[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 16th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12809 05 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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
017/02:16:52
654 -1
2 1
5 1
5
N/A 0
2 -0
1 228
5
000/00:03:45
308 1
0 0
1 215
5
Coasting Arc #1 (Orbit 1114)
---------------------------------------
Vector Time (GMT): 2013/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5393231
86 A = 6788069
74 meter
Y = -221863
95 meter E =
0016675
Z = -4116598
06 I = 51
86232
XDOT = -2669
860304 Wp = 138
60984
YDOT = 6065
997959 meter/sec RA = 140
86032 deg
ZDOT = -3845
820774 TA = 91
83409
MA = 91
64310
Ha = 228
838 n
mi
Hp = 214
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17694330
26 X = 5415309
01
Y = -727900
11 feet Y = -161430
00 meter
Z = -13505899
13 Z = -4090344
94
XDOT = -8759
384199 XDOT = -2718
811433
YDOT = 19901
568107 feet/sec YDOT = 6035
868217 meter/sec
ZDOT = -12617
522226 ZDOT = -3858
909428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8249769
54 X = 2514529
76
Y = 15763819
41 feet Y = 4804812
16 meter
Z = -13396707
56 Z = -4083316
46
XDOT = -20552
724740 XDOT = -6264
470501
YDOT = 45
492438 feet/sec YDOT = 13
866095 meter/sec
ZDOT = -12672
613714 ZDOT = -3862
612660
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 13016
52330082
00016717 00000-0 10270-3 0 9001
2 25544 51
6470 141
7451 0015361 164
3180 195
8450 15
52135765 11157
Satellite: ISS
Catalog Number: 25544
Epoch time: 13016
52330082 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 141
7451 deg
Eccentricity:
0015361
Arg of perigee: 164
3180 deg
Mean anomaly: 195
8450 deg
Mean motion: 15
52135765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1115
Checksum: 272
Coasting Arc #2 (Orbit 1123)
---------------------------------------
Vector Time (GMT): 2013/017/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2489902
46 A = 6791773
71 meter
Y = 5523050
23 meter E =
0014217
Z = -3091162
63 I = 51
88743
XDOT = -5863
016111 Wp = 149
49196
YDOT = 107
597363 meter/sec RA = 137
86081 deg
ZDOT = 4912
855433 TA = 175
22309
MA = 175
20951
Ha = 228
463 n
mi
Hp = 215
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8168971
31 X = -2536461
45
Y = 18120243
55 feet Y = 5494946
27 meter
Z = -10141609
67 Z = -3103371
28
XDOT = -19235
617163 XDOT = -5887
648589
YDOT = 353
009721 feet/sec YDOT = 41
895698 meter/sec
ZDOT = 16118
292103 ZDOT = 4884
313919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15966945
50 X = 4866724
99
Y = -11793524
45 feet Y = -3594666
25 meter
Z = -10192987
66 Z = -3106822
64
XDOT = 16150
819347 XDOT = 4922
769737
YDOT = 8032
307046 feet/sec YDOT = 2448
247188 meter/sec
ZDOT = 15999
591897 ZDOT = 4876
675610
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 13017
10275492
00016717 00000-0 10270-3 0 9010
2 25544 51
6479 138
8694 0013726 167
6596 192
4894 15
51889084 11246
Satellite: ISS
Catalog Number: 25544
Epoch time: 13017
10275492 = yrday
fracday
Element set: 901
Inclination: 51
6479 deg
RA of node: 138
8694 deg
Eccentricity:
0013726
Arg of perigee: 167
6596 deg
Mean anomaly: 192
4894 deg
Mean motion: 15
51889084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1124
Checksum: 340
Coasting Arc #3 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2013/018/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2908149
