[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 21st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3973)
---------------------------------------
Vector Time (GMT): 2013/200/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1760429
54 A = 6790983
28 meter
Y = 4272873
96 meter E =
0003190
Z = 4973085
74 I = 51
35405
XDOT = -5649
644996 Wp = 105
32461
YDOT = 4743
984682 meter/sec RA = 306
97749 deg
ZDOT = -2075
815719 TA = 4
96902
MA = 4
96586
Ha = 227
484 n
mi
Hp = 221
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5775687
47 X = 1688360
76
Y = 14018615
37 feet Y = 4292156
62 meter
Z = 16315898
10 Z = 4981463
18
XDOT = -18535
580694 XDOT = -5692
189687
YDOT = 15564
254207 feet/sec YDOT = 4680
569161 meter/sec
ZDOT = -6810
419025 ZDOT = -2103
363743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -238887
87 X = -72813
02
Y = -15122830
22 feet Y = -4609438
65 meter
Z = 16350278
66 Z = 4983564
94
XDOT = 21757
382437 XDOT = 6631
650167
YDOT = -7833
297955 feet/sec YDOT = -2387
589217 meter/sec
ZDOT = -6926
401286 ZDOT = -2111
167112
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 13200
66170009
00016717 00000-0 10270-3 0 9002
2 25544 51
6505 307
4145 0004709 206
6953 153
3956 15
49959633 39748
Satellite: ISS
Catalog Number: 25544
Epoch time: 13200
66170009 = yrday
fracday
Element set: 900
Inclination: 51
6505 deg
RA of node: 307
4145 deg
Eccentricity:
0004709
Arg of perigee: 206
6953 deg
Mean anomaly: 153
3956 deg
Mean motion: 15
49959633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 314
Coasting Arc #2 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2013/201/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1840438
54 A = 6791543
90 meter
Y = -4387681
71 meter E =
0011732
Z = -4856997
79 I = 51
33732
XDOT = 5346
449077 Wp = 129
35151
YDOT = -4915
315805 meter/sec RA = 302
00208 deg
ZDOT = 2411
090822 TA = 164
46457
MA = 164
42854
Ha = 227
493 n
mi
Hp = 221
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6038184
18 X = -1767644
06
Y = -14395281
20 feet Y = -4407855
01 meter
Z = -15935032
13 Z = -4865762
12
XDOT = 17540
843429 XDOT = 5389
303565
YDOT = -16126
364190 feet/sec YDOT = -4855
289130 meter/sec
ZDOT = 7910
402959 ZDOT = 2437
166532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 617917
81 X = 188341
35
Y = 15561289
38 feet Y = 4743081
00 meter
Z = -15971020
27 Z = -4867966
98
XDOT = -20840
268555 XDOT = -6352
113855
YDOT = 9070
286662 feet/sec YDOT = 2764
623375 meter/sec
ZDOT = 8020
251789 ZDOT = 2444
572745
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 13201
62884292
00016717 00000-0 10270-3 0 9016
2 25544 51
6498 302
6241 0004492 208
6720 151
4184 15
49945390 39899
Satellite: ISS
Catalog Number: 25544
Epoch time: 13201
62884292 = yrday
fracday
Element set: 901
Inclination: 51
6498 deg
RA of node: 302
6241 deg
Eccentricity:
0004492
Arg of perigee: 208
6720 deg
Mean anomaly: 151
4184 deg
Mean motion: 15
49945390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 319
Coasting Arc #3 (Orbit 4004)
---------------------------------------
Vector Time (GMT): 2013/202/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1938686
43 A = 6791966
72 meter
Y = 4491769
82 meter E =
0004491
Z = 4707322
72 I = 51
32414
XDOT = -5053
189806 Wp = 91
96635
YDOT = 5063
978831 meter/sec RA = 297
02605 deg
ZDOT = -2748
836478 TA = 25
39511
MA = 25
37305
Ha = 227
175 n
mi
Hp = 222
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6360519
79 X = 1865447
92
Y = 14736777
62 feet Y = 4513039
38 meter
Z = 15443972
17 Z = 4716563
16
XDOT = -16578
706711 XDOT = -5096
087891
YDOT = 16614
103776 feet/sec YDOT = 5007
231338 meter/sec
ZDOT = -9018
492381 ZDOT = -2773
