[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 8th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 33368 12 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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
070/00:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 220
1
072/03:57:12
907 -2
1 2
9 2
9
N/A -1
9 -0
0 224
1
000/00:06:25
814 0
5 0
1 221
5
Coasting Arc #1 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2014/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4852542
01 A = 6789243
11 meter
Y = -1541316
84 meter E =
0008833
Z = -4500191
68 I = 51
31462
XDOT = -732
066272 Wp = 129
69262
YDOT = -6933
231285 meter/sec RA = 242
67324 deg
ZDOT = 3162
643243 TA = 172
26802
MA = 172
25439
Ha = 225
060 n
mi
Hp = 219
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15920413
43 X = -4813085
67
Y = -5056813
78 feet Y = -1595360
87 meter
Z = -14764408
40 Z = -4523668
51
XDOT = -2401
792232 XDOT = -669
845917
YDOT = -22746
821800 feet/sec YDOT = -6941
069537 meter/sec
ZDOT = 10376
126125 ZDOT = 3159
238751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13869515
07 X = -4227428
19
Y = -9150879
22 feet Y = -2789187
99 meter
Z = -14863264
98 Z = -4530323
17
XDOT = 3110
828816 XDOT = 948
180623
YDOT = -21553
848934 feet/sec YDOT = -6569
613155 meter/sec
ZDOT = 10362
755285 ZDOT = 3158
567811
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 14066
51043796
00016717 00000-0 10270-3 0 9009
2 25544 51
6442 243
5939 0003194 225
3218 134
7673 15
51185302 35559
Satellite: ISS
Catalog Number: 25544
Epoch time: 14066
51043796 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 243
5939 deg
Eccentricity:
0003194
Arg of perigee: 225
3218 deg
Mean anomaly: 134
7673 deg
Mean motion: 15
51185302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 302
Coasting Arc #2 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2014/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5077801
10 A = 6790761
69 meter
Y = 1958832
86 meter E =
0007831
Z = 4054609
28 I = 51
33466
XDOT = 532
203836 Wp = 87
85849
YDOT = 6606
674643 meter/sec RA = 237
68643 deg
ZDOT = -3851
525693 TA = 42
22251
MA = 42
16223
Ha = 224
762 n
mi
Hp = 220
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16659452
43 X = 5035823
78
Y = 6426616
99 feet Y = 2015381
72 meter
Z = 13302523
87 Z = 4079174
17
XDOT = 1746
075577 XDOT = 476
996269
YDOT = 21675
441742 feet/sec YDOT = 6612
317073 meter/sec
ZDOT = -12636
239151 ZDOT = -3849
075007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14400752
51 X = 4389349
37
Y = 10425711
28 feet Y = 3177756
80 meter
Z = 13405923
09 Z = 4086125
36
XDOT = -2977
628040 XDOT = -907
581027
YDOT = 20377
416199 feet/sec YDOT = 6211
036457 meter/sec
ZDOT = -12626
838150 ZDOT = -3848
660268
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 14067
54120993
00016717 00000-0 10270-3 0 9019
2 25544 51
6438 238
4782 0003216 231
2529 128
8335 15
51211453 35713
Satellite: ISS
Catalog Number: 25544
Epoch time: 14067
54120993 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 238
4782 deg
Eccentricity:
0003216
Arg of perigee: 231
2529 deg
Mean anomaly: 128
8335 deg
Mean motion: 15
51211453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 296
Coasting Arc #3 (Orbit 3585)
---------------------------------------
Vector Time (GMT): 2014/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5319287
76 A = 6792263
43 meter
Y = -2320424
05 meter E =
0003636
Z = -3533979
57 I = 51
35829
XDOT = -251
814771 Wp = 132
03890
YDOT = -6218
132802 meter/sec RA = 232
70170 deg
ZDOT = 4462
455769 TA = 186
21020
MA = 186
21471
Ha = 224
760 n
mi
Hp = 219