12 A = 6793758
40 meter
Y = -5700301
22 meter E =
0023509
Z = 2235028
13 I = 51
91555
XDOT = 5340
999344 Wp = 139
85480
YDOT = 568
423535 meter/sec RA = 132
91430 deg
ZDOT = -5485
330059 TA = 15
37901
MA = 15
30768
Ha = 228
379 n
mi
Hp = 215
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9541171
66 X = 2960817
89
Y = -18701775
64 feet Y = -5667486
00 meter
Z = 7332769
44 Z = 2249283
40
XDOT = 17522
963727 XDOT = 5360
892172
YDOT = 1864
906611 feet/sec YDOT = 628
261221 meter/sec
ZDOT = -17996
489694 ZDOT = -5459
335868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17260480
07 X = -5260994
32
Y = 11915697
88 feet Y = 3631904
71 meter
Z = 7392688
85 Z = 2253291
56
XDOT = -13745
209152 XDOT = -4189
539749
YDOT = -8783
097574 feet/sec YDOT = -2677
088141 meter/sec
ZDOT = -17888
449508 ZDOT = -5452
399410
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 13018
13307581
00016717 00000-0 10270-3 0 9020
2 25544 51
6477 133
7509 0013733 171
3084 188
8308 15
51869868 11400
Satellite: ISS
Catalog Number: 25544
Epoch time: 13018
13307581 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 133
7509 deg
Eccentricity:
0013733
Arg of perigee: 171
3084 deg
Mean anomaly: 188
8308 deg
Mean motion: 15
51869868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 314
Coasting Arc #4 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2013/019/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3234095
14 A = 6794939
64 meter
Y = 5833005
29 meter E =
0009254
Z = -1327432
36 I = 51
94074
XDOT = -4768
713347 Wp = 135
88661
YDOT = -1319
467810 meter/sec RA = 127
97097 deg
ZDOT = 5838
289252 TA = 209
75941
MA = 209
81207
Ha = 228
106 n
mi
Hp = 215
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10610548
36 X = -3292632
41
Y = 19137156
48 feet Y = 5796512
34 meter
Z = -4355093
04 Z = -1343285
24
XDOT = -15645
384997 XDOT = -4781
964976
YDOT = -4328
962630 feet/sec YDOT = -1372
868775 meter/sec
ZDOT = 19154
492297 ZDOT = 5815
091227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18218928
68 X = 5553129
46
Y = -12095481
46 feet Y = -3686702
75 meter
Z = -4421684
71 Z = -1347729
50
XDOT = 11106
425527 XDOT = 3385
238501
YDOT = 9783
448755 feet/sec YDOT = 2981
995181 meter/sec
ZDOT = 19058
158691 ZDOT = 5808
926769
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 13019
09898702
00016717 00000-0 10270-3 0 9037
2 25544 51
6482 128
9517 0013572 175
2510 184
8773 15
51933046 11557
Satellite: ISS
Catalog Number: 25544
Epoch time: 13019
09898702 = yrday
fracday
Element set: 903
Inclination: 51
6482 deg
RA of node: 128
9517 deg
Eccentricity:
0013572
Arg of perigee: 175
2510 deg
Mean anomaly: 184
8773 deg
Mean motion: 15
51933046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 318
Coasting Arc #5 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2013/020/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3468809
15 A = 6795786
76 meter
Y = -5816270
88 meter E =
0024108
Z = 335208
81 I = 51
96122
XDOT = 4223
495818 Wp = 156
12751
YDOT = 2163
708096 meter/sec RA = 123
03115 deg
ZDOT = -6033
283070 TA = 20
27363
MA = 20
17807
Ha = 228
089 n
mi
Hp = 216
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11380607
45 X = 3531961
77
Y = -19082253
54 feet Y = -5777127
39 meter
Z = 1099766
42 Z = 352213
03
XDOT = 13856
613576 XDOT = 4228
294716
YDOT = 7098
779842 feet/sec YDOT = 2210
964917 meter/sec
ZDOT = -19794
