[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 22nd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29062 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 3039)
---------------------------------------
Vector Time (GMT): 2013/140/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4096210
22 A = 6798690
47 meter
Y = -5049224
92 meter E =
0013821
Z = -1957272
03 I = 51
34015
XDOT = 2831
499510 Wp = 1
21401
YDOT = -4448
759654 meter/sec RA = 244
88454 deg
ZDOT = 5565
044248 TA = 337
12285
MA = 337
18436
Ha = 228
113 n
mi
Hp = 221
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13439009
90 X = -4029936
22
Y = -16565698
55 feet Y = -5094660
73 meter
Z = -6421496
15 Z = -1977010
45
XDOT = 9289
696554 XDOT = 2854
002179
YDOT = -14595
668155 feet/sec YDOT = -4416
970323 meter/sec
ZDOT = 18258
019186 ZDOT = 5578
854196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21044743
09 X = -6414437
69
Y = -3330547
98 feet Y = -1015151
03 meter
Z = -6503168
98 Z = -1982165
91
XDOT = -3200
686475 XDOT = -975
569238
YDOT = -15449
385979 feet/sec YDOT = -4708
972846 meter/sec
ZDOT = 18316
182675 ZDOT = 5582
772479
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 13140
46110433
00016717 00000-0 10270-3 0 9008
2 25544 51
6485 245
8109 0009551 334
4780 25
5898 15
50344770 30409
Satellite: ISS
Catalog Number: 25544
Epoch time: 13140
46110433 = yrday
fracday
Element set: 900
Inclination: 51
6485 deg
RA of node: 245
8109 deg
Eccentricity:
0009551
Arg of perigee: 334
4780 deg
Mean anomaly: 25
5898 deg
Mean motion: 15
50344770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 291
Coasting Arc #2 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2013/141/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4307777
40 A = 6799237
47 meter
Y = 5041753
40 meter E =
0009009
Z = 1500263
33 I = 51
35629
XDOT = -2879
715261 Wp = 75
33802
YDOT = 4176
397852 meter/sec RA = 239
90995 deg
ZDOT = -5735
204822 TA = 88
25152
MA = 88
14833
Ha = 228
252 n
mi
Hp = 220
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14133127
96 X = 4243791
26
Y = 16541185
70 feet Y = 5089567
88 meter
Z = 4922123
79 Z = 1521035
22
XDOT = -9447
884713 XDOT = -2898
342029
YDOT = 13702
092690 feet/sec YDOT = 4144
091060 meter/sec
ZDOT = -18816
288786 ZDOT = -5749
239612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21596311
95 X = 6582555
88
Y = 2470125
78 feet Y = 752894
34 meter
Z = 5008115
60 Z = 1526473
64
XDOT = 2706
792936 XDOT = 825
030487
YDOT = 14808
075194 feet/sec YDOT = 4513
501319 meter/sec
ZDOT = -18875
354952 ZDOT = -5753
208190
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 13141
49242995
00016717 00000-0 10270-3 0 9012
2 25544 51
6485 240
6991 0009483 338
1802 21
8944 15
50388494 30560
Satellite: ISS
Catalog Number: 25544
Epoch time: 13141
49242995 = yrday
fracday
Element set: 901
Inclination: 51
6485 deg
RA of node: 240
6991 deg
Eccentricity:
0009483
Arg of perigee: 338
1802 deg
Mean anomaly: 21
8944 deg
Mean motion: 15
50388494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 326
Coasting Arc #3 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2013/142/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4507372
94 A = 6799671
34 meter
Y = -4967901
66 meter E =
0016998
Z = -1045503
78 I = 51
37494
XDOT = 2976
007807 Wp = 10
30065
YDOT = -3929
797461 meter/sec RA = 234
93639 deg
ZDOT = 5874
196553 TA = 338
33062
MA = 338
40246
Ha = 228
381 n
mi
Hp = 220
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14787968
97 X = -4446406
91
Y = -16298889
96 feet Y = -5017965
02 meter
Z = -3430130
51 Z = -1067252
79
XDOT = 9763
805140 XDOT = 2991
194595
YDOT = -12893
036290 feet/sec YDOT = -3896
