
46 meter
Z = 16135080
97 Z = 4917972
68
XDOT = -22597
534902 XDOT = -6887
728638
YDOT = 4271
906324 feet/sec YDOT = 1302
077047 meter/sec
ZDOT = 7421
925824 ZDOT = 2262
202991
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
85140365
00016717 00000-0 10270-3 0 9041
2 25544 51
6416 124
5098 0009237 267
2459 92
7638 15
58061134 6746
Satellite: ISS
Catalog Number: 25544
Epoch time: 12096
85140365 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 124
5098 deg
Eccentricity:
0009237
Arg of perigee: 267
2459 deg
Mean anomaly: 92
7638 deg
Mean motion: 15
58061134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 321
Coasting Arc #6 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2012/097/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2976126
19 A = 6766263
01 meter
Y = 3095693
17 meter E =
0005299
Z = -5233491
89 I = 51
92655
XDOT = -4412
986813 Wp = 111
10169
YDOT = 6170
547542 meter/sec RA = 118
81374 deg
ZDOT = 1139
512747 TA = 169
78018
MA = 169
76941
Ha = 212
117 n
mi
Hp = 211
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9764193
55 X = 2966711
78
Y = 10156473
66 feet Y = 3128920
84 meter
Z = -17170248
97 Z = -5219057
02
XDOT = -14478
303193 XDOT = -4487
194706
YDOT = 20244
578550 feet/sec YDOT = 6120
784000 meter/sec
ZDOT = 3738
558881 ZDOT = 1117
893458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3276744
45 X = 998751
71
Y = -13776149
89 feet Y = -4198970
49 meter
Z = -17111151
99 Z = -5215479
13
XDOT = 23859
576226 XDOT = 7272
398834
YDOT = 1138
545262 feet/sec YDOT = 347
028596 meter/sec
ZDOT = 3649
337949 ZDOT = 1112
318207
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
81349696
00016717 00000-0 10270-3 0 9057
2 25544 51
6419 119
6845 0009166 271
4865 88
5239 15
58085008 6895
Satellite: ISS
Catalog Number: 25544
Epoch time: 12097
81349696 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 119
6845 deg
Eccentricity:
0009166
Arg of perigee: 271
4865 deg
Mean anomaly: 88
5239 deg
Mean motion: 15
58085008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 356
Coasting Arc #7 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2012/098/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -867498
01 A = 6771474
01 meter
Y = -5501254
64 meter E =
0003255
Z = 3851945
45 I = 51
95765
XDOT = 5227
980173 Wp = 41
85816
YDOT = -3752
465541 meter/sec RA = 113
80399 deg
ZDOT = -4177
397206 TA = 91
89804
MA = 91
86076
Ha = 212
778 n
mi
Hp = 212
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2846122
08 X = -824629
57
Y = -18048735
71 feet Y = -5510715
53 meter
Z = 12637616
30 Z = 3847835
70
XDOT = 17152
165922 XDOT = 5289
845612
YDOT = -12311
238652 feet/sec YDOT = -3693
657471 meter/sec
ZDOT = -13705
371412 ZDOT = -4151
848942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13452397
64 X = -4100290
80
Y = 12381732
04 feet Y = 3773951
93 meter
Z = 12621106
41 Z = 3846913
23
XDOT = -18867
050698 XDOT = -5750
677053
YDOT = -6620
733898 feet/sec YDOT = -2017
999692 meter/sec
ZDOT = -13600
155191 ZDOT = -4145
327302
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
83970487
00016717 00000-0 10270-3 0 9069
2 25544 51
6414 114
5380 0009109 275
2756 84
7360 15
58110615 7051
Satellite: ISS
Catalog Number: 25544
Epoch time: 12098
83970487 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 114
5380 deg
Eccentricity:
0009109
Arg of perigee: 275
2756 deg
Mean anomaly: 84
7360 deg
Mean motion: 15
58110615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 314
Coasting Arc #8 (Orbit 719)
---------------------------------------
Vector Time (GMT): 2012/099/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1221690
84 A = 6776985
00 meter
Y = 6546350
38 meter E =
0009321
Z = -1222984
34 I = 51
98868
XDOT = -4923
204532 Wp = 338
07719
YDOT = 182
102081 meter/sec RA = 108
82380 deg
ZDOT = 5886
782019 TA = 8
66957
MA = 8
65348
Ha = 213
082 n
mi
Hp = 211
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4008172
06 X = -1288861
59
Y = 21477527
50 feet Y = 6532313
04 meter
Z = -4012415
80 Z = -1229082
85
XDOT = -16152
245841 XDOT = -4953
472021
YDOT = 597
447772 feet/sec YDOT = 126
878839 meter/sec
ZDOT = 19313
