[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 9th 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 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
191/05:39:55
343 4
1 4
4 4
5
N/A 0
2 -0
6 228
9
000/00:09:50
686 1
8 -0
1 220
9
Coasting Arc #1 (Orbit 3800)
---------------------------------------
Vector Time (GMT): 2013/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5161045
64 A = 6794349
79 meter
Y = -2629767
91 meter E =
0012372
Z = -3566720
95 I = 51
66528
XDOT = 4976
782023 Wp = 123
03400
YDOT = 3718
366478 meter/sec RA = 2
13642 deg
ZDOT = 4464
510416 TA = 195
01896
MA = 195
05573
Ha = 229
172 n
mi
Hp = 218
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16932564
43 X = 5207394
62
Y = -8627847
49 feet Y = -2571794
22 meter
Z = -11701840
37 Z = -3541537
15
XDOT = 16328
025009 XDOT = 4913
145470
YDOT = 12199
365086 feet/sec YDOT = 3773
663603 meter/sec
ZDOT = 14647
343883 ZDOT = 4488
532770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12929816
06 X = -3941007
93
Y = -14015578
87 feet Y = -4271948
44 meter
Z = -11596032
26 Z = -3534470
63
XDOT = 6300
572218 XDOT = 1920
414412
YDOT = -18001
046824 feet/sec YDOT = -5486
719072 meter/sec
ZDOT = 14747
256096 ZDOT = 4494
963658
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 13189
50744934
00016717 00000-0 10270-3 0 9005
2 25544 51
6460 2
6580 0008244 140
9316 219
2432 15
50597491 38018
Satellite: ISS
Catalog Number: 25544
Epoch time: 13189
50744934 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 2
6580 deg
Eccentricity:
0008244
Arg of perigee: 140
9316 deg
Mean anomaly: 219
2432 deg
Mean motion: 15
50597491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3801
Checksum: 297
Coasting Arc #2 (Orbit 3816)
---------------------------------------
Vector Time (GMT): 2013/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5365546
75 A = 6795561
87 meter
Y = 2737759
49 meter E =
0019284
Z = 3121147
90 I = 51
63850
XDOT = -4691
250456 Wp = 113
73736
YDOT = -3626
256159 meter/sec RA = 357
17907 deg
ZDOT = -4867
663202 TA = 30
33761
MA = 30
22613
Ha = 229
121 n
mi
Hp = 218
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17603499
85 X = -5410923
65
Y = 8982150
56 feet Y = 2677504
48 meter
Z = 10239986
54 Z = 3094973
05
XDOT = -15391
241652 XDOT = -4626
706781
YDOT = -11897
165876 feet/sec YDOT = -3678
355231 meter/sec
ZDOT = -15970
023630 ZDOT = -4890
296184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13699113
25 X = 4175489
72
Y = 14322591
08 feet Y = 4365525
76 meter
Z = 10130016
83 Z = 3087629
13
XDOT = -5934
701346 XDOT = -1808
896970
YDOT = 17076
162362 feet/sec YDOT = 5204
814288 meter/sec
ZDOT = -16064
137887 ZDOT = -4896
349228
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 13190
53862098
00016717 00000-0 10270-3 0 9013
2 25544 51
6459 357
5446 0008127 145
1052 215
0633 15
50605086 38177
Satellite: ISS
Catalog Number: 25544
Epoch time: 13190
53862098 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 357
5446 deg
Eccentricity:
0008127
Arg of perigee: 145
1052 deg
Mean anomaly: 215
0633 deg
Mean motion: 15
50605086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3817
Checksum: 304
Coasting Arc #3 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2013/191/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4405219
80 A = 6796016
56 meter
Y = -3528234
36 meter E =
0009295
Z = -3797000
