[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 7th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
224/13:30:14
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 219
5
226/17:17:51
120 -2
6 3
7 3
7
N/A 1
8 0
2 228
0
000/00:07:42
239 -1
9 -0
3 221
5
227/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 221
2
Coasting Arc #1 (Orbit 1913)
---------------------------------------
Vector Time (GMT): 2014/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3653198
13 A = 6795677
91 meter
Y = -4830729
61 meter E =
0013025
Z = 3063476
48 I = 51
46916
XDOT = 5766
051142 Wp = 52
94379
YDOT = -1250
111689 meter/sec RA = 209
14947 deg
ZDOT = 4898
025388 TA = 342
29480
MA = 342
34014
Ha = 227
224 n
mi
Hp = 220
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11985558
18 X = -3613789
54
Y = -15848850
43 feet Y = -4871361
83 meter
Z = 10050775
84 Z = 3045825
40
XDOT = 18917
490624 XDOT = 5755
808823
YDOT = -4101
416304 feet/sec YDOT = -1185
689500 meter/sec
ZDOT = 16069
637100 ZDOT = 4926
010852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2989580
26 X = -911224
06
Y = 19682180
49 feet Y = 5999128
61 meter
Z = 9976569
59 Z = 3040858
41
XDOT = -14606
927166 XDOT = -4452
191400
YDOT = -10435
716368 feet/sec YDOT = -3180
806349 meter/sec
ZDOT = 16188
674849 ZDOT = 4934
308094
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 14218
55822188
00016717 00000-0 10270-3 0 9002
2 25544 51
6428 209
9121 0007005 338
0635 22
0215 15
50607240 19149
Satellite: ISS
Catalog Number: 25544
Epoch time: 14218
55822188 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 209
9121 deg
Eccentricity:
0007005
Arg of perigee: 338
0635 deg
Mean anomaly: 22
0215 deg
Mean motion: 15
50607240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1914
Checksum: 275
Coasting Arc #2 (Orbit 1928)
---------------------------------------
Vector Time (GMT): 2014/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3533691
84 A = 6794531
56 meter
Y = 4637642
79 meter E =
0007556
Z = -3498191
99 I = 51
49236
XDOT = -6062
284647 Wp = 23
18546
YDOT = 1213
243796 meter/sec RA = 204
17983 deg
ZDOT = -4511
915360 TA = 197
92149
MA = 197
94815
Ha = 227
404 n
mi
Hp = 220
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11593477
17 X = 3498562
89
Y = 15215363
47 feet Y = 4676962
57 meter
Z = -11477007
85 Z = -3481111
12
XDOT = -19889
385325 XDOT = -6053
483717
YDOT = 3980
458647 feet/sec YDOT = 1145
500867 meter/sec
ZDOT = -14802
871917 ZDOT = -4541
343250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2474750
89 X = 754304
07
Y = -19011449
44 feet Y = -5794689
79 meter
Z = -11405178
90 Z = -3476298
53
XDOT = 15445
540666 XDOT = 4707
800795
YDOT = 10972
926250 feet/sec YDOT = 3344
547921 meter/sec
ZDOT = -14928
045945 ZDOT = -4550
068404
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 14219
52495540
00016717 00000-0 10270-3 0 9019
2 25544 51
6423 205
1176 0007060 343
0971 16
9943 15
50593506 19297
Satellite: ISS
Catalog Number: 25544
Epoch time: 14219
52495540 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 205
1176 deg
Eccentricity:
0007060
Arg of perigee: 343
0971 deg
Mean anomaly: 16
9943 deg
Mean motion: 15
50593506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1929
Checksum: 300
Coasting Arc #3 (Orbit 1944)
---------------------------------------
Vector Time (GMT): 2014/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3353277
29 A = 6793162
92 meter
Y = -4439535
94 meter E =
0010678
Z = 3885563
73 I = 51
51699
XDOT = 6368
097335 Wp = 61
18347
YDOT = -1225
596016 meter/sec RA = 199
21208 deg
ZDOT = 4091
896701 TA = 345
82469
MA = 345
85463
Ha = 227
445 n
mi
Hp = 220
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11001565
91 X = -3322258
64
Y = -14565406
64 feet Y = -4476861
19 meter
Z = 12747912