589301 ZDOT = 5862
791423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19969833
50 X = 6086805
25
Y = -8851550
94 feet Y = -2697952
73 meter
Z = -4037933
57 Z = -1230762
15
XDOT = 9043
062481 XDOT = 2756
325444
YDOT = 11627
452923 feet/sec YDOT = 3544
047651 meter/sec
ZDOT = 19215
008942 ZDOT = 5856
734725
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
80175036
00016717 00000-0 10270-3 0 9075
2 25544 51
6422 109
7120 0009193 279
0421 80
9694 15
58161652 7204
Satellite: ISS
Catalog Number: 25544
Epoch time: 12099
80175036 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 109
7120 deg
Eccentricity:
0009193
Arg of perigee: 279
0421 deg
Mean anomaly: 80
9694 deg
Mean motion: 15
58161652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 720
Checksum: 303
Coasting Arc #9 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2012/100/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2901149
95 A = 6776232
89 meter
Y = -5845261
71 meter E =
0005888
Z = -1812855
97 I = 51
99572
XDOT = 3689
124796 Wp = 229
20154
YDOT = 3597
143005 meter/sec RA = 103
85882 deg
ZDOT = -5686
359291 TA = 330
65685
MA = 330
68990
Ha = 213
249 n
mi
Hp = 211
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9518208
51 X = 2975103
78
Y = -19177367
82 feet Y = -5812405
81 meter
Z = -5947690
19 Z = -1798582
35
XDOT = 12103
427809 XDOT = 3676
250016
YDOT = 11801
650280 feet/sec YDOT = 3638
324936 meter/sec
ZDOT = -18656
034420 ZDOT = -5668
468843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21166913
26 X = -6451675
16
Y = 3320954
57 feet Y = 1012226
95 meter
Z = -5888615
46 Z = -1794849
99
XDOT = 2784
645276 XDOT = 848
759880
YDOT = -15250
393637 feet/sec YDOT = -4648
319981 meter/sec
ZDOT = -18582
786453 ZDOT = -5664
033311
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
82790807
00016717 00000-0 10270-3 0 9080
2 25544 51
6429 104
5651 0009238 282
1468 77
8652 15
58170116 7360
Satellite: ISS
Catalog Number: 25544
Epoch time: 12100
82790807 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 104
5651 deg
Eccentricity:
0009238
Arg of perigee: 282
1468 deg
Mean anomaly: 77
8652 deg
Mean motion: 15
58170116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 314
Coasting Arc #10 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2012/101/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3923171
56 A = 6769765
41 meter
Y = 3494826
63 meter E =
0000884
Z = 4268395
38 I = 51
98124
XDOT = -1851
778769 Wp = 101
00452
YDOT = -6505
751626 meter/sec RA = 98
87406 deg
ZDOT = 3623
897232 TA = 312
16181
MA = 312
16931
Ha = 213
571 n
mi
Hp = 211
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12871297
78 X = -3982694
90
Y = 11465966
63 feet Y = 3450622
54 meter
Z = 14003921
85 Z = 4249192
01
XDOT = -6075
389663 XDOT = -1796
496721
YDOT = -21344
329481 feet/sec YDOT = -6526
150214 meter/sec
ZDOT = 11889
426613 ZDOT = 3615
035670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16916998
18 X = 5156301
04
Y = 3628369
85 feet Y = 1105927
13 meter
Z = 13924748
81 Z = 4244263
44
XDOT = -13271
496055 XDOT = -4045
151997
YDOT = 16376
568431 feet/sec YDOT = 4991
578058 meter/sec
ZDOT = 11853
499892 ZDOT = 3612
946767
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
85403949
00016717 00000-0 10270-3 0 9093
2 25544 51
6432 99
4176 0009141 287
1475 72
8679 15
58225994 7521
Satellite: ISS
Catalog Number: 25544
Epoch time: 12101
85403949 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 99
4176 deg
Eccentricity:
0009141
Arg of perigee: 287
1475 deg
Mean anomaly: 72
8679 deg
Mean motion: 15
58225994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 338
Coasting Arc #11 (Orbit 766)
---------------------------------------
Vector Time (GMT): 2012/102/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4180995
07 A = 6765279
73 meter
Y = -128560
09 meter E =
0007348
Z = -5322627
91 I = 51
97085
XDOT = -231
800105 Wp = 57
13421
YDOT = 7658
805758 meter/sec RA = 93
86019 deg
ZDOT = -363
548186 TA = 209
39575
MA = 209
43709
Ha = 213
636 n
mi
Hp = 211
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13717175
43 X = 4207978
12
Y = -421785
06 feet Y = -81654
81 meter
