[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 19th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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 650)
---------------------------------------
Vector Time (GMT): 2012/352/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -625984
24 A = 6791464
09 meter
Y = -5950446
33 meter E =
0021347
Z = -3216319
44 I = 51
32434
XDOT = 5138
401550 Wp = 58
72986
YDOT = -3095
971199 meter/sec RA = 289
48023 deg
ZDOT = 4762
065207 TA = 263
93459
MA = 264
17788
Ha = 230
555 n
mi
Hp = 212
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2053754
07 X = -543774
56
Y = -19522461
71 feet Y = -5956986
60 meter
Z = -10552229
12 Z = -3219161
13
XDOT = 16858
272803 XDOT = 5149
506616
YDOT = -10157
385824 feet/sec YDOT = -3038
448612 meter/sec
ZDOT = 15623
573515 ZDOT = 4787
053879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12271806
39 X = 3740446
59
Y = -15313868
91 feet Y = -4667667
24 meter
Z = -10563244
93 Z = -3219677
05
XDOT = 17955
510450 XDOT = 5472
839585
YDOT = 3617
720255 feet/sec YDOT = 1102
681134 meter/sec
ZDOT = 15727
586860 ZDOT = 4793
768475
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 12352
64451829
00016717 00000-0 10270-3 0 9009
2 25544 51
6497 290
1820 0017174 53
2526 307
0199 15
51886629 6511
Satellite: ISS
Catalog Number: 25544
Epoch time: 12352
64451829 = yrday
fracday
Element set: 900
Inclination: 51
6497 deg
RA of node: 290
1820 deg
Eccentricity:
0017174
Arg of perigee: 53
2526 deg
Mean anomaly: 307
0199 deg
Mean motion: 15
51886629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 651
Checksum: 314
Coasting Arc #2 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2012/353/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 289345
57 A = 6793504
94 meter
Y = 6365762
10 meter E =
0028158
Z = 2339996
05 I = 51
32146
XDOT = -5007
740556 Wp = 79
15234
YDOT = 2220
870388 meter/sec RA = 284
49306 deg
ZDOT = -5362
134299 TA = 74
64458
MA = 74
33360
Ha = 230
609 n
mi
Hp = 212
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 949296
49 X = 206773
68
Y = 20885046
27 feet Y = 6368535
94 meter
Z = 7677152
40 Z = 2341201
45
XDOT = -16429
595001 XDOT = -5006
154745
YDOT = 7286
320169 feet/sec YDOT = 2164
879854 meter/sec
ZDOT = -17592
304129 ZDOT = -5386
457545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13732847
82 X = -4185772
01
Y = 15761690
51 feet Y = 4804163
27 meter
Z = 7681340
62 Z = 2341272
62
XDOT = -15700
338672 XDOT = -4785
463227
YDOT = -4960
205242 feet/sec YDOT = -1511
870558 meter/sec
ZDOT = -17693
443277 ZDOT = -5392
961511
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 12353
67483220
00016717 00000-0 10270-3 0 9014
2 25544 51
6492 285
0630 0017181 57
4900 302
7909 15
51899978 6677
Satellite: ISS
Catalog Number: 25544
Epoch time: 12353
67483220 = yrday
fracday
Element set: 901
Inclination: 51
6492 deg
RA of node: 285
0630 deg
Eccentricity:
0017181
Arg of perigee: 57
4900 deg
Mean anomaly: 302
7909 deg
Mean motion: 15
51899978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 667
Checksum: 325
Coasting Arc #3 (Orbit 681)
---------------------------------------
Vector Time (GMT): 2012/354/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -81284
26 A = 6794727
23 meter
Y = -6627580
22 meter E =
0025020
Z = -1467543
40 I = 51
31956
XDOT = 4891
382868 Wp = 52
93682
YDOT = -1315
838340 meter/sec RA = 279
50761 deg
ZDOT = 5754
306415 TA = 290
98658
MA = 291
25409