51 Z = 3869349
42
XDOT = 20892
707791 XDOT = 6361
452182
YDOT = -4020
984304 feet/sec YDOT = -1154
421182 meter/sec
ZDOT = 13424
857942 ZDOT = 4122
815268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2117185
59 X = -645318
17
Y = 18177927
76 feet Y = 5540632
38 meter
Z = 12679718
61 Z = 3864778
23
XDOT = -16452
928036 XDOT = -5014
852465
YDOT = -11380
358712 feet/sec YDOT = -3468
733335 meter/sec
ZDOT = 13556
382907 ZDOT = 4131
985510
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 14220
55612422
00016717 00000-0 10270-3 0 9025
2 25544 51
6422 200
0044 0007100 345
1707 14
9234 15
50643256 19456
Satellite: ISS
Catalog Number: 25544
Epoch time: 14220
55612422 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 200
0044 deg
Eccentricity:
0007100
Arg of perigee: 345
1707 deg
Mean anomaly: 14
9234 deg
Mean motion: 15
50643256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1945
Checksum: 255
Coasting Arc #4 (Orbit 1959)
---------------------------------------
Vector Time (GMT): 2014/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3140002
71 A = 6791987
34 meter
Y = 4279332
34 meter E =
0011650
Z = -4249706
60 I = 51
54291
XDOT = -6626
807042 Wp = 33
21943
YDOT = 1274
398453 meter/sec RA = 194
24389 deg
ZDOT = -3608
278960 TA = 199
73415
MA = 199
77927
Ha = 227
612 n
mi
Hp = 220
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10301846
17 X = 3112560
12
Y = 14039804
28 feet Y = 4314292
54 meter
Z = -13942606
96 Z = -4234519
79
XDOT = -21741
492920 XDOT = -6623
037667
YDOT = 4181
097286 feet/sec YDOT = 1200
314387 meter/sec
ZDOT = -11838
185565 ZDOT = -3640
461163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1953024
00 X = 595281
72
Y = -17355308
66 feet Y = -5289898
08 meter
Z = -13878738
63 Z = -4230239
53
XDOT = 17446
656004 XDOT = 5317
740750
YDOT = 11552
293929 feet/sec YDOT = 3521
139189 meter/sec
ZDOT = -11975
103351 ZDOT = -3650
011501
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 14221
52283715
00016717 00000-0 10270-3 0 9033
2 25544 51
6424 195
2096 0007173 350
2692 9
8312 15
50628542 19608
Satellite: ISS
Catalog Number: 25544
Epoch time: 14221
52283715 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 195
2096 deg
Eccentricity:
0007173
Arg of perigee: 350
2692 deg
Mean anomaly: 9
8312 deg
Mean motion: 15
50628542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1960
Checksum: 295
Coasting Arc #5 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2014/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2865161
70 A = 6790660
63 meter
Y = -4131345
59 meter E =
0008018
Z = 4556548
87 I = 51
57000
XDOT = 6882
859171 Wp = 62
72021
YDOT = -1361
892236 meter/sec RA = 189
27800 deg
ZDOT = 3092
550782 TA = 356
28861
MA = 356
29456
Ha = 227
641 n
mi
Hp = 219
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9400136
80 X = -2840884
82
Y = -13554283
45 feet Y = -4163249
93 meter
Z = 14949307
31 Z = 4542689
62
XDOT = 22581
558961 XDOT = 6882
554354
YDOT = -4468
150382 feet/sec YDOT = -1284
925363 meter/sec
ZDOT = 10146
163984 ZDOT = 3125
985213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1995674
21 X = -608281
50
Y = 16426718
11 feet Y = 5006863
68 meter
Z = 14891043
53 Z = 4538790
07
XDOT = -18537
510387 XDOT = -5650
233166
YDOT = -11580
484471 feet/sec YDOT = -3529
731667 meter/sec
ZDOT = 10288
431364 ZDOT = 3135
913880
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 14222
55398396
00016717 00000-0 10270-3 0 9040
2 25544 51
6430 190
0964 0007191 352
2735 7
8304 15
50678528 19767
Satellite: ISS
Catalog Number: 25544
Epoch time: 14222
55398396 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 190
0964 deg
Eccentricity:
0007191
Arg of perigee: 352
2735 deg
Mean anomaly: 7
8304 deg
Mean motion: 15
50678528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 321
