[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 1st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 2482)
---------------------------------------
Vector Time (GMT): 2012/212/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2868708
33 A = 6779544
52 meter
Y = 4446506
15 meter E =
0008380
Z = -4247114
41 I = 51
28918
XDOT = -3609
637284 Wp = 59
18750
YDOT = -5737
759886 meter/sec RA = 262
79272 deg
ZDOT = -3570
054986 TA = 174
14974
MA = 174
13995
Ha = 219
749 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9411772
74 X = -2897585
77
Y = 14588274
77 feet Y = 4414265
44 meter
Z = -13934102
39 Z = -4261119
87
XDOT = -11842
642007 XDOT = -3527
866030
YDOT = -18824
671543 feet/sec YDOT = -5777
667523 meter/sec
ZDOT = -11712
778826 ZDOT = -3587
392048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17305887
59 X = -5274834
54
Y = -529103
64 feet Y = -161270
79 meter
Z = -13992310
04 Z = -4264856
10
XDOT = 10090
186194 XDOT = 3075
488752
YDOT = -18495
505902 feet/sec YDOT = -5637
430199 meter/sec
ZDOT = -11783
717054 ZDOT = -3591
676958
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 12213
00222063
00016717 00000-0 10270-3 0 9001
2 25544 51
6429 263
4890 0001550 339
1702 20
9388 15
54843616 24837
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
00222063 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 263
4890 deg
Eccentricity:
0001550
Arg of perigee: 339
1702 deg
Mean anomaly: 20
9388 deg
Mean motion: 15
54843616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2483
Checksum: 282
Coasting Arc #2 (Orbit 2498)
---------------------------------------
Vector Time (GMT): 2012/213/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3607751
17 A = 6776073
31 meter
Y = -2631314
60 meter E =
0003999
Z = 5093680
69 I = 51
28229
XDOT = 2816
991523 Wp = 110
00785
YDOT = 6955
690236 meter/sec RA = 257
76649 deg
ZDOT = 1595
613730 TA = 324
51974
MA = 324
54633
Ha = 219
692 n
mi
Hp = 213
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11836453
97 X = 3612163
58
Y = -8632921
92 feet Y = -2590946
23 meter
Z = 16711550
81 Z = 5111217
06
XDOT = 9242
098171 XDOT = 2731
251253
YDOT = 22820
506024 feet/sec YDOT = 6986
712055 meter/sec
ZDOT = 5234
953184 ZDOT = 1609
090527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13522058
93 X = 4121523
56
Y = 5417692
84 feet Y = 1651312
78 meter
Z = 16784142
53 Z = 5115806
64
XDOT = -14137
541121 XDOT = -4309
122534
YDOT = 18873
897617 feet/sec YDOT = 5752
763994 meter/sec
ZDOT = 5289
867682 ZDOT = 1612
351669
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 12214
03057228
00016717 00000-0 10270-3 0 9015
2 25544 51
6426 258
3566 0001523 348
7914 11
3205 15
54861309 24996
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
03057228 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 258
3566 deg
Eccentricity:
0001523
Arg of perigee: 348
7914 deg
Mean anomaly: 11
3205 deg
Mean motion: 15
54861309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2499
Checksum: 295
Coasting Arc #3 (Orbit 2513)
---------------------------------------
Vector Time (GMT): 2012/214/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4235995
98 A = 6775206
36 meter
Y = 594166
02 meter E =
0014319
Z = -5266613
11 I = 51
28613
XDOT = -1795
665484 Wp = 88
54158
YDOT = -7420
932691 meter/sec RA = 252
73262 deg
ZDOT = 608
859698 TA = 187
29526
MA = 187
31611
Ha = 219
735 n
mi
Hp = 213
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13897624
61 X = -4216741
87
Y = 1949363
58 feet Y = 546904
44 meter
Z = -17278914
41 Z = -5287144
07
XDOT = -5891
290957 XDOT = -1715
507256
YDOT = -24346
892030 feet/sec YDOT = -7440
564783 meter/sec
ZDOT = 1997
571188 ZDOT = 600