02 I = 51
61435
XDOT = 5790
382590 Wp = 131
38205
YDOT = 2698
811699 meter/sec RA = 353
51257 deg
ZDOT = 4210
845362 TA = 183
21059
MA = 183
21656
Ha = 228
917 n
mi
Hp = 220
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14452820
88 X = 4462790
38
Y = -11575572
06 feet Y = -3478650
12 meter
Z = -12457349
16 Z = -3775460
73
XDOT = 18997
318210 XDOT = 5739
318718
YDOT = 8854
369091 feet/sec YDOT = 2763
277460 meter/sec
ZDOT = 13815
109456 ZDOT = 4238
850331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11371135
87 X = 3465922
21
Y = -14691040
14 feet Y = -4477829
03 meter
Z = -12366650
99 Z = -3769355
22
XDOT = 19400
302109 XDOT = 5913
212083
YDOT = 3290
597993 feet/sec YDOT = 1002
974268 meter/sec
ZDOT = 13931
852409 ZDOT = 4246
428614
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 13191
24754612
00016717 00000-0 10270-3 0 9025
2 25544 51
6508 354
0322 0005055 166
7167 193
4117 15
49780770 38280
Satellite: ISS
Catalog Number: 25544
Epoch time: 13191
24754612 = yrday
fracday
Element set: 902
Inclination: 51
6508 deg
RA of node: 354
0322 deg
Eccentricity:
0005055
Arg of perigee: 166
7167 deg
Mean anomaly: 193
4117 deg
Mean motion: 15
49780770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 309
Coasting Arc #4 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2013/192/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4347510
13 A = 6796617
09 meter
Y = 3782847
17 meter E =
0013663
Z = 3587927
29 I = 51
58601
XDOT = -5770
052211 Wp = 108
23512
YDOT = -2418
176453 meter/sec RA = 348
55751 deg
ZDOT = -4432
352288 TA = 29
34660
MA = 29
26994
Ha = 228
894 n
mi
Hp = 220
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14263484
68 X = -4406916
54
Y = 12410915
90 feet Y = 3733898
09 meter
Z = 11771415
00 Z = 3566663
84
XDOT = -18930
617491 XDOT = -5721
051965
YDOT = -7933
649779 feet/sec YDOT = -2482
426462 meter/sec
ZDOT = -14541
838216 ZDOT = -4460
263440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10717556
72 X = -3266711
29
Y = 15643296
73 feet Y = 4768076
84 meter
Z = 11681835
69 Z = 3560623
52
XDOT = -19096
213033 XDOT = -5820
525732
YDOT = -2113
044366 feet/sec YDOT = -644
055923 meter/sec
ZDOT = -14658
232733 ZDOT = -4467
829337
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 13192
27926709
00016717 00000-0 10270-3 0 9038
2 25544 51
6508 348
9233 0005005 169
9240 190
2011 15
49789638 38443
Satellite: ISS
Catalog Number: 25544
Epoch time: 13192
27926709 = yrday
fracday
Element set: 903
Inclination: 51
6508 deg
RA of node: 348
9233 deg
Eccentricity:
0005005
Arg of perigee: 169
9240 deg
Mean anomaly: 190
2011 deg
Mean motion: 15
49789638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 325
Coasting Arc #5 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2013/193/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4271693
99 A = 6797154
17 meter
Y = -4063676
00 meter E =
0006946
Z = -3391743
89 I = 51
55863
XDOT = 5709
164900 Wp = 131
66508
YDOT = 2144
550484 meter/sec RA = 343
59987 deg
ZDOT = 4622
571234 TA = 188
79249
MA = 188
80467
Ha = 228
646 n
mi
Hp = 221
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14014744
05 X = 4333293
35
Y = -13332270
33 feet Y = -4015562
55 meter
Z = -11127768
68 Z = -3370843
35
XDOT = 18730
855971 XDOT = 5662
304875
YDOT = 7035
926786 feet/sec YDOT = 2208
131640 meter/sec
ZDOT = 15165
916123 ZDOT = 4650
