[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 31st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 2453)
---------------------------------------
Vector Time (GMT): 2012/211/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3173700
21 A = 6780060
84 meter
Y = -4330703
74 meter E =
0006869
Z = -4147095
82 I = 51
28468
XDOT = 3189
235699 Wp = 101
96018
YDOT = -5893
129245 meter/sec RA = 272
01855 deg
ZDOT = 3717
213971 TA = 206
46374
MA = 206
49884
Ha = 219
781 n
mi
Hp = 213
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10412402
27 X = -3104892
08
Y = -14208345
60 feet Y = -4365808
83 meter
Z = -13605957
41 Z = -4162346
70
XDOT = 10463
371715 XDOT = 3236
839664
YDOT = -19334
413535 feet/sec YDOT = -5857
199483 meter/sec
ZDOT = 12195
583893 ZDOT = 3732
821929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8475738
70 X = -2583405
16
Y = -15386804
65 feet Y = -4689898
06 meter
Z = -13668408
06 Z = -4166130
78
XDOT = 11597
385027 XDOT = 3534
882956
YDOT = -17268
512188 feet/sec YDOT = -5263
442515 meter/sec
ZDOT = 12260
551386 ZDOT = 3737
016063
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 12211
13827521
00016717 00000-0 10270-3 0 9003
2 25544 51
6391 272
7864 0001298 333
6878 26
4209 15
54785772 24540
Satellite: ISS
Catalog Number: 25544
Epoch time: 12211
13827521 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 272
7864 deg
Eccentricity:
0001298
Arg of perigee: 333
6878 deg
Mean anomaly: 26
4209 deg
Mean motion: 15
54785772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 317
Coasting Arc #2 (Orbit 2469)
---------------------------------------
Vector Time (GMT): 2012/212/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2448590
60 A = 6784198
99 meter
Y = 5725706
85 meter E =
0012657
Z = 2678883
30 I = 51
29922
XDOT = -3924
659865 Wp = 96
23314
YDOT = 4101
465189 meter/sec RA = 267
00662 deg
ZDOT = -5159
290402 TA = 53
34556
MA = 53
22927
Ha = 219
691 n
mi
Hp = 213
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8033433
73 X = 2371369
38
Y = 18785127
47 feet Y = 5752656
45 meter
Z = 8788987
22 Z = 2690591
33
XDOT = -12876
180660 XDOT = -3945
169343
YDOT = 13456
250621 feet/sec YDOT = 4057
463106 meter/sec
ZDOT = -16926
805782 ZDOT = -5178
405276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5910588
54 X = 1801547
39
Y = 19535636
52 feet Y = 5954462
01 meter
Z = 8836697
16 Z = 2693425
30
XDOT = -12722
362869 XDOT = -3877
776203
YDOT = 11570
749420 feet/sec YDOT = 3526
764423 meter/sec
ZDOT = -17006
053327 ZDOT = -5183
445054
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 12212
16666868
00016717 00000-0 10270-3 0 9013
2 25544 51
6395 267
6545 0001532 334
4035 25
7042 15
54835159 24708
Satellite: ISS
Catalog Number: 25544
Epoch time: 12212
16666868 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 267
6545 deg
Eccentricity:
0001532
Arg of perigee: 334
4035 deg
Mean anomaly: 25
7042 deg
Mean motion: 15
54835159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2470
Checksum: 305
Coasting Arc #3 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2012/213/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1627465
82 A = 6787026
13 meter
Y = -6524518
79 meter E =
0010795
Z = -879229
30 I = 51
30959
XDOT = 4505
960790 Wp = 33
49232
YDOT = -1913
693253 meter/sec RA = 262
00483 deg
ZDOT = 5903
954147 TA = 316
94646
MA = 317
03085
Ha = 219
821 n
mi
Hp = 213
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5339454
80 X = -1550115
35
Y = -21405901
56 feet Y = -6542285
55 meter
Z = -2884610
56 Z = -886948
05
XDOT = 14783
335924 XDOT = 4498
345739
YDOT = -6278
521170 feet/sec YDOT = -1863
347960 meter/sec
ZDOT = 19369