330932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9111096
69 X = -2777062
27
Y = -10535459
57 feet Y = -3211208
08 meter
Z = -17363665
52 Z = -5292445
25
XDOT = 16494
832084 XDOT = 5027
624819
YDOT = -17490
517956 feet/sec YDOT = -5331
109873 meter/sec
ZDOT = 1963
093031 ZDOT = 598
350756
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 12214
99463645
00016717 00000-0 10270-3 0 9025
2 25544 51
6414 253
5441 0001618 348
0448 12
0667 15
54907836 25146
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
99463645 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 253
5441 deg
Eccentricity:
0001618
Arg of perigee: 348
0448 deg
Mean anomaly: 12
0667 deg
Mean motion: 15
54907836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2514
Checksum: 305
Coasting Arc #4 (Orbit 2529)
---------------------------------------
Vector Time (GMT): 2012/215/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4661731
17 A = 6777454
20 meter
Y = 1450394
14 meter E =
0008405
Z = 4697513
08 I = 51
30412
XDOT = 552
393504 Wp = 51
67461
YDOT = 7142
374653 meter/sec RA = 247
70267 deg
ZDOT = -2744
980526 TA = 65
65650
MA = 65
56877
Ha = 219
569 n
mi
Hp = 213
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15294393
61 X = 4622347
20
Y = 4758510
95 feet Y = 1502304
15 meter
Z = 15411788
31 Z = 4720063
39
XDOT = 1812
314646 XDOT = 485
819112
YDOT = 23432
987706 feet/sec YDOT = 7148
179713 meter/sec
ZDOT = -9005
841622 ZDOT = -2742
458556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4500153
16 X = 1371646
68
Y = 15278694
41 feet Y = 4656946
05 meter
Z = 15504684
46 Z = 4725827
82
XDOT = -17319
431271 XDOT = -5278
962651
YDOT = 14258
420154 feet/sec YDOT = 4345
966463 meter/sec
ZDOT = -8996
100101 ZDOT = -2742
011311
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 12216
02295649
00016717 00000-0 10270-3 0 9039
2 25544 51
6414 248
4115 0001690 348
7386 11
3729 15
54949237 25305
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
02295649 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 248
4115 deg
Eccentricity:
0001690
Arg of perigee: 348
7386 deg
Mean anomaly: 11
3729 deg
Mean motion: 15
54949237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2530
Checksum: 308
Coasting Arc #5 (Orbit 2544)
---------------------------------------
Vector Time (GMT): 2012/216/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4824487
40 A = 6781691
90 meter
Y = -3241072
32 meter E =
0005053
Z = -3497548
44 I = 51
32941
XDOT = 874
761081 Wp = 76
56110
YDOT = -6146
089490 meter/sec RA = 242
68327 deg
ZDOT = 4495
398310 TA = 242
10812
MA = 242
15930
Ha = 219
693 n
mi
Hp = 213
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15828370
73 X = -4770896
57
Y = -10633439
37 feet Y = -3294723
05 meter
Z = -11474896
47 Z = -3520854
94
XDOT = 2869
951054 XDOT = 921
585755
YDOT = -20164
335598 feet/sec YDOT = -6136
045613 meter/sec
ZDOT = 14748
682119 ZDOT = 4499
761423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -255734
33 X = -77947
82
Y = -19008755
14 feet Y = -5793868
57 meter
Z = -11570757
53 Z = -3526766
89
XDOT = 16760
010160 XDOT = 5108
451097
YDOT = -9201
247802 feet/sec YDOT = -2804
540330 meter/sec
ZDOT = 14767
241099 ZDOT = 4501
055087
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 12216
98699420
00016717 00000-0 10270-3 0 9040
2 25544 51
6400 243
5984 0001643 352
3837 7
7291 15
54940177 25453
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
98699420 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 243
5984 deg
Eccentricity:
0001643
Arg of perigee: 352
3837 deg
Mean anomaly: 7
7291 deg
Mean motion: 15
54940177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2545
Checksum: 317
