[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 6th 2013
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) : 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 3257)
---------------------------------------
Vector Time (GMT): 2013/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2601206
44 A = 6789715
44 meter
Y = 4039631
57 meter E =
0016757
Z = -4808723
66 I = 51
66025
XDOT = -7048
487194 Wp = 70
22695
YDOT = -1459
976967 meter/sec RA = 175
10860 deg
ZDOT = 2599
214958 TA = 225
36364
MA = 225
50040
Ha = 229
676 n
mi
Hp = 217
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8534141
88 X = -2622825
39
Y = 13253384
40 feet Y = 4010422
71 meter
Z = -15776652
43 Z = -4821412
45
XDOT = -23124
957986 XDOT = -7044
263985
YDOT = -4789
950679 feet/sec YDOT = -1538
774177 meter/sec
ZDOT = 8527
608130 ZDOT = 2564
983785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9845910
99 X = 3001033
67
Y = 12241362
96 feet Y = 3731167
43 meter
Z = -15830148
68 Z = -4825029
32
XDOT = -11077
832661 XDOT = -3376
523395
YDOT = 19698
434308 feet/sec YDOT = 6004
082777 meter/sec
ZDOT = 8384
812241 ZDOT = 2555
690771
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
51161429
00016717 00000-0 10270-3 0 9000
2 25544 51
6481 176
1629 0010524 27
2702 332
9000 15
50627787 32584
Satellite: ISS
Catalog Number: 25544
Epoch time: 13154
51161429 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 176
1629 deg
Eccentricity:
0010524
Arg of perigee: 27
2702 deg
Mean anomaly: 332
9000 deg
Mean motion: 15
50627787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 288
Coasting Arc #2 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2013/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2930085
45 A = 6790668
00 meter
Y = -4131302
63 meter E =
0018423
Z = 4518073
05 I = 51
69274
XDOT = 6843
127399 Wp = 47
97626
YDOT = 1358
005253 meter/sec RA = 170
14895 deg
ZDOT = -3175
808263 TA = 73
99419
MA = 73
79134
Ha = 229
661 n
mi
Hp = 217
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9613141
26 X = 2954116
93
Y = -13554142
49 feet Y = -4098402
60 meter
Z = 14823074
31 Z = 4532365
34
XDOT = 22451
205376 XDOT = 6842
860713
YDOT = 4455
397811 feet/sec YDOT = 1434
528213 meter/sec
ZDOT = -10419
318447 ZDOT = -3142
565042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10011319
90 X = -3051450
31
Y = -13195149
58 feet Y = -4021881
59 meter
Z = 14883289
18 Z = 4536426
54
XDOT = 10134
969278 XDOT = 3089
138636
YDOT = -19360
530080 feet/sec YDOT = -5901
089568 meter/sec
ZDOT = -10280
623363 ZDOT = -3133
534001
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 13155
54275525
00016717 00000-0 10270-3 0 9018
2 25544 51
6464 171
0490 0010585 31
3199 328
8580 15
50683133 32740
Satellite: ISS
Catalog Number: 25544
Epoch time: 13155
54275525 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 171
0490 deg
Eccentricity:
0010585
Arg of perigee: 31
3199 deg
Mean anomaly: 328
8580 deg
Mean motion: 15
50683133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 302
Coasting Arc #3 (Orbit 3288)
---------------------------------------
Vector Time (GMT): 2013/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3168152
32 A = 6791850
13 meter
Y = 4282384
42 meter E =
0014858
Z = -4221299
75 I = 51
72685
XDOT = -6591
705841 Wp = 66
62563
YDOT = -1262
690154 meter/sec RA = 165
19383 deg
ZDOT = 3682
260102 TA = 241
08441
MA = 241
23353
Ha = 229
803 n
mi
Hp = 217
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10394200
53 X = -3195297
19
Y = 14049817
64 feet Y = 4246804
81 meter
Z = -13849408
64 Z = -4236756
04
XDOT = -21626
331500 XDOT = -6594
983920
YDOT = -4142