Coasting Arc #6 (Orbit 1990)
---------------------------------------
Vector Time (GMT): 2014/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2574468
86 A = 6789666
28 meter
Y = 4033641
23 meter E =
0015029
Z = -4830236
13 I = 51
59813
XDOT = -7068
756539 Wp = 44
42009
YDOT = 1476
917402 meter/sec RA = 184
31201 deg
ZDOT = -2528
526729 TA = 200
60791
MA = 200
66859
Ha = 227
788 n
mi
Hp = 219
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8446420
16 X = 2552635
63
Y = 13233731
08 feet Y = 4062308
39 meter
Z = -15847231
41 Z = -4817783
15
XDOT = -23191
458461 XDOT = -7072
463912
YDOT = 4845
529533 feet/sec YDOT = 1397
849205 meter/sec
ZDOT = -8295
691369 ZDOT = -2562
874023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2218675
73 X = 676252
36
Y = -15595077
83 feet Y = -4753379
72 meter
Z = -15794917
55 Z = -4814290
87
XDOT = 19513
801506 XDOT = 5947
806699
YDOT = 11345
249637 feet/sec YDOT = 3458
032089 meter/sec
ZDOT = -8441
869121 ZDOT = -2573
081708
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 14223
52067589
00016717 00000-0 10270-3 0 9056
2 25544 51
6436 185
3018 0007265 356
9653 3
1453 15
50663337 19915
Satellite: ISS
Catalog Number: 25544
Epoch time: 14223
52067589 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 185
3018 deg
Eccentricity:
0007265
Arg of perigee: 356
9653 deg
Mean anomaly: 3
1453 deg
Mean motion: 15
50663337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1991
Checksum: 315
Coasting Arc #7 (Orbit 2006)
---------------------------------------
Vector Time (GMT): 2014/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2226664
24 A = 6788599
61 meter
Y = -3963057
90 meter E =
0006223
Z = 5036637
78 I = 51
62706
XDOT = 7241
543180 Wp = 50
16059
YDOT = -1613
783200 meter/sec RA = 179
34854 deg
ZDOT = 1933
950182 TA = 21
08402
MA = 21
05838
Ha = 227
809 n
mi
Hp = 219
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7305328
88 X = -2206648
83
Y = -13002158
45 feet Y = -3987845
75 meter
Z = 16524402
16 Z = 5025869
96
XDOT = 23758
343766 XDOT = 7249
656339
YDOT = -5294
564305 feet/sec YDOT = -1532
758138 meter/sec
ZDOT = 6344
980912 ZDOT = 1969
147686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2672565
31 X = -814597
91
Y = 14723184
23 feet Y = 4487626
55 meter
Z = 16479231
24 Z = 5022869
68
XDOT = -20504
673654 XDOT = -6249
824530
YDOT = -10982
964189 feet/sec YDOT = -3347
607485 meter/sec
ZDOT = 6494
804860 ZDOT = 1979
616521
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 14224
55180010
00016717 00000-0 10270-3 0 9066
2 25544 51
6444 180
1888 0007273 359
3325
7815 15
50713108 20070
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
55180010 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 180
1888 deg
Eccentricity:
0007273
Arg of perigee: 359
3325 deg
Mean anomaly:
7815 deg
Mean motion: 15
50713108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2007
Checksum: 280
Coasting Arc #8 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2014/224/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3323345
94 A = 6790155
35 meter
Y = -3637254
65 meter E =
0008307
Z = 4664275
44 I = 51
63522
XDOT = 6684
549770 Wp = 63
85274
YDOT = -2400
137026 meter/sec RA = 179
04406 deg
ZDOT = 2890
740224 TA = 357
40763
MA = 357
41194
Ha = 227
845 n
mi
Hp = 219
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10903365
96 X = -3305083
45
Y = -11933250
18 feet Y = -3674316
12 meter
Z = 15302740
94 Z = 4648175
92
XDOT = 21930
937565 XDOT = 6696
849821
YDOT = -7874
465309 feet/sec YDOT = -2325
317167 meter/sec
ZDOT = 9484
055853 ZDOT = 2923
242201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6941490
13 X = 2115766
19
Y = 14668824
76 feet Y = 4471057
79 meter
Z = 15234862
13 Z = 4643585
98
XDOT = -22153
989765 XDOT = -6752
536080
