[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 3rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8880 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
125/08:47:10
504 2
3 8
4 8
5
N/A -6
5 -1
2 216
3
000/00:20:21
008 -4
9 0
2 214
6
Coasting Arc #1 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2012/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6654051
60 A = 6779260
04 meter
Y = 1276891
36 meter E =
0002248
Z = 180714
10 I = 51
60712
XDOT = -1056
028530 Wp = 153
93015
YDOT = -4649
127795 meter/sec RA = 350
34818 deg
ZDOT = -6007
629808 TA = 24
12038
MA = 24
10986
Ha = 215
838 n
mi
Hp = 211
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21830877
94 X = -6668713
39
Y = 4189276
13 feet Y = 1202399
67 meter
Z = 592894
03 Z = 148352
93
XDOT = -3464
660532 XDOT = -974
778457
YDOT = -15253
043946 feet/sec YDOT = -4660
482892 meter/sec
ZDOT = -19710
071550 ZDOT = -6012
562482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14032059
44 X = -4276971
72
Y = 17244670
87 feet Y = 5256175
68 meter
Z = 459808
55 Z = 140149
64
XDOT = -11110
432697 XDOT = -3386
459886
YDOT = -8511
551224 feet/sec YDOT = -2594
320813 meter/sec
ZDOT = -19729
881512 ZDOT = -6013
667885
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 12123
53235444
00016717 00000-0 10270-3 0 9006
2 25544 51
6429 350
7135 0010331 308
8072 51
2159 15
57594389 10908
Satellite: ISS
Catalog Number: 25544
Epoch time: 12123
53235444 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 350
7135 deg
Eccentricity:
0010331
Arg of perigee: 308
8072 deg
Mean anomaly: 51
2159 deg
Mean motion: 15
57594389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 288
Coasting Arc #2 (Orbit 1105)
---------------------------------------
Vector Time (GMT): 2012/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6231056
27 A = 6776158
28 meter
Y = 499966
13 meter E =
0011595
Z = 2594975
13 I = 51
56677
XDOT = -2583
577269 Wp = 28
03993
YDOT = 4977
252256 meter/sec RA = 345
35416 deg
ZDOT = 5245
247195 TA = 1
26440
MA = 1
26148
Ha = 215
938 n
mi
Hp = 210
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20443097
98 X = 6212396
40
Y = 1640308
83 feet Y = 569541
41 meter
Z = 8513697
93 Z = 2625200
52
XDOT = -8476
303376 XDOT = -2664
522583
YDOT = 16329
567770 feet/sec YDOT = 4947
908672 meter/sec
ZDOT = 17208
816255 ZDOT = 5232
499292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16468053
37 X = 5019462
67
Y = -12136107
05 feet Y = -3699085
43 meter
Z = 8637826
37 Z = 2632809
48
XDOT = 3349
317248 XDOT = 1020
871897
YDOT = 16754
349439 feet/sec YDOT = 5106
725709 meter/sec
ZDOT = 17155
952653 ZDOT = 5229
134369
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 12124
55886606
00016717 00000-0 10270-3 0 9012
2 25544 51
6422 345
5678 0010598 313
2082 46
8187 15
57650100 11064
Satellite: ISS
Catalog Number: 25544
Epoch time: 12124
55886606 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 345
5678 deg
Eccentricity:
0010598
Arg of perigee: 313
2082 deg
Mean anomaly: 46
8187 deg
Mean motion: 15
57650100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1106
Checksum: 300
Coasting Arc #3 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2012/125/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3601219
09 A = 6773955
78 meter
Y = -2915604
05 meter E =
0004828
Z = -4943983
88 I = 51
51406
XDOT = 6195
582556 Wp = 14
75560
YDOT = -3963
540446 meter/sec RA = 340
96634 deg
ZDOT = -2171
371947 TA = 234
01574
MA = 234
06052
Ha = 216
314 n
mi
Hp = 214
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11815023
25 X = -3544331
28
Y = -9565630
09 feet Y = -2955557
11 meter
Z = -16220419
54 Z = -4961340
59
XDOT = 20326
714422 XDOT = 6249
991460
YDOT = -13003
741620 feet/sec YDOT = -3893
953424 meter/sec
ZDOT = -7123
923709 ZDOT = -2141
141210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11053997
72 X = -3369258
51
Y = -10324549
07 feet Y = -3146922
56 meter