191783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9954506
97 X = 3034133
72
Y = -16644014
02 feet Y = -5073095
47 meter
Z = -11039669
71 Z = -3364891
33
XDOT = 18631
310579 XDOT = 5678
823465
YDOT = 1010
954751 feet/sec YDOT = 308
139008 meter/sec
ZDOT = 15281
136334 ZDOT = 4657
690355
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 13193
24649549
00016717 00000-0 10270-3 0 9041
2 25544 51
6513 344
1330 0004884 175
3649 184
7548 15
49805873 38592
Satellite: ISS
Catalog Number: 25544
Epoch time: 13193
24649549 = yrday
fracday
Element set: 904
Inclination: 51
6513 deg
RA of node: 344
1330 deg
Eccentricity:
0004884
Arg of perigee: 175
3649 deg
Mean anomaly: 184
7548 deg
Mean motion: 15
49805873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 347
Coasting Arc #6 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2013/194/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4173479
66 A = 6797734
95 meter
Y = 4325453
44 meter E =
0014313
Z = 3157006
46 I = 51
53154
XDOT = -5641
641344 Wp = 114
00110
YDOT = -1911
841857 meter/sec RA = 338
64119 deg
ZDOT = -4827
034107 TA = 29
56418
MA = 29
48333
Ha = 228
591 n
mi
Hp = 221
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13692518
58 X = -4236873
34
Y = 14191120
21 feet Y = 4278428
31 meter
Z = 10357632
74 Z = 3136578
58
XDOT = -18509
321996 XDOT = -5596
395266
YDOT = -6272
447037 feet/sec YDOT = -1974
676988 meter/sec
ZDOT = -15836
726073 ZDOT = -4854
330585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9107133
29 X = -2775854
23
Y = 17541675
92 feet Y = 5346702
82 meter
Z = 10271477
16 Z = 3130746
24
XDOT = -18157
588750 XDOT = -5534
433051
YDOT = -64
527235 feet/sec YDOT = -19
667901 meter/sec
ZDOT = -15950
624209 ZDOT = -4861
750259
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 13194
27819771
00016717 00000-0 10270-3 0 9052
2 25544 51
6513 339
0241 0004832 178
2021 181
9148 15
49823595 38759
Satellite: ISS
Catalog Number: 25544
Epoch time: 13194
27819771 = yrday
fracday
Element set: 905
Inclination: 51
6513 deg
RA of node: 339
0241 deg
Eccentricity:
0004832
Arg of perigee: 178
2021 deg
Mean anomaly: 181
9148 deg
Mean motion: 15
49823595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 325
Coasting Arc #7 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2013/195/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4050823
33 A = 6798284
40 meter
Y = -4608011
16 meter E =
0004705
Z = -2935028
70 I = 51
50497
XDOT = 5544
104621 Wp = 125
72365
YDOT = 1692
157001 meter/sec RA = 333
67975 deg
ZDOT = 4998
049058 TA = 200
81490
MA = 200
83407
Ha = 228
365 n
mi
Hp = 221
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13290102
79 X = 4116307
50
Y = -15118146
84 feet Y = -4562345
99 meter
Z = -9629359
27 Z = -2915191
53
XDOT = 18189
319624 XDOT = 5500
491542
YDOT = 5551
696196 feet/sec YDOT = 1753
910561 meter/sec
ZDOT = 16397
798746 ZDOT = 5024
875750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8135144
90 X = 2479592
16
Y = -18455621
86 feet Y = -5625273
54 meter
Z = -9545637
50 Z = -2909510
31
XDOT = 17573
772280 XDOT = 5356
485791
YDOT = -787
689364 feet/sec YDOT = -240
087718 meter/sec
ZDOT = 16509
762389 ZDOT = 5032
175576
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 13195
24540861
00016717 00000-0 10270-3 0 9062
2 25544 51
6510 334
2337 0004743 184
3384 175
7726 15
49829812 38908
Satellite: ISS
Catalog Number: 25544
