[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 17th 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) : 120 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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 884)
---------------------------------------
Vector Time (GMT): 2013/259/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6632932
02 A = 6800121
47 meter
Y = -1176692
40 meter E =
0014175
Z = 887268
97 I = 51
76750
XDOT = 56
991888 Wp = 114
75148
YDOT = -4847
353883 meter/sec RA = 16
01584 deg
ZDOT = -5933
846986 TA = 55
67921
MA = 55
54513
Ha = 227
818 n
mi
Hp = 219
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21761587
98 X = -6623591
08
Y = -3860539
38 feet Y = -1250813
74 meter
Z = 2910987
42 Z = 855069
88
XDOT = 186
981259 XDOT = 140
016595
YDOT = -15903
392004 feet/sec YDOT = -4846
252945 meter/sec
ZDOT = -19468
001922 ZDOT = -5933
367976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7992259
16 X = 2436040
59
Y = 20624297
51 feet Y = 6286285
88 meter
Z = 2776052
84 Z = 846140
91
XDOT = -12255
369932 XDOT = -3735
436755
YDOT = 7400
990092 feet/sec YDOT = 2255
821780 meter/sec
ZDOT = -19465
254720 ZDOT = -5933
009639
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 13259
38557687
00016717 00000-0 10270-3 0 9006
2 25544 51
6470 16
4027 0002690 48
1832 311
9548 15
50320034 8853
Satellite: ISS
Catalog Number: 25544
Epoch time: 13259
38557687 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 16
4027 deg
Eccentricity:
0002690
Arg of perigee: 48
1832 deg
Mean anomaly: 311
9548 deg
Mean motion: 15
50320034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 885
Checksum: 303
Coasting Arc #2 (Orbit 899)
---------------------------------------
Vector Time (GMT): 2013/260/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6713516
90 A = 6800421
84 meter
Y = 930500
89 meter E =
0013721
Z = -476479
48 I = 51
73891
XDOT = -243
710349 Wp = 44
92126
YDOT = 4768
524818 meter/sec RA = 11
06927 deg
ZDOT = 5993
279212 TA = 309
95467
MA = 310
07512
Ha = 227
952 n
mi
Hp = 219
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22025974
09 X = 6704927
47
Y = 3052824
44 feet Y = 1005527
62 meter
Z = -1563252
90 Z = -443887
04
XDOT = -799
574636 XDOT = -326
128449
YDOT = 15644
766463 feet/sec YDOT = 4765
339395 meter/sec
ZDOT = 19662
989542 ZDOT = 5991
894531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9165588
55 X = -2793671
39
Y = -20269773
66 feet Y = -6178227
01 meter
Z = -1426637
21 Z = -434839
02
XDOT = 12250
311397 XDOT = 3733
894914
YDOT = -6893
763936 feet/sec YDOT = -2101
219248 meter/sec
ZDOT = 19656
455637 ZDOT = 5991
287678
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 13260
35250469
00016717 00000-0 10270-3 0 9014
2 25544 51
6474 11
6102 0002656 59
3231 300
8181 15
50292356 9000
Satellite: ISS
Catalog Number: 25544
Epoch time: 13260
35250469 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 11
6102 deg
Eccentricity:
0002656
Arg of perigee: 59
3231 deg
Mean anomaly: 300
8181 deg
Mean motion: 15
50292356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 900
Checksum: 268
Coasting Arc #3 (Orbit 915)
---------------------------------------
Vector Time (GMT): 2013/261/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6757854
53 A = 6800363
23 meter
Y = -715712
72 meter E =
0012922
Z = 11394
90 I = 51
70881
XDOT = 481
650965 Wp = 122
18561
YDOT = -4722
942530 meter/sec RA = 6
12141 deg
ZDOT = -6013
118868 TA = 57
69198
MA = 57
56689
Ha = 227
859 n
mi
Hp = 219
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22171438
74 X = -6749404
36
Y = -2348138
85 feet Y = -791236
10 meter
Z = 37384
83 Z = -21413
41
XDOT = 1580
219703 XDOT = 563
638153
YDOT = -15495