433209 meter/sec
ZDOT = 19272
298402 ZDOT = 5888
690758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21944763
96 X = -6688764
06
Y = -1462552
63 feet Y = -445786
04 meter
Z = -3520214
48 Z = -1072961
37
XDOT = -2127
414589 XDOT = -648
435967
YDOT = -14372
416006 feet/sec YDOT = -4380
712399 meter/sec
ZDOT = 19333
251595 ZDOT = 5892
775086
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 13142
45927491
00016717 00000-0 10270-3 0 9021
2 25544 51
6493 235
9067 0009736 342
3494 17
7317 15
50411827 30717
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142
45927491 = yrday
fracday
Element set: 902
Inclination: 51
6493 deg
RA of node: 235
9067 deg
Eccentricity:
0009736
Arg of perigee: 342
3494 deg
Mean anomaly: 17
7317 deg
Mean motion: 15
50411827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3071
Checksum: 312
Coasting Arc #4 (Orbit 3086)
---------------------------------------
Vector Time (GMT): 2013/143/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4683261
20 A = 6799868
85 meter
Y = 4900348
22 meter E =
0007889
Z = 543021
22 I = 51
39407
XDOT = -3131
021020 Wp = 81
73003
YDOT = 3660
143888 meter/sec RA = 229
96508 deg
ZDOT = -5951
060232 TA = 92
40482
MA = 92
31449
Ha = 228
477 n
mi
Hp = 220
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15365030
20 X = 4625478
47
Y = 16077257
92 feet Y = 4952396
28 meter
Z = 1781565
70 Z = 565632
59
XDOT = -10272
378673 XDOT = -3142
807532
YDOT = 12008
346089 feet/sec YDOT = 3625
065351 meter/sec
ZDOT = -19524
475827 ZDOT = -5966
299172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22225137
81 X = 6774222
00
Y = 512824
49 feet Y = 156308
90 meter
Z = 1875263
21 Z = 571580
23
XDOT = 1348
532715 XDOT = 411
032771
YDOT = 14047
713844 feet/sec YDOT = 4281
743180 meter/sec
ZDOT = -19588
505997 ZDOT = -5970
576628
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 13143
49055334
00016717 00000-0 10270-3 0 9035
2 25544 51
6490 230
7952 0009628 346
0400 14
0484 15
50460440 30875
Satellite: ISS
Catalog Number: 25544
Epoch time: 13143
49055334 = yrday
fracday
Element set: 903
Inclination: 51
6490 deg
RA of node: 230
7952 deg
Eccentricity:
0009628
Arg of perigee: 346
0400 deg
Mean anomaly: 14
0484 deg
Mean motion: 15
50460440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3087
Checksum: 284
Coasting Arc #5 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2013/144/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4829535
19 A = 6799953
92 meter
Y = -4769189
73 meter E =
0019379
Z = -52650
41 I = 51
41541
XDOT = 3332
010901 Wp = 20
59919
YDOT = -3432
733188 meter/sec RA = 224
99440 deg
ZDOT = 5995
372676 TA = 338
83224
MA = 338
91233
Ha = 228
618 n
mi
Hp = 219
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15844931
72 X = -4775590
37
Y = -15646947
92 feet Y = -4822895
00 meter
Z = -172737
55 Z = -75981
80
XDOT = 10931
794293 XDOT = 3341
024294
YDOT = -11262
247991 feet/sec YDOT = -3395
422735 meter/sec
ZDOT = 19669
857862 ZDOT = 6011
581192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22261507
68 X = -6785307
54
Y = 520905
66 feet Y = 158772
04 meter
Z = -269465
23 Z = -82133
00
XDOT = -548
347092 XDOT = -167
136194
YDOT = -13975
279015 feet/sec YDOT = -4259
665044 meter/sec
ZDOT = 19737
910910 ZDOT = 6016
115245
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 13144
45735455
00016717 00000-0 10270-3 0 9042
2 25544 51
6495 226
0026 0009878 350
1116 9
9839 15
50481794 31027
Satellite: ISS
Catalog Number: 25544
Epoch time: 13144
45735455 = yrday
fracday
Element set: 904
Inclination: 51
6495 deg
RA of node: 226
0026 deg
Eccentricity:
0009878
Arg of perigee: 350
1116 deg
Mean anomaly: 9
9839 deg
Mean motion: 15