Epoch time: 13195
24540861 = yrday
fracday
Element set: 906
Inclination: 51
6510 deg
RA of node: 334
2337 deg
Eccentricity:
0004743
Arg of perigee: 184
3384 deg
Mean anomaly: 175
7726 deg
Mean motion: 15
49829812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 324
Coasting Arc #8 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2013/196/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3907691
78 A = 6798808
39 meter
Y = 4866028
91 meter E =
0014740
Z = 2675202
45 I = 51
47983
XDOT = -5444
673967 Wp = 120
45229
YDOT = -1516
771034 meter/sec RA = 328
71747 deg
ZDOT = -5180
145831 TA = 29
31124
MA = 29
22863
Ha = 228
268 n
mi
Hp = 221
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12820511
09 X = -3974809
69
Y = 15964661
76 feet Y = 4821955
20 meter
Z = 8776910
94 Z = 2656056
58
XDOT = -17863
103566 XDOT = -5402
144826
YDOT = -4976
282919 feet/sec YDOT = -1577
418733 meter/sec
ZDOT = -16995
229104 ZDOT = -5206
492218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7095965
48 X = -2162850
28
Y = 19243080
24 feet Y = 5865290
86 meter
Z = 8696046
93 Z = 2650555
11
XDOT = -17013
686346 XDOT = -5185
771598
YDOT = 1477
049690 feet/sec YDOT = 450
204746 meter/sec
ZDOT = -17105
207264 ZDOT = -5213
667174
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 13196
27709191
00016717 00000-0 10270-3 0 9070
2 25544 51
6510 329
1246 0004678 187
0733 173
0353 15
49858036 39060
Satellite: ISS
Catalog Number: 25544
Epoch time: 13196
27709191 = yrday
fracday
Element set: 907
Inclination: 51
6510 deg
RA of node: 329
1246 deg
Eccentricity:
0004678
Arg of perigee: 187
0733 deg
Mean anomaly: 173
0353 deg
Mean motion: 15
49858036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 324
Coasting Arc #9 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2013/197/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3735561
61 A = 6799341
12 meter
Y = -5137888
82 meter E =
0003088
Z = -2428421
75 I = 51
45488
XDOT = 5326
955688 Wp = 103
27432
YDOT = 1357
425584 meter/sec RA = 323
75217 deg
ZDOT = 5327
371766 TA = 229
56031
MA = 229
58724
Ha = 228
089 n
mi
Hp = 221
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12255779
54 X = 3804533
54
Y = -16856590
62 feet Y = -5095729
60 meter
Z = -7967262
96 Z = -2410107
59
XDOT = 17476
888739 XDOT = 5285
501883
YDOT = 4453
496010 feet/sec YDOT = 1416
762830 meter/sec
ZDOT = 17478
253825 ZDOT = 5353
148977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5927699
64 X = 1806762
85
Y = -20010968
34 feet Y = -6099343
15 meter
Z = -7889840
41 Z = -2404823
36
XDOT = 16396
279820 XDOT = 4997
586089
YDOT = -2070
154789 feet/sec YDOT = -630
983180 meter/sec
ZDOT = 17585
873051 ZDOT = 5360
174106
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 13197
24428556
00016717 00000-0 10270-3 0 9082
2 25544 51
6500 324
3335 0004660 193
1652 166
9377 15
49854096 39210
Satellite: ISS
Catalog Number: 25544
Epoch time: 13197
24428556 = yrday
fracday
Element set: 908
Inclination: 51
6500 deg
RA of node: 324
3335 deg
Eccentricity:
0004660
Arg of perigee: 193
1652 deg
Mean anomaly: 166
9377 deg
Mean motion: 15
49854096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 326
Coasting Arc #10 (Orbit 3936)
---------------------------------------
Vector Time (GMT): 2013/198/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3546310
86 A = 6799771
69 meter
Y = 5379519
14 meter E =
0014894