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17451731
50 X = -5275778
17
Y = -7612939
80 feet Y = -2379664
77 meter
Z = -11594421
17 Z = -3559713
74
XDOT = -826
163946 XDOT = -203
940428
YDOT = -20400
698170 feet/sec YDOT = -6220
680683 meter/sec
ZDOT = 14640
602917 ZDOT = 4461
349331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15076587
35 X = -4595343
82
Y = -11519258
85 feet Y = -3511070
10 meter
Z = -11702716
63 Z = -3566988
03
XDOT = 3107
764306 XDOT = 947
246561
YDOT = -18935
497716 feet/sec YDOT = -5771
539704 meter/sec
ZDOT = 14636
811511 ZDOT = 4461
300149
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 14068
50753060
00016717 00000-0 10270-3 0 9024
2 25544 51
6444 233
6814 0003114 233
3801 126
7064 15
51275459 35864
Satellite: ISS
Catalog Number: 25544
Epoch time: 14068
50753060 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 233
6814 deg
Eccentricity:
0003114
Arg of perigee: 233
3801 deg
Mean anomaly: 126
7064 deg
Mean motion: 15
51275459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3586
Checksum: 292
Coasting Arc #4 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2014/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5537674
04 A = 6793881
76 meter
Y = 2635965
71 meter E =
0010921
Z = 2909208
07 I = 51
38275
XDOT = -126
725008 Wp = 108
48987
YDOT = 5804
636008 meter/sec RA = 227
72046 deg
ZDOT = -5006
142096 TA = 38
24449
MA = 38
16707
Ha = 224
502 n
mi
Hp = 220
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18168221
91 X = 5493654
69
Y = 8648181
48 feet Y = 2697645
68 meter
Z = 9544645
89 Z = 2936001
78
XDOT = -415
764463 XDOT = -167
306427
YDOT = 19044
081391 feet/sec YDOT = 5802
991507 meter/sec
ZDOT = -16424
350709 ZDOT = -5006
856821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15755636
62 X = 4802318
04
Y = 12428614
45 feet Y = 3788241
69 meter
Z = 9657383
33 Z = 2943570
44
XDOT = -3597
561130 XDOT = -1096
536633
YDOT = 17356
195022 feet/sec YDOT = 5290
168243 meter/sec
ZDOT = -16428
179943 ZDOT = -5007
309247
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 14069
53824170
00016717 00000-0 10270-3 0 9030
2 25544 51
6437 228
5649 0003143 239
5425 120
5415 15
51307106 36023
Satellite: ISS
Catalog Number: 25544
Epoch time: 14069
53824170 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 228
5649 deg
Eccentricity:
0003143
Arg of perigee: 239
5425 deg
Mean anomaly: 120
5415 deg
Mean motion: 15
51307106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 287
Coasting Arc #5 (Orbit 3609)
---------------------------------------
Vector Time (GMT): 2014/070/00:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 886509
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1251999
70 A = 6786810
02 meter
Y = -4413954
41 meter E =
0004860
Z = 5000486
94 I = 51
37038
XDOT = 6216
288216 Wp = 153
66848
YDOT = 4018
924017 meter/sec RA = 225
26449 deg
ZDOT = 1986
099243 TA = 276
93037
MA = 276
98565
Ha = 224
374 n
mi
Hp = 220
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4107610
57 X = 1276974
06
Y = -14481477
73 feet Y = -4399813
61 meter
Z = 16405797
03 Z = 5006629
99
XDOT = 20394
646379 XDOT = 6161
238000
YDOT = 13185
446249 feet/sec YDOT = 4088
130931 meter/sec
ZDOT = 6516
073631 ZDOT = 2016
162552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6838890
78 X = -2084493
91
Y = 13376974
96 feet Y = 4077301
97 meter
Z = 16432344
69 Z = 5008578
66
XDOT = -16305
650312 XDOT = -4969
962215
YDOT = -16515
941689 feet/sec YDOT = -5034
059027 meter/sec
ZDOT = 6642
428649 ZDOT = 2024
612252
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 14070
05358503
00016717 00000-0 10270-3 0 9042
2 25544 51