50481794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3102
Checksum: 313
Coasting Arc #6 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2013/145/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4941019
76 A = 6799717
09 meter
Y = 4648775
73 meter E =
0006532
Z = -479237
28 I = 51
43622
XDOT = -3581
295513 Wp = 77
49371
YDOT = 3198
846465 meter/sec RA = 220
02595 deg
ZDOT = -5961
432640 TA = 107
67672
MA = 107
60539
Ha = 228
688 n
mi
Hp = 219
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16210694
75 X = 4890996
96
Y = 15251888
86 feet Y = 4703749
69 meter
Z = -1572300
79 Z = -455354
77
XDOT = -11749
657195 XDOT = -3587
839999
YDOT = 10494
903100 feet/sec YDOT = 3158
762296 meter/sec
ZDOT = -19558
506038 ZDOT = -5978
846066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22217329
73 X = 6771842
10
Y = -1448680
36 feet Y = -441557
77 meter
Z = -1473245
67 Z = -449045
28
XDOT = -370
550824 XDOT = -112
943891
YDOT = 14040
795422 feet/sec YDOT = 4279
634445 meter/sec
ZDOT = -19631
565264 ZDOT = -5983
701092
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 13145
48858686
00016717 00000-0 10270-3 0 9059
2 25544 51
6482 220
8908 0009785 353
8243 6
2785 15
50529644 31186
Satellite: ISS
Catalog Number: 25544
Epoch time: 13145
48858686 = yrday
fracday
Element set: 905
Inclination: 51
6482 deg
RA of node: 220
8908 deg
Eccentricity:
0009785
Arg of perigee: 353
8243 deg
Mean anomaly: 6
2785 deg
Mean motion: 15
50529644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3118
Checksum: 339
Coasting Arc #7 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2013/146/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5005966
21 A = 6799356
00 meter
Y = -4474096
74 meter E =
0020626
Z = 987888
49 I = 51
45942
XDOT = 3870
410438 Wp = 31
59708
YDOT = -3020
436783 meter/sec RA = 215
05772 deg
ZDOT = 5894
628438 TA = 339
12900
MA = 339
21308
Ha = 228
822 n
mi
Hp = 219
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16423773
67 X = -4960362
79
Y = -14678795
08 feet Y = -4529821
76 meter
Z = 3241103
98 Z = 963679
84
XDOT = 12698
196975 XDOT = 3875
263109
YDOT = -9909
569499 feet/sec YDOT = -2977
129073 meter/sec
ZDOT = 19339
332147 ZDOT = 5913
442151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21913055
44 X = -6679099
30
Y = 2380428
60 feet Y = 725554
64 meter
Z = 3140649
97 Z = 957270
11
XDOT = 1239
882052 XDOT = 377
916050
YDOT = -14378
595545 feet/sec YDOT = -4382
595922 meter/sec
ZDOT = 19418
221683 ZDOT = 5918
673969
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 13146
51979558
00016717 00000-0 10270-3 0 9067
2 25544 51
6484 215
7781 0009984 357
9530 2
1578 15
50556136 31344
Satellite: ISS
Catalog Number: 25544
Epoch time: 13146
51979558 = yrday
fracday
Element set: 906
Inclination: 51
6484 deg
RA of node: 215
7781 deg
Eccentricity:
0009984
Arg of perigee: 357
9530 deg
Mean anomaly: 2
1578 deg
Mean motion: 15
50556136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 335
Coasting Arc #8 (Orbit 3148)
---------------------------------------
Vector Time (GMT): 2013/147/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5027641
51 A = 6798656
80 meter
Y = 4319016
76 meter E =
0006315
Z = -1527945
10 I = 51
48164
XDOT = -4187
919427 Wp = 57
81506
YDOT = 2850
582167 meter/sec RA = 210
09125 deg
ZDOT = -5736
645801 TA = 138
86980
MA = 138
82219
Ha = 228
883 n
mi
Hp = 219
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16494886
83 X = 4986394
05
Y = 14170002
48 feet Y = 4375008
59 meter
Z = -5012943
24 Z = -1503620
73
XDOT = -13739
893134 XDOT = -4191
616755
YDOT = 9352
303699 feet/sec YDOT = 2803
730301 meter/sec
ZDOT = -18821
016409 ZDOT = -5756
