ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 36963 27 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 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 2361)
---------------------------------------
Vector Time (GMT): 2013/354/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1682067
68 A = 6800924
73 meter
Y = -6469326
44 meter E =
0009278
Z = -1220568
33 I = 51
31306
XDOT = 4445
151949 Wp = 5
41759
YDOT = -2251
617578 meter/sec RA = 263
83342 deg
ZDOT = 5820
971688 TA = 341
27802
MA = 341
31212
Ha = 226
265 n
mi
Hp = 223
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5518594
77 X = -1603672
08
Y = -21224824
28 feet Y = -6487697
96 meter
Z = -4004489
27 Z = -1228549
72
XDOT = 14583
831854 XDOT = 4441
723187
YDOT = -7387
196779 feet/sec YDOT = -2201
928712 meter/sec
ZDOT = 19097
676141 ZDOT = 5842
557149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13937640
50 X = 4248192
82
Y = -16924201
96 feet Y = -5158496
76 meter
Z = -4037022
86 Z = -1230484
57
XDOT = 13245
060540 XDOT = 4037
094453
YDOT = 6340
378615 feet/sec YDOT = 1932
547402 meter/sec
ZDOT = 19188
840468 ZDOT = 5848
758575
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 13354
60656022
00016717 00000-0 10270-3 0 9000
2 25544 51
6510 264
6792 0005152 293
8748 66
1863 15
49928756 23629
Satellite: ISS
Catalog Number: 25544
Epoch time: 13354
60656022 = yrday
fracday
Element set: 900
Inclination: 51
6510 deg
RA of node: 264
6792 deg
Eccentricity:
0005152
Arg of perigee: 293
8748 deg
Mean anomaly: 66
1863 deg
Mean motion: 15
49928756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2362
Checksum: 323
Coasting Arc #2 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2013/355/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1996759
21 A = 6801215
95 meter
Y = 6435052
45 meter E =
0008477
Z = 893965
47 I = 51
31777
XDOT = -4379
844743 Wp = 130
68015
YDOT = 2182
208064 meter/sec RA = 258
85921 deg
ZDOT = -5893
964084 TA = 39
61978
MA = 39
55786
Ha = 226
407 n
mi
Hp = 222
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6551047
27 X = 1920310
02
Y = 21112376
81 feet Y = 6456953
97 meter
Z = 2932957
57 Z = 903480
21
XDOT = -14369
569367 XDOT = -4375
290130
YDOT = 7159
475277 feet/sec YDOT = 2133
255720 meter/sec
ZDOT = -19337
152506 ZDOT = -5915
229577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12929202
51 X = -3940820
93
Y = 17923562
11 feet Y = 5463101
73 meter
Z = 2971962
05 Z = 905854
03
XDOT = -12984
861240 XDOT = -3957
785706
YDOT = -6128
522061 feet/sec YDOT = -1867
973524 meter/sec
ZDOT = -19426
961039 ZDOT = -5921
337725
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 13355
63817798
00016717 00000-0 10270-3 0 9014
2 25544 51
6505 259
5698 0005042 296
2689 63
7943 15
49929478 23781
Satellite: ISS
Catalog Number: 25544
Epoch time: 13355
63817798 = yrday
fracday
Element set: 901
Inclination: 51
6505 deg
RA of node: 259
5698 deg
Eccentricity:
0005042
Arg of perigee: 296
2689 deg
Mean anomaly: 63
7943 deg
Mean motion: 15
49929478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 369
Coasting Arc #3 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2013/356/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2312156
58 A = 6801200
86 meter
Y = -6363195
57 meter E =
0011137
Z = -568356
54 I = 51
32450
XDOT = 4347
367173 Wp = 13
52618
YDOT = -2107
948531 meter/sec RA = 253
88368 deg
ZDOT = 5948
731714 TA = 340
32255
MA = 340
36549
Ha = 226
400 n
mi
Hp = 222
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7585815
55 X = -2238069
17
Y = -20876625
88 feet Y = -6388637
30 meter
Z = -1864686
81 Z = -579409
09
XDOT = 14263
015658 XDOT = 4341
718532
YDOT = -6915
841638 feet/sec YDOT = -2059
365408 meter/sec
ZDOT = 19516
836331 ZDOT = 5969
836820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11792126
18 X = 3594240
06
Y = -18818929
51 feet Y = -5736009
72 meter
Z = -1910187
06 Z = -582225
02
XDOT = 12780
789160 XDOT = 3895
584536
YDOT = 6029
651300 feet/sec YDOT = 1837
837716 meter/sec
ZDOT = 19605
959583 ZDOT = 5975