235794 ZDOT = -6012
754126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18690920
85 X = -5696992
68
Y = 12005747
58 feet Y = 3659351
86 meter
Z = 1171159
64 Z = 356969
46
XDOT = -8469
498040 XDOT = -2581
503003
YDOT = -11224
065254 feet/sec YDOT = -3421
095089 meter/sec
ZDOT = -19709
094627 ZDOT = -6007
332042
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 13020
12928113
00016717 00000-0 10270-3 0 9044
2 25544 51
6483 123
8329 0013654 179
0459 181
0721 15
51895119 11716
Satellite: ISS
Catalog Number: 25544
Epoch time: 13020
12928113 = yrday
fracday
Element set: 904
Inclination: 51
6483 deg
RA of node: 123
8329 deg
Eccentricity:
0013654
Arg of perigee: 179
0459 deg
Mean anomaly: 181
0721 deg
Mean motion: 15
51895119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 294
Coasting Arc #6 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2013/021/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3620037
69 A = 6795440
84 meter
Y = 5718470
76 meter E =
0010913
Z = 640454
58 I = 51
97680
XDOT = -3695
079173 Wp = 118
91652
YDOT = -3018
862258 meter/sec RA = 118
09210 deg
ZDOT = 5986
819806 TA = 247
95198
MA = 248
06792
Ha = 227
723 n
mi
Hp = 216
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11876764
08 X = -3686824
92
Y = 18761387
02 feet Y = 5677615
78 meter
Z = 2101228
94 Z = 622706
95
XDOT = -12122
963166 XDOT = -3690
129090
YDOT = -9904
403733 feet/sec YDOT = -3060
155548 meter/sec
ZDOT = 19641
797265 ZDOT = 5968
881481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18809162
90 X = 5733032
85
Y = -11813976
89 feet Y = -3600900
15 meter
Z = 2026739
26 Z = 617750
13
XDOT = 5925
049506 XDOT = 1805
955089
YDOT = 12838
213976 feet/sec YDOT = 3913
087620 meter/sec
ZDOT = 19567
527609 ZDOT = 5964
182415
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 13021
15955876
00016717 00000-0 10270-3 0 9055
2 25544 51
6484 118
7136 0013386 183
2299 176
8768 15
51970498 11871
Satellite: ISS
Catalog Number: 25544
Epoch time: 13021
15955876 = yrday
fracday
Element set: 905
Inclination: 51
6484 deg
RA of node: 118
7136 deg
Eccentricity:
0013386
Arg of perigee: 183
2299 deg
Mean anomaly: 176
8768 deg
Mean motion: 15
51970498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 350
Coasting Arc #7 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2013/022/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3715036
66 A = 6794604
32 meter
Y = -5433463
18 meter E =
0019907
Z = -1636723
37 I = 51
98739
XDOT = 3215
527099 Wp = 170
87787
YDOT = 3923
932947 meter/sec RA = 113
15407 deg
ZDOT = -5756
394580 TA = 26
95760
MA = 26
85432
Ha = 227
717 n
mi
Hp = 216
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12188440
48 X = 3783469
36
Y = -17826322
77 feet Y = -5391536
59 meter
Z = -5369827
33 Z = -1618510
32
XDOT = 10549
629590 XDOT = 3199
372572
YDOT = 12873
795759 feet/sec YDOT = 3959
800970 meter/sec
ZDOT = -18885
808989 ZDOT = -5740
813033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18517092
82 X = -5644009
89
Y = 11147551
03 feet Y = 3397773
55 meter
Z = -5293419
46 Z = -1613434
25
XDOT = -3549
125652 XDOT = -1081
773499
YDOT = -14787
524265 feet/sec YDOT = -4507
237396 meter/sec
ZDOT = -18821
448049 ZDOT = -5736
777365
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 13022
12543442
00016717 00000-0 10270-3 0 9066
2 25544 51
6486 113
9148 0013486 187
1291 172
9671 15
51938295 12026
Satellite: ISS