Coasting Arc #6 (Orbit 2560)
---------------------------------------
Vector Time (GMT): 2012/217/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4614744
86 A = 6785466
92 meter
Y = 4638965
61 meter E =
0013275
Z = 1775531
04 I = 51
35751
XDOT = -2433
005662 Wp = 107
72823
YDOT = 4591
664669 meter/sec RA = 237
67954 deg
ZDOT = -5642
263981 TA = 52
68183
MA = 52
56093
Ha = 219
720 n
mi
Hp = 213
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15140239
04 X = 4553903
04
Y = 15219703
43 feet Y = 4690230
37 meter
Z = 5825233
05 Z = 1797801
06
XDOT = -7982
302042 XDOT = -2456
761434
YDOT = 15064
516630 feet/sec YDOT = 4564
324451 meter/sec
ZDOT = -18511
364768 ZDOT = -5654
140906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3520243
26 X = -1072970
15
Y = 21151833
56 feet Y = 6447078
87 meter
Z = 5916703
09 Z = 1803411
10
XDOT = -15279
217449 XDOT = -4657
105478
YDOT = 2676
956769 feet/sec YDOT = 815
936423 meter/sec
ZDOT = -18560
776843 ZDOT = -5657
324782
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 12218
01528473
00016717 00000-0 10270-3 0 9056
2 25544 51
6403 238
4655 0001760 358
1555 1
9591 15
54983573 25619
Satellite: ISS
Catalog Number: 25544
Epoch time: 12218
01528473 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 238
4655 deg
Eccentricity:
0001760
Arg of perigee: 358
1555 deg
Mean anomaly: 1
9591 deg
Mean motion: 15
54983573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2561
Checksum: 309
Coasting Arc #7 (Orbit 2576)
---------------------------------------
Vector Time (GMT): 2012/218/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3999315
82 A = 6786855
49 meter
Y = -5471948
92 meter E =
0013577
Z = 170819
89 I = 51
37796
XDOT = 3960
238320 Wp = 42
10033
YDOT = -2699
109506 meter/sec RA = 232
68407 deg
ZDOT = 5990
368735 TA = 319
74771
MA = 319
84816
Ha = 219
737 n
mi
Hp = 213
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13121114
91 X = -3938659
92
Y = -17952588
33 feet Y = -5516332
61 meter
Z = 560432
70 Z = 151539
04
XDOT = 12992
907873 XDOT = 3961
026547
YDOT = -8855
346148 feet/sec YDOT = -2654
819206 meter/sec
ZDOT = 19653
440732 ZDOT = 6009
609050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6529998
43 X = 1990343
52
Y = -21257953
41 feet Y = -6479424
20 meter
Z = 481358
81 Z = 146718
16
XDOT = 13246
627425 XDOT = 4037
572039
YDOT = 4538
995902 feet/sec YDOT = 1383
485951 meter/sec
ZDOT = 19733
064896 ZDOT = 6014
638180
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 12219
04356035
00016717 00000-0 10270-3 0 9064
2 25544 51
6390 233
3311 0001650
4777 359
6377 15
54977852 25773
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
04356035 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 233
3311 deg
Eccentricity:
0001650
Arg of perigee:
4777 deg
Mean anomaly: 359
6377 deg
Mean motion: 15
54977852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2577
Checksum: 311
Coasting Arc #8 (Orbit 2591)
---------------------------------------
Vector Time (GMT): 2012/219/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2919172
25 A = 6784886
12 meter
Y = 5739743
94 meter E =
0005377
Z = -2134894
88 I = 51
39052
XDOT = -5314
196046 Wp = 126
17419
YDOT = 667
688057 meter/sec RA = 227
69046 deg
ZDOT = -5484
109524 TA = 77
57403
MA = 77
51387
Ha = 219
773 n
mi
Hp = 213
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9577336
78 X = 2865143
01
Y = 18831180
90 feet Y = 5772085
83 meter
Z = -7004248
30 Z = -2120845
09
XDOT = -17435
026396 XDOT = -5294
627039
YDOT = 2190
577614 feet/sec YDOT = 608
370805 meter/sec
ZDOT = -17992
485314 ZDOT = -5509
877830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9002785
85 X = -2744049
13
Y = 19133490