YDOT = 488
285580 feet/sec YDOT = 148
829445 meter/sec
ZDOT = 9622
542081 ZDOT = 2932
950826
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 14224
61624517
00016717 00000-0 10270-3 0 9079
2 25544 51
6455 179
8696 0007235 359
9121
2028 15
50711381 20085
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
61624517 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 179
8696 deg
Eccentricity:
0007235
Arg of perigee: 359
9121 deg
Mean anomaly:
2028 deg
Mean motion: 15
50711381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 298
Coasting Arc #9 (Orbit 2022)
---------------------------------------
Vector Time (GMT): 2014/225/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3000856
73 A = 6789141
60 meter
Y = 3603460
92 meter E =
0016177
Z = -4923757
00 I = 51
66352
XDOT = -6839
100938 Wp = 48
31361
YDOT = 2540
229547 meter/sec RA = 174
08240 deg
ZDOT = -2303
523310 TA = 199
08336
MA = 199
14403
Ha = 227
942 n
mi
Hp = 219
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9845330
47 X = 2984256
66
Y = 11822378
36 feet Y = 3636925
36 meter
Z = -16154058
41 Z = -4909219
99
XDOT = -22437
995205 XDOT = -6855
808457
YDOT = 8334
086440 feet/sec YDOT = 2463
656765 meter/sec
ZDOT = -7557
491175 ZDOT = -2336
786936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6214011
99 X = -1894030
85
Y = -14144268
44 feet Y = -4311173
02 meter
Z = -16092808
66 Z = -4905088
08
XDOT = 22799
364977 XDOT = 6949
246445
YDOT = -1235
583540 feet/sec YDOT = -376
605863 meter/sec
ZDOT = -7699
246520 ZDOT = -2346
730339
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 14225
58291484
00016717 00000-0 10270-3 0 9080
2 25544 51
6460 175
0754 0007374 4
2741 355
8472 15
50716483 20233
Satellite: ISS
Catalog Number: 25544
Epoch time: 14225
58291484 = yrday
fracday
Element set: 908
Inclination: 51
6460 deg
RA of node: 175
0754 deg
Eccentricity:
0007374
Arg of perigee: 4
2741 deg
Mean anomaly: 355
8472 deg
Mean motion: 15
50716483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2023
Checksum: 307
Coasting Arc #10 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2014/226/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2627402
69 A = 6788185
92 meter
Y = -3606097
71 meter E =
0006669
Z = 5110342
11 I = 51
69157
XDOT = 6976
650575 Wp = 51
03288
YDOT = -2697
189438 meter/sec RA = 169
12241 deg
ZDOT = 1686
290973 TA = 22
70549
MA = 22
67601
Ha = 227
976 n
mi
Hp = 219
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8620087
58 X = -2611707
35
Y = -11831029
23 feet Y = -3635391
01 meter
Z = 16766214
27 Z = 5097616
99
XDOT = 22889
273539 XDOT = 6998
101273
YDOT = -8849
046712 feet/sec YDOT = -2619
052007 meter/sec
ZDOT = 5532
450698 ZDOT = 1720
234436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5276464
47 X = 1608266
37
Y = 13719728
67 feet Y = 4181773
30 meter
Z = 16712662
01 Z = 5094019
38
XDOT = -23381
740469 XDOT = -7126
754495
YDOT = 2087
284706 feet/sec YDOT = 636
204378 meter/sec
ZDOT = 5677
131781 ZDOT = 1730
389767
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 14226
61401563
00016717 00000-0 10270-3 0 9097
2 25544 51
6459 169
9621 0007275 6
9396 353
1855 15
50749639 20393
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
61401563 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 169
9621 deg
Eccentricity:
0007275
Arg of perigee: 6
9396 deg
Mean anomaly: 353
1855 deg
Mean motion: 15
50749639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 334
Coasting Arc #11 (Orbit 2040)
---------------------------------------
Vector Time (GMT): 2014/226/17:21:42
239
Vector Time (MET): N/A
Weight (LBS) : 940792
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2909510
17 A = 6790545
59 meter
Y = 3482614
21 meter E =
0014032
Z = -5063507
52 I = 51
69781
XDOT = -6809
656577 Wp = 51
34049