487575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1080782
16 X = -329422
40
Y = -15977683
63 feet Y = -4869997
97 meter
Z = 15481945
57 Z = 4718897
01
XDOT = 19894
580682 XDOT = 6063
868192
YDOT = -10191
842773 feet/sec YDOT = -3106
473677 meter/sec
ZDOT = -9122
401046 ZDOT = -2780
507839
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 13202
66044700
00016717 00000-0 10270-3 0 9024
2 25544 51
6502 297
5145 0004502 214
2567 145
8294 15
49994615 40057
Satellite: ISS
Catalog Number: 25544
Epoch time: 13202
66044700 = yrday
fracday
Element set: 902
Inclination: 51
6502 deg
RA of node: 297
5145 deg
Eccentricity:
0004502
Arg of perigee: 214
2567 deg
Mean anomaly: 145
8294 deg
Mean motion: 15
49994615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 295
Coasting Arc #4 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2013/203/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2062309
99 A = 6792639
50 meter
Y = -4612616
97 meter E =
0009612
Z = -4549342
62 I = 51
31292
XDOT = 4745
452159 Wp = 135
45755
YDOT = -5157
240179 meter/sec RA = 292
04857 deg
ZDOT = 3075
010476 TA = 165
53634
MA = 165
50881
Ha = 227
197 n
mi
Hp = 221
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6766108
88 X = -1988478
45
Y = -15133257
78 feet Y = -4635265
76 meter
Z = -14925664
75 Z = -4559182
03
XDOT = 15569
068762 XDOT = 4787
831613
YDOT = -16920
079327 feet/sec YDOT = -5103
936876 meter/sec
ZDOT = 10088
617048 ZDOT = 3098
165377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1620209
37 X = 493839
82
Y = 16460888
45 feet Y = 5017278
80 meter
Z = -14966137
16 Z = -4561678
61
XDOT = -18809
403681 XDOT = -5733
106242
YDOT = 11120
841870 feet/sec YDOT = 3389
632602 meter/sec
ZDOT = 10186
273989 ZDOT = 3104
776312
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 13203
62756673
00016717 00000-0 10270-3 0 9031
2 25544 51
6499 292
7238 0004286 216
1479 143
9382 15
49985259 40202
Satellite: ISS
Catalog Number: 25544
Epoch time: 13203
62756673 = yrday
fracday
Element set: 903
Inclination: 51
6499 deg
RA of node: 292
7238 deg
Eccentricity:
0004286
Arg of perigee: 216
1479 deg
Mean anomaly: 143
9382 deg
Mean motion: 15
49985259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 337
Coasting Arc #5 (Orbit 4035)
---------------------------------------
Vector Time (GMT): 2013/204/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2201330
69 A = 6793209
87 meter
Y = 4719531
49 meter E =
0006209
Z = 4356619
33 I = 51
30406
XDOT = -4456
392440 Wp = 91
10467
YDOT = 5224
273634 meter/sec RA = 287
07115 deg
ZDOT = -3403
616351 TA = 33
59674
MA = 33
55739
Ha = 226
891 n
mi
Hp = 222
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7222213
54 X = 2127229
48
Y = 15484027
21 feet Y = 4743733
53 meter
Z = 14293370
49 Z = 4367133
29
XDOT = -14620
710105 XDOT = -4497
946743
YDOT = 17140
005360 feet/sec YDOT = 5174
207334 meter/sec
ZDOT = -11166
720312 ZDOT = -3425
365149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2238947
69 X = -682431
26
Y = -16901572
68 feet Y = -5151599
35 meter
Z = 14336661
45 Z = 4369814
41
XDOT = 17733
569649 XDOT = 5405
192029
YDOT = -11910
496331 feet/sec YDOT = -3630
319282 meter/sec
ZDOT = -11258
495342 ZDOT = -3431
589380
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 13204
65914657
00016717 00000-0 10270-3 0 9044
2 25544 51
6494 287
6142 0004269 221
3677 138
7150 15
50028217 40369
Satellite: ISS
Catalog Number: 25544
Epoch time: 13204
65914657 = yrday
fracday
Element set: 904
Inclination: 51
6494 deg
RA of node: 287
6142 deg
Eccentricity:
0004269
Arg of perigee: 221
3677 deg
Mean anomaly: 138
7150 deg
Mean motion: 15
50028217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4036
