[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 13th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 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
347/15:01:59
775 1
8 4
0 4
0
N/A -3
5 -0
4 226
2
000/00:09:59
551 0
5 0
3 223
4
Coasting Arc #1 (Orbit 2224)
---------------------------------------
Vector Time (GMT): 2013/345/17:37:11
705
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1227913
89 A = 6795786
41 meter
Y = 5823019
50 meter E =
0011109
Z = 3270741
18 I = 51
37716
XDOT = -5877
283288 Wp = 94
64916
YDOT = 1414
424068 meter/sec RA = 307
95428 deg
ZDOT = -4711
642302 TA = 47
28995
MA = 47
19646
Ha = 226
337 n
mi
Hp = 221
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4028588
88 X = -1308825
44
Y = 19104394
67 feet Y = 5808835
64 meter
Z = 10730778
14 Z = 3264579
74
XDOT = -19282
425485 XDOT = -5869
774792
YDOT = 4640
498912 feet/sec YDOT = 1348
742723 meter/sec
ZDOT = -15458
144037 ZDOT = -4740
175570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9180925
93 X = -2798346
22
Y = 17248035
24 feet Y = 5257201
14 meter
Z = 10703873
27 Z = 3262540
57
XDOT = -18464
543910 XDOT = -5627
992984
YDOT = -134
260575 feet/sec YDOT = -40
922623 meter/sec
ZDOT = -15578
370659 ZDOT = -4748
287377
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 13345
77318638
00016717 00000-0 10270-3 0 9006
2 25544 51
6512 308
4274 0001653 257
1486 102
9481 15
50369156 22255
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
77318638 = yrday
fracday
Element set: 900
Inclination: 51
6512 deg
RA of node: 308
4274 deg
Eccentricity:
0001653
Arg of perigee: 257
1486 deg
Mean anomaly: 102
9481 deg
Mean motion: 15
50369156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2225
Checksum: 305
Coasting Arc #2 (Orbit 2239)
---------------------------------------
Vector Time (GMT): 2013/346/17:37:11
705
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1154534
99 A = 6796687
05 meter
Y = -6037549
59 meter E =
0002938
Z = -2899620
41 I = 51
36199
XDOT = 5636
604360 Wp = 52
26163
YDOT = -1326
591776 meter/sec RA = 302
97864 deg
ZDOT = 5011
781369 TA = 274
63232
MA = 274
66588
Ha = 226
223 n
mi
Hp = 221
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3787844
46 X = 1236048
12
Y = -19808233
57 feet Y = -6024182
92 meter
Z = -9513190
33 Z = -2893814
07
XDOT = 18492
796456 XDOT = 5626
673549
YDOT = -4352
335224 feet/sec YDOT = -1263
615478 meter/sec
ZDOT = 16442
852260 ZDOT = 5039
139573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8824397
83 X = 2689676
46
Y = -18147378
83 feet Y = -5531321
07 meter
Z = -9487745
65 Z = -2891864
87
XDOT = 17566
702336 XDOT = 5354
330872
YDOT = -105
778110 feet/sec YDOT = -32
241168 meter/sec
ZDOT = 16558
120880 ZDOT = 5046
915244
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 13346
74005279
00016717 00000-0 10270-3 0 9019
2 25544 51
6510 303
6344 0001829 262
8641 97
2302 15
50390098 22403
Satellite: ISS
Catalog Number: 25544
Epoch time: 13346
74005279 = yrday
fracday
Element set: 901
Inclination: 51
6510 deg
RA of node: 303
6344 deg
Eccentricity:
0001829
Arg of perigee: 262
8641 deg
Mean anomaly: 97
2302 deg
Mean motion: 15
50390098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2240
Checksum: 286
Coasting Arc #3 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2013/347/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2431640
53 A = 6791747
95 meter
Y = -3908931
28 meter E =
0008139
Z = -5001007
30 I = 51
32366
XDOT = 4850
384266 Wp = 114
29929
YDOT = -5574
515950 meter/sec RA = 298
52581 deg
ZDOT = 1998
095596 TA = 175
23812
MA = 175
23038
Ha = 226
244 n