896481
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 13356
60529269
00016717 00000-0 10270-3 0 9026
2 25544 51
6496 254
7782 0005250 300
7150 59
3484 15
50004423 23930
Satellite: ISS
Catalog Number: 25544
Epoch time: 13356
60529269 = yrday
fracday
Element set: 902
Inclination: 51
6496 deg
RA of node: 254
7782 deg
Eccentricity:
0005250
Arg of perigee: 300
7150 deg
Mean anomaly: 59
3484 deg
Mean motion: 15
50004423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 300
Coasting Arc #4 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2013/357/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2600596
15 A = 6801295
63 meter
Y = 6276713
21 meter E =
0007425
Z = 209742
06 I = 51
33394
XDOT = -4351
415556 Wp = 138
75487
YDOT = 2006
466450 meter/sec RA = 248
91006 deg
ZDOT = -5976
082818 TA = 38
98027
MA = 38
92678
Ha = 226
535 n
mi
Hp = 222
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8532139
59 X = 2529196
40
Y = 20592891
11 feet Y = 6305395
51 meter
Z = 688130
11 Z = 222202
27
XDOT = -14276
297755 XDOT = -4344
498914
YDOT = 6582
895176 feet/sec YDOT = 1957
845078 meter/sec
ZDOT = -19606
570925 ZDOT = -5997
204569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10646207
58 X = -3244964
07
Y = 19581863
51 feet Y = 5968552
00 meter
Z = 739580
37 Z = 225424
10
XDOT = -12590
719472 XDOT = -3837
651295
YDOT = -6088
042463 feet/sec YDOT = -1855
635343 meter/sec
ZDOT = -19695
749784 ZDOT = -6003
264534
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 13357
63685810
00016717 00000-0 10270-3 0 9036
2 25544 51
6492 249
6682 0005170 303
3446 56
7209 15
50012870 24095
Satellite: ISS
Catalog Number: 25544
Epoch time: 13357
63685810 = yrday
fracday
Element set: 903
Inclination: 51
6492 deg
RA of node: 249
6682 deg
Eccentricity:
0005170
Arg of perigee: 303
3446 deg
Mean anomaly: 56
7209 deg
Mean motion: 15
50012870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 305
Coasting Arc #5 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2013/358/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2879926
68 A = 6801122
74 meter
Y = -6150750
04 meter E =
0012576
Z = 144441
76 I = 51
34496
XDOT = 4392
184385 Wp = 22
37367
YDOT = -1912
240472 meter/sec RA = 243
93517 deg
ZDOT = 5983
150827 TA = 339
18657
MA = 339
23774
Ha = 226
541 n
mi
Hp = 222
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9448578
34 X = -2811635
24
Y = -20179626
11 feet Y = -6182573
38 meter
Z = 473890
29 Z = 130617
06
XDOT = 14410
053758 XDOT = 4384
176657
YDOT = -6273
754830 feet/sec YDOT = -1863
169255 meter/sec
ZDOT = 19629
759932 ZDOT = 6004
468044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9397740
65 X = 2864431
35
Y = -20204612
69 feet Y = -6158365
95 meter
Z = 416666
63 Z = 126999
99
XDOT = 12510
157859 XDOT = 3813
096115
YDOT = 6237
878681 feet/sec YDOT = 1901
305422 meter/sec
ZDOT = 19719
748714 ZDOT = 6010
579408
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 13358
66839535
00016717 00000-0 10270-3 0 9046
2 25544 51
6482 244
5563 0005308 307
4672 52
5996 15
50079074 24259
Satellite: ISS
Catalog Number: 25544
Epoch time: 13358
66839535 = yrday
fracday
Element set: 904
Inclination: 51
6482 deg
RA of node: 244
5563 deg
Eccentricity:
0005308
Arg of perigee: 307
4672 deg
Mean anomaly: 52
5996 deg
Mean motion: 15
50079074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 329
Coasting Arc #6 (Orbit 2439)
---------------------------------------
Vector Time (GMT): 2013/359/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3125266
05 A = 6800947
77 meter
Y = 6013707
92 meter E =
0005794
Z = -528860
75 I = 51
35874
XDOT = -4469
596873 Wp = 145
99264
YDOT = 1802
508745 meter/sec RA = 238
96277 deg
ZDOT = -5952
773560 TA = 39
72371
MA = 39
68129
Ha = 226
670 n
mi
Hp = 222
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10253497
52 X = 3060356
21
Y = 19730012
87 feet Y = 6048293
73 meter
Z = -1735107
45 Z = -513835
97
XDOT = -14664
031736 XDOT = -4460
503833
YDOT = 5913
742602 feet/sec YDOT = 1752
577911 meter/sec
ZDOT = -19530