Checksum: 307
Coasting Arc #6 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2013/205/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2370133
94 A = 6793958
19 meter
Y = -4830548
79 meter E =
0007078
Z = -4155701
69 I = 51
29877
XDOT = 4164
999572 Wp = 141
28030
YDOT = -5239
681160 meter/sec RA = 282
09243 deg
ZDOT = 3713
148802 TA = 167
16145
MA = 167
14342
Ha = 226
907 n
mi
Hp = 222
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7776029
98 X = -2295754
72
Y = -15848257
19 feet Y = -4856637
06 meter
Z = -13634191
90 Z = -4167034
89
XDOT = 13664
696758 XDOT = 4205
244210
YDOT = -17190
554986 feet/sec YDOT = -5192
880650 meter/sec
ZDOT = 12182
246725 ZDOT = 3733
479048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2963462
40 X = 903263
34
Y = 17365937
41 feet Y = 5293137
72 meter
Z = -13680906
24 Z = -4169940
22
XDOT = -16579
225453 XDOT = -5053
347918
YDOT = 12499
094697 feet/sec YDOT = 3809
724063 meter/sec
ZDOT = 12268
078331 ZDOT = 3739
310275
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 13205
62624332
00016717 00000-0 10270-3 0 9051
2 25544 51
6497 282
8231 0004109 223
8548 136
2277 15
50025547 40518
Satellite: ISS
Catalog Number: 25544
Epoch time: 13205
62624332 = yrday
fracday
Element set: 905
Inclination: 51
6497 deg
RA of node: 282
8231 deg
Eccentricity:
0004109
Arg of perigee: 223
8548 deg
Mean anomaly: 136
2277 deg
Mean motion: 15
50025547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 293
Coasting Arc #7 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2013/206/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550102
85 A = 6794643
20 meter
Y = 4924133
55 meter E =
0007918
Z = 3918956
45 I = 51
29457
XDOT = -3901
506698 Wp = 95
89368
YDOT = 5227
654181 meter/sec RA = 277
11389 deg
ZDOT = -4023
514821 TA = 36
41148
MA = 36
35765
Ha = 226
625 n
mi
Hp = 222
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8366479
17 X = 2475813
73
Y = 16155293
80 feet Y = 4952234
93 meter
Z = 12857468
65 Z = 3931164
07
XDOT = -12800
218826 XDOT = -3940
128728
YDOT = 17151
096393 feet/sec YDOT = 5183
809228 meter/sec
ZDOT = -13200
507944 ZDOT = -4042
561287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3755552
54 X = -1144692
41
Y = -17764839
11 feet Y = -5414722
96 meter
Z = 12907839
03 Z = 3934309
34
XDOT = 15478
153738 XDOT = 4717
741259
YDOT = -12936
823187 feet/sec YDOT = -3943
143707 meter/sec
ZDOT = -13280
956060 ZDOT = -4048
035407
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 13206
65779958
00016717 00000-0 10270-3 0 9061
2 25544 51
6484 277
7128 0004058 228
7501 131
3301 15
50060932 40676
Satellite: ISS
Catalog Number: 25544
Epoch time: 13206
65779958 = yrday
fracday
Element set: 906
Inclination: 51
6484 deg
RA of node: 277
7128 deg
Eccentricity:
0004058
Arg of perigee: 228
7501 deg
Mean anomaly: 131
3301 deg
Mean motion: 15
50060932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 311
Coasting Arc #8 (Orbit 4081)
---------------------------------------
Vector Time (GMT): 2013/207/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2760222
95 A = 6795426
68 meter
Y = -5009015
46 meter E =
0004216
Z = -3675215
83 I = 51
29516
XDOT = 3647
307388 Wp = 145
21299
YDOT = -5171
553443 meter/sec RA = 272
13499 deg
ZDOT = 4308
196704 TA = 170
93830
MA = 170
93069
Ha = 226
624 n
mi
Hp = 222
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9055849
58 X = -2686152
98
Y = -16433777
76 feet Y = -5039467
80 meter
Z = -12057794
72 Z = -3688444
73
XDOT = 11966
231587 XDOT = 3683
938017
YDOT = -16967
038856 feet/sec YDOT = -5130
562214 meter/sec
ZDOT = 14134
503621 ZDOT = 4326
003594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4665138
45 X = 1421934
20