Ha = 230
495 n
mi
Hp = 212
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -266680
64 X = -38
25
Y = -21744029
60 feet Y = -6628034
85 meter
Z = -4814774
93 Z = -1467741
24
XDOT = 16047
844055 XDOT = 4877
780299
YDOT = -4317
054920 feet/sec YDOT = -1261
216164 meter/sec
ZDOT = 18878
958054 ZDOT = 5778
035337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14530345
60 X = 4428849
34
Y = -16178477
25 feet Y = -4931199
87 meter
Z = -4814761
65 Z = -1467539
35
XDOT = 13474
882667 XDOT = 4107
144237
YDOT = 6535
219145 feet/sec YDOT = 1991
934795 meter/sec
ZDOT = 18977
517014 ZDOT = 5784
347186
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 12354
64072857
00016717 00000-0 10270-3 0 9023
2 25544 51
6492 280
2641 0017080 60
4697 299
8155 15
51958753 6824
Satellite: ISS
Catalog Number: 25544
Epoch time: 12354
64072857 = yrday
fracday
Element set: 902
Inclination: 51
6492 deg
RA of node: 280
2641 deg
Eccentricity:
0017080
Arg of perigee: 60
4697 deg
Mean anomaly: 299
8155 deg
Mean motion: 15
51958753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 682
Checksum: 331
Coasting Arc #4 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2012/355/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -187386
55 A = 6795592
30 meter
Y = 6776965
72 meter E =
0025195
Z = 434314
05 I = 51
31793
XDOT = -4807
234834 Wp = 92
33617
YDOT = 268
176687 meter/sec RA = 274
52388 deg
ZDOT = -5959
133662 TA = 82
96619
MA = 82
67972
Ha = 230
542 n
mi
Hp = 212
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -614785
27 X = -265263
88
Y = 22234139
50 feet Y = 6774434
79 meter
Z = 1424914
88 Z = 433214
91
XDOT = -15771
767827 XDOT = -4780
928264
YDOT = 879
844775 feet/sec YDOT = 214
566559 meter/sec
ZDOT = -19550
963457 ZDOT = -5982
423055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15218827
91 X = -4638698
75
Y = 16221515
43 feet Y = 4944317
90 meter
Z = 1419512
84 Z = 432667
51
XDOT = -11109
968138 XDOT = -3386
318289
YDOT = -8617
587753 feet/sec YDOT = -2626
640747 meter/sec
ZDOT = -19647
569408 ZDOT = -5988
579156
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 12355
67099809
00016717 00000-0 10270-3 0 9034
2 25544 51
6489 275
1447 0016997 64
8665 295
4248 15
51948373 6985
Satellite: ISS
Catalog Number: 25544
Epoch time: 12355
67099809 = yrday
fracday
Element set: 903
Inclination: 51
6489 deg
RA of node: 275
1447 deg
Eccentricity:
0016997
Arg of perigee: 64
8665 deg
Mean anomaly: 295
4248 deg
Mean motion: 15
51948373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 698
Checksum: 373
Coasting Arc #5 (Orbit 713)
---------------------------------------
Vector Time (GMT): 2012/356/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 365703
16 A = 6795316
67 meter
Y = -6753456
50 meter E =
0029594
Z = 524488
55 I = 51
31599
XDOT = 4776
559813 Wp = 60
38603
YDOT = 739
939479 meter/sec RA = 269
53963 deg
ZDOT = 5957
914822 TA = 305
29826
MA = 305
57468
Ha = 230
389 n
mi
Hp = 211
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1199813
52 X = 438646
70
Y = -22157009
51 feet Y = -6748959
16 meter
Z = 1720762
96 Z = 526441
91
XDOT = 15671
127994 XDOT = 4738
988411
YDOT = 2427
622963 feet/sec YDOT = 793
143546 meter/sec
ZDOT = 19546
964639 ZDOT = 5981
027943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15316852
17 X = 4668576
54
Y = -16054153
15 feet Y = -4893305
88 meter
Z = 1729697
75 Z = 527211
87
XDOT = 9059
660271 XDOT = 2761
384450
YDOT = 10844
058894 feet/sec YDOT = 3305