Z = -16291435
92 Z = -4965629
67
XDOT = 20436
492765 XDOT = 6229
042995
YDOT = -10814
719246 feet/sec YDOT = -3296
326426 meter/sec
ZDOT = -6999
337277 ZDOT = -2133
398002
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 12125
39292345
00016717 00000-0 10270-3 0 9027
2 25544 51
6402 341
3869 0010868 276
8029 83
1888 15
55814102 11191
Satellite: ISS
Catalog Number: 25544
Epoch time: 12125
39292345 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 341
3869 deg
Eccentricity:
0010868
Arg of perigee: 276
8029 deg
Mean anomaly: 83
1888 deg
Mean motion: 15
55814102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1119
Checksum: 312
Coasting Arc #4 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2012/126/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1346192
09 A = 6772424
23 meter
Y = 4013602
76 meter E =
0008795
Z = 5293637
21 I = 51
48030
XDOT = -7103
179591 Wp = 288
03373
YDOT = 2858
728733 meter/sec RA = 335
93889 deg
ZDOT = -358
928401 TA = 165
41011
MA = 165
38470
Ha = 216
695 n
mi
Hp = 214
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4416640
73 X = 1275495
21
Y = 13167988
05 feet Y = 4028261
35 meter
Z = 17367576
16 Z = 5300005
44
XDOT = -23304
394983 XDOT = -7132
874911
YDOT = 9379
031277 feet/sec YDOT = 2779
130554 meter/sec
ZDOT = -1177
586619 ZDOT = -393
508249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3656047
16 X = 1114363
17
Y = 13365645
24 feet Y = 4073848
67 meter
Z = 17393337
02 Z = 5301489
12
XDOT = -22756
435608 XDOT = -6936
161573
YDOT = 7951
771820 feet/sec YDOT = 2423
700051 meter/sec
ZDOT = -1319
928026 ZDOT = -402
314062
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 12126
42064839
00016717 00000-0 10270-3 0 9038
2 25544 51
6398 336
2498 0011036 280
4850 79
5060 15
55841619 11359
Satellite: ISS
Catalog Number: 25544
Epoch time: 12126
42064839 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 336
2498 deg
Eccentricity:
0011036
Arg of perigee: 280
4850 deg
Mean anomaly: 79
5060 deg
Mean motion: 15
55841619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 311
Coasting Arc #5 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2012/127/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 978886
85 A = 6775107
84 meter
Y = -4805314
94 meter E =
0001061
Z = -4674469
71 I = 51
46192
XDOT = 7007
216002 Wp = 220
84209
YDOT = -1322
602197 meter/sec RA = 330
91136 deg
ZDOT = 2825
863916 TA = 77
26269
MA = 77
25084
Ha = 217
086 n
mi
Hp = 214
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3211571
05 X = 1055256
15
Y = -15765468
98 feet Y = -4793941
20 meter
Z = -15336186
70 Z = -4669528
93
XDOT = 22989
553812 XDOT = 7007
757084
YDOT = -4339
246052 feet/sec YDOT = -1244
240279 meter/sec
ZDOT = 9271
207074 ZDOT = 2859
906698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3809844
71 X = 1161240
67
Y = -15652035
36 feet Y = -4770740
38 meter
Z = -15315407
13 Z = -4668136
09
XDOT = 21918
943552 XDOT = 6680
893995
YDOT = -3877
213624 feet/sec YDOT = -1181
774712 meter/sec
ZDOT = 9411
188537 ZDOT = 2868
530266
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 12127
38413096
00016717 00000-0 10270-3 0 9048
2 25544 51
6400 331
4335 0011064 284
4513 75
5413 15
55834803 11503
Satellite: ISS
Catalog Number: 25544
Epoch time: 12127
38413096 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 331
4335 deg
Eccentricity:
0011064
Arg of perigee: 284
4513 deg
Mean anomaly: 75
5413 deg
Mean motion: 15
55834803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1150
Checksum: 275
Coasting Arc #6 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2012/128/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3047706
92 A = 6780038
00 meter
Y = 5142744
22 meter E =
0003550
Z = 3199786
74 I = 51
45229
XDOT = -5968
075561 Wp = 42
17449
YDOT = -558
952289 meter/sec RA = 325
89724 deg
ZDOT = -4780
400422 TA = 100
71186
MA = 100
67189
Ha = 217
427 n
mi
Hp = 214