684231 feet/sec YDOT = -1336
421487 meter/sec
ZDOT = 12080
905845 ZDOT = 3650
229648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10484894
37 X = 3195795
80
Y = 13917475
34 feet Y = 4242046
48 meter
Z = -13914516
52 Z = -4241144
64
XDOT = -9200
890944 XDOT = -2804
431560
YDOT = 18823
935715 feet/sec YDOT = 5737
535606 meter/sec
ZDOT = 11947
251254 ZDOT = 3641
522182
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 13156
50944170
00016717 00000-0 10270-3 0 9025
2 25544 51
6468 166
2559 0010622 34
4419 325
7418 15
50657461 32894
Satellite: ISS
Catalog Number: 25544
Epoch time: 13156
50944170 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 166
2559 deg
Eccentricity:
0010622
Arg of perigee: 34
4419 deg
Mean anomaly: 325
7418 deg
Mean motion: 15
50657461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 313
Coasting Arc #4 (Orbit 3304)
---------------------------------------
Vector Time (GMT): 2013/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3438206
84 A = 6793038
36 meter
Y = -4434873
68 meter E =
0020379
Z = 3821121
60 I = 51
75931
XDOT = 6295
465045 Wp = 61
13063
YDOT = 1247
352691 meter/sec RA = 160
23975 deg
ZDOT = -4190
355807 TA = 73
09374
MA = 72
87041
Ha = 229
774 n
mi
Hp = 217
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11280206
17 X = 3468980
81
Y = -14550110
48 feet Y = -4396253
88 meter
Z = 12536488
18 Z = 3837898
52
XDOT = 20654
412878 XDOT = 6301
404853
YDOT = 4092
364473 feet/sec YDOT = 1317
786276 meter/sec
ZDOT = -13747
886507 ZDOT = -4159
758031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10961619
09 X = -3341101
50
Y = -14731431
50 feet Y = -4490140
32 meter
Z = 12607146
18 Z = 3842658
16
XDOT = 8493
475673 XDOT = 2588
811385
YDOT = -18050
219775 feet/sec YDOT = -5501
706987 meter/sec
ZDOT = -13620
201182 ZDOT = -4151
437320
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 13157
54056279
00016717 00000-0 10270-3 0 9035
2 25544 51
6453 161
1414 0010652 37
9601 322
2299 15
50714558 33055
Satellite: ISS
Catalog Number: 25544
Epoch time: 13157
54056279 = yrday
fracday
Element set: 903
Inclination: 51
6453 deg
RA of node: 161
1414 deg
Eccentricity:
0010652
Arg of perigee: 37
9601 deg
Mean anomaly: 322
2299 deg
Mean motion: 15
50714558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3305
Checksum: 294
Coasting Arc #5 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2013/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602682
02 A = 6794306
18 meter
Y = 4629803
10 meter E =
0014395
Z = -3429967
09 I = 51
79185
XDOT = -5980
456771 Wp = 57
23340
YDOT = -1248
995154 meter/sec RA = 155
29049 deg
ZDOT = 4617
367624 TA = 262
79923
MA = 262
96291
Ha = 229
906 n
mi
Hp = 216
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11819822
90 X = -3637523
69
Y = 15189642
73 feet Y = 4589321
29 meter
Z = -11253172
87 Z = -3447552
79
XDOT = -19620
921164 XDOT = -5988
475914
YDOT = -4097
753131 feet/sec YDOT = -1315
917854 meter/sec
ZDOT = 15148
843912 ZDOT = 4588
295141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11692348
56 X = 3563827
84
Y = 15233179
43 feet Y = 4643073
09 meter
Z = -11327249
84 Z = -3452545
75
XDOT = -7875
139781 XDOT = -2400
342605
YDOT = 17166
421117 feet/sec YDOT = 5232
325156 meter/sec
ZDOT = 15027
517545 ZDOT = 4580
387348
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 13158
50723059
00016717 00000-0 10270-3 0 9040
2 25544 51
6453 156
3482 0010707 41
5842 318
6122 15
50690189 33209
Satellite: ISS
Catalog Number: 25544
Epoch time: 13158
50723059 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 156
3482 deg
Eccentricity:
0010707
Arg of perigee: 41
5842 deg
Mean anomaly: 318