218275 feet/sec YDOT = -4717
098801 meter/sec
ZDOT = -19728
080276 ZDOT = -6010
579278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10176896
27 X = 3101917
98
Y = 19837051
19 feet Y = 6046333
20 meter
Z = -100159
96 Z = -30528
76
XDOT = -12452
346473 XDOT = -3795
475205
YDOT = 6319
642024 feet/sec YDOT = 1926
226889 meter/sec
ZDOT = -19716
709085 ZDOT = -6009
652929
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 13261
38388242
00016717 00000-0 10270-3 0 9020
2 25544 51
6474 6
4983 0002759 57
6931 302
4487 15
50339698 9166
Satellite: ISS
Catalog Number: 25544
Epoch time: 13261
38388242 = yrday
fracday
Element set: 902
Inclination: 51
6474 deg
RA of node: 6
4983 deg
Eccentricity:
0002759
Arg of perigee: 57
6931 deg
Mean anomaly: 302
4487 deg
Mean motion: 15
50339698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 916
Checksum: 330
Coasting Arc #4 (Orbit 931)
---------------------------------------
Vector Time (GMT): 2013/262/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6764979
37 A = 6800315
61 meter
Y = 463341
92 meter E =
0015478
Z = 411127
93 I = 51
67894
XDOT = -696
727291 Wp = 52
54636
YDOT = 4724
335851 meter/sec RA = 1
17150 deg
ZDOT = 5994
301327 TA = 311
87781
MA = 312
00977
Ha = 227
941 n
mi
Hp = 219
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22194814
22 X = 6757298
24
Y = 1520150
66 feet Y = 538949
33 meter
Z = 1348844
91 Z = 443972
90
XDOT = -2285
850693 XDOT = -778
622800
YDOT = 15499
789538 feet/sec YDOT = 4716
087549 meter/sec
ZDOT = 19666
342937 ZDOT = 5990
717095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11209716
61 X = -3416721
62
Y = -19206050
57 feet Y = -5854004
21 meter
Z = 1486571
15 Z = 453106
89
XDOT = 12774
908821 XDOT = 3893
792209
YDOT = -5901
574481 feet/sec YDOT = -1798
799902 meter/sec
ZDOT = 19650
589910 ZDOT = 5989
499805
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 13262
41525299
00016717 00000-0 10270-3 0 9031
2 25544 51
6485 1
3869 0002727 67
7220 292
4220 15
50328054 9328
Satellite: ISS
Catalog Number: 25544
Epoch time: 13262
41525299 = yrday
fracday
Element set: 903
Inclination: 51
6485 deg
RA of node: 1
3869 deg
Eccentricity:
0002727
Arg of perigee: 67
7220 deg
Mean anomaly: 292
4220 deg
Mean motion: 15
50328054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 932
Checksum: 293
Coasting Arc #5 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2013/263/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6734262
22 A = 6799958
87 meter
Y = -254602
11 meter E =
0011025
Z = -882244
34 I = 51
64689
XDOT = 948
642141 Wp = 126
28116
YDOT = -4761
226478 meter/sec RA = 356
21936 deg
ZDOT = -5925
134893 TA = 63
24674
MA = 63
13396
Ha = 227
890 n
mi
Hp = 219
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22094036
15 X = -6726628
96
Y = -835308
77 feet Y = -329866
36 meter
Z = -2894502
44 Z = -914940
39
XDOT = 3112
342982 XDOT = 1030
595586
YDOT = -15620
821777 feet/sec YDOT = -4750
160761 meter/sec
ZDOT = -19439
418939 ZDOT = -5920
326719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12034526
69 X = 3668123
74
Y = 18525704
77 feet Y = 5646634
81 meter
Z = -3031624
75 Z = -924039
22
XDOT = -13281
074615 XDOT = -4048
071543
YDOT = 5479
586335 feet/sec YDOT = 1670
177915 meter/sec
ZDOT = -19418
526282 ZDOT = -5918
766811
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 13263
38215336
00016717 00000-0 10270-3 0 9047
2 25544 51
6481 356
5946 0002808 66
6413 293
5033 15
50354099 9475
Satellite: ISS
Catalog Number: 25544
Epoch time: 13263
38215336 = yrday
fracday
Element set: 904
Inclination: 51
6481 deg
RA of node: 356
5946 deg
Eccentricity:
0002808
Arg of perigee: 66
6413 deg
Mean anomaly: 293
5033 deg
Mean motion: 15
