[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 22nd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
060/10:21:47
800 3
0 4
9 4
9
N/A -3
8 -0
0 220
2
000/00:01:35
600 0
2 0
0 201
8
Coasting Arc #1 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2012/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4995614
51 A = 6770708
18 meter
Y = 3267301
41 meter E =
0032321
Z = 3177910
94 I = 51
60022
XDOT = -5122
550208 Wp = 75
19484
YDOT = -3109
011212 meter/sec RA = 351
77229 deg
ZDOT = -4807
171131 TA = 67
96100
MA = 67
61801
Ha = 220
640 n
mi
Hp = 199
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16389811
39 X = -5047215
97
Y = 10719492
81 feet Y = 3211149
04 meter
Z = 10426217
00 Z = 3153517
64
XDOT = -16806
267088 XDOT = -5064
052430
YDOT = -10200
168020 feet/sec YDOT = -3165
967946 meter/sec
ZDOT = -15771
558829 ZDOT = -4831
913244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19623558
02 X = -5981260
49
Y = 728490
49 feet Y = 222043
90 meter
Z = 10325924
48 Z = 3147341
78
XDOT = -9028
255509 XDOT = -2751
812279
YDOT = -15913
220735 feet/sec YDOT = -4850
349680 meter/sec
ZDOT = -15872
732838 ZDOT = -4838
008969
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 12051
53864572
00016717 00000-0 10270-3 0 9006
2 25544 51
6417 352
1258 0020494 64
0746 296
2519 15
59095364 39674
Satellite: ISS
Catalog Number: 25544
Epoch time: 12051
53864572 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 352
1258 deg
Eccentricity:
0020494
Arg of perigee: 64
0746 deg
Mean anomaly: 296
2519 deg
Mean motion: 15
59095364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 324
Coasting Arc #2 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6567281
50 A = 6774896
40 meter
Y = -1616855
31 meter E =
0031918
Z = -89470
29 I = 51
58444
XDOT = 1198
071674 Wp = 58
86812
YDOT = 4621
764440 meter/sec RA = 346
77002 deg
ZDOT = 6019
035194 TA = 300
16456
MA = 300
48041
Ha = 220
585 n
mi
Hp = 199
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21546199
16 X = 6585308
03
Y = -5304643
41 feet Y = -1543315
14 meter
Z = -293537
69 Z = -57523
69
XDOT = 3930
681344 XDOT = 1117
062811
YDOT = 15163
269161 feet/sec YDOT = 4634
709564 meter/sec
ZDOT = 19747
490794 ZDOT = 6024
658071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21315754
38 X = 6497041
93
Y = 6170602
66 feet Y = 1880799
69 meter
Z = -162426
27 Z = -49507
53
XDOT = -3825
527649 XDOT = -1166
020827
YDOT = 13485
566723 feet/sec YDOT = 4110
400737 meter/sec
ZDOT = 19770
150343 ZDOT = 6025
941825
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 12052
50009798
00016717 00000-0 10270-3 0 9016
2 25544 51
6417 347
2975 0020443 67
6255 292
7064 15
59108224 39826
Satellite: ISS
Catalog Number: 25544
Epoch time: 12052
50009798 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 347
2975 deg
Eccentricity:
0020443
Arg of perigee: 67
6255 deg
Mean anomaly: 292
7064 deg
Mean motion: 15
59108224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 316
Coasting Arc #3 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2012/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5979533
23 A = 6770463
38 meter
Y = -651994
49 meter E =
0024498
Z = -3135421
61 I = 51
54184
XDOT = 3080
054980 Wp = 76
32374
YDOT = -5067
471751 meter/sec RA = 341
76550 deg
ZDOT = -4846
407744 TA = 139
85426
MA = 139
67302
Ha = 220
517 n
mi
Hp = 199
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19617891
17 X = -5956567
28
Y = -2139089
54 feet Y = -718733
22 meter
Z = -10286816
32 Z = -3164413
37
XDOT = 10105
167256 XDOT = 3160
033742
YDOT = -16625
563489 feet/sec YDOT = -5032
581966 meter/sec
ZDOT = -15900
287874 ZDOT = -4831
250579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16067986
69 X = -4897522
34
Y = -11348961
73 feet Y = -3459163
54 meter
Z = -10405614
80 Z = -3171631
39
XDOT = 16153
781566 XDOT = 4923
672621
YDOT = -8427
407779 feet/sec YDOT = -2568