6122 deg
Mean motion: 15
50690189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 293
Coasting Arc #6 (Orbit 3335)
---------------------------------------
Vector Time (GMT): 2013/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3790008
86 A = 6795499
80 meter
Y = -4811708
58 meter E =
0021385
Z = 2932845
92 I = 51
82313
XDOT = 5625
948709 Wp = 74
41076
YDOT = 1345
142794 meter/sec RA = 150
34237 deg
ZDOT = -5027
206725 TA = 72
26489
MA = 72
03160
Ha = 229
873 n
mi
Hp = 216
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12434412
27 X = 3829285
65
Y = -15786445
48 feet Y = -4769107
12 meter
Z = 9622197
91 Z = 2951352
31
XDOT = 18457
836972 XDOT = 5634
909898
YDOT = 4413
198142 feet/sec YDOT = 1408
106522 meter/sec
ZDOT = -16493
460385 ZDOT = -4999
854191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12383598
35 X = -3774520
78
Y = -15778673
13 feet Y = -4809339
57 meter
Z = 9700161
23 Z = 2956609
14
XDOT = 7555
277044 XDOT = 2302
848443
YDOT = -16071
304542 feet/sec YDOT = -4898
533624 meter/sec
ZDOT = -16379
319742 ZDOT = -4992
416657
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 13159
53833150
00016717 00000-0 10270-3 0 9059
2 25544 51
6447 151
2332 0010706 44
5159 315
6850 15
50744091 33367
Satellite: ISS
Catalog Number: 25544
Epoch time: 13159
53833150 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 151
2332 deg
Eccentricity:
0010706
Arg of perigee: 44
5159 deg
Mean anomaly: 315
6850 deg
Mean motion: 15
50744091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3336
Checksum: 290
Coasting Arc #7 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2013/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3865309
72 A = 6796612
24 meter
Y = 5015753
54 meter E =
0016126
Z = -2461873
37 I = 51
85288
XDOT = -5283
632502 Wp = 49
17670
YDOT = -1461
342991 meter/sec RA = 145
39876 deg
ZDOT = 5351
519527 TA = 283
38693
MA = 283
56665
Ha = 229
978 n
mi
Hp = 216
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12681462
33 X = -3909150
50
Y = 16455884
33 feet Y = 4972284
44 meter
Z = -8077012
36 Z = -2480756
55
XDOT = -17334
752303 XDOT = -5292
895114
YDOT = -4794
432384 feet/sec YDOT = -1520
480469 meter/sec
ZDOT = 17557
478762 ZDOT = 5325
829274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13249285
98 X = 4038382
37
Y = 15961834
65 feet Y = 4865167
20 meter
Z = -8156592
44 Z = -2486129
38
XDOT = -7373
078444 XDOT = -2247
314310
YDOT = 14982
257534 feet/sec YDOT = 4566
592096 meter/sec
ZDOT = 17450
287361 ZDOT = 5318
847587
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 13160
50498028
00016717 00000-0 10270-3 0 9060
2 25544 51
6446 146
4399 0010767 48
7333 311
4743 15
50729066 33519
Satellite: ISS
Catalog Number: 25544
Epoch time: 13160
50498028 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 146
4399 deg
Eccentricity:
0010767
Arg of perigee: 48
7333 deg
Mean anomaly: 311
4743 deg
Mean motion: 15
50729066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 313
Coasting Arc #8 (Orbit 3366)
---------------------------------------
Vector Time (GMT): 2013/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3958787
99 A = 6797572
94 meter
Y = -5188087
20 meter E =
0021238
Z = 1886661
30 I = 51
88138
XDOT = 4912
480446 Wp = 86
79056
YDOT = 1678
654958 meter/sec RA = 140
45641 deg
ZDOT = -5635
920032 TA = 72
53773
MA = 72
30569
Ha = 229
962 n
mi
Hp = 216
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12988149
56 X = 4007343
16
Y = -17021283
47 feet Y = -5143546
32 meter
Z = 6189833
68 Z = 1906009
98
XDOT = 16117
061831 XDOT = 4920
722079
YDOT = 5507
398157 feet/sec YDOT = 1733
636299 meter/sec
ZDOT = -18490