Catalog Number: 25544
Epoch time: 13022
12543442 = yrday
fracday
Element set: 906
Inclination: 51
6486 deg
RA of node: 113
9148 deg
Eccentricity:
0013486
Arg of perigee: 187
1291 deg
Mean anomaly: 172
9671 deg
Mean motion: 15
51938295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1202
Checksum: 306
Coasting Arc #8 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2013/023/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3758042
30 A = 6792856
12 meter
Y = 5056813
81 meter E =
0014417
Z = 2545406
12 I = 51
99301
XDOT = -2796
652234 Wp = 131
69304
YDOT = -4762
781587 meter/sec RA = 108
21367 deg
ZDOT = 5304
275381 TA = 256
69318
MA = 256
85398
Ha = 227
338 n
mi
Hp = 216
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12329535
11 X = -3826674
08
Y = 16590596
50 feet Y = 5014405
14 meter
Z = 8351069
94 Z = 2526983
72
XDOT = -9175
368223 XDOT = -2768
952333
YDOT = -15625
923841 feet/sec YDOT = -4793
900927 meter/sec
ZDOT = 17402
478283 ZDOT = 5290
756690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17975474
56 X = 5478924
64
Y = -10268003
32 feet Y = -3129687
41 meter
Z = 8273821
35 Z = 2521860
75
XDOT = 1523
003585 XDOT = 464
211493
YDOT = 16720
591482 feet/sec YDOT = 5096
436284 meter/sec
ZDOT = 17346
799179 ZDOT = 5287
304390
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 13023
15568716
00016717 00000-0 10270-3 0 9072
2 25544 51
6484 108
7952 0013186 190
9608 169
1258 15
51994292 12185
Satellite: ISS
Catalog Number: 25544
Epoch time: 13023
15568716 = yrday
fracday
Element set: 907
Inclination: 51
6484 deg
RA of node: 108
7952 deg
Eccentricity:
0013186
Arg of perigee: 190
9608 deg
Mean anomaly: 169
1258 deg
Mean motion: 15
51994292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 331
Coasting Arc #9 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2013/024/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3789415
45 A = 6790695
25 meter
Y = -4482144
38 meter E =
0013027
Z = -3402964
49 I = 51
99413
XDOT = 2427
652181 Wp = 173
92804
YDOT = 5582
367140 meter/sec RA = 103
27169 deg
ZDOT = -4663
574121 TA = 45
60804
MA = 45
50145
Ha = 227
278 n
mi
Hp = 217
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12432465
38 X = 3855784
50
Y = -14705198
09 feet Y = -4439397
48 meter
Z = -11164581
66 Z = -3384395
20
XDOT = 7964
738126 XDOT = 2387
702542
YDOT = 18314
852823 feet/sec YDOT = 5609
291553 meter/sec
ZDOT = -15300
440030 ZDOT = -4651
877732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17184380
26 X = -5237799
10
Y = 8788478
74 feet Y = 2678728
32 meter
Z = -11086777
98 Z = -3379249
93
XDOT = 220
413802 XDOT = 67
182127
YDOT = -18750
909018 feet/sec YDOT = -5715
277069 meter/sec
ZDOT = -15252
442551 ZDOT = -4648
944489
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 13024
12153739
00016717 00000-0 10270-3 0 9086
2 25544 51
6480 103
9963 0013271 194
9538 165
1223 15
51996254 12336
Satellite: ISS
Catalog Number: 25544
Epoch time: 13024
12153739 = yrday
fracday
Element set: 908
Inclination: 51
6480 deg
RA of node: 103
9963 deg
Eccentricity:
0013271
Arg of perigee: 194
9538 deg
Mean anomaly: 165
1223 deg
Mean motion: 15
51996254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 306
Coasting Arc #10 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2013/025/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3808607
65 A = 6788444
28 meter
Y = 3836268
97 meter E =