269151 meter/sec
ZDOT = 19642
717340 ZDOT = 5987
100245
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 12356
70124221
00016717 00000-0 10270-3 0 9047
2 25544 51
6485 270
0252 0016936 68
0208 292
2741 15
52033971 7143
Satellite: ISS
Catalog Number: 25544
Epoch time: 12356
70124221 = yrday
fracday
Element set: 904
Inclination: 51
6485 deg
RA of node: 270
0252 deg
Eccentricity:
0016936
Arg of perigee: 68
0208 deg
Mean anomaly: 292
2741 deg
Mean motion: 15
52033971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 714
Checksum: 284
Coasting Arc #6 (Orbit 728)
---------------------------------------
Vector Time (GMT): 2012/357/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -638614
82 A = 6794398
11 meter
Y = 6582262
00 meter E =
0020929
Z = -1573873
41 I = 51
31366
XDOT = -4766
051553 Wp = 92
99228
YDOT = -1811
758012 meter/sec RA = 264
55527 deg
ZDOT = -5710
374459 TA = 104
26157
MA = 104
02905
Ha = 230
413 n
mi
Hp = 211
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2095192
99 X = -704526
06
Y = 21595347
78 feet Y = 6574752
19 meter
Z = -5163626
68 Z = -1577135
42
XDOT = -15636
652078 XDOT = -4717
698094
YDOT = -5944
087966 feet/sec YDOT = -1864
784224 meter/sec
ZDOT = -18734
824340 ZDOT = -5733
410456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15353917
83 X = -4679874
15
Y = 15325072
17 feet Y = 4671082
00 meter
Z = -5177961
99 Z = -1578242
81
XDOT = -7053
089871 XDOT = -2149
781793
YDOT = -13354
420927 feet/sec YDOT = -4070
427499 meter/sec
ZDOT = -18830
130112 ZDOT = -5739
423658
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 12357
66707869
00016717 00000-0 10270-3 0 9059
2 25544 51
6481 265
2256 0016817 71
8143 288
4838 15
52021014 7292
Satellite: ISS
Catalog Number: 25544
Epoch time: 12357
66707869 = yrday
fracday
Element set: 905
Inclination: 51
6481 deg
RA of node: 265
2256 deg
Eccentricity:
0016817
Arg of perigee: 71
8143 deg
Mean anomaly: 288
4838 deg
Mean motion: 15
52021014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 729
Checksum: 325
Coasting Arc #7 (Orbit 744)
---------------------------------------
Vector Time (GMT): 2012/358/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 867963
54 A = 6792652
02 meter
Y = -6249042
38 meter E =
0030484
Z = 2478881
54 I = 51
31176
XDOT = 4818
034548 Wp = 75
14254
YDOT = 2785
140259 meter/sec RA = 259
56797 deg
ZDOT = 5287
233770 TA = 312
79470
MA = 313
05063
Ha = 230
283 n
mi
Hp = 211
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2847649
40 X = 925735
26
Y = -20502107
54 feet Y = -6239013
45 meter
Z = 8132813
45 Z = 2483237
88
XDOT = 15807
199960 XDOT = 4760
848186
YDOT = 9137
599275 feet/sec YDOT = 2838
698343 meter/sec
ZDOT = 17346
567487 ZDOT = 5310
500953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14979404
43 X = 4565722
47
Y = -14274324
75 feet Y = -4350814
18 meter
Z = 8151642
23 Z = 2484620
55
XDOT = 5524
654577 XDOT = 1683
914715
YDOT = 15846
152752 feet/sec YDOT = 4829
907359 meter/sec
ZDOT = 17442
720006 ZDOT = 5316
541058
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 12358
69728101
00016717 00000-0 10270-3 0 9066
2 25544 51
6476 260
1056 0016784 75
2104 285
0906 15
52091576 7453
Satellite: ISS
Catalog Number: 25544
Epoch time: 12358
69728101 = yrday
fracday
Element set: 906
Inclination: 51
6476 deg
RA of node: 260
1056 deg
Eccentricity:
0016784
Arg of perigee: 75
2104 deg
Mean anomaly: 285
0906 deg
Mean motion: 15
52091576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 745