551287 ZDOT = -5612
035336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14010313
97 X = -4270343
70
Y = -16158924
54 feet Y = -4925240
20 meter
Z = 6271397
06 Z = 1911521
82
XDOT = 7532
892012 XDOT = 2296
025485
YDOT = -13739
116943 feet/sec YDOT = -4187
682844 meter/sec
ZDOT = -18390
923622 ZDOT = -5605
553520
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 13161
53606080
00016717 00000-0 10270-3 0 9074
2 25544 51
6449 141
3250 0010745 51
2860 308
9250 15
50769462 33677
Satellite: ISS
Catalog Number: 25544
Epoch time: 13161
53606080 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 141
3250 deg
Eccentricity:
0010745
Arg of perigee: 51
2860 deg
Mean anomaly: 308
9250 deg
Mean motion: 15
50769462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3367
Checksum: 295
Coasting Arc #9 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2013/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3943124
86 A = 6798294
28 meter
Y = 5361873
76 meter E =
0019167
Z = -1355560
15 I = 51
90692
XDOT = -4583
698835 Wp = 48
06521
YDOT = -1911
697624 meter/sec RA = 135
51783 deg
ZDOT = 5837
027549 TA = 297
24511
MA = 297
44025
Ha = 230
010 n
mi
Hp = 216
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12936761
37 X = -3996204
49
Y = 17591449
35 feet Y = 5317482
65 meter
Z = -4447375
81 Z = -1374843
69
XDOT = -15038
382004 XDOT = -4590
335828
YDOT = -6271
973833 feet/sec YDOT = -1962
993333 meter/sec
ZDOT = 19150
352851 ZDOT = 5814
743983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14853978
69 X = 4527492
70
Y = 15982746
81 feet Y = 4871541
23 meter
Z = -4528703
81 Z = -1380348
92
XDOT = -7839
676436 XDOT = -2389
533378
YDOT = 12626
235025 feet/sec YDOT = 3848
476436 meter/sec
ZDOT = 19057
439243 ZDOT = 5808
707481
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 13162
50268987
00016717 00000-0 10270-3 0 9083
2 25544 51
6449 136
5317 0010765 55
7622 304
4548 15
50772200 33826
Satellite: ISS
Catalog Number: 25544
Epoch time: 13162
50268987 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 136
5317 deg
Eccentricity:
0010765
Arg of perigee: 55
7622 deg
Mean anomaly: 304
4548 deg
Mean motion: 15
50772200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 313
Coasting Arc #10 (Orbit 3397)
---------------------------------------
Vector Time (GMT): 2013/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3946916
96 A = 6798807
41 meter
Y = -5483599
42 meter E =
0019858
Z = 727107
91 I = 51
93088
XDOT = 4240
215429 Wp = 96
94211
YDOT = 2241
675237 meter/sec RA = 130
58033 deg
ZDOT = -5973
545726 TA = 75
24640
MA = 75
02643
Ha = 230
023 n
mi
Hp = 216
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12949202
64 X = 4004410
33
Y = -17990811
73 feet Y = -5439141
13 meter
Z = 2385524
65 Z = 746420
61
XDOT = 13911
467943 XDOT = 4243
851190
YDOT = 7354
577549 feet/sec YDOT = 2289
113064 meter/sec
ZDOT = -19598
247132 ZDOT = -5952
938077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15516049
07 X = -4729291
76
Y = -15817964
42 feet Y = -4821315
55 meter
Z = 2467003
59 Z = 751942
69
XDOT = 8489
117639 XDOT = 2587
483056
YDOT = -11438
270971 feet/sec YDOT = -3486
384992 meter/sec
ZDOT = -19512
376038 ZDOT = -5947
372216
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 13163
53374957
00016717 00000-0 10270-3 0 9093
2 25544 51
6458 131
4170 0010737 58
2791 301
9405 15
50791618 33986
Satellite: ISS
Catalog Number: 25544
Epoch time: 13163
53374957 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 131
4170 deg
Eccentricity:
0010737
Arg of perigee: 58
2791 deg
Mean anomaly: 301
9405 deg
Mean motion: 15
50791618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3398
