[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 10th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 3832)
---------------------------------------
Vector Time (GMT): 2013/191/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5296255
91 A = 6798609
41 meter
Y = 3079111
02 meter E =
0015907
Z = 2926084
14 I = 51
61086
XDOT = -4729
635721 Wp = 117
07951
YDOT = -3354
111970 meter/sec RA = 352
06297 deg
ZDOT = -5017
244813 TA = 29
56267
MA = 29
47284
Ha = 229
116 n
mi
Hp = 220
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17376167
70 X = -5344507
47
Y = 10102070
27 feet Y = 3019614
86 meter
Z = 9600013
58 Z = 2900238
92
XDOT = -15517
177562 XDOT = -4667
405769
YDOT = -11004
304364 feet/sec YDOT = -3406
653298 meter/sec
ZDOT = -16460
776945 ZDOT = -5040
069778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17331736
92 X = 5282713
41
Y = 10279495
63 feet Y = 3133190
27 meter
Z = 9491372
59 Z = 2892970
37
XDOT = -1324
735429 XDOT = -403
779359
YDOT = 17562
709600 feet/sec YDOT = 5353
113886 meter/sec
ZDOT = -16555
739195 ZDOT = -5046
189307
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
56997058
00016717 00000-0 10270-3 0 9001
2 25544 51
6481 352
4321 0005443 169
5973 190
5291 15
49731708 38332
Satellite: ISS
Catalog Number: 25544
Epoch time: 13191
56997058 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 352
4321 deg
Eccentricity:
0005443
Arg of perigee: 169
5973 deg
Mean anomaly: 190
5291 deg
Mean motion: 15
49731708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3833
Checksum: 327
Coasting Arc #2 (Orbit 3847)
---------------------------------------
Vector Time (GMT): 2013/192/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5222567
56 A = 6799004
55 meter
Y = -3406677
91 meter E =
0005396
Z = -2718152
06 I = 51
58394
XDOT = 4715
820869 Wp = 117
86471
YDOT = 3117
655995 meter/sec RA = 347
10845 deg
ZDOT = 5158
841592 TA = 211
47078
MA = 211
50307
Ha = 228
924 n
mi
Hp = 221
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17134407
99 X = 5273477
46
Y = -11176764
80 feet Y = -3347990
98 meter
Z = -8917821
72 Z = -2692658
31
XDOT = 15471
853245 XDOT = 4655
548204
YDOT = 10228
530166 feet/sec YDOT = 3170
053858 meter/sec
ZDOT = 16925
333307 ZDOT = 5181
604134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18310737
48 X = -5581112
79
Y = -9226358
30 feet Y = -2812194
01 meter
Z = -8810604
88 Z = -2685472
37
XDOT = 431
354421 XDOT = 131
476827
YDOT = -17092
075748 feet/sec YDOT = -5209
664688 meter/sec
ZDOT = 17020
072332 ZDOT = 5187
718047
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
53722456
00016717 00000-0 10270-3 0 9018
2 25544 51
6498 347
6428 0005404 172
5245 187
5987 15
49763732 38483
Satellite: ISS
Catalog Number: 25544
Epoch time: 13192
53722456 = yrday
fracday
Element set: 901
Inclination: 51
6498 deg
RA of node: 347
6428 deg
Eccentricity:
0005404
Arg of perigee: 172
5245 deg
Mean anomaly: 187
5987 deg
Mean motion: 15
49763732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3848
Checksum: 345
Coasting Arc #3 (Orbit 3863)
---------------------------------------
Vector Time (GMT): 2013/193/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5122681
44 A = 6799553
36 meter
Y = 3709402
86 meter E =
0016282
Z = 2469958
27 I = 51
55560
XDOT = -4688
346487 Wp = 123
37003
YDOT = -2923
845513 meter/sec RA = 342
15170 deg
ZDOT = -5315
963452 TA = 28
95461
MA = 28
86438
Ha = 228
870 n
mi
Hp = 221
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16806697
63 X = -5175778
28
Y = 12169956
89 feet Y = 3651820
75 meter
Z = 8103537
62 Z = 2444944
36
XDOT = -15381
714195 XDOT = -4629
479805
YDOT = -9592
669007 feet/sec YDOT = -2975