Z = 2144882
05 I = 51
43255
XDOT = -5213
213156 Wp = 127
51509
YDOT = -1244
204548 meter/sec RA = 318
78644 deg
ZDOT = -5481
565702 TA = 28
65884
MA = 28
57706
Ha = 227
933 n
mi
Hp = 221
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11634878
17 X = -3616621
49
Y = 17649341
01 feet Y = 5339468
74 meter
Z = 7037014
59 Z = 2127484
08
XDOT = -17103
717704 XDOT = -5172
284807
YDOT = -4082
035919 feet/sec YDOT = -1302
272686 meter/sec
ZDOT = -17984
139442 ZDOT = -5506
791683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4717010
27 X = -1437744
73
Y = 20631292
13 feet Y = 6288417
84 meter
Z = 6963390
08 Z = 2122441
30
XDOT = -15837
258856 XDOT = -4827
196499
YDOT = 2503
929137 feet/sec YDOT = 763
197601 meter/sec
ZDOT = -18089
469170 ZDOT = -5513
670203
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 13198
27595000
00016717 00000-0 10270-3 0 9096
2 25544 51
6500 319
2240 0004567 196
3421 163
7583 15
49892980 39378
Satellite: ISS
Catalog Number: 25544
Epoch time: 13198
27595000 = yrday
fracday
Element set: 909
Inclination: 51
6500 deg
RA of node: 319
2240 deg
Eccentricity:
0004567
Arg of perigee: 196
3421 deg
Mean anomaly: 163
7583 deg
Mean motion: 15
49892980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3937
Checksum: 328
Coasting Arc #11 (Orbit 3951)
---------------------------------------
Vector Time (GMT): 2013/199/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3325745
48 A = 6800254
67 meter
Y = -5627143
01 meter E =
0003104
Z = -1875142
88 I = 51
41029
XDOT = 5093
144759 Wp = 65
40170
YDOT = 1146
828394 meter/sec RA = 313
81763 deg
ZDOT = 5600
242714 TA = 273
94026
MA = 273
97574
Ha = 227
825 n
mi
Hp = 221
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10911238
46 X = 3397531
15
Y = -18461755
29 feet Y = -5589550
85 meter
Z = -6152043
57 Z = -1858812
96
XDOT = 16709
792516 XDOT = 5052
737738
YDOT = 3762
560347 feet/sec YDOT = 1203
556645 meter/sec
ZDOT = 18373
499718 ZDOT = 5624
886675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3384488
84 X = 1031592
20
Y = -21196304
88 feet Y = -6460633
73 meter
Z = -6082850
29 Z = -1854052
77
XDOT = 15270
242754 XDOT = 4654
369991
YDOT = -2855
864110 feet/sec YDOT = -870
467381 meter/sec
ZDOT = 18476
410813 ZDOT = 5631
610016
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 13199
24312687
00016717 00000-0 10270-3 0 9104
2 25544 51
6487 314
4324 0004633 201
4019 158
6938 15
49879313 39526
Satellite: ISS
Catalog Number: 25544
Epoch time: 13199
24312687 = yrday
fracday
Element set: 910
Inclination: 51
6487 deg
RA of node: 314
4324 deg
Eccentricity:
0004633
Arg of perigee: 201
4019 deg
Mean anomaly: 158
6938 deg
Mean motion: 15
49879313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 324
Coasting Arc #12 (Orbit 3967)
---------------------------------------
Vector Time (GMT): 2013/200/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3093016
05 A = 6800554
02 meter
Y = 5839067
05 meter E =
0014742
Z = 1570169
19 I = 51
39153
XDOT = -4983
657462 Wp = 135
04952
YDOT = -1095
373709 meter/sec RA = 308
84904 deg
ZDOT = -5720
969399 TA = 27
74160
MA = 27
66304
Ha = 227
600 n
mi
Hp = 221
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10147690
45 X = -3165707
30
Y = 19157044
13 feet Y = 5804072
36 meter
Z = 5151473
74 Z = 1554967
82
XDOT = -16350
582225 XDOT = -4943
247586
YDOT = -3593
745766 feet/sec YDOT = -1150