YDOT = 2932
043306 meter/sec RA = 168
32769 deg
ZDOT = -1891
230745 TA = 200
27272
MA = 200
32849
Ha = 228
017 n
mi
Hp = 221
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9545637
04 X = 2894947
18
Y = 11425899
62 feet Y = 3515068
56 meter
Z = -16612557
48 Z = -5049409
21
XDOT = -22341
392968 XDOT = -6832
750350
YDOT = 9619
564651 feet/sec YDOT = 2855
764115 meter/sec
ZDOT = -6204
825278 ZDOT = -1924
366998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14837909
39 X = -4522594
78
Y = -1864705
26 feet Y = -568362
16 meter
Z = -16553149
36 Z = -5045399
93
XDOT = 9750
113742 XDOT = 2971
834669
YDOT = -21102
812637 feet/sec YDOT = -6432
137292 meter/sec
ZDOT = -6346
112442 ZDOT = -1934
295072
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 14226
74290707
00016717 00000-0 10270-3 0 9109
2 25544 51
6464 169
3232 0005865 344
2517 15
8451 15
50034904 20416
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
74290707 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 169
3232 deg
Eccentricity:
0005865
Arg of perigee: 344
2517 deg
Mean anomaly: 15
8451 deg
Mean motion: 15
50034904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2041
Checksum: 289
Coasting Arc #12 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2014/227/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4100446
92 A = 6795788
94 meter
Y = 4057252
48 meter E =
0006461
Z = -3591776
02 I = 51
73506
XDOT = -5895
351290 Wp = 41
05310
YDOT = -2027
389529 meter/sec RA = 164
71814 deg
ZDOT = 4449
425916 TA = 276
63211
MA = 276
70564
Ha = 228
089 n
mi
Hp = 221
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13452909
84 X = -4128063
74
Y = 13311195
79 feet Y = 4011244
07 meter
Z = -11784042
07 Z = -3611762
49
XDOT = -19341
703707 XDOT = -5893
856105
YDOT = -6651
540450 feet/sec YDOT = -2093
306615 meter/sec
ZDOT = 14597
854055 ZDOT = 4420
791078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18444766
21 X = 5621964
74
Y = 3991909
13 feet Y = 1216733
90 meter
Z = -11869609
31 Z = -3617856
92
XDOT = 5275
078098 XDOT = 1607
843804
YDOT = 18580
714850 feet/sec YDOT = 5663
401886 meter/sec
ZDOT = 14476
432239 ZDOT = 4412
416547
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 14227
45210355
00016717 00000-0 10270-3 0 9110
2 25544 51
6441 165
8091 0005767 348
6647 11
4373 15
50014980 20527
Satellite: ISS
Catalog Number: 25544
Epoch time: 14227
45210355 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 165
8091 deg
Eccentricity:
0005767
Arg of perigee: 348
6647 deg
Mean anomaly: 11
4373 deg
Mean motion: 15
50014980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2052
Checksum: 291
Coasting Arc #13 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2014/228/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4105870
53 A = 6796506
79 meter
Y = -4287683
24 meter E =
0012935
Z = 3304733
97 I = 51
76804
XDOT = 5743
827792 Wp = 65
63697
YDOT = 1846
762252 meter/sec RA = 159
77147 deg
ZDOT = -4720
424867 TA = 76
10501
MA = 75
96117
Ha = 228
142 n
mi
Hp = 221
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13470703
84 X = 4137458
01
Y = -14067202
24 feet Y = -4241592
04 meter
Z = 10842303
07 Z = 3324756
42
XDOT = 18844
579369 XDOT = 5745
680125
YDOT = 6058
931274 feet/sec YDOT = 1911
003670 meter/sec
ZDOT = -15486
958225 ZDOT = -4692
517908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19151349
91 X = -5837331
45
Y = -3271798
29 feet Y = -997244
12 meter
Z = 10928069
77 Z = 3330875
67
XDOT = -5782
112304 XDOT = -1762
387830
YDOT = -17701
899280 feet/sec YDOT = -5395
538900 meter/sec
ZDOT = -15368
593164 ZDOT = -4684
347196
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 14228
48364996
00016717 00000-0 10270-3 0 9126
2 25544 51
6445 160
6983 0005812 352
0402 8
0655 15
50059498 20688
Satellite: ISS