Z = -17462689
99 Z = -5302251
21
XDOT = -760
499033 XDOT = -315
659153
YDOT = 25127
315479 feet/sec YDOT = 7655
744740 meter/sec
ZDOT = -1192
743391 ZDOT = -364
878046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8726072
43 X = -2659706
88
Y = -10729045
64 feet Y = -3270213
11 meter
Z = -17378940
86 Z = -5297101
17
XDOT = 19644
241453 XDOT = 5987
564795
YDOT = -14016
303432 feet/sec YDOT = -4272
169286 meter/sec
ZDOT = -1198
795599 ZDOT = -365
392899
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
81601259
00016717 00000-0 10270-3 0 9106
2 25544 51
6435 94
5922 0009252 290
6478 69
3684 15
58298299 7675
Satellite: ISS
Catalog Number: 25544
Epoch time: 12102
81601259 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 94
5922 deg
Eccentricity:
0009252
Arg of perigee: 290
6478 deg
Mean anomaly: 69
3684 deg
Mean motion: 15
58298299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 767
Checksum: 335
Coasting Arc #12 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2012/103/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3673248
66 A = 6768092
67 meter
Y = -3329887
91 meter E =
0007401
Z = 4611524
41 I = 51
98213
XDOT = 2237
831312 Wp = 354
00867
YDOT = -6680
325645 meter/sec RA = 88
84252 deg
ZDOT = -3034
479918 TA = 126
16626
MA = 126
09777
Ha = 213
723 n
mi
Hp = 210
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12051340
74 X = -3658141
91
Y = -10924829
11 feet Y = -3370879
89 meter
Z = 15129673
26 Z = 4593716
70
XDOT = 7341
966248 XDOT = 2327
106561
YDOT = -21917
078887 feet/sec YDOT = -6654
801730 meter/sec
ZDOT = -9955
642774 ZDOT = -3023
391649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1030989
44 X = -314245
58
Y = 16301078
81 feet Y = 4968568
82 meter
Z = 15056746
26 Z = 4589296
26
XDOT = -20592
032132 XDOT = -6276
451394
YDOT = 7871
233795 feet/sec YDOT = 2399
152061 meter/sec
ZDOT = -9909
550538 ZDOT = -3020
431004
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
84209145
00016717 00000-0 10270-3 0 9119
2 25544 51
6438 89
4450 0009371 294
5587 65
4591 15
58357729 7839
Satellite: ISS
Catalog Number: 25544
Epoch time: 12103
84209145 = yrday
fracday
Element set: 911
Inclination: 51
6438 deg
RA of node: 89
4450 deg
Eccentricity:
0009371
Arg of perigee: 294
5587 deg
Mean anomaly: 65
4591 deg
Mean motion: 15
58357729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 332
Coasting Arc #13 (Orbit 797)
---------------------------------------
Vector Time (GMT): 2012/104/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2478739
32 A = 6774748
34 meter
Y = 5841820
18 meter E =
0009426
Z = -2353661
78 I = 52
00232
XDOT = -3854
197454 Wp = 333
41333
YDOT = 3822
907027 meter/sec RA = 83
85094 deg
ZDOT = 5429
345113 TA =
40107
MA =
40031
Ha = 213
965 n
mi
Hp = 210
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8132346
86 X = 2424664
21
Y = 19166076
71 feet Y = 5869236
54 meter
Z = -7721987
47 Z = -2341751
77
XDOT = -12645
004771 XDOT = -3923
033997
YDOT = 12542
345890 feet/sec YDOT = 3779
422322 meter/sec
ZDOT = 17812
812050 ZDOT = 5410
454295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9637320
83 X = 2937455
39
Y = -18475446
12 feet Y = -5631315
98 meter
Z = -7673499
24 Z = -2338882
57
XDOT = 16438
254634 XDOT = 5010
380012
YDOT = 1208
552981 feet/sec YDOT = 368
366949 meter/sec
ZDOT = 17734
867377 ZDOT = 5405
587576
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 12104
80401731
00016717 00000-0 10270-3 0 9122
2 25544 51
6434 84
6186 0009386 297
9692 62
0513 15
58351174 7989
Satellite: ISS
Catalog Number: 25544
Epoch time: 12104
80401731 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 84
6186 deg
Eccentricity:
0009386
Arg of perigee: 297
9692 deg
Mean anomaly: 62
0513 deg
Mean motion: 15
58351174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 798
Checksum: 315
Coasting Arc #14 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2012/105/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -747482
26 A = 6776830
75 meter
Y = -6695190
23 meter E =
0003594
Z = -713364
10 I = 52
00485
XDOT = 4790
381253 Wp = 200
02900
YDOT = 104
187642 meter/sec RA = 78
88488 deg
ZDOT = -5991
732631 TA = 347