6441 226
0108 0002988 249
5361 110
5470 15
51350123 36103
Satellite: ISS
Catalog Number: 25544
Epoch time: 14070
05358503 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 226
0108 deg
Eccentricity:
0002988
Arg of perigee: 249
5361 deg
Mean anomaly: 110
5470 deg
Mean motion: 15
51350123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3610
Checksum: 269
Coasting Arc #6 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2014/071/00:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 886509
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1731516
18 A = 6785802
46 meter
Y = 3992806
86 meter E =
0011309
Z = -5216361
69 I = 51
39006
XDOT = -6312
422880 Wp = 83
22311
YDOT = -4186
753138 meter/sec RA = 220
27575 deg
ZDOT = -1110
132563 TA = 176
08674
MA = 176
07789
Ha = 224
332 n
mi
Hp = 219
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5680827
36 X = -1750696
92
Y = 13099760
05 feet Y = 3973336
11 meter
Z = -17114047
53 Z = -5224820
06
XDOT = -20710
048820 XDOT = -6259
743926
YDOT = -13736
066725 feet/sec YDOT = -4257
048276 meter/sec
ZDOT = -3642
167203 ZDOT = -1140
668542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7894658
15 X = 2406291
81
Y = -11845144
30 feet Y = -3610399
98 meter
Z = -17150308
01 Z = -5227413
88
XDOT = 16933
570270 XDOT = 5161
352218
YDOT = 16741
623108 feet/sec YDOT = 5102
846723 meter/sec
ZDOT = -3770
512424 ZDOT = -1149
252187
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 14071
01983260
00016717 00000-0 10270-3 0 9054
2 25544 51
6443 221
2133 0002884 254
5967 105
4863 15
51381199 36255
Satellite: ISS
Catalog Number: 25544
Epoch time: 14071
01983260 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 221
2133 deg
Eccentricity:
0002884
Arg of perigee: 254
5967 deg
Mean anomaly: 105
4863 deg
Mean motion: 15
51381199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3625
Checksum: 303
Coasting Arc #7 (Orbit 3640)
---------------------------------------
Vector Time (GMT): 2014/072/00:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 886509
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2260561
97 A = 6785212
62 meter
Y = -3582104
25 meter E =
0001006
Z = 5301134
45 I = 51
41335
XDOT = 6343
499514 Wp = 207
37857
YDOT = 4296
598857 meter/sec RA = 215
28864 deg
ZDOT = 197
397077 TA = 240
72818
MA = 240
73823
Ha = 224
099 n
mi
Hp = 219
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7416541
91 X = 2274699
03
Y = -11752310
53 feet Y = -3556745
48 meter
Z = 17392173
38 Z = 5312150
57
XDOT = 20812
006281 XDOT = 6294
023640
YDOT = 14096
452942 feet/sec YDOT = 4367
259325 meter/sec
ZDOT = 647
628206 ZDOT = 228
091733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9173365
46 X = -2796041
79
Y = 10360219
34 feet Y = 3157794
85 meter
Z = 17439174
67 Z = 5315460
44
XDOT = -17395
730216 XDOT = -5302
218570
YDOT = -16714
951943 feet/sec YDOT = -5094
717352 meter/sec
ZDOT = 776
645938 ZDOT = 236
721682
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 14072
05046450
00016717 00000-0 10270-3 0 9061
2 25544 51
6447 216
0970 0002933 261
9544 98
1275 15
51437270 36413
Satellite: ISS
Catalog Number: 25544
Epoch time: 14072
05046450 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 216
0970 deg
Eccentricity:
0002933
Arg of perigee: 261
9544 deg
Mean anomaly: 98
1275 deg
Mean motion: 15
51437270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3641
Checksum: 298
Coasting Arc #8 (Orbit 3642)
---------------------------------------
Vector Time (GMT): 2014/072/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4286922
55 A = 6788296
42 meter
Y = 1836709
03 meter E =
0007520
Z = -4939513