Checksum: 313
Coasting Arc #8 (Orbit 759)
---------------------------------------
Vector Time (GMT): 2012/359/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1222006
45 A = 6790354
40 meter
Y = 5769968
26 meter E =
0021504
Z = -3386795
50 I = 51
30981
XDOT = -4849
336364 Wp = 81
63698
YDOT = -3715
971035 meter/sec RA = 254
57810 deg
ZDOT = -4603
196574 TA = 138
00472
MA = 137
83965
Ha = 230
301 n
mi
Hp = 211
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4009207
51 X = -1269984
32
Y = 18930342
06 feet Y = 5756035
09 meter
Z = -11111533
79 Z = -3392847
93
XDOT = -15909
896208 XDOT = -4785
061864
YDOT = -12191
506019 feet/sec YDOT = -3769
839516 meter/sec
ZDOT = -15102
350966 ZDOT = -4626
598705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14677447
32 X = -4473685
94
Y = 12586900
99 feet Y = 3836487
42 meter
Z = -11137335
50 Z = -3394659
86
XDOT = -4166
086787 XDOT = -1269
823253
YDOT = -18242
492813 feet/sec YDOT = -5560
311809 meter/sec
ZDOT = -15198
959466 ZDOT = -4632
642845
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 12359
66307738
00016717 00000-0 10270-3 0 9074
2 25544 51
6466 255
3056 0016773 78
8713 281
4324 15
52104225 7608
Satellite: ISS
Catalog Number: 25544
Epoch time: 12359
66307738 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 255
3056 deg
Eccentricity:
0016773
Arg of perigee: 78
8713 deg
Mean anomaly: 281
4324 deg
Mean motion: 15
52104225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 760
Checksum: 316
Coasting Arc #9 (Orbit 775)
---------------------------------------
Vector Time (GMT): 2012/360/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1571953
50 A = 6788021
69 meter
Y = -5166169
34 meter E =
0026837
Z = 4089839
20 I = 51
31093
XDOT = 4919
922824 Wp = 90
46040
YDOT = 4515
325860 meter/sec RA = 249
58462 deg
ZDOT = 3790
831258 TA = 320
20883
MA = 320
40535
Ha = 230
229 n
mi
Hp = 211
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5157327
75 X = 1609738
37
Y = -16949374
47 feet Y = -5148379
95 meter
Z = 13418107
60 Z = 4097566
88
XDOT = 16141
479080 XDOT = 4850
650858
YDOT = 14814
061222 feet/sec YDOT = 4569
955779 meter/sec
ZDOT = 12437
110426 ZDOT = 3814
564231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14186349
86 X = 4323999
44
Y = -10571133
41 feet Y = -3222081
46 meter
Z = 13450782
59 Z = 4099798
53
XDOT = 3278
544314 XDOT = 999
300307
YDOT = 20440
184103 feet/sec YDOT = 6230
168115 meter/sec
ZDOT = 12535
006657 ZDOT = 3820
670029
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 12360
69323965
00016717 00000-0 10270-3 0 9080
2 25544 51
6463 250
1855 0016749 82
4370 277
8683 15
52126161 7765
Satellite: ISS
Catalog Number: 25544
Epoch time: 12360
69323965 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 250
1855 deg
Eccentricity:
0016749
Arg of perigee: 82
4370 deg
Mean anomaly: 277
8683 deg
Mean motion: 15
52126161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 776
Checksum: 329
Coasting Arc #10 (Orbit 790)
---------------------------------------
Vector Time (GMT): 2012/361/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2055746
59 A = 6785657
03 meter
Y = 4459455
19 meter E =
0027334
Z = -4708714
69 I = 51
31369
XDOT = -4906
288693 Wp = 80
42739
YDOT = -5169
915940 meter/sec RA = 244
58726 deg
ZDOT = -2763
576109 TA = 162
03130
MA = 161
93448
Ha = 230
219 n
mi
Hp = 211
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6744575
41 X = -2082586
59