08 feet Y = 5831887
78 meter
Z = -6946772
79 Z = -2117376
35
XDOT = -10940
444344 XDOT = -3334
647436
YDOT = -11703
528508 feet/sec YDOT = -3567
235489 meter/sec
ZDOT = -18098
871414 ZDOT = -5516
536007
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 12220
00755381
00016717 00000-0 10270-3 0 9070
2 25544 51
6387 228
5188 0001639 4
6082 355
5086 15
55001559 25921
Satellite: ISS
Catalog Number: 25544
Epoch time: 12220
00755381 = yrday
fracday
Element set: 907
Inclination: 51
6387 deg
RA of node: 228
5188 deg
Eccentricity:
0001639
Arg of perigee: 4
6082 deg
Mean anomaly: 355
5086 deg
Mean motion: 15
55001559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2592
Checksum: 305
Coasting Arc #9 (Orbit 2607)
---------------------------------------
Vector Time (GMT): 2012/220/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1455343
40 A = 6780670
97 meter
Y = -5437407
13 meter E =
0011648
Z = 3770493
45 I = 51
39768
XDOT = 6297
044348 Wp = 89
11294
YDOT = 1239
264491 meter/sec RA = 222
68651 deg
ZDOT = 4206
596262 TA = 316
29635
MA = 316
38852
Ha = 219
711 n
mi
Hp = 213
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4774748
70 X = -1412749
07
Y = -17839262
23 feet Y = -5453443
54 meter
Z = 12370385
34 Z = 3763526
95
XDOT = 20659
594318 XDOT = 6262
284112
YDOT = 4065
828381 feet/sec YDOT = 1309
487577 meter/sec
ZDOT = 13801
168840 ZDOT = 4237
102324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10882165
23 X = 3316883
96
Y = -14943722
55 feet Y = -4554846
63 meter
Z = 12342105
65 Z = 3761873
80
XDOT = 8609
372876 XDOT = 2624
136853
YDOT = 17801
886785 feet/sec YDOT = 5426
015092 meter/sec
ZDOT = 13926
948175 ZDOT = 4244
933804
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 12221
03579748
00016717 00000-0 10270-3 0 9086
2 25544 51
6384 223
3843 0001563 5
4327 354
6843 15
55039034 26084
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
03579748 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 223
3843 deg
Eccentricity:
0001563
Arg of perigee: 5
4327 deg
Mean anomaly: 354
6843 deg
Mean motion: 15
55039034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2608
Checksum: 304
Coasting Arc #10 (Orbit 2622)
---------------------------------------
Vector Time (GMT): 2012/221/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -322775
34 A = 6776472
09 meter
Y = 4687062
81 meter E =
0012993
Z = -4895634
02 I = 51
40639
XDOT = -6719
442233 Wp = 67
74389
YDOT = -2866
919751 meter/sec RA = 217
67059 deg
ZDOT = -2301
843390 TA = 179
64401
MA = 179
64309
Ha = 219
790 n
mi
Hp = 212
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1058974
20 X = -351381
35
Y = 15377502
65 feet Y = 4683293
48 meter
Z = -16061791
40 Z = -4897271
43
XDOT = -22045
414151 XDOT = -6675
702592
YDOT = -9405
904694 feet/sec YDOT = -2941
816127 meter/sec
ZDOT = -7551
979625 ZDOT = -2334
379693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12442430
76 X = -3792452
89
Y = 9085423
47 feet Y = 2769237
07 meter
Z = -16068950
01 Z = -4897815
96
XDOT = -6157
209390 XDOT = -1876
717422
YDOT = -22025
635576 feet/sec YDOT = -6713
413724 meter/sec
ZDOT = -7686
009137 ZDOT = -2342
695585
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 12221
99976237
00016717 00000-0 10270-3 0 9096
2 25544 51
6378 218
5715 0001565 18
3862 341
7347 15
55057537 26231
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
99976237 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 218
5715 deg
Eccentricity:
0001565
Arg of perigee: 18
3862 deg
Mean anomaly: 341
7347 deg
Mean motion: 15
55057537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2623
Checksum: 331
Coasting Arc #11 (Orbit 2638)
---------------------------------------