944071 meter/sec
ZDOT = -17440
824974 ZDOT = -5338
595921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19143721
76 X = 5835006
39
Y = 8110830
54 feet Y = 2472181
15 meter
Z = 7998287
50 Z = 2437878
03
XDOT = 299
884092 XDOT = 91
404671
YDOT = 16638
313537 feet/sec YDOT = 5071
357966 meter/sec
ZDOT = -17535
049778 ZDOT = -5344
683172
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
56895407
00016717 00000-0 10270-3 0 9020
2 25544 51
6494 342
5335 0005385 176
7439 183
3747 15
49759773 38645
Satellite: ISS
Catalog Number: 25544
Epoch time: 13193
56895407 = yrday
fracday
Element set: 902
Inclination: 51
6494 deg
RA of node: 342
5335 deg
Eccentricity:
0005385
Arg of perigee: 176
7439 deg
Mean anomaly: 183
3747 deg
Mean motion: 15
49759773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3864
Checksum: 359
Coasting Arc #4 (Orbit 3878)
---------------------------------------
Vector Time (GMT): 2013/194/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4997253
97 A = 6799918
68 meter
Y = -4033129
40 meter E =
0004224
Z = -2241132
66 I = 51
52949
XDOT = 4642
000875 Wp = 100
22564
YDOT = 2734
820217 meter/sec RA = 337
19364 deg
ZDOT = 5437
146653 TA = 234
88554
MA = 234
92514
Ha = 228
670 n
mi
Hp = 221
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16395190
18 X = 5052868
58
Y = -13232051
83 feet Y = -3976935
86 meter
Z = -7352797
45 Z = -2216721
86
XDOT = 15229
661664 XDOT = 4584
662619
YDOT = 8972
507275 feet/sec YDOT = 2786
409102 meter/sec
ZDOT = 17838
407654 ZDOT = 5459
557716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19957423
74 X = -6083022
76
Y = -6862319
71 feet Y = -2091635
05 meter
Z = -7250027
08 Z = -2209808
25
XDOT = -961
555613 XDOT = -293
082151
YDOT = -16120
162179 feet/sec YDOT = -4913
425432 meter/sec
ZDOT = 17931
734361 ZDOT = 5465
592633
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
53619176
00016717 00000-0 10270-3 0 9036
2 25544 51
6506 337
7443 0005257 180
1388 179
9762 15
49785910 38791
Satellite: ISS
Catalog Number: 25544
Epoch time: 13194
53619176 = yrday
fracday
Element set: 903
Inclination: 51
6506 deg
RA of node: 337
7443 deg
Eccentricity:
0005257
Arg of perigee: 180
1388 deg
Mean anomaly: 179
9762 deg
Mean motion: 15
49785910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3879
Checksum: 351
Coasting Arc #5 (Orbit 3894)
---------------------------------------
Vector Time (GMT): 2013/195/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4848054
62 A = 6800384
62 meter
Y = 4326072
85 meter E =
0016366
Z = 1973182
70 I = 51
50287
XDOT = -4587
528880 Wp = 129
90976
YDOT = -2591
224232 meter/sec RA = 332
23348 deg
ZDOT = -5569
901829 TA = 28
29581
MA = 28
20701
Ha = 228
590 n
mi
Hp = 221
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15905691
01 X = -4905654
50
Y = 14193152
41 feet Y = 4271536
68 meter
Z = 6473696
54 Z = 1949491
79
XDOT = -15050
947770 XDOT = -4531
155421
YDOT = -8501
391836 feet/sec YDOT = -2642
209379 meter/sec
ZDOT = -18273
956131 ZDOT = -5592
050677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20605985
07 X = 6280704
25
Y = 5577823
65 feet Y = 1700120
65 meter
Z = 6373899
21 Z = 1942764
48
XDOT = 1465
133683 XDOT = 446
572747
YDOT = 15652
691409 feet/sec YDOT = 4770
940342 meter/sec
ZDOT = -18366
206187 ZDOT = -5598
019646
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
56790412
00016717 00000-0 10270-3 0 9044
2 25544 51
6504 332
6352 0005282 184
2027 175
9080 15
49789022 38950
Satellite: ISS
Catalog Number: 25544
Epoch time: 13195
56790412 = yrday
fracday
Element set: 904
Inclination: 51
6504 deg
RA of node: 332
6352 deg
Eccentricity:
0005282
Arg of perigee: 184
2027 deg
Mean anomaly: 175
9080 deg