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9999038
44 X = -3120531
75
Y = 16872520
40 feet Y = 5108255
45 meter
Z = 10497987
99 Z = 3184804
32
XDOT = -19580
300396 XDOT = -5938
159126
YDOT = -1833
832968 feet/sec YDOT = -625
523376 meter/sec
ZDOT = -15683
728417 ZDOT = -4809
320997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10313733
71 X = -3143626
03
Y = 16720913
20 feet Y = 5096534
34 meter
Z = 10435919
93 Z = 3180868
39
XDOT = -18235
597372 XDOT = -5558
210079
YDOT = -1373
637855 feet/sec YDOT = -418
684818 meter/sec
ZDOT = -15802
480038 ZDOT = -4816
595916
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 12128
41183355
00016717 00000-0 10270-3 0 9056
2 25544 51
6398 326
2965 0011008 288
6801 71
3158 15
55848299 11665
Satellite: ISS
Catalog Number: 25544
Epoch time: 12128
41183355 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 326
2965 deg
Eccentricity:
0011008
Arg of perigee: 288
6801 deg
Mean anomaly: 71
3158 deg
Mean motion: 15
55848299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1166
Checksum: 325
Coasting Arc #7 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2012/129/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4570317
67 A = 6783741
08 meter
Y = -4872976
03 meter E =
0012510
Z = -1127751
43 I = 51
44066
XDOT = 4216
919188 Wp = 338
59207
YDOT = 2595
867611 meter/sec RA = 320
89737 deg
ZDOT = 5863
671177 TA = 9
11790
MA = 9
09520
Ha = 217
678 n
mi
Hp = 214
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14994480
53 X = 4629947
03
Y = -15987454
17 feet Y = -4821534
41 meter
Z = -3699971
88 Z = -1105404
32
XDOT = 13835
036707 XDOT = 4159
093476
YDOT = 8516
626019 feet/sec YDOT = 2642
699968 meter/sec
ZDOT = 19237
766330 ZDOT = 5884
016834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14980556
76 X = 4566073
70
Y = -16021564
86 feet Y = -4883372
97 meter
Z = -3607673
46 Z = -1099618
87
XDOT = 12568
602801 XDOT = 3830
910134
YDOT = 7394
387826 feet/sec YDOT = 2253
809409 meter/sec
ZDOT = 19321
088348 ZDOT = 5889
067728
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 12129
37529236
00016717 00000-0 10270-3 0 9065
2 25544 51
6401 321
4794 0011184 292
2417 67
7550 15
55876385 11815
Satellite: ISS
Catalog Number: 25544
Epoch time: 12129
37529236 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 321
4794 deg
Eccentricity:
0011184
Arg of perigee: 292
2417 deg
Mean anomaly: 67
7550 deg
Mean motion: 15
55876385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1181
Checksum: 314
Coasting Arc #8 (Orbit 1196)
---------------------------------------
Vector Time (GMT): 2012/130/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5393554
17 A = 6783731
61 meter
Y = 3945763
47 meter E =
0005134
Z = -1152362
22 I = 51
41743
XDOT = -2048
609106 Wp = 240
60094
YDOT = -4513
915021 meter/sec RA = 315
90469 deg
ZDOT = -5850
338068 TA = 311
95437
MA = 311
99812
Ha = 217
942 n
mi
Hp = 214
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17695387
70 X = -5431677
67
Y = 12945418
21 feet Y = 3885236
36 meter
Z = -3780715
96 Z = -1178656
34
XDOT = -6721
158483 XDOT = -1969
561475
YDOT = -14809
432482 feet/sec YDOT = -4536
381332 meter/sec
ZDOT = -19194
022534 ZDOT = -5860
098600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17416782
61 X = -5308635
34
Y = 13286636
25 feet Y = 4049766
73 meter
Z = -3889137
74 Z = -1185409
18
XDOT = -5922
307198 XDOT = -1805
119234
YDOT = -13409
230534 feet/sec YDOT = -4087
133467 meter/sec
ZDOT = -19233
668778 ZDOT = -5862
422243
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 12130
40297137
00016717 00000-0 10270-3 0 9074
2 25544 51
6400 316
3426 0011227 295
3158 64
6832 15
55849573 11978
Satellite: ISS
Catalog Number: 25544
Epoch time: 12130
40297137 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 316
3426 deg
Eccentricity:
0011227
Arg of perigee: 295
3158 deg
Mean anomaly: 64
6832 deg
Mean motion: 15
55849573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1197