Checksum: 323
Coasting Arc #11 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2013/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3853407
42 A = 6798977
61 meter
Y = 5588701
77 meter E =
0022130
Z = -160333
49 I = 51
95079
XDOT = -3964
259563 Wp = 53
11976
YDOT = -2577
052016 meter/sec RA = 125
64546 deg
ZDOT = 6034
899695 TA = 305
16201
MA = 305
36913
Ha = 230
014 n
mi
Hp = 216
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12642412
79 X = -3914836
24
Y = 18335635
73 feet Y = 5545267
09 meter
Z = -526028
50 Z = -179201
54
XDOT = -13006
100928 XDOT = -3964
463601
YDOT = -8454
895065 feet/sec YDOT = -2621
384665 meter/sec
ZDOT = 19799
539683 ZDOT = 6015
640955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16172144
76 X = 4929269
72
Y = 15310053
48 feet Y = 4666504
30 meter
Z = -605673
98 Z = -184609
43
XDOT = -9256
575328 XDOT = -2821
404160
YDOT = 10491
777221 feet/sec YDOT = 3197
893697 meter/sec
ZDOT = 19719
347573 ZDOT = 6010
457140
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 13164
50035824
00016717 00000-0 10270-3 0 9100
2 25544 51
6458 126
6237 0010702 62
5124 297
7114 15
50810852 34135
Satellite: ISS
Catalog Number: 25544
Epoch time: 13164
50035824 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 126
6237 deg
Eccentricity:
0010702
Arg of perigee: 62
5124 deg
Mean anomaly: 297
7114 deg
Mean motion: 15
50810852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 279
Coasting Arc #12 (Orbit 3428)
---------------------------------------
Vector Time (GMT): 2013/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3787165
81 A = 6798871
84 meter
Y = -5623122
82 meter E =
0017507
Z = -491247
66 I = 51
96859
XDOT = 3688
090086 Wp = 102
69185
YDOT = 2992
726087 meter/sec RA = 120
71117 deg
ZDOT = -6007
990179 TA = 82
57258
MA = 82
37368
Ha = 230
039 n
mi
Hp = 216
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12425084
69 X = 3852149
66
Y = -18448565
69 feet Y = -5580408
95 meter
Z = -1611704
92 Z = -472692
68
XDOT = 12100
033090 XDOT = 3683
535795
YDOT = 9818
655141 feet/sec YDOT = 3033
943745 meter/sec
ZDOT = -19711
253868 ZDOT = -5990
084583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16573073
08 X = -5051472
67
Y = -14842909
95 feet Y = -4524118
95 meter
Z = -1533352
93 Z = -467365
97
XDOT = 10315
193161 XDOT = 3144
070875
YDOT = -9554
521629 feet/sec YDOT = -2912
218193 meter/sec
ZDOT = -19636
772263 ZDOT = -5985
288186
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 13165
53139642
00016717 00000-0 10270-3 0 9118
2 25544 51
6467 121
5092 0010684 65
2903 294
9359 15
50817768 34292
Satellite: ISS
Catalog Number: 25544
Epoch time: 13165
53139642 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 121
5092 deg
Eccentricity:
0010684
Arg of perigee: 65
2903 deg
Mean anomaly: 294
9359 deg
Mean motion: 15
50817768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3429
Checksum: 324
Coasting Arc #13 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2013/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3642650
39 A = 6798455
20 meter
Y = 5628033
29 meter E =
0024054
Z = 1064972
50 I = 51
98201
XDOT = -3496
244415 Wp = 62
14546
YDOT = -3399
975941 meter/sec RA = 115
77817 deg
ZDOT = 5918
360138 TA = 309
34143
MA = 309
55436
Ha = 230
021 n
mi
Hp = 216
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11950952
72 X = -3710486
89
Y = 18464676
16 feet Y = 5586919
49 meter
Z = 3494004
26 Z = 1047112
53
XDOT = -11470
618161 XDOT = -3486
715087
YDOT = -11154
776709 feet/sec YDOT = -3439
020371 meter/sec
ZDOT = 19417
192055 ZDOT = 5901
398557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16897489