Vector Time (GMT): 2012/222/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2214680
35 A = 6774715
07 meter
Y = -3596165
76 meter E =
0003266
Z = 5294479
97 I = 51
42501
XDOT = 6489
221182 Wp = 68
61752
YDOT = 4093
648102 meter/sec RA = 212
64566 deg
ZDOT = 67
220209 TA = 20
74703
MA = 20
73378
Ha = 219
785 n
mi
Hp = 213
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7266011
66 X = 2229009
64
Y = -11798444
11 feet Y = -3571319
87 meter
Z = 17370341
10 Z = 5305273
40
XDOT = 21290
095740 XDOT = 6442
636332
YDOT = 13430
604009 feet/sec YDOT = 4165
954135 meter/sec
ZDOT = 220
538742 ZDOT = 98
631273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13612863
05 X = 4149200
66
Y = -2264485
45 feet Y = -690215
16 meter
Z = 17415195
20 Z = 5308151
50
XDOT = 3533
774399 XDOT = 1077
094437
YDOT = 23904
998278 feet/sec YDOT = 7286
243475 meter/sec
ZDOT = 349
833576 ZDOT = 106
629274
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 12223
02797574
00016717 00000-0 10270-3 0 9109
2 25544 51
6376 213
4374 0001554 23
7073 336
4152 15
55033569 26397
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
02797574 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 213
4374 deg
Eccentricity:
0001554
Arg of perigee: 23
7073 deg
Mean anomaly: 336
4152 deg
Mean motion: 15
55033569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2639
Checksum: 300
Coasting Arc #12 (Orbit 2653)
---------------------------------------
Vector Time (GMT): 2012/223/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4015710
57 A = 6776052
19 meter
Y = 2342035
61 meter E =
0012925
Z = -4941679
97 I = 51
45645
XDOT = -5512
872204 Wp = 99
87153
YDOT = -4848
947022 meter/sec RA = 207
62185 deg
ZDOT = 2184
499925 TA = 191
49785
MA = 191
52741
Ha = 219
777 n
mi
Hp = 212
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13174903
45 X = -4017595
90
Y = 7683843
86 feet Y = 2297119
09 meter
Z = -16212860
81 Z = -4961192
42
XDOT = -18086
851063 XDOT = -5468
852258
YDOT = -15908
618840 feet/sec YDOT = -4910
349343 meter/sec
ZDOT = 7166
994503 ZDOT = 2157
825617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14433159
86 X = -4399227
13
Y = -4656052
36 feet Y = -1419164
76 meter
Z = -16293601
99 Z = -4966289
89
XDOT = -515
725239 XDOT = -157
193053
YDOT = -23066
962081 feet/sec YDOT = -7030
810042 meter/sec
ZDOT = 7057
300110 ZDOT = 2151
065074
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 12223
99190812
00016717 00000-0 10270-3 0 9118
2 25544 51
6376 208
6240 0001470 30
3939 329
7299 15
55102648 26546
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
99190812 = yrday
fracday
Element set: 911
Inclination: 51
6376 deg
RA of node: 208
6240 deg
Eccentricity:
0001470
Arg of perigee: 30
3939 deg
Mean anomaly: 329
7299 deg
Mean motion: 15
55102648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2654
Checksum: 308
Coasting Arc #13 (Orbit 2669)
---------------------------------------
Vector Time (GMT): 2012/224/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5491698
02 A = 6780111
58 meter
Y = -1018329
31 meter E =
0012234
Z = 3835709
97 I = 51
49716
XDOT = 3862
149130 Wp = 76
76336
YDOT = 5177
119042 meter/sec RA = 202
60987 deg
ZDOT = -4141
214800 TA = 56
90158
MA = 56
78419
Ha = 219
675 n
mi
Hp = 212
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18017381
94 X = 5484044
23
Y = -3340975
41 feet Y = -956960
69 meter
Z = 12584350
31 Z = 3862369
46
XDOT = 12671
092947 XDOT = 3824
087332
YDOT = 16985
298695 feet/sec YDOT = 5220
095366 meter/sec
ZDOT = -13586
662729 ZDOT = -4122
545082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14615070
64 X = 4454673
53
Y = 10927195
17 feet Y = 3330609
09 meter
Z = 12694493
19 Z = 3869281