999066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21539031
13 X = 6565096
69
Y = -3153182
78 feet Y = -961090
11 meter
Z = -4911968
84 Z = -1497168
10
XDOT = -2127
743989 XDOT = -648
536368
YDOT = 14843
680903 feet/sec YDOT = 4524
353939 meter/sec
ZDOT = -18906
319907 ZDOT = -5762
646308
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 13147
48653223
00016717 00000-0 10270-3 0 9073
2 25544 51
6469 210
9852 0009959 1
5684 358
5497 15
50598297 31495
Satellite: ISS
Catalog Number: 25544
Epoch time: 13147
48653223 = yrday
fracday
Element set: 907
Inclination: 51
6469 deg
RA of node: 210
9852 deg
Eccentricity:
0009959
Arg of perigee: 1
5684 deg
Mean anomaly: 358
5497 deg
Mean motion: 15
50598297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3149
Checksum: 352
Coasting Arc #9 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2013/148/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4988699
40 A = 6797830
23 meter
Y = -4124826
63 meter E =
0020548
Z = 2032532
53 I = 51
50637
XDOT = 4535
956186 Wp = 42
79706
YDOT = -2744
152107 meter/sec RA = 205
12496 deg
ZDOT = 5545
961490 TA = 339
70746
MA = 339
78900
Ha = 229
005 n
mi
Hp = 218
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16367124
01 X = -4952077
44
Y = -13532895
77 feet Y = -4180408
89 meter
Z = 6668413
81 Z = 2008386
29
XDOT = 14881
746018 XDOT = 4539
363934
YDOT = -9003
123710 feet/sec YDOT = -2693
409796 meter/sec
ZDOT = 18195
411711 ZDOT = 5568
004750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20918330
90 X = -6375907
26
Y = 3843530
40 feet Y = 1171508
07 meter
Z = 6568140
21 Z = 2001969
14
XDOT = 2900
193358 XDOT = 883
978936
YDOT = -15571
080144 feet/sec YDOT = -4746
065228 meter/sec
ZDOT = 18287
765990 ZDOT = 5574
111074
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 13148
51769569
00016717 00000-0 10270-3 0 9080
2 25544 51
6472 205
8718 0010082 5
4901 354
6358 15
50630309 31659
Satellite: ISS
Catalog Number: 25544
Epoch time: 13148
51769569 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 205
8718 deg
Eccentricity:
0010082
Arg of perigee: 5
4901 deg
Mean anomaly: 354
6358 deg
Mean motion: 15
50630309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3165
Checksum: 313
Coasting Arc #10 (Orbit 3179)
---------------------------------------
Vector Time (GMT): 2013/149/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4903306
89 A = 6796718
21 meter
Y = 3962784
07 meter E =
0008703
Z = -2554976
25 I = 51
53029
XDOT = -4884
147317 Wp = 40
94876
YDOT = 2656
443166 meter/sec RA = 200
15994 deg
ZDOT = -5256
881267 TA = 167
71862
MA = 167
69739
Ha = 229
059 n
mi
Hp = 218
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16086964
85 X = 4871041
14
Y = 13001260
06 feet Y = 4017435
79 meter
Z = -8382468
01 Z = -2531234
40
XDOT = -16024
105371 XDOT = -4887
952731
YDOT = 8715
364719 feet/sec YDOT = 2601
804805 meter/sec
ZDOT = -17246
985785 ZDOT = -5280
616993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20266421
32 X = 6177205
22
Y = -4328861
83 feet Y = -1319437
09 meter
Z = -8283845
31 Z = -2524916
05
XDOT = -3588
375939 XDOT = -1093
736986
YDOT = 16370
949854 feet/sec YDOT = 4989
865515 meter/sec
ZDOT = -17346
404144 ZDOT = -5287
183983
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 13149
48439122
00016717 00000-0 10270-3 0 9097
2 25544 51
6463 201
0780 0010134 9
3188 350
8149 15
50666934 31800
Satellite: ISS
Catalog Number: 25544
Epoch time: 13149
48439122 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 201
0780 deg
Eccentricity:
0010134
Arg of perigee: 9
3188 deg
Mean anomaly: 350
8149 deg
Mean motion: 15
50666934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3180
Checksum: 301