Checksum: 306
Coasting Arc #9 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2012/131/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5464697
06 A = 6779701
40 meter
Y = -2368833
16 meter E =
0006941
Z = 3229230
59 I = 51
38285
XDOT = -195
625157 Wp = 24
52379
YDOT = 6021
862827 meter/sec RA = 310
90101 deg
ZDOT = 4750
968599 TA = 13
06732
MA = 13
04935
Ha = 218
132 n
mi
Hp = 213
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17928796
14 X = 5475092
74
Y = -7771762
35 feet Y = -2307665
67 meter
Z = 10594588
55 Z = 3255803
03
XDOT = -641
814818 XDOT = -286
027547
YDOT = 19756
767806 feet/sec YDOT = 6019
169385 meter/sec
ZDOT = 15587
167319 ZDOT = 4749
799143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17567115
98 X = 5354456
95
Y = -8420701
98 feet Y = -2566629
96 meter
Z = 10703996
53 Z = 3262578
14
XDOT = -625
997623 XDOT = -190
804075
YDOT = 18490
431945 feet/sec YDOT = 5635
883657 meter/sec
ZDOT = 15581
763539 ZDOT = 4749
321527
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 12131
43063753
00016717 00000-0 10270-3 0 9084
2 25544 51
6396 311
2042 0011350 300
6074 59
3960 15
55884964 12139
Satellite: ISS
Catalog Number: 25544
Epoch time: 12131
43063753 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 311
2042 deg
Eccentricity:
0011350
Arg of perigee: 300
6074 deg
Mean anomaly: 59
3960 deg
Mean motion: 15
55884964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1213
Checksum: 287
Coasting Arc #10 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2012/132/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4877027
93 A = 6774648
77 meter
Y = 334642
18 meter E =
0009950
Z = -4695396
77 I = 51
34624
XDOT = 2198
911967 Wp = 4
44708
YDOT = -6806
180781 meter/sec RA = 305
87925 deg
ZDOT = -2759
700754 TA = 238
05635
MA = 238
15315
Ha = 218
369 n
mi
Hp = 213
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16000747
80 X = -4857598
26
Y = 1097907
42 feet Y = 280213
16 meter
Z = -15404845
06 Z = -4719042
00
XDOT = 7214
278108 XDOT = 2288
262672
YDOT = -22329
989440 feet/sec YDOT = -6781
091431 meter/sec
ZDOT = -9054
136333 ZDOT = -2748
801897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15824547
63 X = -4823322
12
Y = 1951785
47 feet Y = 594904
21 meter
Z = -15502025
93 Z = -4725017
50
XDOT = 6198
763675 XDOT = 1889
383168
YDOT = -21535
584383 feet/sec YDOT = -6564
046120 meter/sec
ZDOT = -9008
689190 ZDOT = -2745
848465
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 12132
39406237
00016717 00000-0 10270-3 0 9099
2 25544 51
6387 306
3880 0011460 303
6659 56
3401 15
55919651 12283
Satellite: ISS
Catalog Number: 25544
Epoch time: 12132
39406237 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 306
3880 deg
Eccentricity:
0011460
Arg of perigee: 303
6659 deg
Mean anomaly: 56
3401 deg
Mean motion: 15
55919651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 306
Coasting Arc #11 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2012/133/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3769229
12 A = 6772144
03 meter
Y = 1941852
14 meter E =
0009261
Z = 5286058
87 I = 51
32107
XDOT = -3763
762684 Wp = 314
34228
YDOT = 6675
433408 meter/sec RA = 300
84072 deg
ZDOT = 238
126990 TA = 133
41618
MA = 133
33906
Ha = 218
556 n
mi
Hp = 213
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12366237
25 X = 3721556
25
Y = 6370905
98 feet Y = 1983735
21 meter
Z = 17342712
84 Z = 5304253
95
XDOT = -12348
302770 XDOT = -3839
285775
YDOT = 21901
028241 feet/sec YDOT = 6632
922402 meter/sec
ZDOT = 781
256529 ZDOT = 219
659598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12681950
32 X = 3865458
46
Y = 5485290
04 feet Y = 1671916
40 meter
Z = 17417281
20 Z = 5308787
31
XDOT = -10366
492281 XDOT = -3159
706847
YDOT = 21798
159951 feet/sec YDOT = 6644
079153 meter/sec
ZDOT = 704
735023 ZDOT = 214
803235
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 12133
42170542