877479 meter/sec
ZDOT = -18769
584643 ZDOT = -5745
081415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2041689
43 X = -622306
94
Y = 21597682
25 feet Y = 6582973
55 meter
Z = 5086970
47 Z = 1550508
60
XDOT = -14794
855438 XDOT = -4509
471938
YDOT = 3063
761348 feet/sec YDOT = 933
834459 meter/sec
ZDOT = -18870
281678 ZDOT = -5751
661855
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
27477278
00016717 00000-0 10270-3 0 9119
2 25544 51
6490 309
3227 0004503 205
4816 154
6113 15
49928880 39682
Satellite: ISS
Catalog Number: 25544
Epoch time: 13200
27477278 = yrday
fracday
Element set: 911
Inclination: 51
6490 deg
RA of node: 309
3227 deg
Eccentricity:
0004503
Arg of perigee: 205
4816 deg
Mean anomaly: 154
6113 deg
Mean motion: 15
49928880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3968
Checksum: 315
Coasting Arc #13 (Orbit 3982)
---------------------------------------
Vector Time (GMT): 2013/201/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2829128
66 A = 6800955
42 meter
Y = -6048968
99 meter E =
0004469
Z = -1280231
18 I = 51
37288
XDOT = 4879
066628 Wp = 47
12609
YDOT = 1056
447702 meter/sec RA = 303
87757 deg
ZDOT = 5806
332296 TA = 298
92771
MA = 298
97252
Ha = 227
577 n
mi
Hp = 221
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9281918
17 X = 2902778
23
Y = -19845698
80 feet Y = -6016919
93 meter
Z = -4200233
52 Z = -1266309
55
XDOT = 16007
436444 XDOT = 4838
685276
YDOT = 3466
035768 feet/sec YDOT = 1110
781975 meter/sec
ZDOT = 19049
646641 ZDOT = 5829
936178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 595609
06 X = 181541
64
Y = -21912203
03 feet Y = -6678839
48 meter
Z = -4141054
88 Z = -1262193
53
XDOT = 14352
188554 XDOT = 4374
547071
YDOT = -3218
591182 feet/sec YDOT = -981
026592 meter/sec
ZDOT = 19148
229237 ZDOT = 5836
380272
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
24193350
00016717 00000-0 10270-3 0 9124
2 25544 51
6477 304
5309 0004632 208
7564 151
3332 15
49905457 39833
Satellite: ISS
Catalog Number: 25544
Epoch time: 13201
24193350 = yrday
fracday
Element set: 912
Inclination: 51
6477 deg
RA of node: 304
5309 deg
Eccentricity:
0004632
Arg of perigee: 208
7564 deg
Mean anomaly: 151
3332 deg
Mean motion: 15
49905457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3983
Checksum: 301
Coasting Arc #14 (Orbit 3998)
---------------------------------------
Vector Time (GMT): 2013/202/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2559749
41 A = 6801091
06 meter
Y = 6218438
14 meter E =
0014260
Z = 956969
73 I = 51
35796
XDOT = -4791
759853 Wp = 142
85313
YDOT = -1060
952130 meter/sec RA = 298
90684 deg
ZDOT = -5888
229777 TA = 26
75500
MA = 26
68151
Ha = 227
286 n
mi
Hp = 222
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8398127
99 X = -2633743
72
Y = 20401699
95 feet Y = 6189399
56 meter
Z = 3139664
47 Z = 944355
94
XDOT = -15720
996893 XDOT = -4750
936955
YDOT = -3480
814075 feet/sec YDOT = -1114
307633 meter/sec
ZDOT = -19318
339163 ZDOT = -5911
408323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 822244
48 X = 250620
12
Y = 22054847
80 feet Y = 6722317
61 meter
Z = 3085937
49 Z = 940593
75
XDOT = -14028
906198 XDOT = -4276
010609
YDOT = 3255
902808 feet/sec YDOT = 992
399176 meter/sec
ZDOT = -19415
148171 ZDOT = -5917
737162
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
27356142
00016717 00000-0 10270-3 0 9139