Coasting Arc #11 (Orbit 3195)
---------------------------------------
Vector Time (GMT): 2013/150/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4747882
50 A = 6795504
99 meter
Y = -3780992
35 meter E =
0019162
Z = 3028707
21 I = 51
55598
XDOT = 5251
782196 Wp = 53
44384
YDOT = -2633
178097 meter/sec RA = 195
19549 deg
ZDOT = 4935
083445 TA = 341
31264
MA = 341
38290
Ha = 229
181 n
mi
Hp = 218
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15577042
31 X = -4719962
40
Y = -12404830
55 feet Y = -3833930
31 meter
Z = 9936703
45 Z = 3005709
92
XDOT = 17230
256550 XDOT = 5256
863330
YDOT = -8639
035752 feet/sec YDOT = -2574
421351 meter/sec
ZDOT = 16191
218653 ZDOT = 4960
608267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19410810
84 X = -5916415
14
Y = 4651267
54 feet Y = 1417706
35 meter
Z = 9841152
20 Z = 2999583
19
XDOT = 4112
685793 XDOT = 1253
546630
YDOT = -17394
176411 feet/sec YDOT = -5301
744970 meter/sec
ZDOT = 16298
113113 ZDOT = 4967
664877
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 13150
51551036
00016717 00000-0 10270-3 0 9104
2 25544 51
6466 195
9643 0010203 13
1435 346
9980 15
50701872 31964
Satellite: ISS
Catalog Number: 25544
Epoch time: 13150
51551036 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 195
9643 deg
Eccentricity:
0010203
Arg of perigee: 13
1435 deg
Mean anomaly: 346
9980 deg
Mean motion: 15
50701872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3196
Checksum: 292
Coasting Arc #12 (Orbit 3210)
---------------------------------------
Vector Time (GMT): 2013/151/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4550339
57 A = 6794123
21 meter
Y = 3645738
39 meter E =
0012837
Z = -3504513
22 I = 51
58155
XDOT = -5586
215177 Wp = 38
92189
YDOT = 2630
932450 meter/sec RA = 190
23179 deg
ZDOT = -4515
585871 TA = 182
18834
MA = 182
19396
Ha = 229
211 n
mi
Hp = 218
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14928935
60 X = 4526257
96
Y = 11961083
96 feet Y = 3696488
75 meter
Z = -11497746
80 Z = -3482466
28
XDOT = -18327
477616 XDOT = -5593
284105
YDOT = 8631
668143 feet/sec YDOT = 2568
424651 meter/sec
ZDOT = -14814
914275 ZDOT = -4542
740258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18588722
58 X = 5665842
64
Y = -4743237
52 feet Y = -1445738
80 meter
Z = -11406135
17 Z = -3476590
00
XDOT = -4468
321183 XDOT = -1361
944296
YDOT = 18393
553509 feet/sec YDOT = 5606
355110 meter/sec
ZDOT = -14928
622258 ZDOT = -4550
244064
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 13151
48216514
00016717 00000-0 10270-3 0 9111
2 25544 51
6467 191
1702 0010286 17
0655 343
0840 15
50734319 32110
Satellite: ISS
Catalog Number: 25544
Epoch time: 13151
48216514 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 191
1702 deg
Eccentricity:
0010286
Arg of perigee: 17
0655 deg
Mean anomaly: 343
0840 deg
Mean motion: 15
50734319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3211
Checksum: 275
Coasting Arc #13 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2013/152/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4279240
11 A = 6792696
07 meter
Y = -3511894
99 meter E =
0016736
Z = 3917408
98 I = 51
60727
XDOT = 5928
770081 Wp = 62
11419
YDOT = -2686
126052 meter/sec RA = 185
26893 deg
ZDOT = 4062
702617 TA = 345
36276
MA = 345
41116
Ha = 229
345 n
mi
Hp = 217
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14039501
68 X = -4258681
12
Y = -11521965
18 feet Y = -3559633
44 meter
Z = 12852391
66 Z = 3896670
42
XDOT = 19451
345410 XDOT = 5938
630664
YDOT = -8812
749514 feet/sec YDOT = -2619
771922 meter/sec
ZDOT = 13329
076827 ZDOT = 4091
527992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17630133
69 X = -5373664
75