Mean motion: 15
49789022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3895
Checksum: 318
Coasting Arc #6 (Orbit 3909)
---------------------------------------
Vector Time (GMT): 2013/196/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4669999
60 A = 6800706
19 meter
Y = -4633462
27 meter E =
0004162
Z = -1724750
60 I = 51
47820
XDOT = 4524
062023 Wp = 75
62249
YDOT = 2454
959923 meter/sec RA = 327
27163 deg
ZDOT = 5666
908386 TA = 265
46346
MA = 265
51100
Ha = 228
398 n
mi
Hp = 221
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15321521
01 X = 4729843
23
Y = -15201647
86 feet Y = -4580904
67 meter
Z = -5658630
57 Z = -1701919
17
XDOT = 14842
723173 XDOT = 4468
745700
YDOT = 8054
330456 feet/sec YDOT = 2505
241219 meter/sec
ZDOT = 18592
219115 ZDOT = 5688
751565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21202381
43 X = -6462485
86
Y = -4168702
17 feet Y = -1270620
42 meter
Z = -5562386
87 Z = -1695415
52
XDOT = -1909
157035 XDOT = -581
911064
YDOT = -15163
487683 feet/sec YDOT = -4621
831046 meter/sec
ZDOT = 18683
209575 ZDOT = 5694
642279
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
53512566
00016717 00000-0 10270-3 0 9055
2 25544 51
6511 327
8457 0005081 187
9809 172
1261 15
49805729 39106
Satellite: ISS
Catalog Number: 25544
Epoch time: 13196
53512566 = yrday
fracday
Element set: 905
Inclination: 51
6511 deg
RA of node: 327
8457 deg
Eccentricity:
0005081
Arg of perigee: 187
9809 deg
Mean anomaly: 172
1261 deg
Mean motion: 15
49805729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3910
Checksum: 325
Coasting Arc #7 (Orbit 3925)
---------------------------------------
Vector Time (GMT): 2013/197/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4472303
09 A = 6801059
54 meter
Y = 4904159
72 meter E =
0016143
Z = 1438706
60 I = 51
45396
XDOT = -4458
776324 Wp = 136
64793
YDOT = -2365
273041 meter/sec RA = 322
30820 deg
ZDOT = -5770
732014 TA = 27
63640
MA = 27
55068
Ha = 228
298 n
mi
Hp = 221
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14672910
39 X = -4533798
91
Y = 16089762
85 feet Y = 4853803
65 meter
Z = 4720165
99 Z = 1416831
57
XDOT = -14628
531246 XDOT = -4403
963343
YDOT = -7760
082156 feet/sec YDOT = -2414
827005 meter/sec
ZDOT = -18932
847816 ZDOT = -5792
259340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21620273
39 X = 6589859
33
Y = 2757025
58 feet Y = 840341
40 meter
Z = 4627885
42 Z = 1410579
48
XDOT = 2209
435566 XDOT = 673
435960
YDOT = 14756
681334 feet/sec YDOT = 4497
836470 meter/sec
ZDOT = -19022
529463 ZDOT = -5798
066980
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
56682090
00016717 00000-0 10270-3 0 9060
2 25544 51
6509 322
7367 0005157 191
6777 168
4255 15
49815978 39262
Satellite: ISS
Catalog Number: 25544
Epoch time: 13197
56682090 = yrday
fracday
Element set: 906
Inclination: 51
6509 deg
RA of node: 322
7367 deg
Eccentricity:
0005157
Arg of perigee: 191
6777 deg
Mean anomaly: 168
4255 deg
Mean motion: 15
49815978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3926
Checksum: 356
Coasting Arc #8 (Orbit 3940)
---------------------------------------
Vector Time (GMT): 2013/198/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4244234
86 A = 6801306
63 meter
Y = -5182114
69 meter E =
0005126
Z = -1172691
35 I = 51
43179
XDOT = 4394
575676 Wp = 59
19533
YDOT = 2282
615216 meter/sec RA = 317
34267 deg
ZDOT = 5839
735624 TA = 288
06271
MA = 288
11855
Ha = 228
118 n
mi
Hp = 221
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13924655
05 X = 4307563
56
Y = -17001688
62 feet Y = -5134298
78 meter
Z = -3847412
57 Z = -1151919
91
XDOT = 14417
899201 XDOT = 4340
356548
YDOT = 7488
895065 feet/sec YDOT = 2331