928304 ZDOT = 5925
824758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3361549
41 X = -1024600
26
Y = -21800033
54 feet Y = -6644650
22 meter
Z = -2915801
81 Z = -888736
39
XDOT = 13583
152764 XDOT = 4140
144962
YDOT = -4678
462696 feet/sec YDOT = -1425
995430 meter/sec
ZDOT = 19460
325383 ZDOT = 5931
507177
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
13078181
00016717 00000-0 10270-3 0 9027
2 25544 51
6381 262
8422 0001275 341
8612 18
2495 15
54804910 24857
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
13078181 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 262
8422 deg
Eccentricity:
0001275
Arg of perigee: 341
8612 deg
Mean anomaly: 18
2495 deg
Mean motion: 15
54804910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 288
Coasting Arc #4 (Orbit 2500)
---------------------------------------
Vector Time (GMT): 2012/214/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 653969
12 A = 6786723
15 meter
Y = 6665660
43 meter E =
0008315
Z = -1075516
87 I = 51
31410
XDOT = -4922
088647 Wp = 136
90419
YDOT = -457
492597 meter/sec RA = 257
00882 deg
ZDOT = -5861
102478 TA = 54
81508
MA = 54
73724
Ha = 219
842 n
mi
Hp = 213
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2145567
97 X = 584608
22
Y = 21868964
66 feet Y = 6672585
78 meter
Z = -3528598
67 Z = -1072507
95
XDOT = -16148
584799 XDOT = -4888
135834
YDOT = -1500
959964 feet/sec YDOT = -512
344154 meter/sec
ZDOT = -19229
338840 ZDOT = -5884
930749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 555961
55 X = 169457
08
Y = 21968816
09 feet Y = 6696095
15 meter
Z = -3516832
69 Z = -1071930
60
XDOT = -14275
240485 XDOT = -4351
093300
YDOT = -2715
444707 feet/sec YDOT = -827
667547 meter/sec
ZDOT = -19327
585075 ZDOT = -5891
047931
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
15915748
00016717 00000-0 10270-3 0 9030
2 25544 51
6379 257
7099 0001445 350
9386 9
1741 15
54856427 25017
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
15915748 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 257
7099 deg
Eccentricity:
0001445
Arg of perigee: 350
9386 deg
Mean anomaly: 9
1741 deg
Mean motion: 15
54856427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2501
Checksum: 321
Coasting Arc #5 (Orbit 2516)
---------------------------------------
Vector Time (GMT): 2012/215/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 414898
25 A = 6783769
31 meter
Y = -6131139
17 meter E =
0013431
Z = 2857719
04 I = 51
31094
XDOT = 5118
773038 Wp = 76
02374
YDOT = 2701
915669 meter/sec RA = 252
00652 deg
ZDOT = 5036
946778 TA = 316
67506
MA = 316
78058
Ha = 219
839 n
mi
Hp = 213
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1361214
73 X = 469545
28
Y = -20115285
98 feet Y = -6126194
12 meter
Z = 9375718
65 Z = 2859866
96
XDOT = 16793
874798 XDOT = 5063
711497
YDOT = 8864
552721 feet/sec YDOT = 2758
848834 meter/sec
ZDOT = 16525
415938 ZDOT = 5061
679320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2433062
21 X = 741597
36
Y = -20009515
79 feet Y = -6098900
41 meter
Z = 9385159
67 Z = 2860596
67
XDOT = 14708
412684 XDOT = 4483
124186
YDOT = 9612
955901 feet/sec YDOT = 2930
028959 meter/sec
ZDOT = 16627
188282 ZDOT = 5067
966989
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 12215
18752446
00016717 00000-0 10270-3 0 9049
2 25544 51
6369 252
5763 0001168 353
1680 6
9457 15
54847174 25176
Satellite: ISS
Catalog Number: 25544
Epoch time: 12215
18752446 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 252
5763 deg
Eccentricity:
0001168
Arg of perigee: 353
1680 deg
Mean anomaly: 6
9457 deg
Mean motion: 15
54847174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2517