mi
Hp = 223
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7977823
25 X = -2363455
47
Y = -12824577
68 feet Y = -3935741
84 meter
Z = -16407504
27 Z = -5012654
76
XDOT = 15913
334207 XDOT = 4902
652939
YDOT = -18289
094323 feet/sec YDOT = -5519
983750 meter/sec
ZDOT = 6555
431747 ZDOT = 2021
785147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5162122
10 X = 1573414
82
Y = -14137898
67 feet Y = -4309231
51 meter
Z = -16455818
71 Z = -5015733
54
XDOT = 23160
445788 XDOT = 7059
303876
YDOT = 706
564075 feet/sec YDOT = 215
360730 meter/sec
ZDOT = 6655
995105 ZDOT = 2028
747308
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 13347
64244758
00016717 00000-0 10270-3 0 9027
2 25544 51
6507 299
1600 0004870 269
0230 91
0362 15
49662794 22541
Satellite: ISS
Catalog Number: 25544
Epoch time: 13347
64244758 = yrday
fracday
Element set: 902
Inclination: 51
6507 deg
RA of node: 299
1600 deg
Eccentricity:
0004870
Arg of perigee: 269
0230 deg
Mean anomaly: 91
0362 deg
Mean motion: 15
49662794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 312
Coasting Arc #4 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2013/348/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2583615
59 A = 6791940
04 meter
Y = 3916581
28 meter E =
0003794
Z = 4911521
22 I = 51
31084
XDOT = -4487
383602 Wp = 10
11636
YDOT = 5786
230947 meter/sec RA = 293
55108 deg
ZDOT = -2249
661087 TA = 102
00665
MA = 101
96412
Ha = 226
065 n
mi
Hp = 223
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8476429
11 X = 2515768
44
Y = 12849676
13 feet Y = 3945093
15 meter
Z = 16113914
76 Z = 4923907
84
XDOT = -14722
387145 XDOT = -4540
824662
YDOT = 18983
697333 feet/sec YDOT = 5735
751549 meter/sec
ZDOT = -7380
777846 ZDOT = -2271
589912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4620080
81 X = -1408200
63
Y = 14627334
65 feet Y = 4458411
60 meter
Z = 16165339
78 Z = 4927195
57
XDOT = -22917
878337 XDOT = -6985
369317
YDOT = 1035
370204 feet/sec YDOT = 315
580838 meter/sec
ZDOT = -7473
971570 ZDOT = -2278
066534
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 13348
67423881
00016717 00000-0 10270-3 0 9038
2 25544 51
6506 294
0515 0004939 273
3052 86
7533 15
49718040 22700
Satellite: ISS
Catalog Number: 25544
Epoch time: 13348
67423881 = yrday
fracday
Element set: 903
Inclination: 51
6506 deg
RA of node: 294
0515 deg
Eccentricity:
0004939
Arg of perigee: 273
3052 deg
Mean anomaly: 86
7533 deg
Mean motion: 15
49718040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 312
Coasting Arc #5 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2013/349/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2752198
04 A = 6792317
00 meter
Y = -3926061
50 meter E =
0006771
Z = -4817623
84 I = 51
30141
XDOT = 4113
594835 Wp = 116
12952
YDOT = -5952
315729 meter/sec RA = 288
57481 deg
ZDOT = 2500
584794 TA = 178
61361
MA = 178
61174
Ha = 226
156 n
mi
Hp = 223
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9029521
14 X = -2684688
53
Y = -12880779
19 feet Y = -3956460
39 meter
Z = -15805852
51 Z = -4830830
27
XDOT = 13496
046048 XDOT = 4167
701972
YDOT = -19528
594912 feet/sec YDOT = -5906
012605 meter/sec
ZDOT = 8204
018352 ZDOT = 2520
699249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4032048
06 X = 1228968
25
Y = -15147659
02 feet Y = -4617006
47 meter
Z = -15860728
63 Z = -4834350
09
XDOT = 22482
011352 XDOT = 6852
517060
YDOT = -2696
117505 feet/sec YDOT = -821
776615 meter/sec
ZDOT = 8289
608880 ZDOT = 2526
672787
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 13349
64152593
00016717 00000-0 10270-3 0 9046
2 25544 51
6514 289