00016717 00000-0 10270-3 0 9103
2 25544 51
6389 301
2504 0011384 307
6672 52
3449 15
55923949 12447
Satellite: ISS
Catalog Number: 25544
Epoch time: 12133
42170542 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 301
2504 deg
Eccentricity:
0011384
Arg of perigee: 307
6672 deg
Mean anomaly: 52
3449 deg
Mean motion: 15
55923949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 294
Coasting Arc #12 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2012/134/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2374109
65 A = 6773825
58 meter
Y = -4060359
54 meter E =
0004937
Z = -4875616
05 I = 51
31089
XDOT = 4750
170290 Wp = 35
33801
YDOT = -5557
349810 meter/sec RA = 295
79855 deg
ZDOT = 2320
210695 TA = 257
43618
MA = 257
49141
Ha = 218
699 n
mi
Hp = 213
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7789073
67 X = -2304844
70
Y = -13321389
57 feet Y = -4086520
89 meter
Z = -15996115
64 Z = -4886981
28
XDOT = 15584
548196 XDOT = 4800
689556
YDOT = -18232
774967 feet/sec YDOT = -5503
948062 meter/sec
ZDOT = 7612
239812 ZDOT = 2343
409458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8836050
29 X = -2693228
13
Y = -12592445
18 feet Y = -3838177
29 meter
Z = -16042423
25 Z = -4889730
61
XDOT = 12951
884373 XDOT = 3947
734357
YDOT = -18886
744560 feet/sec YDOT = -5756
679742 meter/sec
ZDOT = 7708
084730 ZDOT = 2349
424226
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 12134
38510827
00016717 00000-0 10270-3 0 9114
2 25544 51
6374 296
4327 0011461 311
1145 48
9019 15
55965601 12591
Satellite: ISS
Catalog Number: 25544
Epoch time: 12134
38510827 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 296
4327 deg
Eccentricity:
0011461
Arg of perigee: 311
1145 deg
Mean anomaly: 48
9019 deg
Mean motion: 15
55965601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 299
Coasting Arc #13 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2012/135/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 852303
62 A = 6778553
09 meter
Y = 5726171
87 meter E =
0009515
Z = 3531221
33 I = 51
31519
XDOT = -5149
755083 Wp = 23
64908
YDOT = 3521
108211 meter/sec RA = 290
76990 deg
ZDOT = -4454
067091 TA = 114
50734
MA = 114
40810
Ha = 218
963 n
mi
Hp = 212
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2796271
73 X = 771055
07
Y = 18786653
12 feet Y = 5735248
51 meter
Z = 11585371
83 Z = 3535164
57
XDOT = -16895
521926 XDOT = -5167
109086
YDOT = 11552
192292 feet/sec YDOT = 3463
423514 meter/sec
ZDOT = -14613
081007 ZDOT = -4479
126629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4688424
63 X = 1429031
83
Y = 18396005
36 feet Y = 5607102
43 meter
Z = 11601033
27 Z = 3535994
94
XDOT = -14155
308030 XDOT = -4314
537888
YDOT = 12914
531728 feet/sec YDOT = 3936
349271 meter/sec
ZDOT = -14716
371745 ZDOT = -4485
550108
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 12135
41272535
00016717 00000-0 10270-3 0 9121
2 25544 51
6378 291
2952 0011695 314
8759 45
1444 15
56012299 12758
Satellite: ISS
Catalog Number: 25544
Epoch time: 12135
41272535 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 291
2952 deg
Eccentricity:
0011695
Arg of perigee: 314
8759 deg
Mean anomaly: 45
1444 deg
Mean motion: 15
56012299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 313
Coasting Arc #14 (Orbit 1289)
---------------------------------------
Vector Time (GMT): 2012/136/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 594565
57 A = 6782977
93 meter
Y = -6574109
03 meter E =
0015409
Z = -1515140
20 I = 51
31833
XDOT = 5021
786120 Wp = 350
03593
YDOT = -867
832499 meter/sec RA = 285
75728 deg
ZDOT = 5742
257907 TA = 353
31051
MA = 353
33105
Ha = 219
126 n
mi
Hp = 212
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1950674
44 X = 675394
69
Y = -21568599
17 feet Y = -6567008
26 meter
Z = -4970932
42 Z = -1512055
58
XDOT = 16475
676247 XDOT = 5003
222283
YDOT = -2847
219485 feet/sec YDOT = -811
779677 meter/sec
ZDOT = 18839