Checksum: 319
Coasting Arc #6 (Orbit 2531)
---------------------------------------
Vector Time (GMT): 2012/216/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1601780
13 A = 6779362
39 meter
Y = 5010754
89 meter E =
0009047
Z = -4285865
91 I = 51
30723
XDOT = -5012
994259 Wp = 62
62981
YDOT = -4606
204417 meter/sec RA = 246
99376 deg
ZDOT = -3513
383614 TA = 171
39303
MA = 171
37751
Ha = 219
934 n
mi
Hp = 213
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5255184
14 X = -1636873
11
Y = 16439484
55 feet Y = 4992646
70 meter
Z = -14061239
86 Z = -4293732
19
XDOT = -16446
831560 XDOT = -4944
047347
YDOT = -15112
219217 feet/sec YDOT = -4661
877226 meter/sec
ZDOT = -11526
849128 ZDOT = -3537
568595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5807237
06 X = -1770045
86
Y = 16224144
08 feet Y = 4945119
12 meter
Z = -14094155
72 Z = -4295898
66
XDOT = -14590
212805 XDOT = -4447
096863
YDOT = -15317
569274 feet/sec YDOT = -4668
795115 meter/sec
ZDOT = -11626
198407 ZDOT = -3543
665275
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
15160982
00016717 00000-0 10270-3 0 9056
2 25544 51
6373 247
7647 0001263 5
8490 354
2677 15
54867763 25320
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
15160982 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 247
7647 deg
Eccentricity:
0001263
Arg of perigee: 5
8490 deg
Mean anomaly: 354
2677 deg
Mean motion: 15
54867763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2532
Checksum: 320
Coasting Arc #7 (Orbit 2547)
---------------------------------------
Vector Time (GMT): 2012/217/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2801893
59 A = 6776032
78 meter
Y = -3449430
99 meter E =
0004355
Z = 5112038
40 I = 51
30820
XDOT = 4565
719100 Wp = 110
85561
YDOT = 5974
252852 meter/sec RA = 241
96756 deg
ZDOT = 1526
188175 TA = 324
36501
MA = 324
39408
Ha = 219
854 n
mi
Hp = 213
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9192564
28 X = 2815425
00
Y = -11317030
81 feet Y = -3418022
87 meter
Z = 16771779
54 Z = 5125682
42
XDOT = 14979
393372 XDOT = 4491
160721
YDOT = 19600
567099 feet/sec YDOT = 6024
892666 meter/sec
ZDOT = 5007
179053 ZDOT = 1548
186720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9335101
21 X = 2845338
85
Y = -11114513
69 feet Y = -3387703
77 meter
Z = 16828383
28 Z = 5129291
22
XDOT = 13705
907324 XDOT = 4177
560552
YDOT = 19242
306596 feet/sec YDOT = 5865
055050 meter/sec
ZDOT = 5097
397917 ZDOT = 1553
686885
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 12217
17995811
00016717 00000-0 10270-3 0 9067
2 25544 51
6366 242
6307 0001249 6
0151 354
1017 15
54854735 25489
Satellite: ISS
Catalog Number: 25544
Epoch time: 12217
17995811 = yrday
fracday
Element set: 906
Inclination: 51
6366 deg
RA of node: 242
6307 deg
Eccentricity:
0001249
Arg of perigee: 6
0151 deg
Mean anomaly: 354
1017 deg
Mean motion: 15
54854735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2548
Checksum: 300
Coasting Arc #8 (Orbit 2562)
---------------------------------------
Vector Time (GMT): 2012/218/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3951125
38 A = 6775287
40 meter
Y = 1652742
54 meter E =
0014930
Z = -5262898
92 I = 51
32240
XDOT = -3695
177969 Wp = 90
99031
YDOT = -6673
871743 meter/sec RA = 236
93732 deg
ZDOT = 679
740792 TA = 185
52937
MA = 185
54588
Ha = 219
960 n
mi
Hp = 213
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12963009
79 X = -3943747
51
Y = 5422383
65 feet Y = 1608599
83 meter
Z = -17266728
74 Z = -5282075
05
XDOT = -12123
287300 XDOT = -3623
576695
YDOT = -21895
904667 feet/sec YDOT = -6714
793173 meter/sec
ZDOT = 2230
120708 ZDOT = 661