673891 meter/sec
ZDOT = -15837
724179 ZDOT = -4827
338330
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 12053
52562708
00016717 00000-0 10270-3 0 9025
2 25544 51
6426 342
1458 0020468 71
4638 288
8739 15
59157607 39982
Satellite: ISS
Catalog Number: 25544
Epoch time: 12053
52562708 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 342
1458 deg
Eccentricity:
0020468
Arg of perigee: 71
4638 deg
Mean anomaly: 288
8739 deg
Mean motion: 15
59157607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 341
Coasting Arc #4 (Orbit 4013)
---------------------------------------
Vector Time (GMT): 2012/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3431195
55 A = 6763590
08 meter
Y = 2890072
37 meter E =
0024025
Z = 5040401
48 I = 51
49037
XDOT = -6185
759090 Wp = 84
53999
YDOT = 4211
976249 meter/sec RA = 336
72482 deg
ZDOT = 1790
737143 TA = 348
13013
MA = 348
18666
Ha = 220
317 n
mi
Hp = 199
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11257203
23 X = 3374138
52
Y = 9481864
73 feet Y = 2928123
64 meter
Z = 16536750
25 Z = 5056930
83
XDOT = -20294
485204 XDOT = -6241
097339
YDOT = 13818
819716 feet/sec YDOT = 4142
494054 meter/sec
ZDOT = 5875
121860 ZDOT = 1760
552747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5397848
50 X = 1645264
22
Y = 13610877
59 feet Y = 4148595
49 meter
Z = 16604268
58 Z = 5060981
06
XDOT = -23445
486643 XDOT = -7146
184329
YDOT = 2262
006728 feet/sec YDOT = 689
459651 meter/sec
ZDOT = 5751
035970 ZDOT = 1752
915764
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 12054
55113441
00016717 00000-0 10270-3 0 9036
2 25544 51
6423 336
9953 0020261 75
4746 284
8655 15
59210427 40148
Satellite: ISS
Catalog Number: 25544
Epoch time: 12054
55113441 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 336
9953 deg
Eccentricity:
0020261
Arg of perigee: 75
4746 deg
Mean anomaly: 284
8655 deg
Mean motion: 15
59210427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4014
Checksum: 298
Coasting Arc #5 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2012/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 92852
80 A = 6764004
80 meter
Y = -4579171
17 meter E =
0032273
Z = -5005030
05 I = 51
46429
XDOT = 7105
404871 Wp = 88
42305
YDOT = -2025
281878 meter/sec RA = 331
66036 deg
ZDOT = 1996
808751 TA = 200
99430
MA = 201
12710
Ha = 220
456 n
mi
Hp = 199
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 304635
18 X = 168364
03
Y = -15023527
47 feet Y = -4577711
18 meter
Z = -16420702
27 Z = -5004395
07
XDOT = 23311
695772 XDOT = 7117
824001
YDOT = -6644
625584 feet/sec YDOT = -1945
755197 meter/sec
ZDOT = 6551
209814 ZDOT = 2031
356311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7185438
33 X = 2190121
60
Y = -13201005
76 feet Y = -4023666
55 meter
Z = -16417721
11 Z = -5004121
39
XDOT = 22787
357272 XDOT = 6945
586497
YDOT = 4128
601926 feet/sec YDOT = 1258
397867 meter/sec
ZDOT = 6692
989861 ZDOT = 2040
023310
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 12055
51253142
00016717 00000-0 10270-3 0 9047
2 25544 51
6428 332
1658 0020347 78
7325 281
6116 15
59201778 40299
Satellite: ISS
Catalog Number: 25544
Epoch time: 12055
51253142 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 332
1658 deg
Eccentricity:
0020347
Arg of perigee: 78
7325 deg
Mean anomaly: 281
6116 deg
Mean motion: 15
59201778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 300
Coasting Arc #6 (Orbit 4044)
---------------------------------------
Vector Time (GMT): 2012/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3456536
95 A = 6771039
07 meter
Y = 5036924
18 meter E =
0033387
Z = 2892512
11 I = 51
46128
XDOT = -5728
119757 Wp = 88
66933
YDOT = -1017
100058 meter/sec RA = 326
61714 deg
ZDOT = -5023
076021 TA = 58
16140
MA = 57
83680
Ha = 220
471 n
mi
Hp = 199
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11340344
31 X = -3526654
94
Y = 16525341
81 feet Y = 4997879