428829 ZDOT = 5766
608665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -673315
73 X = -205226
63
Y = -21649206
91 feet Y = -6598678
27 meter
Z = -4957646
22 Z = -1511090
57
XDOT = 14310
775807 XDOT = 4361
924466
YDOT = -4777
587337 feet/sec YDOT = -1456
208620 meter/sec
ZDOT = 18939
555877 ZDOT = 5772
776631
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 12136
37610761
00016717 00000-0 10270-3 0 9135
2 25544 51
6363 286
4773 0011553 318
4292 41
5980 15
55982053 12909
Satellite: ISS
Catalog Number: 25544
Epoch time: 12136
37610761 = yrday
fracday
Element set: 913
Inclination: 51
6363 deg
RA of node: 286
4773 deg
Eccentricity:
0011553
Arg of perigee: 318
4292 deg
Mean anomaly: 41
5980 deg
Mean motion: 15
55982053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1290
Checksum: 308
Coasting Arc #15 (Orbit 1305)
---------------------------------------
Vector Time (GMT): 2012/137/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1884881
05 A = 6783515
92 meter
Y = 6467333
36 meter E =
0001430
Z = -805229
70 I = 51
31337
XDOT = -4434
274676 Wp = 339
49599
YDOT = -2029
144764 meter/sec RA = 280
75587 deg
ZDOT = -5913
146481 TA = 209
24994
MA = 209
25795
Ha = 219
329 n
mi
Hp = 212
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6183992
95 X = -1953148
32
Y = 21218285
31 feet Y = 6445873
77 meter
Z = -2641829
72 Z = -814552
15
XDOT = -14548
145264 XDOT = -4382
529670
YDOT = -6657
299095 feet/sec YDOT = -2078
442098 meter/sec
ZDOT = -19400
086881 ZDOT = -5934
562648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3149296
44 X = -959905
56
Y = 21870809
02 feet Y = 6666222
59 meter
Z = -2680729
22 Z = -817086
27
XDOT = -13622
325978 XDOT = -4152
084958
YDOT = -4351
993212 feet/sec YDOT = -1326
487531 meter/sec
ZDOT = -19487
888435 ZDOT = -5939
908395
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 12137
40370172
00016717 00000-0 10270-3 0 9140
2 25544 51
6362 281
3396 0011608 322
9393 37
0958 15
56030438 13061
Satellite: ISS
Catalog Number: 25544
Epoch time: 12137
40370172 = yrday
fracday
Element set: 914
Inclination: 51
6362 deg
RA of node: 281
3396 deg
Eccentricity:
0011608
Arg of perigee: 322
9393 deg
Mean anomaly: 37
0958 deg
Mean motion: 15
56030438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1306
Checksum: 295
Coasting Arc #16 (Orbit 1321)
---------------------------------------
Vector Time (GMT): 2012/138/08:57:21
008
Vector Time (MET): N/A
Weight (LBS) : 911751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2929285
02 A = 6779963
49 meter
Y = -5333069
58 meter E =
0012901
Z = 2971070
05 I = 51
29625
XDOT = 3518
058899 Wp = 30
71167
YDOT = 4691
985426 meter/sec RA = 275
74633 deg
ZDOT = 4954
907321 TA = 3
50025
MA = 3
49124
Ha = 219
315 n
mi
Hp = 212
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9610515
15 X = 2974269
75
Y = -17496947
44 feet Y = -5300061
09 meter
Z = 9747605
15 Z = 2985409
69
XDOT = 11542
187989 XDOT = 3441
260470
YDOT = 15393
652971 feet/sec YDOT = 4730
896944 meter/sec
ZDOT = 16256
257616 ZDOT = 4971
811812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6696380
88 X = 2041056
89
Y = -18775036
79 feet Y = -5722631
21 meter
Z = 9807010
45 Z = 2989176
78
XDOT = 12341
273133 XDOT = 3761
620051
YDOT = 12926
741205 feet/sec YDOT = 3940
070719 meter/sec
ZDOT = 16325
280079 ZDOT = 4975
945368
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 12138
43128333
00016717 00000-0 10270-3 0 9155
2 25544 51
6355 276
1999 0011471 325
8931 34
1485 15
56044322 13220
Satellite: ISS
Catalog Number: 25544
Epoch time: 12138
43128333 = yrday
fracday
Element set: 915
Inclination: 51
6355 deg
RA of node: 276
1999 deg
Eccentricity:
0011471
Arg of perigee: 325
8931 deg
Mean anomaly: 34
1485 deg
Mean motion: 15
56044322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1322
Checksum: 299
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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