2 25544 51
6481 299
4213 0004467 213
8399 146
2467 15
49964467 39998
Satellite: ISS
Catalog Number: 25544
Epoch time: 13202
27356142 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 299
4213 deg
Eccentricity:
0004467
Arg of perigee: 213
8399 deg
Mean anomaly: 146
2467 deg
Mean motion: 15
49964467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3999
Checksum: 341
Coasting Arc #15 (Orbit 4013)
---------------------------------------
Vector Time (GMT): 2013/203/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2261809
99 A = 6801375
67 meter
Y = -6378475
82 meter E =
0006090
Z = -650408
42 I = 51
34347
XDOT = 4718
909400 Wp = 44
65720
YDOT = 1071
964276 meter/sec RA = 293
93353 deg
ZDOT = 5935
736249 TA = 308
30607
MA = 308
36082
Ha = 227
341 n
mi
Hp = 222
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7420636
45 X = 2336126
83
Y = -20926757
95 feet Y = -6352767
24 meter
Z = -2133885
90 Z = -639241
15
XDOT = 15481
986220 XDOT = 4677
738150
YDOT = 3516
943163 feet/sec YDOT = 1124
503270 meter/sec
ZDOT = 19474
200291 ZDOT = 5958
559922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2315419
44 X = -705739
85
Y = -22086990
08 feet Y = -6732114
58 meter
Z = -2086196
24 Z = -635872
61
XDOT = 13766
262275 XDOT = 4195
956741
YDOT = -3279
432906 feet/sec YDOT = -999
571150 meter/sec
ZDOT = 19569
529732 ZDOT = 5964
792662
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
24070638
00016717 00000-0 10270-3 0 9141
2 25544 51
6470 294
6297 0004623 215
2116 144
8730 15
49933354 40149
Satellite: ISS
Catalog Number: 25544
Epoch time: 13203
24070638 = yrday
fracday
Element set: 914
Inclination: 51
6470 deg
RA of node: 294
6297 deg
Eccentricity:
0004623
Arg of perigee: 215
2116 deg
Mean anomaly: 144
8730 deg
Mean motion: 15
49933354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4014
Checksum: 294
Coasting Arc #16 (Orbit 4029)
---------------------------------------
Vector Time (GMT): 2013/204/05:44:50
686
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1966674
88 A = 6801334
20 meter
Y = 6494681
45 meter E =
0013416
Z = 312800
00 I = 51
33238
XDOT = -4669
371214 Wp = 150
70475
YDOT = -1121
536074 meter/sec RA = 288
96093 deg
ZDOT = -5973
861877 TA = 25
91428
MA = 25
84715
Ha = 227
012 n
mi
Hp = 222
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6452345
42 X = -2040673
12
Y = 21308010
01 feet Y = 6472275
08 meter
Z = 1026246
70 Z = 303067
08
XDOT = -15319
459363 XDOT = -4627
464200
YDOT = -3679
580294 feet/sec YDOT = -1173
517134 meter/sec
ZDOT = -19599
284374 ZDOT = -5996
443032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3737719
45 X = 1139256
89
Y = 21949426
92 feet Y = 6690185
32 meter
Z = 984553
61 Z = 300091
94
XDOT = -13641
225797 XDOT = -4157
845623
YDOT = 3221
254334 feet/sec YDOT = 981
838321 meter/sec
ZDOT = -19693
597862 ZDOT = -6002
608628
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
27231682
00016717 00000-0 10270-3 0 9154
2 25544 51
6470 289
5199 0004430 221
0242 139
0576 15
49995718 40308
Satellite: ISS
Catalog Number: 25544
Epoch time: 13204
27231682 = yrday
fracday
Element set: 915
Inclination: 51
6470 deg
RA of node: 289
5199 deg
Eccentricity:
0004430
Arg of perigee: 221
0242 deg
Mean anomaly: 139
0576 deg
Mean motion: 15
49995718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4030
Checksum: 306
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