096981 ZDOT = -5974
464266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8176482
20 X = -2492191
77
Y = 20682482
69 feet Y = 6304020
73 meter
Z = -1672801
74 Z = -509869
97
XDOT = -12487
243180 XDOT = -3806
111721
YDOT = -6513
600030 feet/sec YDOT = -1985
345289 meter/sec
ZDOT = -19621
643661 ZDOT = -5980
676988
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 13359
63543946
00016717 00000-0 10270-3 0 9053
2 25544 51
6480 239
7653 0005286 310
5903 49
4787 15
50101325 24405
Satellite: ISS
Catalog Number: 25544
Epoch time: 13359
63543946 = yrday
fracday
Element set: 905
Inclination: 51
6480 deg
RA of node: 239
7653 deg
Eccentricity:
0005286
Arg of perigee: 310
5903 deg
Mean anomaly: 49
4787 deg
Mean motion: 15
50101325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2440
Checksum: 312
Coasting Arc #7 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2013/360/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3350391
17 A = 6800589
52 meter
Y = -5838651
02 meter E =
0013459
Z = 904335
69 I = 51
37380
XDOT = 4584
039033 Wp = 31
99201
YDOT = -1712
035845 meter/sec RA = 233
98930 deg
ZDOT = 5900
380294 TA = 337
82074
MA = 337
87891
Ha = 226
682 n
mi
Hp = 222
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10992097
00 X = -3289246
08
Y = -19155679
19 feet Y = -5875775
38 meter
Z = 2966980
59 Z = 888208
06
XDOT = 15039
498139 XDOT = 4574
180240
YDOT = -5616
915501 feet/sec YDOT = -1660
829559 meter/sec
ZDOT = 19358
203064 ZDOT = 5922
625137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6893474
83 X = 2101131
13
Y = -20991408
64 feet Y = -6398181
35 meter
Z = 2899997
18 Z = 883919
14
XDOT = 12615
730215 XDOT = 3845
274570
YDOT = 6843
826206 feet/sec YDOT = 2085
998227 meter/sec
ZDOT = 19452
072547 ZDOT = 5928
991712
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 13360
66692738
00016717 00000-0 10270-3 0 9063
2 25544 51
6471 234
6529 0005311 313
9875 46
0837 15
50151403 24563
Satellite: ISS
Catalog Number: 25544
Epoch time: 13360
66692738 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 234
6529 deg
Eccentricity:
0005311
Arg of perigee: 313
9875 deg
Mean anomaly: 46
0837 deg
Mean motion: 15
50151403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 310
Coasting Arc #8 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2013/361/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3534612
62 A = 6800097
48 meter
Y = 5658598
86 meter E =
0003608
Z = -1305670
66 I = 51
39126
XDOT = -4730
185135 Wp = 148
56289
YDOT = 1618
516978 meter/sec RA = 229
01860 deg
ZDOT = -5801
054017 TA = 45
66484
MA = 45
63528
Ha = 226
804 n
mi
Hp = 222
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11596498
08 X = 3477416
81
Y = 18564956
89 feet Y = 5697805
42 meter
Z = -4283696
40 Z = -1288638
42
XDOT = -15518
980103 XDOT = -4719
752187
YDOT = 5310
095072 feet/sec YDOT = 1565
679678 meter/sec
ZDOT = -19032
329452 ZDOT = -5824
007449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5681541
39 X = -1731733
82
Y = 21153209
39 feet Y = 6447498
22 meter
Z = -4212869
17 Z = -1284082
52
XDOT = -12831
388369 XDOT = -3911
007175
YDOT = -7249
310622 feet/sec YDOT = -2209
589877 meter/sec
ZDOT = -19129
173590 ZDOT = -5830
572110
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 13361
63392475
00016717 00000-0 10270-3 0 9077
2 25544 51
6468 229
8617 0005344 318
1472 41
9269 15
50191688 24718
Satellite: ISS
Catalog Number: 25544
Epoch time: 13361
63392475 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 229
8617 deg
Eccentricity:
0005344
Arg of perigee: 318
1472 deg
Mean anomaly: 41
9269 deg
Mean motion: 15
50191688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2471
Checksum: 329
Coasting Arc #9 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2013/362/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3687380
01 A = 6799530
59 meter
Y = -5445786
62 meter E =
0013686
Z = 1692461
48 I = 51
40972
XDOT = 4910
148648 Wp = 42
29836
YDOT = -1554
745927 meter/sec RA = 224
04716 deg
ZDOT = 5678
215595 TA = 336
29498