86 I = 51
42574
XDOT = -4880
608329 Wp = 116
84078
YDOT = -5474
816517 meter/sec RA = 214
44740 deg
ZDOT = 2199
313883 TA = 174
71795
MA = 174
71001
Ha = 224
148 n
mi
Hp = 221
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14064706
54 X = -4283148
21
Y = 6025948
25 feet Y = 1788790
38 meter
Z = -16205754
12 Z = -4960329
88
XDOT = -16012
494518 XDOT = -4829
708369
YDOT = -17961
996448 feet/sec YDOT = -5529
109728 meter/sec
ZDOT = 7215
596728 ZDOT = 2175
729259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4360423
95 X = 1329057
22
Y = -14568806
25 feet Y = -4440572
14 meter
Z = -16293896
91 Z = -4966379
78
XDOT = 23018
327340 XDOT = 7015
986173
YDOT = -1072
760259 feet/sec YDOT = -326
977327 meter/sec
ZDOT = 7116
757507 ZDOT = 2169
187688
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 14072
17929115
00016717 00000-0 10270-3 0 9073
2 25544 51
6476 215
4581 0005203 270
5788 89
4767 15
50910228 36434
Satellite: ISS
Catalog Number: 25544
Epoch time: 14072
17929115 = yrday
fracday
Element set: 907
Inclination: 51
6476 deg
RA of node: 215
4581 deg
Eccentricity:
0005203
Arg of perigee: 270
5788 deg
Mean anomaly: 89
4767 deg
Mean motion: 15
50910228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3643
Checksum: 321
Coasting Arc #9 (Orbit 3658)
---------------------------------------
Vector Time (GMT): 2014/073/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4661304
90 A = 6789210
74 meter
Y = -1629937
91 meter E =
0004538
Z = 4659484
32 I = 51
45563
XDOT = 4729
277101 Wp = 26
06957
YDOT = 5300
428708 meter/sec RA = 209
46927 deg
ZDOT = -2871
916357 TA = 92
59157
MA = 92
53962
Ha = 223
962 n
mi
Hp = 221
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15292995
10 X = 4656550
81
Y = -5347565
31 feet Y = -1577838
12 meter
Z = 15287022
05 Z = 4682116
67
XDOT = 15516
000986 XDOT = 4683
605691
YDOT = 17389
857967 feet/sec YDOT = 5353
058743 meter/sec
ZDOT = -9422
297758 ZDOT = -2849
054188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5413050
08 X = -1649897
67
Y = 15173437
36 feet Y = 4624863
71 meter
Z = 15382811
33 Z = 4688680
89
XDOT = -22209
152685 XDOT = -6769
349738
YDOT = 1548
886366 feet/sec YDOT = 472
100564 meter/sec
ZDOT = -9326
470361 ZDOT = -2842
708166
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 14073
21024681
00016717 00000-0 10270-3 0 9084
2 25544 51
6476 210
3436 0005269 276
1067 83
9483 15
50979934 36591
Satellite: ISS
Catalog Number: 25544
Epoch time: 14073
21024681 = yrday
fracday
Element set: 908
Inclination: 51
6476 deg
RA of node: 210
3436 deg
Eccentricity:
0005269
Arg of perigee: 276
1067 deg
Mean anomaly: 83
9483 deg
Mean motion: 15
50979934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3659
Checksum: 329
Coasting Arc #10 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2014/074/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5041080
75 A = 6790471
84 meter
Y = 1471238
02 meter E =
0003503
Z = -4308802
74 I = 51
48831
XDOT = -4492
236343 Wp = 126
20772
YDOT = -5115
172223 meter/sec RA = 204
49339 deg
ZDOT = 3509
089316 TA = 179
63328
MA = 179
63303
Ha = 224
070 n
mi
Hp = 221
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16538978
85 X = -5036227
24
Y = 4826896
38 feet Y = 1414891
89 meter
Z = -14136491
92 Z = -4333279
78
XDOT = -14738
308211 XDOT = -4451
749317
YDOT = -16782
061099 feet/sec YDOT = -5165
180370 meter/sec
ZDOT = 11512
760223 ZDOT = 3487
366029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6333330
85 X = 1930399
24
Y = -15930690
39 feet Y = -4855674
43 meter
Z = -14240055
40 Z = -4340368
89
XDOT = 21180
692798 XDOT = 6455
875165
YDOT = -1789
164402 feet/sec YDOT = -545