Y = 18138171
41 feet Y = 5528514
65 meter
Z = -12112435
66 Z = -3691870
39
XDOT = -14361
948432 XDOT = -4377
521882
YDOT = 13185
030833 feet/sec YDOT = 4018
797398 meter/sec
ZDOT = 14209
748305 ZDOT = 4331
131283
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 13207
62487381
00016717 00000-0 10270-3 0 9076
2 25544 51
6492 272
9216 0003980 232
0211 128
0580 15
50063552 40829
Satellite: ISS
Catalog Number: 25544
Epoch time: 13207
62487381 = yrday
fracday
Element set: 907
Inclination: 51
6492 deg
RA of node: 272
9216 deg
Eccentricity:
0003980
Arg of perigee: 232
0211 deg
Mean anomaly: 128
0580 deg
Mean motion: 15
50063552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 289
Coasting Arc #9 (Orbit 4097)
---------------------------------------
Vector Time (GMT): 2013/208/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2975709
52 A = 6796166
27 meter
Y = 5073200
30 meter E =
0009351
Z = 3395081
83 I = 51
29622
XDOT = -3429
816836 Wp = 103
27279
YDOT = 5089
515646 meter/sec RA = 267
15614 deg
ZDOT = -4590
405408 TA = 36
88919
MA = 36
82490
Ha = 226
358 n
mi
Hp = 222
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9762826
51 X = 2902266
54
Y = 16644357
94 feet Y = 5106065
86 meter
Z = 11138719
90 Z = 3409359
10
XDOT = -11252
679909 XDOT = -3464
175314
YDOT = 16697
885978 feet/sec YDOT = 5050
969247 meter/sec
ZDOT = -15060
385197 ZDOT = -4607
150303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5621919
21 X = -1713560
97
Y = -18423436
21 feet Y = -5615463
36 meter
Z = 11197746
93 Z = 3413073
26
XDOT = 13344
342908 XDOT = 4067
355718
YDOT = -13285
796499 feet/sec YDOT = -4049
510773 meter/sec
ZDOT = -15131
167954 ZDOT = -4611
979992
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 13208
65640717
00016717 00000-0 10270-3 0 9085
2 25544 51
6477 267
8106 0003926 237
2058 122
8715 15
50093702 40988
Satellite: ISS
Catalog Number: 25544
Epoch time: 13208
65640717 = yrday
fracday
Element set: 908
Inclination: 51
6477 deg
RA of node: 267
8106 deg
Eccentricity:
0003926
Arg of perigee: 237
2058 deg
Mean anomaly: 122
8715 deg
Mean motion: 15
50093702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 317
Coasting Arc #10 (Orbit 4112)
---------------------------------------
Vector Time (GMT): 2013/209/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3217735
08 A = 6796938
10 meter
Y = -5117002
04 meter E =
0001276
Z = -3110020
73 I = 51
30203
XDOT = 3231
644870 Wp = 129
14802
YDOT = -4974
455010 meter/sec RA = 262
17824 deg
ZDOT = 4841
586526 TA = 194
96378
MA = 194
96755
Ha = 226
352 n
mi
Hp = 222
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10556873
63 X = -3145169
00
Y = -16788064
43 feet Y = -5152578
96 meter
Z = -10203480
07 Z = -3125475
93
XDOT = 10602
509417 XDOT = 3263
511228
YDOT = -16320
390454 feet/sec YDOT = -4938
138674 meter/sec
ZDOT = 15884
470230 ZDOT = 4857
362680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6689084
41 X = 2038832
93
Y = 18634204
03 feet Y = 5679705
39 meter
Z = -10267438
01 Z = -3129515
11
XDOT = -12370
715846 XDOT = -3770
594190
YDOT = 13228
793691 feet/sec YDOT = 4032
136317 meter/sec
ZDOT = 15951
178780 ZDOT = 4861
919292
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 13209
62345975
00016717 00000-0 10270-3 0 9092
2 25544 51
6484 263
0195 0003895 240
6253 119
4509 15
50098507 41131
Satellite: ISS
Catalog Number: 25544
Epoch time: 13209
62345975 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 263
0195 deg
Eccentricity:
0003895
Arg of perigee: 240
6253 deg
Mean anomaly: 119
4509 deg
Mean motion: 15
50098507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4113
Checksum: 317
Coasting Arc #11 (Orbit 4128)
---------------------------------------