MA = 336
35797
Ha = 226
825 n
mi
Hp = 221
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12097703
45 X = -3634431
50
Y = -17866754
02 feet Y = -5486725
33 meter
Z = 5552695
15 Z = 1674676
69
XDOT = 16109
411575 XDOT = 4899
585936
YDOT = -5100
872463 feet/sec YDOT = -1499
896992 meter/sec
ZDOT = 18629
316256 ZDOT = 5702
042937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4460653
96 X = 1359607
33
Y = -21130419
23 feet Y = -6440551
78 meter
Z = 5478658
68 Z = 1669895
16
XDOT = 13223
164534 XDOT = 4030
420550
YDOT = 7662
237378 feet/sec YDOT = 2335
449953 meter/sec
ZDOT = 18729
838145 ZDOT = 5708
854667
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 13362
66536415
00016717 00000-0 10270-3 0 9086
2 25544 51
6460 224
7491 0005261 320
8897 39
1873 15
50223820 24874
Satellite: ISS
Catalog Number: 25544
Epoch time: 13362
66536415 = yrday
fracday
Element set: 908
Inclination: 51
6460 deg
RA of node: 224
7491 deg
Eccentricity:
0005261
Arg of perigee: 320
8897 deg
Mean anomaly: 39
1873 deg
Mean motion: 15
50223820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2487
Checksum: 314
Coasting Arc #10 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2013/363/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3793642
61 A = 6798726
70 meter
Y = 5236892
66 meter E =
0001377
Z = -2099104
21 I = 51
43021
XDOT = -5111
406242 Wp = 111
79913
YDOT = 1499
411220 meter/sec RA = 219
07828 deg
ZDOT = -5500
327469 TA = 91
46031
MA = 91
44453
Ha = 226
932 n
mi
Hp = 221
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12446334
02 X = 3744997
44
Y = 17181406
37 feet Y = 5279043
80 meter
Z = -6886824
83 Z = -2080792
69
XDOT = -16769
705520 XDOT = -5101
073994
YDOT = 4919
328151 feet/sec YDOT = 1442
310512 meter/sec
ZDOT = -18045
693795 ZDOT = -5525
132989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3358972
72 X = -1023814
88
Y = 20973180
82 feet Y = 6392625
51 meter
Z = -6810528
63 Z = -2075849
13
XDOT = -13709
780669 XDOT = -4178
741148
YDOT = -8085
898704 feet/sec YDOT = -2464
581925 meter/sec
ZDOT = -18150
336753 ZDOT = -5532
222642
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 13363
63231557
00016717 00000-0 10270-3 0 9094
2 25544 51
6458 219
9575 0005326 325
9842 34
0967 15
50277152 25021
Satellite: ISS
Catalog Number: 25544
Epoch time: 13363
63231557 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 219
9575 deg
Eccentricity:
0005326
Arg of perigee: 325
9842 deg
Mean anomaly: 34
0967 deg
Mean motion: 15
50277152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 319
Coasting Arc #11 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2013/364/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3858345
77 A = 6797929
38 meter
Y = -5004197
29 meter E =
0013186
Z = 2484493
77 I = 51
45135
XDOT = 5340
165857 Wp = 53
01109
YDOT = -1481
444754 meter/sec RA = 214
10893 deg
ZDOT = 5297
524485 TA = 334
88533
MA = 334
94940
Ha = 226
963 n
mi
Hp = 221
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12658614
72 X = -3814169
91
Y = -16417970
11 feet Y = -5047097
05 meter
Z = 8151226
29 Z = 2465857
09
XDOT = 17520
229191 XDOT = 5330
600974
YDOT = -4860
383052 feet/sec YDOT = -1421
781691 meter/sec
ZDOT = 17380
329675 ZDOT = 5323
443030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2308053
41 X = 703494
68
Y = -20633081
12 feet Y = -6288963
12 meter
Z = 8073513
00 Z = 2460806
76
XDOT = 14376
306985 XDOT = 4381
898369
YDOT = 8466
867838 feet/sec YDOT = 2580
701317 meter/sec
ZDOT = 17489
670141 ZDOT = 5330
851459
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 13364
66370634
00016717 00000-0 10270-3 0 9100
2 25544 51
6448 214
8448 0005183 328
3070 31
7768 15
50299201 25183
Satellite: ISS
Catalog Number: 25544
Epoch time: 13364
66370634 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 214
8448 deg
Eccentricity:
0005183
Arg of perigee: 328
3070 deg
Mean anomaly: 31
7768 deg
Mean motion: 15
50299201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 307
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