964039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12882356
03 X = -3926542
12
Y = 5361264
33 feet Y = 1634113
37 meter
Z = -17345994
82 Z = -5287059
22
XDOT = -11643
513661 XDOT = -3548
942964
YDOT = -21012
725056 feet/sec YDOT = -6404
678597 meter/sec
ZDOT = 2157
368791 ZDOT = 657
566008
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
14402506
00016717 00000-0 10270-3 0 9070
2 25544 51
6377 237
8193 0001152 16
6994 343
4197 15
54889084 25637
Satellite: ISS
Catalog Number: 25544
Epoch time: 12218
14402506 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 237
8193 deg
Eccentricity:
0001152
Arg of perigee: 16
6994 deg
Mean anomaly: 343
4197 deg
Mean motion: 15
54889084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2563
Checksum: 321
Coasting Arc #9 (Orbit 2578)
---------------------------------------
Vector Time (GMT): 2012/219/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4901248
54 A = 6777791
95 meter
Y = 194553
93 meter E =
0008785
Z = 4673047
75 I = 51
34772
XDOT = 2416
169567 Wp = 58
45426
YDOT = 6719
643515 meter/sec RA = 231
90926 deg
ZDOT = -2805
502802 TA = 59
50919
MA = 59
42247
Ha = 219
901 n
mi
Hp = 213
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16080211
74 X = 4876008
43
Y = 638300
31 feet Y = 249221
65 meter
Z = 15331521
50 Z = 4696796
16
XDOT = 7927
065508 XDOT = 2354
477862
YDOT = 22046
074525 feet/sec YDOT = 6746
317667 meter/sec
ZDOT = -9204
405517 ZDOT = -2793
915220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15992948
28 X = 4874650
63
Y = 438785
81 feet Y = 133741
92 meter
Z = 15429493
21 Z = 4702909
53
XDOT = 8290
979921 XDOT = 2527
090680
YDOT = 20777
432110 feet/sec YDOT = 6332
961307 meter/sec
ZDOT = -9157
182715 ZDOT = -2791
109292
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
17235465
00016717 00000-0 10270-3 0 9083
2 25544 51
6373 232
6852 0001142 21
0123 339
1077 15
54864210 25791
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
17235465 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 232
6852 deg
Eccentricity:
0001142
Arg of perigee: 21
0123 deg
Mean anomaly: 339
1077 deg
Mean motion: 15
54864210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2579
Checksum: 288
Coasting Arc #10 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2012/220/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5529326
76 A = 6781881
92 meter
Y = -1861003
07 meter E =
0005557
Z = -3461925
93 I = 51
38294
XDOT = -773
099450 Wp = 82
18236
YDOT = -6128
801721 meter/sec RA = 226
89527 deg
ZDOT = 4536
402141 TA = 237
03968
MA = 237
09312
Ha = 219
937 n
mi
Hp = 213
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18140835
84 X = -5491288
62
Y = -6105653
12 feet Y = -1922622
77 meter
Z = -11358024
72 Z = -3488694
46
XDOT = -2536
415519 XDOT = -726
545048
YDOT = -20107
617195 feet/sec YDOT = -6137
186685 meter/sec
ZDOT = 14883
209125 ZDOT = 4532
759598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18244657
72 X = -5560971
67
Y = -5566305
35 feet Y = -1696609
87 meter
Z = -11468319
84 Z = -3495543
89
XDOT = -3630
003382 XDOT = -1106
425031
YDOT = -18689
224285 feet/sec YDOT = -5696
475562 meter/sec
ZDOT = 14868
710027 ZDOT = 4531
982816
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
13640300
00016717 00000-0 10270-3 0 9090
2 25544 51
6388 227
8735 0001190 22
0911 338
0293 15
54907038 25943
Satellite: ISS
Catalog Number: 25544
Epoch time: 12220
13640300 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 227
8735 deg
Eccentricity:
0001190
Arg of perigee: 22
0911 deg
Mean anomaly: 338
0293 deg
Mean motion: 15
54907038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 287