30 meter
Z = 9489869
13 Z = 2875549
79
XDOT = -18793
043821 XDOT = -5691
919950
YDOT = -3336
942447 feet/sec YDOT = -1080
953548 meter/sec
ZDOT = -16479
908205 ZDOT = -5050
814577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17494324
55 X = -5332270
12
Y = 9846902
27 feet Y = 3001335
81 meter
Z = 9419929
47 Z = 2871194
50
XDOT = -14613
164479 XDOT = -4454
092533
YDOT = -9927
421173 feet/sec YDOT = -3025
877974 meter/sec
ZDOT = -16593
520759 ZDOT = -5057
705127
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 12056
53800069
00016717 00000-0 10270-3 0 9057
2 25544 51
6423 327
0140 0020359 82
7691 277
5778 15
59225752 40451
Satellite: ISS
Catalog Number: 25544
Epoch time: 12056
53800069 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 327
0140 deg
Eccentricity:
0020359
Arg of perigee: 82
7691 deg
Mean anomaly: 277
5778 deg
Mean motion: 15
59225752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4045
Checksum: 312
Coasting Arc #7 (Orbit 4060)
---------------------------------------
Vector Time (GMT): 2012/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5443991
18 A = 6774420
42 meter
Y = -4007071
76 meter E =
0031384
Z = 301756
73 I = 51
44841
XDOT = 2606
433248 Wp = 71
39210
YDOT = 4030
281152 meter/sec RA = 321
60623 deg
ZDOT = 5995
097403 TA = 291
87696
MA = 292
21040
Ha = 220
365 n
mi
Hp = 199
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17860863
45 X = 5486928
60
Y = -13146560
90 feet Y = -3945953
59 meter
Z = 990015
51 Z = 328307
78
XDOT = 8551
290183 XDOT = 2532
049580
YDOT = 13222
707193 feet/sec YDOT = 4059
012554 meter/sec
ZDOT = 19668
954735 ZDOT = 6007
578158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21741231
81 X = 6626727
46
Y = -4351242
16 feet Y = -1326258
61 meter
Z = 1099167
14 Z = 335026
14
XDOT = 1723
017557 XDOT = 525
175751
YDOT = 13964
515125 feet/sec YDOT = 4256
384210 meter/sec
ZDOT = 19719
779878 ZDOT = 6010
588907
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 12057
56344907
00016717 00000-0 10270-3 0 9066
2 25544 51
6425 321
8626 0020271 86
2306 274
1167 15
59257068 40617
Satellite: ISS
Catalog Number: 25544
Epoch time: 12057
56344907 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 321
8626 deg
Eccentricity:
0020271
Arg of perigee: 86
2306 deg
Mean anomaly: 274
1167 deg
Mean motion: 15
59257068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4061
Checksum: 307
Coasting Arc #8 (Orbit 4075)
---------------------------------------
Vector Time (GMT): 2012/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5623982
87 A = 6769094
52 meter
Y = 1499119
85 meter E =
0025243
Z = -3478477
91 I = 51
40838
XDOT = 1163
047264 Wp = 88
65182
YDOT = -6071
181744 meter/sec RA = 316
58820 deg
ZDOT = -4524
803122 TA = 132
36975
MA = 132
15576
Ha = 220
230 n
mi
Hp = 199
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18451387
37 X = -5623430
83
Y = 4918372
22 feet Y = 1436231
81 meter
Z = -11412329
09 Z = -3505797
50
XDOT = 3815
771865 XDOT = 1252
830281
YDOT = -19918
575277 feet/sec YDOT = -6057
674189 meter/sec
ZDOT = -14845
154600 ZDOT = -4518
934578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18789576
40 X = -5727062
89
Y = -3004139
49 feet Y = -915661
72 meter
Z = -11524421
95 Z = -3512643
81
XDOT = 11468
870642 XDOT = 3495
711772
YDOT = -15225
929144 feet/sec YDOT = -4640
863203 meter/sec
ZDOT = -14820
608315 ZDOT = -4517
321414
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 12058
52478739
00016717 00000-0 10270-3 0 9075
2 25544 51
6430 317
0321 0020139 89
9327 270
4136 15
59295382 40760
Satellite: ISS
Catalog Number: 25544
Epoch time: 12058
52478739 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 317
0321 deg
Eccentricity:
0020139
Arg of perigee: 89
9327 deg
Mean anomaly: 270
4136 deg
Mean motion: 15
59295382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4076
Checksum: 319
Coasting Arc #9 (Orbit 4091)