50354099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 947
Checksum: 316
Coasting Arc #6 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2013/264/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6665473
99 A = 6799534
48 meter
Y = 21439
22 meter E =
0016473
Z = 1304611
56 I = 51
61607
XDOT = -1164
876655 Wp = 61
85474
YDOT = 4845
989509 meter/sec RA = 351
26512 deg
ZDOT = 5823
365015 TA = 312
32962
MA = 312
46906
Ha = 227
896 n
mi
Hp = 219
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21868352
97 X = 6658401
34
Y = 70338
66 feet Y = 95937
42 meter
Z = 4280221
65 Z = 1336974
95
XDOT = -3821
773801 XDOT = -1247
267594
YDOT = 15898
915713 feet/sec YDOT = 4832
503210 meter/sec
ZDOT = 19105
528264 ZDOT = 5817
505334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12830688
69 X = -3910793
91
Y = -17675483
23 feet Y = -5387487
29 meter
Z = 4415974
07 Z = 1345988
90
XDOT = 13873
436676 XDOT = 4228
623499
YDOT = -5265
277915 feet/sec YDOT = -1604
856708 meter/sec
ZDOT = 19080
211948 ZDOT = 5815
648602
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 13264
41350491
00016717 00000-0 10270-3 0 9055
2 25544 51
6493 351
4835 0002767 74
4897 285
6559 15
50363965 9631
Satellite: ISS
Catalog Number: 25544
Epoch time: 13264
41350491 = yrday
fracday
Element set: 905
Inclination: 51
6493 deg
RA of node: 351
4835 deg
Eccentricity:
0002767
Arg of perigee: 74
4897 deg
Mean anomaly: 285
6559 deg
Mean motion: 15
50363965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 963
Checksum: 340
Coasting Arc #7 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2013/265/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6561704
87 A = 6798899
21 meter
Y = 155753
20 meter E =
0008825
Z = -1767624
81 I = 51
58326
XDOT = 1400
700804 Wp = 123
74539
YDOT = -4963
015376 meter/sec RA = 346
30801 deg
ZDOT = -5662
111482 TA = 75
63847
MA = 75
54051
Ha = 227
898 n
mi
Hp = 219
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21527903
10 X = -6554372
11
Y = 511001
31 feet Y = 82416
84 meter
Z = -5799294
01 Z = -1799483
55
XDOT = 4595
475078 XDOT = 1483
599547
YDOT = -16282
858845 feet/sec YDOT = -4946
889000 meter/sec
ZDOT = -18576
481239 ZDOT = -5655
104985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13384839
64 X = 4079699
12
Y = 16822298
76 feet Y = 5127436
66 meter
Z = -5932948
47 Z = -1808362
69
XDOT = -14597
968257 XDOT = -4449
460725
YDOT = 5102
511718 feet/sec YDOT = 1555
245572 meter/sec
ZDOT = -18546
336653 ZDOT = -5652
923412
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 13265
38038915
00016717 00000-0 10270-3 0 9067
2 25544 51
6487 346
6911 0002826 74
4222 285
7240 15
50367500 9786
Satellite: ISS
Catalog Number: 25544
Epoch time: 13265
38038915 = yrday
fracday
Element set: 906
Inclination: 51
6487 deg
RA of node: 346
6911 deg
Eccentricity:
0002826
Arg of perigee: 74
4222 deg
Mean anomaly: 285
7240 deg
Mean motion: 15
50367500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 978
Checksum: 317
Coasting Arc #8 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2013/266/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6423102
01 A = 6798128
50 meter
Y = -344219
34 meter E =
0016617
Z = 2176507
12 I = 51
55230
XDOT = -1590
562819 Wp = 72
26574
YDOT = 5124
525191 meter/sec RA = 341
34857 deg
ZDOT = 5474
821621 TA = 311
89231
MA = 312
03394
Ha = 227
839 n
mi
Hp = 219
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21073169
32 X = 6415900
76
Y = -1129328
53 feet Y = -272432
17 meter
Z = 7140771
39 Z = 2207692
87
XDOT = -5218
381953 XDOT = -1674
343684
YDOT = 16812
746688 feet/sec YDOT = 5106
270613 meter/sec
ZDOT = 17962
013191 ZDOT = 5466
890701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13872578
34 X = -4228361
88