454455 meter/sec
ZDOT = 19159
237610 ZDOT = 5860
952560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21956483
32 X = -6692336
12
Y = -1238327
29 feet Y = -377442
16 meter
Z = -3759707
88 Z = -1145958
96
XDOT = -2473
301733 XDOT = -753
862368
YDOT = -14364
046703 feet/sec YDOT = -4378
161435 meter/sec
ZDOT = 19247
633650 ZDOT = 5866
678737
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
53402648
00016717 00000-0 10270-3 0 9078
2 25544 51
6515 317
9467 0004909 195
8866 164
2132 15
49825395 39414
Satellite: ISS
Catalog Number: 25544
Epoch time: 13198
53402648 = yrday
fracday
Element set: 907
Inclination: 51
6515 deg
RA of node: 317
9467 deg
Eccentricity:
0004909
Arg of perigee: 195
8866 deg
Mean anomaly: 164
2132 deg
Mean motion: 15
49825395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 346
Coasting Arc #9 (Orbit 3956)
---------------------------------------
Vector Time (GMT): 2013/199/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4002338
25 A = 6801527
15 meter
Y = 5418032
04 meter E =
0015573
Z = 871027
50 I = 51
41040
XDOT = -4335
351429 Wp = 143
52573
YDOT = -2245
626987 meter/sec RA = 312
37631 deg
ZDOT = -5910
104937 TA = 27
03114
MA = 26
95012
Ha = 228
004 n
mi
Hp = 221
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13131031
02 X = -4066857
60
Y = 17775695
68 feet Y = 5372914
52 meter
Z = 2857701
77 Z = 851428
44
XDOT = -14223
593928 XDOT = -4281
208522
YDOT = -7367
542607 feet/sec YDOT = -2293
804247 meter/sec
ZDOT = -19390
108060 ZDOT = -5931
034363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22108962
69 X = 6738811
83
Y = -244291
58 feet Y = -74460
07 meter
Z = 2774866
18 Z = 845779
21
XDOT = 2618
066331 XDOT = 797
986618
YDOT = 14080
276531 feet/sec YDOT = 4291
668287 meter/sec
ZDOT = -19477
309059 ZDOT = -5936
683801
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
56570496
00016717 00000-0 10270-3 0 9080
2 25544 51
6512 312
8378 0005017 199
1109 160
9854 15
49839902 39574
Satellite: ISS
Catalog Number: 25544
Epoch time: 13199
56570496 = yrday
fracday
Element set: 908
Inclination: 51
6512 deg
RA of node: 312
8378 deg
Eccentricity:
0005017
Arg of perigee: 199
1109 deg
Mean anomaly: 160
9854 deg
Mean motion: 15
49839902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3957
Checksum: 348
Coasting Arc #10 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2013/200/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3730643
84 A = 6801664
62 meter
Y = -5653905
04 meter E =
0006456
Z = -590189
30 I = 51
39168
XDOT = 4286
526445 Wp = 53
53444
YDOT = 2212
722243 meter/sec RA = 307
40776 deg
ZDOT = 5947
346704 TA = 300
08812
MA = 300
15212
Ha = 227
833 n
mi
Hp = 221
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12239645
13 X = 3796456
72
Y = -18549557
23 feet Y = -5611818
57 meter
Z = -1936316
59 Z = -571907
13
XDOT = 14063
406971 XDOT = 4232
574310
YDOT = 7259
587413 feet/sec YDOT = 2260
354487 meter/sec
ZDOT = 19512
292335 ZDOT = 5968
039360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22156711
31 X = -6753365
61
Y = 1807965
39 feet Y = 551067
85 meter
Z = -1858954
92 Z = -566609
46
XDOT = -2759
187977 XDOT = -841
000495
YDOT = -13835
872038 feet/sec YDOT = -4217
173797 meter/sec
ZDOT = 19598
512229 ZDOT = 5973
626528
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
53289492
00016717 00000-0 10270-3 0 9094
2 25544 51
6519 308
0477 0004761 203
8666 156
2265 15
49846267 39727
Satellite: ISS
Catalog Number: 25544
Epoch time: 13200
53289492 = yrday
fracday
Element set: 909
Inclination: 51
6519 deg
RA of node: 308
0477 deg
Eccentricity:
0004761
Arg of perigee: 203
8666 deg
Mean anomaly: 156
2265 deg
Mean motion: 15