---------------------------------------
Vector Time (GMT): 2012/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4015305
99 A = 6762677
58 meter
Y = 1681551
16 meter E =
0023709
Z = 5155614
15 I = 51
36561
XDOT = -4245
836293 Wp = 98
34804
YDOT = 6294
918390 meter/sec RA = 311
53162 deg
ZDOT = 1245
319582 TA = 339
64697
MA = 339
74130
Ha = 220
063 n
mi
Hp = 199
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13173576
08 X = 3971159
52
Y = 5516900
15 feet Y = 1726206
30 meter
Z = 16914744
57 Z = 5175012
81
XDOT = -13929
909099 XDOT = -4321
961206
YDOT = 20652
619389 feet/sec YDOT = 6247
013275 meter/sec
ZDOT = 4085
694168 ZDOT = 1224
508353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9862078
99 X = 3005961
68
Y = 10199380
33 feet Y = 3108771
12 meter
Z = 16994114
18 Z = 5179806
00
XDOT = -20189
051971 XDOT = -6153
623041
YDOT = 12811
721871 feet/sec YDOT = 3905
012826 meter/sec
ZDOT = 3999
890525 ZDOT = 1219
166632
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 12059
55019563
00016717 00000-0 10270-3 0 9086
2 25544 51
6427 311
8802 0020127 93
8021 266
5436 15
59345024 40920
Satellite: ISS
Catalog Number: 25544
Epoch time: 12059
55019563 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 311
8802 deg
Eccentricity:
0020127
Arg of perigee: 93
8021 deg
Mean anomaly: 266
5436 deg
Mean motion: 15
59345024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4092
Checksum: 300
Coasting Arc #10 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2012/060/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2988262
12 A = 6764932
32 meter
Y = -3048551
31 meter E =
0030964
Z = -5274918
45 I = 51
34570
XDOT = 4930
731632 Wp = 96
07338
YDOT = -5823
938602 meter/sec RA = 306
81351 deg
ZDOT = 572
261823 TA = 179
42356
MA = 179
41998
Ha = 220
151 n
mi
Hp = 201
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9804009
59 X = -2928326
39
Y = -10001808
77 feet Y = -3081633
09 meter
Z = -17306162
90 Z = -5289289
40
XDOT = 16176
941051 XDOT = 4992
709729
YDOT = -19107
410111 feet/sec YDOT = -5768
453547 meter/sec
ZDOT = 1877
499419 ZDOT = 596
365742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 581681
06 X = 177296
39
Y = -13920589
29 feet Y = -4242995
62 meter
Z = -17364817
82 Z = -5292796
47
XDOT = 23972
473833 XDOT = 7306
810024
YDOT = -1465
394153 feet/sec YDOT = -446
652138 meter/sec
ZDOT = 1976
756595 ZDOT = 602
515410
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 12060
44741361
00016717 00000-0 10270-3 0 9095
2 25544 51
6423 307
3716 0016255 97
9065 262
3936 15
58451073 41066
Satellite: ISS
Catalog Number: 25544
Epoch time: 12060
44741361 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 307
3716 deg
Eccentricity:
0016255
Arg of perigee: 97
9065 deg
Mean anomaly: 262
3936 deg
Mean motion: 15
58451073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 305
Coasting Arc #11 (Orbit 4121)
---------------------------------------
Vector Time (GMT): 2012/061/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 471945
66 A = 6769700
00 meter
Y = 5388552
83 meter E =
0026386
Z = 4047142
47 I = 51
34407
XDOT = -5723
437603 Wp = 91
75548
YDOT = 3404
258669 meter/sec RA = 301
75547 deg
ZDOT = -3844
290807 TA = 38
14580
MA = 37
95934
Ha = 220
077 n
mi
Hp = 201
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1548378
14 X = 391994
82
Y = 17678979
09 feet Y = 5393383
59 meter
Z = 13278026
46 Z = 4049240
66
XDOT = -18777
682424 XDOT = -5742
404849
YDOT = 11168
827654 feet/sec YDOT = 3340
149412 meter/sec
ZDOT = -12612
502647 ZDOT = -3872
140925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11586729
28 X = -3531635
08
Y = 13434075
87 feet Y = 4094706
32 meter
Z = 13286198
60 Z = 4049633
33
XDOT = -20091
348415 XDOT = -6123
842997
YDOT = -4674
030453 feet/sec YDOT = -1424
644482 meter/sec
ZDOT = -12726
918104 ZDOT = -3879
164638
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 12061