Y = 14630758
49 feet Y = 4436317
02 meter
Z = -15448539
02 Z = -4718766
05
XDOT = -16096
747680 XDOT = -4834
688187
YDOT = -16961
666470 feet/sec YDOT = -5224
380466 meter/sec
ZDOT = -9066
850752 ZDOT = -2787
237227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13930414
54 X = -4245990
35
Y = 8011581
70 feet Y = 2441930
10 meter
Z = -15490766
88 Z = -4721585
74
XDOT = -2562
812702 XDOT = -781
145311
YDOT = -22116
870733 feet/sec YDOT = -6741
222199 meter/sec
ZDOT = -9164
385156 ZDOT = -2793
304596
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 12361
65899660
00016717 00000-0 10270-3 0 9098
2 25544 51
6450 245
3849 0016768 86
4211 273
8858 15
52168106 7911
Satellite: ISS
Catalog Number: 25544
Epoch time: 12361
65899660 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 245
3849 deg
Eccentricity:
0016768
Arg of perigee: 86
4211 deg
Mean anomaly: 273
8858 deg
Mean motion: 15
52168106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 791
Checksum: 343
Coasting Arc #11 (Orbit 806)
---------------------------------------
Vector Time (GMT): 2012/362/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2552830
15 A = 6784009
04 meter
Y = -3680511
16 meter E =
0021209
Z = 5077577
13 I = 51
32194
XDOT = 4882
502525 Wp = 98
11620
YDOT = 5690
767353 meter/sec RA = 239
58778 deg
ZDOT = 1661
327544 TA = 335
74734
MA = 335
84702
Ha = 230
165 n
mi
Hp = 211
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8375427
01 X = 2569131
15
Y = -12075167
84 feet Y = -3651873
27 meter
Z = 16658717
63 Z = 5090017
73
XDOT = 16018
709073 XDOT = 4810
433998
YDOT = 18670
496565 feet/sec YDOT = 5744
963396 meter/sec
ZDOT = 5450
549686 ZDOT = 1684
871958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13672000
32 X = 4167225
70
Y = -5224659
73 feet Y = -1592476
28 meter
Z = 16710765
00 Z = 5093441
17
XDOT = 2145
721867 XDOT = 654
016025
YDOT = 23451
648579 feet/sec YDOT = 7148
062487 meter/sec
ZDOT = 5547
555185 ZDOT = 1690
894820
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 12362
68911884
00016717 00000-0 10270-3 0 9107
2 25544 51
6447 240
2646 0016790 90
0741 270
2334 15
52164199 8076
Satellite: ISS
Catalog Number: 25544
Epoch time: 12362
68911884 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 240
2646 deg
Eccentricity:
0016790
Arg of perigee: 90
0741 deg
Mean anomaly: 270
2334 deg
Mean motion: 15
52164199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 807
Checksum: 307
Coasting Arc #12 (Orbit 821)
---------------------------------------
Vector Time (GMT): 2012/363/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3159136
23 A = 6782988
85 meter
Y = 2872395
29 meter E =
0031452
Z = -5297822
09 I = 51
33431
XDOT = -4708
615300 Wp = 90
64581
YDOT = -6002
072730 meter/sec RA = 234
58594 deg
ZDOT = -449
111883 TA = 175
05311
MA = 175
02196
Ha = 230
137 n
mi
Hp = 211
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10364620
17 X = -3165285
84
Y = 9423869
05 feet Y = 2837034
07 meter
Z = -17381306
08 Z = -5313183
47
XDOT = -15448
212925 XDOT = -4638
967244
YDOT = -19691
839664 feet/sec YDOT = -6054
337937 meter/sec
ZDOT = -1473
464182 ZDOT = -471
817371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13761236
35 X = -4194424
84
Y = 2152113
82 feet Y = 655964
29 meter
Z = -17445378
77 Z = -5317351
45
XDOT = -1769
316157 XDOT = -539
287565
YDOT = -23944
883230 feet/sec YDOT = -7298
400408 meter/sec
ZDOT = -1566
971367 ZDOT = -477
612873
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 12363