Catalog Number: 25544
Epoch time: 14228
48364996 = yrday
fracday
Element set: 912
Inclination: 51
6445 deg
RA of node: 160
6983 deg
Eccentricity:
0005812
Arg of perigee: 352
0402 deg
Mean anomaly: 8
0655 deg
Mean motion: 15
50059498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2068
Checksum: 318
Coasting Arc #14 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2014/229/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4048141
49 A = 6797259
12 meter
Y = 4538062
41 meter E =
0008146
Z = -3030972
17 I = 51
79929
XDOT = -5591
147228 Wp = 28
18917
YDOT = -1683
933328 meter/sec RA = 154
82718 deg
ZDOT = 4958
689881 TA = 297
22520
MA = 297
30818
Ha = 228
237 n
mi
Hp = 220
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13281304
11 X = -4083862
90
Y = 14888656
19 feet Y = 4492593
70 meter
Z = -9944134
43 Z = -3050724
16
XDOT = -18343
658884 XDOT = -5595
989097
YDOT = -5524
715644 feet/sec YDOT = -1746
484140 meter/sec
ZDOT = 16268
667587 ZDOT = 4931
517341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19773380
86 X = 6026926
48
Y = 2321090
54 feet Y = 707468
40 meter
Z = -10028802
50 Z = -3056779
00
XDOT = 6194
826753 XDOT = 1888
183194
YDOT = 16845
867863 feet/sec YDOT = 5134
620525 meter/sec
ZDOT = 16153
389249 ZDOT = 4923
553043
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 14229
45071427
00016717 00000-0 10270-3 0 9139
2 25544 51
6443 155
9070 0005847 355
0844 5
0248 15
50051832 20837
Satellite: ISS
Catalog Number: 25544
Epoch time: 14229
45071427 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 155
9070 deg
Eccentricity:
0005847
Arg of perigee: 355
0844 deg
Mean anomaly: 5
0248 deg
Mean motion: 15
50051832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 290
Coasting Arc #15 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2014/230/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4003698
69 A = 6797951
27 meter
Y = -4778880
38 meter E =
0013478
Z = 2703399
79 I = 51
83058
XDOT = 5407
662464 Wp = 76
55376
YDOT = 1580
158461 meter/sec RA = 149
88507 deg
ZDOT = -5190
567873 TA = 73
04636
MA = 72
89867
Ha = 228
301 n
mi
Hp = 220
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13135494
39 X = 4043707
54
Y = -15678741
40 feet Y = -4733884
71 meter
Z = 8869421
87 Z = 2722946
23
XDOT = 17741
674752 XDOT = 5414
804743
YDOT = 5184
246920 feet/sec YDOT = 1640
670327 meter/sec
ZDOT = -17029
422157 ZDOT = -5164
281113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20369009
38 X = -6208474
06
Y = -1404728
75 feet Y = -428161
32 meter
Z = 8953266
62 Z = 2728955
67
XDOT = -6367
465354 XDOT = -1940
803440
YDOT = -16012
647899 feet/sec YDOT = -4880
655080 meter/sec
ZDOT = -16917
882804 ZDOT = -5156
570679
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 14230
48223853
00016717 00000-0 10270-3 0 9147
2 25544 51
6452 150
7959 0005857 358
9806 1
1332 15
50091660 20998
Satellite: ISS
Catalog Number: 25544
Epoch time: 14230
48223853 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 150
7959 deg
Eccentricity:
0005857
Arg of perigee: 358
9806 deg
Mean anomaly: 1
1332 deg
Mean motion: 15
50091660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2099
Checksum: 309
Coasting Arc #16 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2014/231/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3891668
87 A = 6798624
56 meter
Y = 5027829
85 meter E =
0010532
Z = -2394871
04 I = 51
85916
XDOT = -5237
197766 Wp = 24
05744
YDOT = -1495
116990 meter/sec RA = 144
94518 deg
ZDOT = 5389
282314 TA = 309
31540
MA = 309
40872
Ha = 228
376 n
mi
Hp = 220
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12767942
49 X = -3935968
60
Y = 16495504
77 feet Y = 4984062
99 meter
Z = -7857188
45 Z = -2413883
62
XDOT = -17182
407368 XDOT = -5246
268883
YDOT = -4905
239467 feet/sec YDOT = -1553