Coasting Arc #11 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2012/221/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5693284
23 A = 6785706
91 meter
Y = 3245197
28 meter E =
0013996
Z = 1737538
45 I = 51
41690
XDOT = -1139
058720 Wp = 110
32097
YDOT = 5047
695538 meter/sec RA = 221
89550 deg
ZDOT = -5662
972582 TA = 50
54031
MA = 50
41656
Ha = 219
941 n
mi
Hp = 213
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18678754
03 X = 5648132
13
Y = 10646972
70 feet Y = 3308610
65 meter
Z = 5700585
45 Z = 1765086
28
XDOT = -3737
069290 XDOT = -1167
909229
YDOT = 16560
680900 feet/sec YDOT = 5034
796605 meter/sec
ZDOT = -18579
306370 ZDOT = -5668
576069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19122658
25 X = 5828586
23
Y = 9760740
72 feet Y = 2975073
77 meter
Z = 5813986
27 Z = 1772103
01
XDOT = -2130
586268 XDOT = -649
402694
YDOT = 15316
836009 feet/sec YDOT = 4668
571615 meter/sec
ZDOT = -18602
864062 ZDOT = -5670
152966
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
16471254
00016717 00000-0 10270-3 0 9106
2 25544 51
6384 222
7401 0001156 24
4137 335
7071 15
54917461 26109
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
16471254 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 222
7401 deg
Eccentricity:
0001156
Arg of perigee: 24
4137 deg
Mean anomaly: 335
7071 deg
Mean motion: 15
54917461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 269
Coasting Arc #12 (Orbit 2625)
---------------------------------------
Vector Time (GMT): 2012/222/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5322573
52 A = 6786957
51 meter
Y = -4195555
04 meter E =
0013618
Z = 198968
14 I = 51
44599
XDOT = 3104
883142 Wp = 45
85264
YDOT = -3642
988029 meter/sec RA = 216
90649 deg
ZDOT = 5994
546029 TA = 316
29788
MA = 316
40561
Ha = 219
961 n
mi
Hp = 213
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17462511
56 X = -5276228
91
Y = -13764944
34 feet Y = -4254816
24 meter
Z = 652782
61 Z = 173224
00
XDOT = 10186
624481 XDOT = 3116
269097
YDOT = -11952
060464 feet/sec YDOT = -3608
203754 meter/sec
ZDOT = 19667
145763 ZDOT = 6009
656877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18312609
89 X = -5581683
49
Y = -12616986
64 feet Y = -3845657
53 meter
Z = 546895
83 Z = 166693
85
XDOT = 8359
384574 XDOT = 2547
940418
YDOT = -11236
103099 feet/sec YDOT = -3424
764225 meter/sec
ZDOT = 19729
819348 ZDOT = 6013
648937
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 12222
19301172
00016717 00000-0 10270-3 0 9112
2 25544 51
6398 217
6076 0001245 29
5967 330
5256 15
54941683 26269
Satellite: ISS
Catalog Number: 25544
Epoch time: 12222
19301172 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 217
6076 deg
Eccentricity:
0001245
Arg of perigee: 29
5967 deg
Mean anomaly: 330
5256 deg
Mean motion: 15
54941683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2626
Checksum: 305
Coasting Arc #13 (Orbit 2640)
---------------------------------------
Vector Time (GMT): 2012/223/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4359372
38 A = 6784990
84 meter
Y = 4732555
32 meter E =
0006124
Z = -2149772
40 I = 51
46422
XDOT = -4941
576689 Wp = 127
58449
YDOT = 2067
471789 meter/sec RA = 211
91799 deg
ZDOT = -5483
690201 TA = 76
31381
MA = 76
24564
Ha = 219
981 n
mi
Hp = 213
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14302402
84 X = 4316571
00
Y = 15526756
30 feet Y = 4781065
28 meter
Z = -7053059
06 Z = -2128698
75
XDOT = -16212
521944 XDOT = -4937
690001
YDOT = 6783
043927 feet/sec YDOT = 2012
233912 meter/sec
ZDOT = -17991
109582 ZDOT = -5507
686458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15559458
25 X = 4742522
87
Y = 14309294
43 feet Y = 4361472
94 meter