52
XDOT = -3047
392902 XDOT = -928
845356
YDOT = 19823
378146 feet/sec YDOT = 6042
165659 meter/sec
ZDOT = -13510
025517 ZDOT = -4117
855778
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 12225
02008684
00016717 00000-0 10270-3 0 9120
2 25544 51
6371 203
4900 0001416 31
6444 328
4794 15
55112092 26700
Satellite: ISS
Catalog Number: 25544
Epoch time: 12225
02008684 = yrday
fracday
Element set: 912
Inclination: 51
6371 deg
RA of node: 203
4900 deg
Eccentricity:
0001416
Arg of perigee: 31
6444 deg
Mean anomaly: 328
4794 deg
Mean motion: 15
55112092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2670
Checksum: 274
Coasting Arc #14 (Orbit 2684)
---------------------------------------
Vector Time (GMT): 2012/225/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6417271
52 A = 6784251
93 meter
Y = -217159
91 meter E =
0007501
Z = -2184260
18 I = 51
54072
XDOT = -1685
208782 Wp = 43
13696
YDOT = -5097
029647 meter/sec RA = 197
61401 deg
ZDOT = 5474
310440 TA = 292
57775
MA = 292
65709
Ha = 219
721 n
mi
Hp = 212
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21054040
43 X = -6403755
76
Y = -712466
91 feet Y = -288846
16 meter
Z = -7166207
93 Z = -2215401
74
XDOT = -5528
900202 XDOT = -1654
680085
YDOT = -16722
538213 feet/sec YDOT = -5115
704255 meter/sec
ZDOT = 17960
336090 ZDOT = 5466
197806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13987458
46 X = -4263377
34
Y = -15693060
74 feet Y = -4783244
91 meter
Z = -7294766
22 Z = -2223444
74
XDOT = 7061
419468 XDOT = 2152
320654
YDOT = -14602
567274 feet/sec YDOT = -4450
862505 meter/sec
ZDOT = 17927
267209 ZDOT = 5464
231045
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 12225
98398873
00016717 00000-0 10270-3 0 9138
2 25544 51
6379 198
6767 0001431 41
1112 319
0148 15
55152147 26859
Satellite: ISS
Catalog Number: 25544
Epoch time: 12225
98398873 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 198
6767 deg
Eccentricity:
0001431
Arg of perigee: 41
1112 deg
Mean anomaly: 319
0148 deg
Mean motion: 15
55152147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2685
Checksum: 321
Coasting Arc #15 (Orbit 2700)
---------------------------------------
Vector Time (GMT): 2012/226/23:30:35
086
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6641808
21 A = 6786165
53 meter
Y = 1357211
78 meter E =
0012455
Z = 161401
30 I = 51
57641
XDOT = -807
083140 Wp = 126
04496
YDOT = 4701
558586 meter/sec RA = 192
63122 deg
ZDOT = -6005
916956 TA = 52
21403
MA = 52
10130
Ha = 219
690 n
mi
Hp = 212
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21790709
34 X = 6625353
91
Y = 4452794
56 feet Y = 1431392
60 meter
Z = 529531
82 Z = 193626
44
XDOT = -2647
910564 XDOT = -830
422064
YDOT = 15425
060977 feet/sec YDOT = 4692
403023 meter/sec
ZDOT = -19704
451955 ZDOT = -6009
894165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12140393
06 X = 3700391
80
Y = 18631016
20 feet Y = 5678733
74 meter
Z = 662486
72 Z = 201925
95
XDOT = -11391
809179 XDOT = -3472
223438
YDOT = 8153
970752 feet/sec YDOT = 2485
330285 meter/sec
ZDOT = -19721
264962 ZDOT = -6011
041560
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 12227
01213206
00016717 00000-0 10270-3 0 9141
2 25544 51
6374 193
5422 0001516 37
9240 322
2020 15
55211499 27015
Satellite: ISS
Catalog Number: 25544
Epoch time: 12227
01213206 = yrday
fracday
Element set: 914
Inclination: 51
6374 deg
RA of node: 193
5422 deg
Eccentricity:
0001516
Arg of perigee: 37
9240 deg
Mean anomaly: 322
2020 deg
Mean motion: 15
55211499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2701
Checksum: 260
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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