Y = -15843594
76 feet Y = -4829127
68 meter
Z = 7271625
67 Z = 2216391
50
XDOT = 15361
474954 XDOT = 4682
177566
YDOT = -5178
463042 feet/sec YDOT = -1578
395535 meter/sec
ZDOT = 17927
966807 ZDOT = 5464
444283
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 13266
41172182
00016717 00000-0 10270-3 0 9078
2 25544 51
6497 341
5797 0002796 80
0245 280
1222 15
50397144 9941
Satellite: ISS
Catalog Number: 25544
Epoch time: 13266
41172182 = yrday
fracday
Element set: 907
Inclination: 51
6497 deg
RA of node: 341
5797 deg
Eccentricity:
0002796
Arg of perigee: 80
0245 deg
Mean anomaly: 280
1222 deg
Mean motion: 15
50397144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 994
Checksum: 313
Coasting Arc #9 (Orbit 1008)
---------------------------------------
Vector Time (GMT): 2013/267/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6257209
26 A = 6797258
01 meter
Y = 465929
24 meter E =
0007265
Z = -2616224
97 I = 51
52019
XDOT = 1782
011259 Wp = 109
39122
YDOT = -5308
907555 meter/sec RA = 336
38619 deg
ZDOT = -5221
734307 TA = 100
05522
MA = 99
97324
Ha = 227
889 n
mi
Hp = 219
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20528901
79 X = -6249245
29
Y = 1528639
25 feet Y = 396001
46 meter
Z = -8583415
24 Z = -2646602
94
XDOT = 5846
493631 XDOT = 1866
610227
YDOT = -17417
675705 feet/sec YDOT = -5288
507406 meter/sec
ZDOT = -17131
674236 ZDOT = -5212
871417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14103734
32 X = 4298818
22
Y = 14921546
14 feet Y = 4548087
26 meter
Z = -8710895
64 Z = -2655080
99
XDOT = -16182
105238 XDOT = -4932
305677
YDOT = 5343
118245 feet/sec YDOT = 1628
582441 meter/sec
ZDOT = -17093
691775 ZDOT = -5210
157253
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 13267
37858966
00016717 00000-0 10270-3 0 9086
2 25544 51
6494 336
7872 0002830 81
0656 279
0815 15
50384054 10093
Satellite: ISS
Catalog Number: 25544
Epoch time: 13267
37858966 = yrday
fracday
Element set: 908
Inclination: 51
6494 deg
RA of node: 336
7872 deg
Eccentricity:
0002830
Arg of perigee: 81
0656 deg
Mean anomaly: 279
0815 deg
Mean motion: 15
50384054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1009
Checksum: 333
Coasting Arc #10 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2013/268/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6063390
01 A = 6796225
88 meter
Y = -587200
90 meter E =
0015909
Z = 2997126
55 I = 51
49009
XDOT = -1920
969039 Wp = 83
38669
YDOT = 5530
826293 meter/sec RA = 331
42120 deg
ZDOT = 4949
015216 TA = 310
95767
MA = 311
09523
Ha = 227
786 n
mi
Hp = 219
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19893011
83 X = 6054946
21
Y = -1926512
15 feet Y = -519443
20 meter
Z = 9833092
36 Z = 3026561
74
XDOT = -6302
391859 XDOT = -2006
714367
YDOT = 18145
755554 feet/sec YDOT = 5508
865754 meter/sec
ZDOT = 16236
926562 ZDOT = 4939
474536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14247949
39 X = -4342774
97
Y = -13928189
14 feet Y = -4245312
05 meter
Z = 9956633
95 Z = 3034782
03
XDOT = 16989
323117 XDOT = 5178
345686
YDOT = -5753
246308 feet/sec YDOT = -1753
589475 meter/sec
ZDOT = 16196
069705 ZDOT = 4936
562046
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 13268
40990395
00016717 00000-0 10270-3 0 9095
2 25544 51
6502 331
6755 0002838 84
8922 275
2553 15
50426457 10251
Satellite: ISS
Catalog Number: 25544
Epoch time: 13268
40990395 = yrday
fracday
Element set: 909
Inclination: 51
6502 deg
RA of node: 331
6755 deg
Eccentricity:
0002838
Arg of perigee: 84
8922 deg
Mean anomaly: 275
2553 deg
Mean motion: 15
50426457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1025
Checksum: 320
Coasting Arc #11 (Orbit 1039)
---------------------------------------