49846267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 335
Coasting Arc #11 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2013/201/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3452451
01 A = 6801731
02 meter
Y = 5843546
42 meter E =
0014594
Z = 276256
40 I = 51
37350
XDOT = -4249
435529 Wp = 150
48683
YDOT = -2222
118744 meter/sec RA = 302
43897 deg
ZDOT = -5980
016429 TA = 26
52917
MA = 26
45454
Ha = 227
699 n
mi
Hp = 222
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11326939
01 X = -3518880
18
Y = 19171740
22 feet Y = 5804567
47 meter
Z = 906353
01 Z = 259324
30
XDOT = -13941
717616 XDOT = -4195
222533
YDOT = -7290
415828 feet/sec YDOT = -2269
334725 meter/sec
ZDOT = -19619
476472 ZDOT = -6000
528170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22025595
57 X = 6713401
53
Y = -3294420
56 feet Y = -1004139
39 meter
Z = 834613
18 Z = 254390
10
XDOT = 2815
060449 XDOT = 858
030425
YDOT = 13717
896862 feet/sec YDOT = 4181
214963 meter/sec
ZDOT = -19704
944512 ZDOT = -6006
067087
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
56455720
00016717 00000-0 10270-3 0 9109
2 25544 51
6512 302
9389 0004857 206
7756 153
3144 15
49863744 39883
Satellite: ISS
Catalog Number: 25544
Epoch time: 13201
56455720 = yrday
fracday
Element set: 910
Inclination: 51
6512 deg
RA of node: 302
9389 deg
Eccentricity:
0004857
Arg of perigee: 206
7756 deg
Mean anomaly: 153
3144 deg
Mean motion: 15
49863744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 326
Coasting Arc #12 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2013/202/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3147236
20 A = 6801738
57 meter
Y = -6026283
09 meter E =
0007732
Z = 15993
82 I = 51
35852
XDOT = 4230
450262 Wp = 54
04203
YDOT = 2230
628940 meter/sec RA = 297
46813 deg
ZDOT = 5981
960001 TA = 306
13054
MA = 306
20207
Ha = 227
542 n
mi
Hp = 222
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10325578
07 X = 3214311
80
Y = -19771269
98 feet Y = -5990713
67 meter
Z = 52473
16 Z = 31444
74
XDOT = 13879
429995 XDOT = 4176
134240
YDOT = 7318
336416 feet/sec YDOT = 2277
632092 meter/sec
ZDOT = 19625
853023 ZDOT = 6002
379129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21775801
91 X = -6637264
42
Y = 4829487
64 feet Y = 1472027
83 meter
Z = 118038
15 Z = 35978
03
XDOT = -2904
765790 XDOT = -885
372613
YDOT = -13651
569032 feet/sec YDOT = -4160
998241 meter/sec
ZDOT = 19710
940325 ZDOT = 6007
894611
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
59621098
00016717 00000-0 10270-3 0 9117
2 25544 51
6518 297
8294 0004631 212
2460 147
8408 15
49868303 40047
Satellite: ISS
Catalog Number: 25544
Epoch time: 13202
59621098 = yrday
fracday
Element set: 911
Inclination: 51
6518 deg
RA of node: 297
8294 deg
Eccentricity:
0004631
Arg of perigee: 212
2460 deg
Mean anomaly: 147
8408 deg
Mean motion: 15
49868303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 308
Coasting Arc #13 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2013/203/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2844107
25 A = 6801622
89 meter
Y = 6160321
72 meter E =
0013162
Z = -338167
81 I = 51
34394
XDOT = -4229
090002 Wp = 157
42009
YDOT = -2275
477866 meter/sec RA = 292
49714 deg
ZDOT = -5973
218482 TA = 26
23459
MA = 26
16798
Ha = 227
374 n
mi
Hp = 222
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9331060
52 X = -2911139
23
Y = 20211029
28 feet Y = 6128142
36 meter
Z = -1109474
46 Z = -352146
13
XDOT = -13874
967197 XDOT = -4174
315162
YDOT = -7465
478562 feet/sec YDOT = -2322
463365 meter/sec
ZDOT = -19597
173496 ZDOT = -5993
629754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21363399