2617 0004933 276
5291 83
5301 15
49724535 22852
Satellite: ISS
Catalog Number: 25544
Epoch time: 13349
64152593 = yrday
fracday
Element set: 904
Inclination: 51
6514 deg
RA of node: 289
2617 deg
Eccentricity:
0004933
Arg of perigee: 276
5291 deg
Mean anomaly: 83
5301 deg
Mean motion: 15
49724535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 322
Coasting Arc #6 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2013/350/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2921009
94 A = 6792602
77 meter
Y = 3940385
07 meter E =
0004970
Z = 4699190
40 I = 51
29402
XDOT = -3749
348701 Wp = 25
19548
YDOT = 6081
534204 meter/sec RA = 283
59832 deg
ZDOT = -2763
425836 TA = 92
36749
MA = 92
31058
Ha = 226
080 n
mi
Hp = 223
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9583365
96 X = 2853903
11
Y = 12927772
56 feet Y = 3972673
96 meter
Z = 15417291
32 Z = 4713217
87
XDOT = -12301
012798 XDOT = -3803
651083
YDOT = 19952
540039 feet/sec YDOT = 6039
303269 meter/sec
ZDOT = -9066
357730 ZDOT = -2781
771157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3438676
07 X = -1048108
47
Y = 15663384
64 feet Y = 4774199
64 meter
Z = 15475624
92 Z = 4716970
47
XDOT = -21924
798021 XDOT = -6682
678437
YDOT = 4239
385057 feet/sec YDOT = 1292
164565 meter/sec
ZDOT = -9144
527859 ZDOT = -2787
252092
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 13350
67327801
00016717 00000-0 10270-3 0 9058
2 25544 51
6514 284
1530 0005004 280
9638 79
0949 15
49784067 23017
Satellite: ISS
Catalog Number: 25544
Epoch time: 13350
67327801 = yrday
fracday
Element set: 905
Inclination: 51
6514 deg
RA of node: 284
1530 deg
Eccentricity:
0005004
Arg of perigee: 280
9638 deg
Mean anomaly: 79
0949 deg
Mean motion: 15
49784067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 309
Coasting Arc #7 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/351/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3110423
38 A = 6793090
48 meter
Y = -3947588
51 meter E =
0005084
Z = -4575444
68 I = 51
28946
XDOT = 3384
037700 Wp = 116
11764
YDOT = -6167
557781 meter/sec RA = 278
62083 deg
ZDOT = 3021
161082 TA = 184
25769
MA = 184
26202
Ha = 226
175 n
mi
Hp = 223
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10204801
10 X = -3043823
12
Y = -12951405
88 feet Y = -3981998
37 meter
Z = -15011301
43 Z = -4590393
49
XDOT = 11102
485892 XDOT = 3438
077208
YDOT = -20234
769622 feet/sec YDOT = -6129
413491 meter/sec
ZDOT = 9911
945808 ZDOT = 3037
731027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2765992
29 X = 843074
45
Y = -16197358
04 feet Y = -4936954
73 meter
Z = -15073517
50 Z = -4594408
13
XDOT = 21211
749109 XDOT = 6465
341128
YDOT = -5666
425029 feet/sec YDOT = -1727
126349 meter/sec
ZDOT = 9982
660105 ZDOT = 3042
714800
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 13351
64052880
00016717 00000-0 10270-3 0 9069
2 25544 51
6516 279
3631 0005034 283
9369 76
1221 15
49784884 23168
Satellite: ISS
Catalog Number: 25544
Epoch time: 13351
64052880 = yrday
fracday
Element set: 906
Inclination: 51
6516 deg
RA of node: 279
3631 deg
Eccentricity:
0005034
Arg of perigee: 283
9369 deg
Mean anomaly: 76
1221 deg
Mean motion: 15
49784884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 321
Coasting Arc #8 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/352/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3300855
15 A = 6793472
36 meter
Y = 3959749
32 meter E =
0006144
Z = 4423945
13 I = 51
28762
XDOT = -3037
691846 Wp = 38
16145
YDOT = 6215
424951 meter/sec RA = 273
64349 deg
ZDOT = -3289
526300 TA = 85
26380
MA = 85
19364
Ha = 226