0016004
Z = 4111321
58 I = 51
99265
XDOT = -2128
421141 Wp = 157
00679
YDOT = -6266
210306 meter/sec RA = 98
32584 deg
ZDOT = 3855
893642 TA = 253
19340
MA = 253
36902
Ha = 226
980 n
mi
Hp = 217
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12495431
93 X = -3871193
85
Y = 12586184
29 feet Y = 3793328
61 meter
Z = 13488587
86 Z = 4092668
24
XDOT = -6983
008993 XDOT = -2076
923377
YDOT = -20558
432761 feet/sec YDOT = -6289
723883 meter/sec
ZDOT = 12650
569693 ZDOT = 3845
678963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16323850
98 X = 4975509
78
Y = -7083797
40 feet Y = -2159141
45 meter
Z = 13410501
86 Z = 4087520
97
XDOT = -1504
844033 XDOT = -458
676461
YDOT = 20523
452069 feet/sec YDOT = 6255
548191 meter/sec
ZDOT = 12608
822440 ZDOT = 3843
169080
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 13025
15176610
00016717 00000-0 10270-3 0 9094
2 25544 51
6479 98
8766 0013035 198
4143 161
6538 15
52009495 12496
Satellite: ISS
Catalog Number: 25544
Epoch time: 13025
15176610 = yrday
fracday
Element set: 909
Inclination: 51
6479 deg
RA of node: 98
8766 deg
Eccentricity:
0013035
Arg of perigee: 198
4143 deg
Mean anomaly: 161
6538 deg
Mean motion: 15
52009495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1249
Checksum: 324
Coasting Arc #11 (Orbit 1263)
---------------------------------------
Vector Time (GMT): 2013/026/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3857206
55 A = 6786132
17 meter
Y = -3015897
98 meter E =
0009969
Z = -4698997
54 I = 51
98764
XDOT = 1855
542174 Wp = 149
77904
YDOT = 6852
824092 meter/sec RA = 93
37635 deg
ZDOT = -2886
154584 TA = 91
72409
MA = 91
60990
Ha = 226
841 n
mi
Hp = 217
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12654877
13 X = 3913470
23
Y = -9894678
41 feet Y = -2972449
54 meter
Z = -15416658
59 Z = -4680123
43
XDOT = 6087
736791 XDOT = 1792
794380
YDOT = 22483
018675 feet/sec YDOT = 6873
223176 meter/sec
ZDOT = -9469
011102 ZDOT = -2877
292922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15414089
56 X = -4698214
50
Y = 4783654
27 feet Y = 1458057
82 meter
Z = -15337745
37 Z = -4674944
79
XDOT = 2496
417549 XDOT = 760
908069
YDOT = -22084
084925 feet/sec YDOT = -6731
229085 meter/sec
ZDOT = -9432
968167 ZDOT = -2875
168697
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 13026
11759147
00016717 00000-0 10270-3 0 9105
2 25544 51
6467 94
0768 0013132 202
3157 157
7425 15
52048480 12646
Satellite: ISS
Catalog Number: 25544
Epoch time: 13026
11759147 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 94
0768 deg
Eccentricity:
0013132
Arg of perigee: 202
3157 deg
Mean anomaly: 157
7425 deg
Mean motion: 15
52048480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1264
Checksum: 295
Coasting Arc #12 (Orbit 1279)
---------------------------------------
Vector Time (GMT): 2013/027/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3924911
47 A = 6784557
08 meter
Y = 2171678
83 meter E =
0014886
Z = 5095092
97 I = 51
98311
XDOT = -1627
851189 Wp = 184
17412
YDOT = -7259
582778 meter/sec RA = 88
42432 deg
ZDOT = 1826
154843 TA = 248
13418
MA = 248
29255
Ha = 226
640 n
mi
Hp = 217
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12877006
13 X = -3973653
93
Y = 7124930
54 feet Y = 2127515
41 meter
Z = 16716184
27 Z = 5075908
19
XDOT = -5340
719125 XDOT = -1555
422768
YDOT = -23817
528799 feet/sec YDOT = -7277
381482 meter/sec