Y = 4609698
80 feet Y = 1405036
19 meter
Z = 12766218
07 Z = 3891143
27
XDOT = 4640
014816 XDOT = 1414
276516
YDOT = -19553
387610 feet/sec YDOT = -5959
872543 meter/sec
ZDOT = 13449
779748 ZDOT = 4099
492867
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 13152
51324043
00016717 00000-0 10270-3 0 9124
2 25544 51
6465 186
0565 0010353 20
9814 339
1760 15
50770711 32273
Satellite: ISS
Catalog Number: 25544
Epoch time: 13152
51324043 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 186
0565 deg
Eccentricity:
0010353
Arg of perigee: 20
9814 deg
Mean anomaly: 339
1760 deg
Mean motion: 15
50770711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 281
Coasting Arc #14 (Orbit 3241)
---------------------------------------
Vector Time (GMT): 2013/153/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3979069
31 A = 6791278
82 meter
Y = 3437899
34 meter E =
0017301
Z = -4315908
71 I = 51
63410
XDOT = -6204
462776 Wp = 44
98810
YDOT = 2755
167470 meter/sec RA = 180
30648 deg
ZDOT = -3522
283668 TA = 189
02473
MA = 189
05587
Ha = 229
330 n
mi
Hp = 217
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13054689
35 X = 3961295
95
Y = 11279197
30 feet Y = 3482296
70 meter
Z = -14159805
49 Z = -4296621
53
XDOT = -20355
849001 XDOT = -6217
700069
YDOT = 9039
263354 feet/sec YDOT = 2685
711465 meter/sec
ZDOT = -11556
048781 ZDOT = -3552
456635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16787378
76 X = 5116793
05
Y = -4253458
10 feet Y = -1296454
03 meter
Z = -14079677
05 Z = -4291485
57
XDOT = -4596
614130 XDOT = -1401
047987
YDOT = 20564
811011 feet/sec YDOT = 6268
154396 meter/sec
ZDOT = -11682
399845 ZDOT = -3560
795473
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 13153
47985400
00016717 00000-0 10270-3 0 9131
2 25544 51
6472 181
2621 0010396 24
6840 335
4807 15
50798999 32424
Satellite: ISS
Catalog Number: 25544
Epoch time: 13153
47985400 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 181
2621 deg
Eccentricity:
0010396
Arg of perigee: 24
6840 deg
Mean anomaly: 335
4807 deg
Mean motion: 15
50798999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3242
Checksum: 319
Coasting Arc #15 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2013/154/10:58:21
532
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3608161
49 A = 6789885
53 meter
Y = -3385273
32 meter E =
0013880
Z = 4636412
03 I = 51
65944
XDOT = 6478
142131 Wp = 66
07142
YDOT = -2866
197772 meter/sec RA = 175
34465 deg
ZDOT = 2947
220918 TA = 354
59714
MA = 354
61210
Ha = 229
470 n
mi
Hp = 217
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11837800
15 X = -3592561
16
Y = -11106539
76 feet Y = -3425535
17 meter
Z = 15211325
57 Z = 4618921
35
XDOT = 21253
747149 XDOT = 6495
394131
YDOT = -9403
535997 feet/sec YDOT = -2793
658856 meter/sec
ZDOT = 9669
359968 ZDOT = 2978
733213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15889148
33 X = -4843012
41
Y = 3637064
61 feet Y = 1108577
29 meter
Z = 15138688
51 Z = 4614272
26
XDOT = 4385
422502 XDOT = 1336
676779
YDOT = -21658
062238 feet/sec YDOT = -6601
377370 meter/sec
ZDOT = 9801
332396 ZDOT = 2987
446114
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 13154
51088519
00016717 00000-0 10270-3 0 9143
2 25544 51
6461 176
1480 0010495 28
7597 331
4131 15
50838748 32582
Satellite: ISS
Catalog Number: 25544
Epoch time: 13154
51088519 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 176
1480 deg
Eccentricity:
0010495
Arg of perigee: 28
7597 deg
Mean anomaly: 331
4131 deg
Mean motion: 15
50838748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 319
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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