200 n
mi
Hp = 223
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10829577
27 X = 3234840
78
Y = 12991303
54 feet Y = 3996292
01 meter
Z = 14514255
66 Z = 4439820
40
XDOT = -9966
180596 XDOT = -3090
988766
YDOT = 20391
814143 feet/sec YDOT = 6181
157890 meter/sec
ZDOT = -10792
409122 ZDOT = -3304
411890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2085220
14 X = -635575
10
Y = 16726679
30 feet Y = 5098291
85 meter
Z = 14580376
73 Z = 4444098
83
XDOT = -20406
718846 XDOT = -6219
967904
YDOT = 6939
549365 feet/sec YDOT = 2115
174646 meter/sec
ZDOT = -10856
041773 ZDOT = -3308
921532
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 13352
67224234
00016717 00000-0 10270-3 0 9078
2 25544 51
6516 274
2543 0005104 288
5021 71
5575 15
49847563 23321
Satellite: ISS
Catalog Number: 25544
Epoch time: 13352
67224234 = yrday
fracday
Element set: 907
Inclination: 51
6516 deg
RA of node: 274
2543 deg
Eccentricity:
0005104
Arg of perigee: 288
5021 deg
Mean anomaly: 71
5575 deg
Mean motion: 15
49847563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 303
Coasting Arc #9 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2013/353/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3513022
57 A = 6794063
15 meter
Y = -3954662
95 meter E =
0003195
Z = -4266936
18 I = 51
28782
XDOT = 2699
652366 Wp = 108
92673
YDOT = -6225
345948 meter/sec RA = 268
66524 deg
ZDOT = 3548
261827 TA = 197
49913
MA = 197
51014
Ha = 226
279 n
mi
Hp = 223
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11525664
61 X = -3447812
07
Y = -12974615
98 feet Y = -3993582
79 meter
Z = -13999134
45 Z = -4283844
01
XDOT = 8857
127185 XDOT = 2751
828535
YDOT = -20424
363346 feet/sec YDOT = -6194
865321 meter/sec
ZDOT = 11641
278959 ZDOT = 3561
502552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1296792
08 X = 395262
23
Y = -17248818
62 feet Y = -5257439
91 meter
Z = -14069611
11 Z = -4288417
46
XDOT = 19493
609790 XDOT = 5941
652264
YDOT = -8073
198789 feet/sec YDOT = -2460
710991 meter/sec
ZDOT = 11697
987583 ZDOT = 3565
546615
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 13353
63945747
00016717 00000-0 10270-3 0 9085
2 25544 51
6509 269
4640 0005134 291
0834 68
9768 15
49842894 23473
Satellite: ISS
Catalog Number: 25544
Epoch time: 13353
63945747 = yrday
fracday
Element set: 908
Inclination: 51
6509 deg
RA of node: 269
4640 deg
Eccentricity:
0005134
Arg of perigee: 291
0834 deg
Mean anomaly: 68
9768 deg
Mean motion: 15
49842894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 352
Coasting Arc #10 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/354/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3726065
07 A = 6794534
42 meter
Y = 3953831
28 meter E =
0007237
Z = 4078852
96 I = 51
29157
XDOT = -2390
410955 Wp = 50
27855
YDOT = 6197
739838 meter/sec RA = 263
68773 deg
ZDOT = -3815
036182 TA = 79
42123
MA = 79
33971
Ha = 226
371 n
mi
Hp = 223
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12224622
93 X = 3661761
72
Y = 12971887
40 feet Y = 3995138
63 meter
Z = 13382063
51 Z = 4096797
84
XDOT = -7842
555627 XDOT = -2441
005535
YDOT = 20333
792120 feet/sec YDOT = 6170
726165 meter/sec
ZDOT = -12516
522908 ZDOT = -3826
770869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -498487
52 X = -151939
00
Y = 17761020
25 feet Y = 5413558
97 meter
Z = 13456915
03 Z = 4101667
70
XDOT = -18527
278659 XDOT = -5647
114535
YDOT = 9023
937612 feet/sec YDOT = 2750
496184 meter/sec
ZDOT = -12566
883544 ZDOT = -3830
386104
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
67113314
00016717 00000-0 10270-3 0 9098
2 25544 51