ZDOT = 5991
321663 ZDOT = 1818
422915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14617681
11 X = 4455469
20
Y = -2361596
18 feet Y = -719814
52 meter
Z = 16636075
29 Z = 5070675
75
XDOT = -3091
739895 XDOT = -942
362320
YDOT = 23175
519087 feet/sec YDOT = 7063
898218 meter/sec
ZDOT = 5960
032949 ZDOT = 1816
618043
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 13027
14779547
00016717 00000-0 10270-3 0 9116
2 25544 51
6467 88
9572 0013015 205
6557 154
3951 15
52035374 12804
Satellite: ISS
Catalog Number: 25544
Epoch time: 13027
14779547 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 88
9572 deg
Eccentricity:
0013015
Arg of perigee: 205
6557 deg
Mean anomaly: 154
3951 deg
Mean motion: 15
52035374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1280
Checksum: 314
Coasting Arc #13 (Orbit 1294)
---------------------------------------
Vector Time (GMT): 2013/028/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4045235
13 A = 6783417
37 meter
Y = -1208627
92 meter E =
0013028
Z = -5315539
04 I = 51
97651
XDOT = 1382
650313 Wp = 140
90605
YDOT = 7504
955911 meter/sec RA = 83
46817 deg
ZDOT = -664
940339 TA = 122
83031
MA = 122
70481
Ha = 226
410 n
mi
Hp = 217
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13271768
81 X = 4084270
46
Y = -3965314
70 feet Y = -1163173
36 meter
Z = -17439432
54 Z = -5295793
29
XDOT = 4536
254307 XDOT = 1301
855570
YDOT = 24622
558764 feet/sec YDOT = 7519
965819 meter/sec
ZDOT = -2181
562793 ZDOT = -658
420027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13945218
92 X = -4250502
73
Y = -509127
65 feet Y = -155182
11 meter
Z = -17357103
26 Z = -5290445
07
XDOT = 3506
549545 XDOT = 1068
796301
YDOT = -23770
273622 feet/sec YDOT = -7245
179400 meter/sec
ZDOT = -2155
350364 ZDOT = -656
950791
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 13028
11359718
00016717 00000-0 10270-3 0 9129
2 25544 51
6452 84
1563 0013071 209
2857 150
7563 15
52094836 12954
Satellite: ISS
Catalog Number: 25544
Epoch time: 13028
11359718 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 84
1563 deg
Eccentricity:
0013071
Arg of perigee: 209
2857 deg
Mean anomaly: 150
7563 deg
Mean motion: 15
52094836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1295
Checksum: 307
Coasting Arc #14 (Orbit 1310)
---------------------------------------
Vector Time (GMT): 2013/029/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4193721
84 A = 6783399
40 meter
Y = 284233
92 meter E =
0010960
Z = 5327286
58 I = 51
97203
XDOT = -1136
533208 Wp = 204
19981
YDOT = -7561
434563 meter/sec RA = 78
51275 deg
ZDOT = -501
348870 TA = 250
50539
MA = 250
62381
Ha = 226
267 n
mi
Hp = 218
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13758929
93 X = -4222466
47
Y = 932525
99 feet Y = 237176
53 meter
Z = 17477974
34 Z = 5306844
48
XDOT = -3728
783491 XDOT = -1049
459812
YDOT = -24807
856179 feet/sec YDOT = -7573
657151 meter/sec
ZDOT = -1644
845374 ZDOT = -506
658209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13498446
94 X = 4114326
63
Y = 3307223
56 feet Y = 1008041
74 meter
Z = 17392859
08 Z = 5301343
45
XDOT = -3723
814305 XDOT = -1135
018600
YDOT = 23785
466185 feet/sec YDOT = 7249
810093 meter/sec
ZDOT = -1666
006108 ZDOT = -507
798662
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 13029
14377554
00016717 00000-0 10270-3 0 9132
2 25544 51
6453 79
0368 0013075 212