47338145
00016717 00000-0 10270-3 0 9103
2 25544 51
6418 302
2234 0016256 101
5792 258
7189 15
58477177 41229
Satellite: ISS
Catalog Number: 25544
Epoch time: 12061
47338145 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 302
2234 deg
Eccentricity:
0016256
Arg of perigee: 101
5792 deg
Mean anomaly: 258
7189 deg
Mean motion: 15
58477177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4122
Checksum: 306
Coasting Arc #12 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2012/062/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1875110
11 A = 6775677
32 meter
Y = -6344441
22 meter E =
0020844
Z = -1473863
83 I = 51
35013
XDOT = 5063
742000 Wp = 83
10250
YDOT = 176
592799 meter/sec RA = 296
72784 deg
ZDOT = 5754
693973 TA = 260
73074
MA = 260
96653
Ha = 219
979 n
mi
Hp = 201
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6151936
06 X = 1953075
16
Y = -20815095
85 feet Y = -6323036
72 meter
Z = -4835511
26 Z = -1464565
09
XDOT = 16613
326773 XDOT = 5033
436356
YDOT = 579
372699 feet/sec YDOT = 233
049516 meter/sec
ZDOT = 18880
229570 ZDOT = 5779
219425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19005277
28 X = 5792808
52
Y = -10501707
44 feet Y = -3200920
43 meter
Z = -4796902
95 Z = -1462096
02
XDOT = 10587
017221 XDOT = 3226
922849
YDOT = 10599
379294 feet/sec YDOT = 3230
690809 meter/sec
ZDOT = 18980
737213 ZDOT = 5785
328703
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 12062
43520809
00016717 00000-0 10270-3 0 9111
2 25544 51
6425 297
3968 0016136 105
2624 255
0317 15
58517868 41378
Satellite: ISS
Catalog Number: 25544
Epoch time: 12062
43520809 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 297
3968 deg
Eccentricity:
0016136
Arg of perigee: 105
2624 deg
Mean anomaly: 255
0317 deg
Mean motion: 15
58517868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 313
Coasting Arc #13 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2012/063/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3638891
15 A = 6775359
89 meter
Y = 5451674
58 meter E =
0022805
Z = -1704059
45 I = 51
33642
XDOT = -3310
417242 Wp = 119
51893
YDOT = -3962
570188 meter/sec RA = 291
71646 deg
ZDOT = -5676
320737 TA = 79
27970
MA = 79
02302
Ha = 219
888 n
mi
Hp = 202
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11938619
27 X = -3691304
64
Y = 17886071
47 feet Y = 5410689
11 meter
Z = -5590746
22 Z = -1721864
30
XDOT = -10860
948958 XDOT = -3238
287149
YDOT = -13000
558361 feet/sec YDOT = -3999
186315 meter/sec
ZDOT = -18623
099531 ZDOT = -5692
226900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20951234
87 X = -6385936
39
Y = 4760448
72 feet Y = 1450984
77 meter
Z = -5664142
58 Z = -1726430
66
XDOT = 1515
992830 XDOT = 462
074614
YDOT = -15300
382163 feet/sec YDOT = -4663
556483 meter/sec
ZDOT = -18687
991499 ZDOT = -5696
099809
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 12063
46113854
00016717 00000-0 10270-3 0 9124
2 25544 51
6427 292
2478 0016026 109
4771 250
8116 15
58504820 41539
Satellite: ISS
Catalog Number: 25544
Epoch time: 12063
46113854 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 292
2478 deg
Eccentricity:
0016026
Arg of perigee: 109
4771 deg
Mean anomaly: 250
8116 deg
Mean motion: 15
58504820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4153
Checksum: 297
Coasting Arc #14 (Orbit 4168)
---------------------------------------
Vector Time (GMT): 2012/064/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4398268
85 A = 6768838
21 meter
Y = -2943015
67 meter E =
0026045
Z = 4204837
37 I = 51
30454
XDOT = 1009
734162 Wp = 109
82949
YDOT = 6707
621856 meter/sec RA = 286
68443 deg
ZDOT = 3611
621376 TA = 303
02099
MA = 303
27097
Ha = 219
745 n
mi
Hp = 202
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14430015
90 X = 4410425
61
Y = -9655563
22 feet Y = -2893763
26 meter
Z = 13795398
20 Z = 4226233
25
XDOT = 3312
776122 XDOT = 917
109053