733406 meter/sec
ZDOT = 17681
372420 ZDOT = 5363
819015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20826833
98 X = 6348019
00
Y = 275038
75 feet Y = 83831
81 meter
Z = -7938814
99 Z = -2419750
81
XDOT = 6475
233115 XDOT = 1973
651054
YDOT = 15257
364068 feet/sec YDOT = 4650
444568 meter/sec
ZDOT = 17573
310208 ZDOT = 5356
344951
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 14231
44928199
00016717 00000-0 10270-3 0 9150
2 25544 51
6450 146
0046 0005896 1
6968 358
4202 15
50088193 21144
Satellite: ISS
Catalog Number: 25544
Epoch time: 14231
44928199 = yrday
fracday
Element set: 915
Inclination: 51
6450 deg
RA of node: 146
0046 deg
Eccentricity:
0005896
Arg of perigee: 1
6968 deg
Mean anomaly: 358
4202 deg
Mean motion: 15
50088193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 308
Coasting Arc #17 (Orbit 2129)
---------------------------------------
Vector Time (GMT): 2014/232/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3793119
11 A = 6799227
46 meter
Y = -5260982
57 meter E =
0013597
Z = 2030444
74 I = 51
88748
XDOT = 5044
849439 Wp = 86
69572
YDOT = 1473
865841 meter/sec RA = 140
00740 deg
ZDOT = -5572
590682 TA = 70
98812
MA = 70
84085
Ha = 228
446 n
mi
Hp = 220
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12444616
52 X = 3841803
61
Y = -17260441
49 feet Y = -5218293
23 meter
Z = 6661564
10 Z = 2048989
21
XDOT = 16551
343305 XDOT = 5055
062856
YDOT = 4835
517852 feet/sec YDOT = 1530
337662 meter/sec
ZDOT = -18282
777827 ZDOT = -5548
059071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21238641
92 X = -6473538
06
Y = 802129
00 feet Y = 244488
92 meter
Z = 6741248
80 Z = 2054732
63
XDOT = -6354
389356 XDOT = -1936
817876
YDOT = -14575
778613 feet/sec YDOT = -4442
697321 meter/sec
ZDOT = -18178
663660 ZDOT = -5540
856684
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 14232
48078428
00016717 00000-0 10270-3 0 9167
2 25544 51
6461 140
8934 0005876 5
9343 354
1877 15
50120113 21304
Satellite: ISS
Catalog Number: 25544
Epoch time: 14232
48078428 = yrday
fracday
Element set: 916
Inclination: 51
6461 deg
RA of node: 140
8934 deg
Eccentricity:
0005876
Arg of perigee: 5
9343 deg
Mean anomaly: 354
1877 deg
Mean motion: 15
50120113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2130
Checksum: 295
Coasting Arc #18 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2014/233/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3626521
33 A = 6799751
69 meter
Y = 5489752
65 meter E =
0013100
Z = -1691297
77 I = 51
91251
XDOT = -4879
694047 Wp = 25
61773
YDOT = -1468
746638 meter/sec RA = 135
07153 deg
ZDOT = 5723
794796 TA = 315
94191
MA = 316
04622
Ha = 228
509 n
mi
Hp = 220
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11898035
88 X = -3679423
84
Y = 18010999
49 feet Y = 5448902
72 meter
Z = -5548877
18 Z = -1709043
19
XDOT = -16009
494905 XDOT = -4890
711409
YDOT = -4818
722566 feet/sec YDOT = -1523
376029 meter/sec
ZDOT = 18778
854319 ZDOT = 5700
063591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21467866
85 X = 6543405
82
Y = -2058421
35 feet Y = -627406
83 meter
Z = -5625210
47 Z = -1714564
15
XDOT = 6214
393442 XDOT = 1894
147121
YDOT = 14016
255214 feet/sec YDOT = 4272
154589 meter/sec
ZDOT = 18678
133682 ZDOT = 5693
095146
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 14233
44780712
00016717 00000-0 10270-3 0 9171
2 25544 51
6460 136
1020 0005927 8
5845 351
5406 15
50123946 21452
Satellite: ISS
Catalog Number: 25544
Epoch time: 14233
44780712 = yrday
fracday
Element set: 917
Inclination: 51
6460 deg
RA of node: 136
1020 deg
Eccentricity:
0005927
Arg of perigee: 8
5845 deg
Mean anomaly: 351
5406 deg
Mean motion: 15
50123946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 287
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