64991
MA = 347
65872
Ha = 213
982 n
mi
Hp = 210
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2452369
62 X = -669094
38
Y = -21965847
20 feet Y = -6703110
78 meter
Z = -2340433
40 Z = -716804
56
XDOT = 15716
473928 XDOT = 4817
966589
YDOT = 341
822973 feet/sec YDOT = 157
910557 meter/sec
ZDOT = -19657
915455 ZDOT = -5968
394234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15168292
17 X = -4623295
45
Y = 16073941
93 feet Y = 4899337
50 meter
Z = -2354037
36 Z = -717510
59
XDOT = -8816
180428 XDOT = -2687
171794
YDOT = -11186
992660 feet/sec YDOT = -3409
795363 meter/sec
ZDOT = -19561
999351 ZDOT = -5962
497402
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 12105
83004491
00016717 00000-0 10270-3 0 9139
2 25544 51
6431 79
4713 0009268 300
4470 59
5769 15
58361195 8144
Satellite: ISS
Catalog Number: 25544
Epoch time: 12105
83004491 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 79
4713 deg
Eccentricity:
0009268
Arg of perigee: 300
4470 deg
Mean anomaly: 59
5769 deg
Mean motion: 15
58361195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 307
Coasting Arc #15 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2012/106/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1263899
58 A = 6771538
66 meter
Y = 5622848
65 meter E =
0006659
Z = 3546663
50 I = 51
98017
XDOT = -4807
873089 Wp = 42
16554
YDOT = -3928
975540 meter/sec RA = 73
90785 deg
ZDOT = 4515
536248 TA = 359
53859
MA = 359
53921
Ha = 214
232 n
mi
Hp = 210
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4146652
18 X = -1343910
36
Y = 18447666
18 feet Y = 5608267
83 meter
Z = 11636035
12 Z = 3540328
80
XDOT = -15773
861841 XDOT = -4785
516596
YDOT = -12890
339699 feet/sec YDOT = -3982
614828 meter/sec
ZDOT = 14814
751470 ZDOT = 4492
234419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16641059
49 X = 5072194
93
Y = -9011221
32 feet Y = -2746620
26 meter
Z = 11609541
51 Z = 3538588
25
XDOT = 133
967744 XDOT = 40
833368
YDOT = 19211
229276 feet/sec YDOT = 5855
582683 meter/sec
ZDOT = 14719
295907 ZDOT = 4486
441392
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 12106
85604379
00016717 00000-0 10270-3 0 9144
2 25544 51
6424 74
3218 0009394 305
6006 54
4273 15
58420592 8301
Satellite: ISS
Catalog Number: 25544
Epoch time: 12106
85604379 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 74
3218 deg
Eccentricity:
0009394
Arg of perigee: 305
6006 deg
Mean anomaly: 54
4273 deg
Mean motion: 15
58420592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 299
Coasting Arc #16 (Orbit 844)
---------------------------------------
Vector Time (GMT): 2012/107/19:11:04
694
Vector Time (MET): N/A
Weight (LBS) : 924693
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3174623
03 A = 6765397
95 meter
Y = -3009312
99 meter E =
0010505
Z = -5168196
72 I = 51
94969
XDOT = 3758
247578 Wp = 35
94519
YDOT = 6519
597256 meter/sec RA = 68
89890 deg
ZDOT = -1480
889012 TA = 219
82272
MA = 219
89985
Ha = 214
248 n
mi
Hp = 209
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10415429
90 X = 3233143
83
Y = -9873074
11 feet Y = -2973485
60 meter
Z = -16956025
99 Z = -5152632
12
XDOT = 12330
208588 XDOT = 3692
258639
YDOT = 21389
754776 feet/sec YDOT = 6561
255220 meter/sec
ZDOT = -4858
559750 ZDOT = -1462
792390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14382095
79 X = -4383662
80
Y = -1134823
33 feet Y = -345894
15 meter
Z = -16891805
31 Z = -5148622
26
XDOT = 7420
241339 XDOT = 2261
689560
YDOT = -22487
868101 feet/sec YDOT = -6854
302197 meter/sec
ZDOT = -4784
717656 ZDOT = -1458
381941
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 12107
81789128
00016717 00000-0 10270-3 0 9158
2 25544 51
6414 69
4948 0009385 308
4595 51
5717 15
58487562 8456
Satellite: ISS
Catalog Number: 25544
Epoch time: 12107
81789128 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 69
4948 deg
Eccentricity:
0009385
Arg of perigee: 308
4595 deg
Mean anomaly: 51
5717 deg
Mean motion: 15
58487562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 845
Checksum: 348
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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