65483743
00016717 00000-0 10270-3 0 9114
2 25544 51
6437 235
4636 0016786 94
0488 266
2582 15
52226457 8220
Satellite: ISS
Catalog Number: 25544
Epoch time: 12363
65483743 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 235
4636 deg
Eccentricity:
0016786
Arg of perigee: 94
0488 deg
Mean anomaly: 266
2582 deg
Mean motion: 15
52226457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 822
Checksum: 328
Coasting Arc #13 (Orbit 837)
---------------------------------------
Vector Time (GMT): 2012/364/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3764354
67 A = 6783056
48 meter
Y = -2044917
54 meter E =
0019410
Z = 5242139
09 I = 51
35279
XDOT = 4460
967441 Wp = 92
55891
YDOT = 6203
247308 meter/sec RA = 229
58501 deg
ZDOT = -781
905882 TA = 4
94035
MA = 4
92122
Ha = 230
012 n
mi
Hp = 211
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12350244
98 X = 3761476
84
Y = -6709047
06 feet Y = -2002838
80 meter
Z = 17198619
08 Z = 5260418
70
XDOT = 14635
719950 XDOT = 4395
068140
YDOT = 20351
861248 feet/sec YDOT = 6252
764254 meter/sec
ZDOT = -2565
308013 ZDOT = -760
394451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13927570
38 X = 4245123
45
Y = 969317
64 feet Y = 295448
02 meter
Z = 17274708
93 Z = 5265331
28
XDOT = 1406
576438 XDOT = 428
724498
YDOT = 24025
639795 feet/sec YDOT = 7323
015009 meter/sec
ZDOT = -2476
759082 ZDOT = -754
916168
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 12364
68491909
00016717 00000-0 10270-3 0 9122
2 25544 51
6433 230
3429 0016775 97
8706 262
4351 15
52228991 8386
Satellite: ISS
Catalog Number: 25544
Epoch time: 12364
68491909 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 230
3429 deg
Eccentricity:
0016775
Arg of perigee: 97
8706 deg
Mean anomaly: 262
4351 deg
Mean motion: 15
52228991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 838
Checksum: 332
Coasting Arc #14 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2012/365/15:18:31
632
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4418993
43 A = 6784004
24 meter
Y = 1270596
93 meter E =
0029682
Z = -5015256
88 I = 51
37688
XDOT = -4023
812248 Wp = 103
15944
YDOT = -6188
287011 meter/sec RA = 224
58561 deg
ZDOT = 1980
974476 TA = 186
19824
MA = 186
23505
Ha = 230
037 n
mi
Hp = 211
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14498009
94 X = -4408510
50
Y = 4168625
09 feet Y = 1221240
02 meter
Z = -16454254
84 Z = -5036698
22
XDOT = -13201
483753 XDOT = -3963
937427
YDOT = -20302
778906 feet/sec YDOT = -6232
949187 meter/sec
ZDOT = 6499
260092 ZDOT = 1961
572206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14437863
82 X = -4400660
89
Y = -4022037
36 feet Y = -1225916
99 meter
Z = -16543383
38 Z = -5042423
25
XDOT = -886
157776 XDOT = -270
100890
YDOT = -23178
592977 feet/sec YDOT = -7064
835139 meter/sec
ZDOT = 6419
442900 ZDOT = 1956
646196
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 12365
65060093
00016717 00000-0 10270-3 0 9137
2 25544 51
6432 225
5415 0016831 101
5713 258
7329 15
52286515 8536
Satellite: ISS
Catalog Number: 25544
Epoch time: 12365
65060093 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 225
5415 deg
Eccentricity:
0016831
Arg of perigee: 101
5713 deg
Mean anomaly: 258
7329 deg
Mean motion: 15
52286515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 853
Checksum: 297
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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