59 X = 5150354
83
Y = 14098438
98 feet Y = 4297204
20 meter
Z = 3418547
38 Z = 1041973
24
XDOT = -11433
548008 XDOT = -3484
945433
YDOT = 8938
566498 feet/sec YDOT = 2724
475069 meter/sec
ZDOT = 19346
711989 ZDOT = 5896
877814
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 13166
56242299
00016717 00000-0 10270-3 0 9126
2 25544 51
6465 116
3959 0010637 69
3287 290
9003 15
50839975 34456
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
56242299 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 116
3959 deg
Eccentricity:
0010637
Arg of perigee: 69
3287 deg
Mean anomaly: 290
9003 deg
Mean motion: 15
50839975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 336
Coasting Arc #14 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2013/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3539108
56 A = 6797664
67 meter
Y = -5549105
55 meter E =
0015153
Z = -1705555
09 I = 51
99279
XDOT = 3315
109866 Wp = 100
87333
YDOT = 3858
736306 meter/sec RA = 110
84492 deg
ZDOT = -5721
412965 TA = 97
69094
MA = 97
51883
Ha = 230
021 n
mi
Hp = 216
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11611248
55 X = 3609181
97
Y = -18205726
86 feet Y = -5509137
06 meter
Z = -5595653
18 Z = -1688192
60
XDOT = 10876
344706 XDOT = 3299
507408
YDOT = 12659
896016 feet/sec YDOT = 3895
721172 meter/sec
ZDOT = -18771
039911 ZDOT = -5705
346004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16913642
09 X = -5155278
11
Y = -13454147
79 feet Y = -4100824
25 meter
Z = -5522276
37 Z = -1683189
84
XDOT = 12739
492537 XDOT = 3882
997325
YDOT = -8400
539970 feet/sec YDOT = -2560
484583 meter/sec
ZDOT = -18704
364995 ZDOT = -5701
090451
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 13167
52900043
00016717 00000-0 10270-3 0 9132
2 25544 51
6473 111
6010 0010638 72
2603 287
9708 15
50852417 34608
Satellite: ISS
Catalog Number: 25544
Epoch time: 13167
52900043 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 111
6010 deg
Eccentricity:
0010638
Arg of perigee: 72
2603 deg
Mean anomaly: 287
9708 deg
Mean motion: 15
50852417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3460
Checksum: 284
Coasting Arc #15 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2013/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3380647
09 A = 6796735
93 meter
Y = 5434733
15 meter E =
0024438
Z = 2254111
95 I = 51
99961
XDOT = -3224
773338 Wp = 73
53432
YDOT = -4294
877470 meter/sec RA = 105
91195 deg
ZDOT = 5476
404799 TA = 311
39816
MA = 311
60798
Ha = 230
038 n
mi
Hp = 216
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11091361
83 X = -3452118
12
Y = 17830489
34 feet Y = 5396528
82 meter
Z = 7395380
40 Z = 2237515
80
XDOT = -10579
965020 XDOT = -3203
110471
YDOT = -14090
805347 feet/sec YDOT = -4330
818242 meter/sec
ZDOT = 17967
207345 ZDOT = 5460
791312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16812393
05 X = 5124417
40
Y = 12622242
73 feet Y = 3847259
58 meter
Z = 7325212
41 Z = 2232724
74
XDOT = -14032
336561 XDOT = -4277
056184
YDOT = 8219
790819 feet/sec YDOT = 2505
392242 meter/sec
ZDOT = 17902
492679 ZDOT = 5456
679769
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 13168
56000517
00016717 00000-0 10270-3 0 9145
2 25544 51
6471 106
4874 0010611 76
0964 284
1367 15
50864278 34764
Satellite: ISS
Catalog Number: 25544
Epoch time: 13168
56000517 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 106
4874 deg
Eccentricity:
0010611
Arg of perigee: 76
0964 deg
Mean anomaly: 284
1367 deg
Mean motion: 15
50864278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3476
Checksum: 313
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