Vector Time (GMT): 2013/210/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3457700
33 A = 6797655
78 meter
Y = 5137938
59 meter E =
0010350
Z = 2788709
33 I = 51
30855
XDOT = -3077
677814 Wp = 111
98937
YDOT = 4837
599305 meter/sec RA = 257
20023 deg
ZDOT = -5085
417942 TA = 36
27219
MA = 36
20206
Ha = 226
094 n
mi
Hp = 222
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11344161
19 X = 3386443
11
Y = 16856753
89 feet Y = 5176206
25 meter
Z = 9149308
84 Z = 2805333
52
XDOT = -10097
368155 XDOT = -3106
840778
YDOT = 15871
388797 feet/sec YDOT = 4803
019910 meter/sec
ZDOT = -16684
442066 ZDOT = -5100
439543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7773703
84 X = -2369424
93
Y = -18738862
74 feet Y = -5711605
36 meter
Z = 9218164
08 Z = 2809696
41
XDOT = 11537
063684 XDOT = 3516
497011
YDOT = -13043
164788 feet/sec YDOT = -3975
556627 meter/sec
ZDOT = -16747
971422 ZDOT = -5104
781689
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 13210
65497068
00016717 00000-0 10270-3 0 9100
2 25544 51
6472 257
9081 0003880 246
7899 113
2843 15
50126910 41291
Satellite: ISS
Catalog Number: 25544
Epoch time: 13210
65497068 = yrday
fracday
Element set: 910
Inclination: 51
6472 deg
RA of node: 257
9081 deg
Eccentricity:
0003880
Arg of perigee: 246
7899 deg
Mean anomaly: 113
2843 deg
Mean motion: 15
50126910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4129
Checksum: 315
Coasting Arc #12 (Orbit 4143)
---------------------------------------
Vector Time (GMT): 2013/211/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3717102
21 A = 6798356
51 meter
Y = -5129061
03 meter E =
0002212
Z = -2465311
88 I = 51
31878
XDOT = 2950
369601 Wp = 11
84983
YDOT = -4681
523830 meter/sec RA = 252
22407 deg
ZDOT = 5294
391386 TA = 320
46482
MA = 320
48095
Ha = 226
105 n
mi
Hp = 222
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12195217
22 X = -3647495
95
Y = -16827628
05 feet Y = -5170238
70 meter
Z = -8088293
56 Z = -2483200
28
XDOT = 9679
690293 XDOT = 2976
781635
YDOT = -15359
330152 feet/sec YDOT = -4648
383531 meter/sec
ZDOT = 17370
050479 ZDOT = 5308
787804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8943930
85 X = 2726110
12
Y = 18726809
39 feet Y = 5707931
50 meter
Z = -8162450
18 Z = -2487914
82
XDOT = -10795
315320 XDOT = -3290
412110
YDOT = 12749
253487 feet/sec YDOT = 3885
972463 meter/sec
ZDOT = 17430
940629 ZDOT = 5312
950704
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 13211
62200230
00016717 00000-0 10270-3 0 9112
2 25544 51
6473 253
1173 0003834 249
4503 110
6237 15
50132441 41444
Satellite: ISS
Catalog Number: 25544
Epoch time: 13211
62200230 = yrday
fracday
Element set: 911
Inclination: 51
6473 deg
RA of node: 253
1173 deg
Eccentricity:
0003834
Arg of perigee: 249
4503 deg
Mean anomaly: 110
6237 deg
Mean motion: 15
50132441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4144
Checksum: 250
Coasting Arc #13 (Orbit 4159)
---------------------------------------
Vector Time (GMT): 2013/212/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3965661
20 A = 6798978
39 meter
Y = 5097079
16 meter E =
0010839
Z = 2106525
75 I = 51
33054
XDOT = -2872
588051 Wp = 121
48358
YDOT = 4510
129854 meter/sec RA = 247
24782 deg
ZDOT = -5489
773690 TA = 35
11432
MA = 35
04292
Ha = 225
875 n
mi
Hp = 222
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13010699
47 X = 3898136
98
Y = 16722700
67 feet Y = 5141048
02 meter
Z = 6911173
71 Z = 2125626
69
XDOT = -9424
501481 XDOT = -2896
140235
YDOT = 14797
013956 feet/sec YDOT = 4477
875411 meter/sec
ZDOT = -18011
068536 ZDOT = -5503
785254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10093652
87 X = -3076545
39
Y = -18599557