Z = -6966482
77 Z = -2123383
95
XDOT = -14454
443534 XDOT = -4405
714389
YDOT = 6933
281577 feet/sec YDOT = 2113
264225 meter/sec
ZDOT = -18090
327054 ZDOT = -5513
931686
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
15703277
00016717 00000-0 10270-3 0 9122
2 25544 51
6395 212
7955 0001247 31
7351 328
3877 15
54961760 26411
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
15703277 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 212
7955 deg
Eccentricity:
0001247
Arg of perigee: 31
7351 deg
Mean anomaly: 328
3877 deg
Mean motion: 15
54961760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 307
Coasting Arc #14 (Orbit 2656)
---------------------------------------
Vector Time (GMT): 2012/224/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2886525
59 A = 6780799
64 meter
Y = -4832344
30 meter E =
0012204
Z = 3770712
35 I = 51
47777
XDOT = 6390
846207 Wp = 91
77673
YDOT = -518
531307 meter/sec RA = 206
92117 deg
ZDOT = 4215
566372 TA = 313
57009
MA = 313
67136
Ha = 219
939 n
mi
Hp = 213
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9470228
31 X = -2850591
88
Y = -15854147
96 feet Y = -4864422
46 meter
Z = 12371103
50 Z = 3756776
95
XDOT = 20967
343200 XDOT = 6375
691473
YDOT = -1701
218199 feet/sec YDOT = -447
149798 meter/sec
ZDOT = 13830
598333 ZDOT = 4246
575691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11059194
06 X = -3370842
35
Y = -14837227
48 feet Y = -4522386
94 meter
Z = 12313989
64 Z = 3753304
04
XDOT = 19531
823285 XDOT = 5953
299737
YDOT = -2940
255182 feet/sec YDOT = -896
189780 meter/sec
ZDOT = 13958
643425 ZDOT = 4254
594516
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 12224
18531035
00016717 00000-0 10270-3 0 9138
2 25544 51
6403 207
6627 0001192 34
4408 325
6822 15
55004378 26573
Satellite: ISS
Catalog Number: 25544
Epoch time: 12224
18531035 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 207
6627 deg
Eccentricity:
0001192
Arg of perigee: 34
4408 deg
Mean anomaly: 325
6822 deg
Mean motion: 15
55004378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2657
Checksum: 285
Coasting Arc #15 (Orbit 2671)
---------------------------------------
Vector Time (GMT): 2012/225/03:05:50
879
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 995640
17 A = 6776756
69 meter
Y = 4595884
17 meter E =
0012937
Z = -4891804
40 I = 51
49156
XDOT = -7238
771438 Wp = 69
77374
YDOT = -912
454322 meter/sec RA = 201
91243 deg
ZDOT = -2331
219481 TA = 177
34058
MA = 177
33369
Ha = 219
952 n
mi
Hp = 213
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3266535
99 X = 967937
05
Y = 15078360
13 feet Y = 4606863
36 meter
Z = -16049227
02 Z = -4887034
76
XDOT = -23749
250125 XDOT = -7216
705778
YDOT = -2993
616542 feet/sec YDOT = -993
279282 meter/sec
ZDOT = -7648
357878 ZDOT = -2366
331142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5083431
25 X = 1549429
84
Y = 14587843
49 feet Y = 4446374
70 meter
Z = -16029923
22 Z = -4885920
60
XDOT = -22825
471923 XDOT = -6957
203842
YDOT = -607
327202 feet/sec YDOT = -185
113331 meter/sec
ZDOT = -7793
233506 ZDOT = -2375
377573
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
14931316
00016717 00000-0 10270-3 0 9142
2 25544 51
6402 202
8511 0001245 33
7266 326
3966 15
54976779 26720
Satellite: ISS
Catalog Number: 25544
Epoch time: 12225
14931316 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 202
8511 deg
Eccentricity:
0001245
Arg of perigee: 33
7266 deg
Mean anomaly: 326
3966 deg
Mean motion: 15
54976779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2672
Checksum: 306
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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