87 X = 6511564
28
Y = -6246933
07 feet Y = -1904065
20 meter
Z = -1168889
06 Z = -356277
39
XDOT = 2949
305526 XDOT = 898
948324
YDOT = 13716
782162 feet/sec YDOT = 4180
875203 meter/sec
ZDOT = -19682
229777 ZDOT = -5999
143636
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
56337844
00016717 00000-0 10270-3 0 9129
2 25544 51
6507 293
0400 0004669 214
9264 145
1581 15
49891239 40197
Satellite: ISS
Catalog Number: 25544
Epoch time: 13203
56337844 = yrday
fracday
Element set: 912
Inclination: 51
6507 deg
RA of node: 293
0400 deg
Eccentricity:
0004669
Arg of perigee: 214
9264 deg
Mean anomaly: 145
1581 deg
Mean motion: 15
49891239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 310
Coasting Arc #14 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2013/204/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2518731
42 A = 6801501
43 meter
Y = -6281591
88 meter E =
0008788
Z = 637816
09 I = 51
33274
XDOT = 4251
426885 Wp = 57
89250
YDOT = 2313
149739 meter/sec RA = 287
52426 deg
ZDOT = 5936
702402 TA = 309
00944
MA = 309
08766
Ha = 227
247 n
mi
Hp = 222
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8263554
52 X = 2585688
08
Y = -20608897
23 feet Y = -6253051
50 meter
Z = 2092572
46 Z = 650213
73
XDOT = 13948
250934 XDOT = 4196
406563
YDOT = 7589
073948 feet/sec YDOT = 2360
383812 meter/sec
ZDOT = 19477
370085 ZDOT = 5957
221491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20829092
78 X = -6348707
48
Y = 7677113
97 feet Y = 2339984
34 meter
Z = 2145379
37 Z = 653911
63
XDOT = -3065
065987 XDOT = -934
232113
YDOT = -13832
652271 feet/sec YDOT = -4216
192412 meter/sec
ZDOT = 19562
880121 ZDOT = 5962
765861
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
59501659
00016717 00000-0 10270-3 0 9131
2 25544 51
6508 287
9305 0004482 220
4675 139
6143 15
49888492 40352
Satellite: ISS
Catalog Number: 25544
Epoch time: 13204
59501659 = yrday
fracday
Element set: 913
Inclination: 51
6508 deg
RA of node: 287
9305 deg
Eccentricity:
0004482
Arg of perigee: 220
4675 deg
Mean anomaly: 139
6143 deg
Mean motion: 15
49888492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 327
Coasting Arc #15 (Orbit 4049)
---------------------------------------
Vector Time (GMT): 2013/205/12:45:47
379
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2204902
16 A = 6801180
06 meter
Y = 6353907
19 meter E =
0011293
Z = -963714
47 I = 51
32268
XDOT = -4295
486945 Wp = 164
09295
YDOT = -2378
865550 meter/sec RA = 282
55099 deg
ZDOT = -5883
545069 TA = 26
37528
MA = 26
31784
Ha = 227
045 n
mi
Hp = 222
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7233930
96 X = -2271107
70
Y = 20846152
20 feet Y = 6328880
45 meter
Z = -3161792
88 Z = -974585
95
XDOT = -14092
804938 XDOT = -4239
986687
YDOT = -7804
677002 feet/sec YDOT = -2426
589801 meter/sec
ZDOT = -19302
969387 ZDOT = -5904
276993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20160118
76 X = 6144804
20
Y = -8953532
57 feet Y = -2729036
73 meter
Z = -3208211
17 Z = -977862
77
XDOT = 3177
328231 XDOT = 968
449645
YDOT = 14070
381124 feet/sec YDOT = 4288
652167 meter/sec
ZDOT = -19389
367540 ZDOT = -5909
879226
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
56216928
00016717 00000-0 10270-3 0 9142
2 25544 51
6498 283
1405 0004457 223
4191 136
6609 15
49922465 40507
Satellite: ISS
Catalog Number: 25544
Epoch time: 13205
56216928 = yrday
fracday
Element set: 914
Inclination: 51
6498 deg
RA of node: 283
1405 deg
Eccentricity:
0004457
Arg of perigee: 223
4191 deg
Mean anomaly: 136
6609 deg
Mean motion: 15
49922465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4050
Checksum: 313
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