Vector Time (GMT): 2013/269/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5854452
89 A = 6795201
51 meter
Y = 634216
88 meter E =
0007735
Z = -3397856
02 I = 51
45994
XDOT = 2045
287912 Wp = 87
99931
YDOT = -5760
354975 meter/sec RA = 326
45364 deg
ZDOT = -4608
029028 TA = 131
71533
MA = 131
64915
Ha = 227
870 n
mi
Hp = 219
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19207522
61 X = -5844603
75
Y = 2080764
03 feet Y = 568803
47 meter
Z = -11147821
58 Z = -3426272
73
XDOT = 6710
262177 XDOT = 2131
934158
YDOT = -18898
802412 feet/sec YDOT = -5736
999151 meter/sec
ZDOT = -15118
205473 ZDOT = -4597
882240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14145715
55 X = 4311614
10
Y = 13056940
73 feet Y = 3979755
53 meter
Z = -11267096
35 Z = -3434210
97
XDOT = -17764
349009 XDOT = -5414
573578
YDOT = 6262
115955 feet/sec YDOT = 1908
692943 meter/sec
ZDOT = -15074
775463 ZDOT = -4594
791561
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 13269
37675512
00016717 00000-0 10270-3 0 9105
2 25544 51
6502 326
8833 0002836 86
8758 273
2717 15
50404584 10405
Satellite: ISS
Catalog Number: 25544
Epoch time: 13269
37675512 = yrday
fracday
Element set: 910
Inclination: 51
6502 deg
RA of node: 326
8833 deg
Eccentricity:
0002836
Arg of perigee: 86
8758 deg
Mean anomaly: 273
2717 deg
Mean motion: 15
50404584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1040
Checksum: 314
Coasting Arc #12 (Orbit 1055)
---------------------------------------
Vector Time (GMT): 2013/270/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5627304
02 A = 6794029
43 meter
Y = -671743
06 meter E =
0014409
Z = 3735703
76 I = 51
43177
XDOT = -2115
239038 Wp = 94
74748
YDOT = 6017
918968 meter/sec RA = 321
48318 deg
ZDOT = 4253
066568 TA = 309
99385
MA = 310
12025
Ha = 227
738 n
mi
Hp = 219
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18462283
53 X = 5616250
24
Y = -2203881
43 feet Y = -608876
48 meter
Z = 12256245
94 Z = 3763014
02
XDOT = -6939
760625 XDOT = -2203
035860
YDOT = 19743
828636 feet/sec YDOT = 5993
774461 meter/sec
ZDOT = 13953
630473 ZDOT = 4242
577146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13955547
69 X = -4253650
94
Y = -12170969
28 feet Y = -3709711
44 meter
Z = 12370883
82 Z = 3770645
39
XDOT = 18476
833774 XDOT = 5631
738934
YDOT = -6998
069702 feet/sec YDOT = -2133
011645 meter/sec
ZDOT = 13908
730152 ZDOT = 4239
380950
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 13270
40805146
00016717 00000-0 10270-3 0 9110
2 25544 51
6506 321
7714 0002881 89
6195 270
5286 15
50452789 10565
Satellite: ISS
Catalog Number: 25544
Epoch time: 13270
40805146 = yrday
fracday
Element set: 911
Inclination: 51
6506 deg
RA of node: 321
7714 deg
Eccentricity:
0002881
Arg of perigee: 89
6195 deg
Mean anomaly: 270
5286 deg
Mean motion: 15
50452789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1056
Checksum: 309
Coasting Arc #13 (Orbit 1070)
---------------------------------------
Vector Time (GMT): 2013/271/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5400616
97 A = 6792974
07 meter
Y = 632398
81 meter E =
0010138
Z = -4081886
35 I = 51
40450
XDOT = 2158
507739 Wp = 76
49431
YDOT = -6263
294553 meter/sec RA = 316
51068 deg
ZDOT = -3831
947540 TA = 153
69261
MA = 153
64109
Ha = 227
846 n
mi
Hp = 219
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17718559
60 X = -5387458
44
Y = 2074799
25 feet Y = 572078
90 meter
Z = -13392015
59 Z = -4108090
23
XDOT = 7081
718303 XDOT = 2246
999471
YDOT = -20548
866643 feet/sec YDOT = -6238
662297 meter/sec
ZDOT = -12572
006364 ZDOT = -3821
246181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13555860
43 X = 4131826
26
Y = 11468771
94 feet Y = 3495681
69 meter
Z = -13502005