9646 147
0691 15
52081052 13118
Satellite: ISS
Catalog Number: 25544
Epoch time: 13029
14377554 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 79
0368 deg
Eccentricity:
0013075
Arg of perigee: 212
9646 deg
Mean anomaly: 147
0691 deg
Mean motion: 15
52081052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1311
Checksum: 294
Coasting Arc #15 (Orbit 1325)
---------------------------------------
Vector Time (GMT): 2013/030/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4389827
86 A = 6784118
77 meter
Y = 683530
63 meter E =
0014527
Z = -5135051
91 I = 51
96679
XDOT = 822
119261 Wp = 158
20540
YDOT = 7426
478839 meter/sec RA = 73
55479 deg
ZDOT = 1679
755370 TA = 128
02905
MA = 127
89784
Ha = 225
979 n
mi
Hp = 218
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14402322
38 X = 4406802
43
Y = 2242554
56 feet Y = 732715
13 meter
Z = -16847283
17 Z = -5113685
73
XDOT = 2697
241670 XDOT = 730
854060
YDOT = 24365
088053 feet/sec YDOT = 7435
162072 meter/sec
ZDOT = 5511
008431 ZDOT = 1683
527081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13257194
79 X = -4040792
97
Y = -6299864
41 feet Y = -1920198
67 meter
Z = -16758442
23 Z = -5107973
19
XDOT = 3963
430833 XDOT = 1208
053718
YDOT = -23141
530561 feet/sec YDOT = -7053
538515 meter/sec
ZDOT = 5525
780090 ZDOT = 1684
257771
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 13030
10955476
00016717 00000-0 10270-3 0 9146
2 25544 51
6442 74
2350 0013056 216
0979 143
9293 15
52132772 13262
Satellite: ISS
Catalog Number: 25544
Epoch time: 13030
10955476 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 74
2350 deg
Eccentricity:
0013056
Arg of perigee: 216
0979 deg
Mean anomaly: 143
9293 deg
Mean motion: 15
52132772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1326
Checksum: 292
Coasting Arc #16 (Orbit 1341)
---------------------------------------
Vector Time (GMT): 2013/031/02:18:45
308
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4594683
77 A = 6785726
52 meter
Y = -1550952
03 meter E =
0006612
Z = 4744829
55 I = 51
96273
XDOT = -457
529200 Wp = 192
07996
YDOT = -7128
968420 meter/sec RA = 68
60073 deg
ZDOT = -2780
300166 TA = 285
30316
MA = 285
37622
Ha = 225
844 n
mi
Hp = 218
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15074421
80 X = -4600047
94
Y = -5088425
29 feet Y = -1602362
43 meter
Z = 15567026
07 Z = 4722496
38
XDOT = -1501
080051 XDOT = -364
271825
YDOT = -23389
004004 feet/sec YDOT = -7133
563503 meter/sec
ZDOT = -9121
719705 ZDOT = -2782
295906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13235554
38 X = 4034196
98
Y = 8990527
94 feet Y = 2740312
92 meter
Z = 15474271
32 Z = 4716557
90
XDOT = -4261
884613 XDOT = -1299
022430
YDOT = 21947
330955 feet/sec YDOT = 6689
546475 meter/sec
ZDOT = -9129
129175 ZDOT = -2782
558573
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 13031
13970761
00016717 00000-0 10270-3 0 9155
2 25544 51
6444 69
1154 0013088 220
1536 139
8650 15
52129566 13425
Satellite: ISS
Catalog Number: 25544
Epoch time: 13031
13970761 = yrday
fracday
Element set: 915
Inclination: 51
6444 deg
RA of node: 69
1154 deg
Eccentricity:
0013088
Arg of perigee: 220
1536 deg
Mean anomaly: 139
8650 deg
Mean motion: 15
52129566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1342
Checksum: 294
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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