28 feet Y = -5669145
06 meter
Z = 6990420
70 Z = 2130680
23
XDOT = 10225
607856 XDOT = 3116
765275
YDOT = -12359
539240 feet/sec YDOT = -3767
187560 meter/sec
ZDOT = -18070
323955 ZDOT = -5507
834741
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 13212
65349094
00016717 00000-0 10270-3 0 9129
2 25544 51
6464 248
0057 0003888 256
7269 103
3448 15
50159095 41602
Satellite: ISS
Catalog Number: 25544
Epoch time: 13212
65349094 = yrday
fracday
Element set: 912
Inclination: 51
6464 deg
RA of node: 248
0057 deg
Eccentricity:
0003888
Arg of perigee: 256
7269 deg
Mean anomaly: 103
3448 deg
Mean motion: 15
50159095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4160
Checksum: 315
Coasting Arc #14 (Orbit 4174)
---------------------------------------
Vector Time (GMT): 2013/213/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4223901
32 A = 6799533
80 meter
Y = -5029035
62 meter E =
0005130
Z = -1749248
80 I = 51
34474
XDOT = 2825
292423 Wp = 10
34006
YDOT = -4334
908549 meter/sec RA = 242
27378 deg
ZDOT = 5648
042553 TA = 330
41666
MA = 330
44567
Ha = 225
901 n
mi
Hp = 222
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13857943
97 X = -4158854
35
Y = -16499460
69 feet Y = -5075906
14 meter
Z = -5739005
23 Z = -1769610
22
XDOT = 9269
332097 XDOT = 2846
120003
YDOT = -14222
140910 feet/sec YDOT = -4303
198268 meter/sec
ZDOT = 18530
323338 ZDOT = 5661
817702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11289910
55 X = 3441164
73
Y = 18325806
26 feet Y = 5585705
75 meter
Z = -5823550
46 Z = -1775018
18
XDOT = -9778
703942 XDOT = -2980
548961
YDOT = 11923
638424 feet/sec YDOT = 3634
324992 meter/sec
ZDOT = 18588
565234 ZDOT = 5665
794683
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 13213
62050168
00016717 00000-0 10270-3 0 9139
2 25544 51
6460 243
2147 0003799 258
3533 101
7192 15
50167978 41751
Satellite: ISS
Catalog Number: 25544
Epoch time: 13213
62050168 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 243
2147 deg
Eccentricity:
0003799
Arg of perigee: 258
3533 deg
Mean anomaly: 101
7192 deg
Mean motion: 15
50167978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4175
Checksum: 304
Coasting Arc #15 (Orbit 4190)
---------------------------------------
Vector Time (GMT): 2013/214/14:48:29
974
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4461798
96 A = 6799999
35 meter
Y = 4940113
81 meter E =
0010753
Z = 1358263
02 I = 51
36130
XDOT = -2829
782149 Wp = 131
48303
YDOT = 4152
724971 meter/sec RA = 237
29988 deg
ZDOT = -5785
324729 TA = 33
68699
MA = 33
61869
Ha = 225
749 n
mi
Hp = 222
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14638448
02 X = 4399627
94
Y = 16207722
46 feet Y = 4989660
76 meter
Z = 4456243
50 Z = 1379787
04
XDOT = -9284
062167 XDOT = -2847
905382
YDOT = 13624
425757 feet/sec YDOT = 4120
979610 meter/sec
ZDOT = -18980
724176 ZDOT = -5799
115096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12422707
42 X = -3786441
22
Y = -17940057
04 feet Y = -5468129
39 meter
Z = 4545682
34 Z = 1385523
98
XDOT = 9521
476082 XDOT = 2902
145910
YDOT = -11435
955950 feet/sec YDOT = -3485
679374 meter/sec
ZDOT = -19039
005147 ZDOT = -5803
088769
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 13214
65196786
00016717 00000-0 10270-3 0 9141
2 25544 51
6457 238
1029 0003918 266
1489 93
9214 15
50188038 41914
Satellite: ISS
Catalog Number: 25544
Epoch time: 13214
65196786 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 238
1029 deg
Eccentricity:
0003918
Arg of perigee: 266
1489 deg
Mean anomaly: 93
9214 deg
Mean motion: 15
50188038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4191
Checksum: 329
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