337310 meter/sec
ZDOT = 11421
704393 ZDOT = 3481
335499
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 14074
17673882
00016717 00000-0 10270-3 0 9094
2 25544 51
6484 205
5482 0005328 280
4297 79
6254 15
51005002 36748
Satellite: ISS
Catalog Number: 25544
Epoch time: 14074
17673882 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 205
5482 deg
Eccentricity:
0005328
Arg of perigee: 280
4297 deg
Mean anomaly: 79
6254 deg
Mean motion: 15
51005002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 316
Coasting Arc #11 (Orbit 3689)
---------------------------------------
Vector Time (GMT): 2014/075/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5417564
67 A = 6791803
98 meter
Y = -1340967
72 meter E =
0006728
Z = 3867883
11 I = 51
52222
XDOT = 4165
897437 Wp = 61
95907
YDOT = 4944
634877 meter/sec RA = 199
52131 deg
ZDOT = -4112
136187 TA = 71
35384
MA = 71
28080
Ha = 224
133 n
mi
Hp = 221
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17774162
30 X = 5413368
22
Y = -4399500
39 feet Y = -1280407
87 meter
Z = 12689905
23 Z = 3894190
72
XDOT = 13667
642509 XDOT = 4130
271100
YDOT = 16222
555372 feet/sec YDOT = 4991
020748 meter/sec
ZDOT = -13491
260455 ZDOT = -4091
986323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7148955
60 X = -2179001
67
Y = 16772958
92 feet Y = 5112397
88 meter
Z = 12801188
48 Z = 3901802
25
XDOT = -20008
893225 XDOT = -6098
710655
YDOT = 1725
243264 feet/sec YDOT = 525
854147 meter/sec
ZDOT = -13406
816330 ZDOT = -4086
397617
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 14075
20763147
00016717 00000-0 10270-3 0 9105
2 25544 51
6486 200
4335 0005330 285
9427 74
1137 15
51070227 36908
Satellite: ISS
Catalog Number: 25544
Epoch time: 14075
20763147 = yrday
fracday
Element set: 910
Inclination: 51
6486 deg
RA of node: 200
4335 deg
Eccentricity:
0005330
Arg of perigee: 285
9427 deg
Mean anomaly: 74
1137 deg
Mean motion: 15
51070227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3690
Checksum: 287
Coasting Arc #12 (Orbit 3704)
---------------------------------------
Vector Time (GMT): 2014/076/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5765459
89 A = 6793275
96 meter
Y = 1260623
52 meter E =
0001970
Z = -3362015
85 I = 51
55715
XDOT = -3758
355641 Wp = 350
81438
YDOT = -4789
733359 meter/sec RA = 194
55193 deg
ZDOT = 4650
699622 TA = 329
98898
MA = 330
00027
Ha = 224
200 n
mi
Hp = 221
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18915550
83 X = -5762796
42
Y = 4135903
95 feet Y = 1196164
80 meter
Z = -11030235
73 Z = -3390017
29
XDOT = -12330
563126 XDOT = -3727
107977
YDOT = -15714
348290 feet/sec YDOT = -4831
586230 meter/sec
ZDOT = 15258
200859 ZDOT = 4632
518794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7750301
03 X = 2362291
75
Y = -17669461
43 feet Y = -5385651
84 meter
Z = -11148669
50 Z = -3398114
46
XDOT = 18728
209527 XDOT = 5708
358264
YDOT = -1361
396337 feet/sec YDOT = -414
953604 meter/sec
ZDOT = 15182
044436 ZDOT = 4627
487144
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 14076
17406332
00016717 00000-0 10270-3 0 9113
2 25544 51
6488 195
6378 0005493 289
9919 70
0641 15
51097252 37051
Satellite: ISS
Catalog Number: 25544
Epoch time: 14076
17406332 = yrday
fracday
Element set: 911
Inclination: 51
6488 deg
RA of node: 195
6378 deg
Eccentricity:
0005493
Arg of perigee: 289
9919 deg
Mean anomaly: 70
0641 deg
Mean motion: 15
51097252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 328
Coasting Arc #13 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2014/077/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6084089
47 A = 6794655
53 meter