27 Z = -4115411
21
XDOT = -19066
464586 XDOT = -5811
458406
YDOT = 7811
260133 feet/sec YDOT = 2380
872089 meter/sec
ZDOT = -12526
187977 ZDOT = -3817
982095
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 13271
37488577
00016717 00000-0 10270-3 0 9123
2 25544 51
6506 316
9796 0002846 92
1386 268
0091 15
50427187 10710
Satellite: ISS
Catalog Number: 25544
Epoch time: 13271
37488577 = yrday
fracday
Element set: 912
Inclination: 51
6506 deg
RA of node: 316
9796 deg
Eccentricity:
0002846
Arg of perigee: 92
1386 deg
Mean anomaly: 268
0091 deg
Mean motion: 15
50427187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1071
Checksum: 327
Coasting Arc #14 (Orbit 1086)
---------------------------------------
Vector Time (GMT): 2013/272/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5166961
38 A = 6791802
74 meter
Y = -577990
64 meter E =
0012245
Z = 4361728
79 I = 51
37948
XDOT = -2150
700971 Wp = 105
56137
YDOT = 6525
818507 meter/sec RA = 311
53500 deg
ZDOT = 3401
296290 TA = 309
78637
MA = 309
89413
Ha = 227
684 n
mi
Hp = 219
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16951973
03 X = 5151852
42
Y = -1896294
75 feet Y = -520294
44 meter
Z = 14310133
84 Z = 4386792
84
XDOT = -7056
105548 XDOT = -2240
036879
YDOT = 21410
165704 feet/sec YDOT = 6501
268831 meter/sec
ZDOT = 11159
108563 ZDOT = 3390
630718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13085859
14 X = -3988569
87
Y = -10802950
07 feet Y = -3292739
18 meter
Z = 14415332
60 Z = 4393793
38
XDOT = 19555
800817 XDOT = 5960
608089
YDOT = -8810
036512 feet/sec YDOT = -2685
299129 meter/sec
ZDOT = 11113
410698 ZDOT = 3387
367581
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 13272
40616427
00016717 00000-0 10270-3 0 9136
2 25544 51
6507 311
8674 0002898 94
4611 265
6871 15
50477349 10874
Satellite: ISS
Catalog Number: 25544
Epoch time: 13272
40616427 = yrday
fracday
Element set: 913
Inclination: 51
6507 deg
RA of node: 311
8674 deg
Eccentricity:
0002898
Arg of perigee: 94
4611 deg
Mean anomaly: 265
6871 deg
Mean motion: 15
50477349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1087
Checksum: 324
Coasting Arc #15 (Orbit 1101)
---------------------------------------
Vector Time (GMT): 2013/273/08:26:23
739
Vector Time (MET): N/A
Weight (LBS) : 914038
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4951086
11 A = 6790864
85 meter
Y = 450216
52 meter E =
0013116
Z = -4638632
50 I = 51
35584
XDOT = 2110
150398 Wp = 75
67630
YDOT = -6754
097246 meter/sec RA = 306
55777 deg
ZDOT = -2911
593343 TA = 165
18661
MA = 165
14815
Ha = 227
817 n
mi
Hp = 219
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16243720
85 X = -4933219
27
Y = 1477088
32 feet Y = 394949
70 meter
Z = -15218610
56 Z = -4662641
14
XDOT = 6923
065611 XDOT = 2199
663137
YDOT = -22159
111700 feet/sec YDOT = -6730
000037 meter/sec
ZDOT = -9552
471597 ZDOT = -2901
124211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12468367
13 X = 3800358
30
Y = 10368382
14 feet Y = 3160282
88 meter
Z = -15319361
52 Z = -4669341
39
XDOT = -19844
537999 XDOT = -6048
615182
YDOT = 9834
421572 feet/sec YDOT = 2997
531695 meter/sec
ZDOT = -9507
575032 ZDOT = -2897
908870
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 13273
37298152
00016717 00000-0 10270-3 0 9145
2 25544 51
6501 307
0757 0002855 97
0102 263
1373 15
50449901 11025
Satellite: ISS
Catalog Number: 25544
Epoch time: 13273
37298152 = yrday
fracday
Element set: 914
Inclination: 51
6501 deg
RA of node: 307
0757 deg
Eccentricity:
0002855
Arg of perigee: 97
0102 deg
Mean anomaly: 263
1373 deg
Mean motion: 15
50449901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1102
Checksum: 284
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