YDOT = 22006
633385 feet/sec YDOT = 6718
395669 meter/sec
ZDOT = 11849
151495 ZDOT = 3616
301097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17096653
65 X = 5211060
03
Y = 2593486
45 feet Y = 790494
67 meter
Z = 13883318
54 Z = 4231635
49
XDOT = -12310
724137 XDOT = -3752
308717
YDOT = 17153
761944 feet/sec YDOT = 5228
466641 meter/sec
ZDOT = 11867
830627 ZDOT = 3617
314775
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 12064
48704935
00016717 00000-0 10270-3 0 9134
2 25544 51
6425 287
0996 0016037 112
4846 247
8009 15
58555674 41690
Satellite: ISS
Catalog Number: 25544
Epoch time: 12064
48704935 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 287
0996 deg
Eccentricity:
0016037
Arg of perigee: 112
4846 deg
Mean anomaly: 247
8009 deg
Mean motion: 15
58555674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4169
Checksum: 338
Coasting Arc #15 (Orbit 4183)
---------------------------------------
Vector Time (GMT): 2012/065/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4205166
09 A = 6764368
08 meter
Y = -601687
97 meter E =
0029820
Z = -5289190
37 I = 51
28193
XDOT = 1358
794594 Wp = 102
51040
YDOT = -7529
129986 meter/sec RA = 281
61864 deg
ZDOT = -231
252835 TA = 165
31387
MA = 165
22705
Ha = 219
632 n
mi
Hp = 201
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13796476
69 X = -4172432
22
Y = -1974041
91 feet Y = -648530
17 meter
Z = -17352986
79 Z = -5309538
87
XDOT = 4457
987514 XDOT = 1444
009203
YDOT = -24701
870033 feet/sec YDOT = -7513
458665 meter/sec
ZDOT = -758
703526 ZDOT = -224
444386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8930296
85 X = -2721954
48
Y = -10563578
66 feet Y = -3219778
78 meter
Z = -17436351
83 Z = -5314600
04
XDOT = 18961
737950 XDOT = 5779
537727
YDOT = -14864
744169 feet/sec YDOT = -4530
774023 meter/sec
ZDOT = -730
246365 ZDOT = -222
579092
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 12065
44882199
00016717 00000-0 10270-3 0 9141
2 25544 51
6421 282
2721 0015829 116
1140 244
1646 15
58609000 41842
Satellite: ISS
Catalog Number: 25544
Epoch time: 12065
44882199 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 282
2721 deg
Eccentricity:
0015829
Arg of perigee: 116
1140 deg
Mean anomaly: 244
1646 deg
Mean motion: 15
58609000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4184
Checksum: 297
Coasting Arc #16 (Orbit 4199)
---------------------------------------
Vector Time (GMT): 2012/066/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3121482
21 A = 6767642
95 meter
Y = 4017795
04 meter E =
0022497
Z = 4441043
07 I = 51
28820
XDOT = -3308
699356 Wp = 101
22426
YDOT = 6147
281728 meter/sec RA = 276
55048 deg
ZDOT = -3226
276403 TA = 21
34458
MA = 21
25090
Ha = 219
358 n
mi
Hp = 202
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10241083
38 X = 3054749
29
Y = 13181742
27 feet Y = 4052328
75 meter
Z = 14570351
27 Z = 4456044
23
XDOT = -10855
312848 XDOT = -3361
521395
YDOT = 20168
247139 feet/sec YDOT = 6109
986109 meter/sec
ZDOT = -10584
896336 ZDOT = -3242
478552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -868979
00 X = -264864
80
Y = 16616126
18 feet Y = 5064595
26 meter
Z = 14631557
68 Z = 4459698
78
XDOT = -20105
359077 XDOT = -6128
113447
YDOT = 8355
576681 feet/sec YDOT = 2546
779772 meter/sec
ZDOT = -10651
746092 ZDOT = -3246
652209
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 12066
47469384
00016717 00000-0 10270-3 0 9153
2 25544 51
6419 277
1232 0015657 119
6955 240
5761 15
58667434 42002
Satellite: ISS
Catalog Number: 25544
Epoch time: 12066
47469384 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 277
1232 deg
Eccentricity:
0015657
Arg of perigee: 119
6955 deg
Mean anomaly: 240
5761 deg
Mean motion: 15
58667434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4200
Checksum: 329
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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