Y = -1199411
34 meter E =
0008264
Z = 2769851
02 I = 51
59262
XDOT = 3260
112429 Wp = 90
69417
YDOT = 4671
315764 meter/sec RA = 189
58703 deg
ZDOT = -5125
023635 TA = 57
94348
MA = 57
86325
Ha = 224
388 n
mi
Hp = 221
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19960923
46 X = 6083594
32
Y = -3935076
58 feet Y = -1131377
49 meter
Z = 9087437
74 Z = 2799405
68
XDOT = 10695
906918 XDOT = 3232
530168
YDOT = 15325
839121 feet/sec YDOT = 4707
617414 meter/sec
ZDOT = -16814
382006 ZDOT = -5109
254180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8217112
50 X = -2504575
89
Y = 18550336
05 feet Y = 5654142
43 meter
Z = 9212432
49 Z = 2807949
42
XDOT = -17395
555147 XDOT = -5302
165209
YDOT = 633
107225 feet/sec YDOT = 192
971082 meter/sec
ZDOT = -16748
389363 ZDOT = -5104
909078
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 14077
20489258
00016717 00000-0 10270-3 0 9127
2 25544 51
6489 190
5229 0005421 295
1734 64
8855 15
51155665 37215
Satellite: ISS
Catalog Number: 25544
Epoch time: 14077
20489258 = yrday
fracday
Element set: 912
Inclination: 51
6489 deg
RA of node: 190
5229 deg
Eccentricity:
0005421
Arg of perigee: 295
1734 deg
Mean anomaly: 64
8855 deg
Mean motion: 15
51155665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 326
Coasting Arc #14 (Orbit 3735)
---------------------------------------
Vector Time (GMT): 2014/078/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6341030
52 A = 6795903
75 meter
Y = 1177027
08 meter E =
0007398
Z = -2127293
94 I = 51
62719
XDOT = -2698
898814 Wp = 354
73971
YDOT = -4594
301047 meter/sec RA = 184
62439 deg
ZDOT = 5508
528236 TA = 341
70996
MA = 341
73655
Ha = 224
444 n
mi
Hp = 221
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20803905
92 X = -6343387
27
Y = 3861637
41 feet Y = 1106104
13 meter
Z = -6979310
83 Z = -2158103
78
XDOT = -8854
654903 XDOT = -2674
082485
YDOT = -15073
166164 feet/sec YDOT = -4624
342324 meter/sec
ZDOT = 18072
599200 ZDOT = 5495
478249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8437323
41 X = 2571696
18
Y = -19356923
06 feet Y = -5899990
15 meter
Z = -7109615
16 Z = -2167010
70
XDOT = 16096
523783 XDOT = 4906
220449
YDOT = 405
020176 feet/sec YDOT = 123
450150 meter/sec
ZDOT = 18018
079998 ZDOT = 5491
910783
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 14078
17126412
00016717 00000-0 10270-3 0 9135
2 25544 51
6482 185
7266 0005642 299
1507 60
9079 15
51188098 37369
Satellite: ISS
Catalog Number: 25544
Epoch time: 14078
17126412 = yrday
fracday
Element set: 913
Inclination: 51
6482 deg
RA of node: 185
7266 deg
Eccentricity:
0005642
Arg of perigee: 299
1507 deg
Mean anomaly: 60
9079 deg
Mean motion: 15
51188098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3736
Checksum: 328
Coasting Arc #15 (Orbit 3751)
---------------------------------------
Vector Time (GMT): 2014/079/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6543655
21 A = 6796855
26 meter
Y = -1154698
68 meter E =
0008336
Z = 1411874
94 I = 51
66153
XDOT = 2061
595124 Wp = 116
17510
YDOT = 4570
312962 meter/sec RA = 179
66633 deg
ZDOT = -5794
121770 TA = 48
45914
MA = 48
38767
Ha = 224
619 n
mi
Hp = 220
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21468685
09 X = 6549222
50
Y = -3788381
49 feet Y = -1081492
02 meter
Z = 4632135
62 Z = 1443676
93
XDOT = 6763
763529 XDOT = 2038
481776
YDOT = 14994
465097 feet/sec YDOT = 4593
237078 meter/sec
ZDOT = -19009
585859 ZDOT = -5784
163492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8535383
72 X = -2601584
96
Y = 20028462
54 feet Y = 6104675
38 meter
Z = 4766641
07 Z = 1452872
20
XDOT = -14857
849105 XDOT = -4528
672407
YDOT = -1800
130037 feet/sec YDOT = -548
679635 meter/sec
ZDOT = -18968
122329 ZDOT = -5781
483686
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 14079
20202981
00016717 00000-0 10270-3 0 9147
2 25544 51
6480 180
6113 0005531 303
5494 56
5129 15
51237114 37523
Satellite: ISS
Catalog Number: 25544
Epoch time: 14079
20202981 = yrday
fracday
Element set: 914
Inclination: 51
6480 deg
RA of node: 180
6113 deg
Eccentricity:
0005531
Arg of perigee: 303
5494 deg
Mean anomaly: 56
5129 deg
Mean motion: 15
51237114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 284
Coasting Arc #16 (Orbit 3766)
---------------------------------------
Vector Time (GMT): 2014/080/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6658541
70 A = 6797394
09 meter
Y = 1147800
49 meter E =
0011724
Z = -669609
73 I = 51
69351
XDOT = -1391
227642 Wp = 11
49594
YDOT = -4605
918167 meter/sec RA = 174
70943 deg
ZDOT = 5968
299971 TA = 341
28422
MA = 341
32730
Ha = 224
690 n
mi
Hp = 220
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21845609
26 X = -6667629
02
Y = 3765749
63 feet Y = 1073289
52 meter
Z = -2196882
32 Z = -701978
36
XDOT = -4564
395151 XDOT = -1368
612079
YDOT = -15111
280077 feet/sec YDOT = -4621
348672 meter/sec
ZDOT = 19581
036651 ZDOT = 5961
596975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8417087
59 X = 2565528
30
Y = -20492531
30 feet Y = -6246123
54 meter
Z = -2333795
90 Z = -711340
99
XDOT = 13794
819393 XDOT = 4204
660951
YDOT = 3449
513225 feet/sec YDOT = 1051
411631 meter/sec
ZDOT = 19553
330643 ZDOT = 5959
855180
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 14080
16834145
00016717 00000-0 10270-3 0 9158
2 25544 51
6467 175
8141 0005715 307
6296 52
4336 15
51285004 37676
Satellite: ISS
Catalog Number: 25544
Epoch time: 14080
16834145 = yrday
fracday
Element set: 915
Inclination: 51
6467 deg
RA of node: 175
8141 deg
Eccentricity:
0005715
Arg of perigee: 307
6296 deg
Mean anomaly: 52
4336 deg
Mean motion: 15
51285004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3767
Checksum: 308
Coasting Arc #17 (Orbit 3782)
---------------------------------------
Vector Time (GMT): 2014/081/04:00:25
814
Vector Time (MET): N/A
Weight (LBS) : 886211
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6701274
55 A = 6797482
92 meter
Y = -1114063
48 meter E =
0006296
Z = -120889
71 I = 51
72454
XDOT = 676
050237 Wp = 138
85096
YDOT = 4699
178494 meter/sec RA = 169
75654 deg
ZDOT = -6012
874494 TA = 42
44775
MA = 42
39907
Ha = 224
808 n
mi
Hp = 220
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21985808
90 X = 6713821
45
Y = -3655063
92 feet Y = -1039055
39 meter
Z = -396619
79 Z = -88305
16
XDOT = 2218
012587 XDOT = 652
661446
YDOT = 15417
252278 feet/sec YDOT = 4706
607193 meter/sec
ZDOT = -19727
278522 ZDOT = -6009
647568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8238776
54 X = -2511179
09
Y = 20711064
33 feet Y = 6312732
41 meter
Z = -258781
34 Z = -78876
55
XDOT = -12895
854890 XDOT = -3930
656570
YDOT = -5364
754012 feet/sec YDOT = -1635
177023 meter/sec
ZDOT = -19714
273715 ZDOT = -6008
910628
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 14081
19904362
00016717 00000-0 10270-3 0 9162
2 25544 51
6463 170
6981 0005658 311
5243 48
5422 15
51325731 37831
Satellite: ISS
Catalog Number: 25544
Epoch time: 14081
19904362 = yrday
fracday
Element set: 916
Inclination: 51
6463 deg
RA of node: 170
6981 deg
Eccentricity:
0005658
Arg of perigee: 311
5243 deg
Mean anomaly: 48
5422 deg
Mean motion: 15
51325731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3783
Checksum: 307
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