6508 264
3549 0005223 295
6963 64
3648 15
49906788 23634
Satellite: ISS
Catalog Number: 25544
Epoch time: 13354
67113314 = yrday
fracday
Element set: 909
Inclination: 51
6508 deg
RA of node: 264
3549 deg
Eccentricity:
0005223
Arg of perigee: 295
6963 deg
Mean anomaly: 64
3648 deg
Mean motion: 15
49906788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 336
Coasting Arc #11 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2013/355/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3958770
34 A = 6795206
64 meter
Y = -3925483
69 meter E =
0001773
Z = -3885941
43 I = 51
29668
XDOT = 2097
741579 Wp = 68
16842
YDOT = -6140
242196 meter/sec RA = 258
70931 deg
ZDOT = 4067
814465 TA = 244
71545
MA = 244
73382
Ha = 226
427 n
mi
Hp = 222
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12988091
65 X = -3895703
80
Y = -12878883
50 feet Y = -3969400
29 meter
Z = -12749151
68 Z = -3905019
70
XDOT = 6882
354263 XDOT = 2146
487056
YDOT = -20145
151562 feet/sec YDOT = -6116
511639 meter/sec
ZDOT = 13345
847981 ZDOT = 4078
122996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -425995
65 X = -129843
47
Y = -18230133
13 feet Y = -5556544
58 meter
Z = -12828788
21 Z = -3910214
65
XDOT = 17507
469114 XDOT = 5336
276586
YDOT = -9827
037335 feet/sec YDOT = -2995
280980 meter/sec
ZDOT = 13390
190757 ZDOT = 4081
330143
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
63831348
00016717 00000-0 10270-3 0 9101
2 25544 51
6494 259
5638 0005203 297
9464 62
1159 15
49897894 23788
Satellite: ISS
Catalog Number: 25544
Epoch time: 13355
63831348 = yrday
fracday
Element set: 910
Inclination: 51
6494 deg
RA of node: 259
5638 deg
Eccentricity:
0005203
Arg of perigee: 297
9464 deg
Mean anomaly: 62
1159 deg
Mean motion: 15
49897894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 353
Coasting Arc #12 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2013/356/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4190889
88 A = 6795745
39 meter
Y = 3900231
34 meter E =
0008185
Z = 3658720
29 I = 51
30605
XDOT = -1843
466899 Wp = 62
11071
YDOT = 6048
154127 meter/sec RA = 253
73239 deg
ZDOT = -4324
583352 TA = 74
26310
MA = 74
17284
Ha = 226
555 n
mi
Hp = 222
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13749638
72 X = 4129192
23
Y = 12796034
57 feet Y = 3946751
37 meter
Z = 12003675
48 Z = 3678929
43
XDOT = -6048
119746 XDOT = -1889
954213
YDOT = 19843
025351 feet/sec YDOT = 6027
279614 meter/sec
ZDOT = -14188
265590 ZDOT = -4333
651260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1358506
30 X = 414072
72
Y = 18679184
31 feet Y = 5693415
38 meter
Z = 12088086
06 Z = 3684448
63
XDOT = -16480
721843 XDOT = -5023
324018
YDOT = 10429
364459 feet/sec YDOT = 3178
870287 meter/sec
ZDOT = -14227
365249 ZDOT = -4336
500928
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
66995222
00016717 00000-0 10270-3 0 9118
2 25544 51
6495 254
4542 0005336 302
4546 57
6089 15
49961504 23946
Satellite: ISS
Catalog Number: 25544
Epoch time: 13356
66995222 = yrday
fracday
Element set: 911
Inclination: 51
6495 deg
RA of node: 254
4542 deg
Eccentricity:
0005336
Arg of perigee: 302
4546 deg
Mean anomaly: 57
6089 deg
Mean motion: 15
49961504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 328
Coasting Arc #13 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2013/357/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4437416
80 A = 6796464
86 meter
Y = -3838208
14 meter E =
0002898
Z = -3428337
18 I = 51
31625
XDOT = 1612
149958 Wp = 13
23767
YDOT = -5936
747427 meter/sec RA = 248
75469 deg
ZDOT = 4563
382880 TA = 306
49818
MA = 306
52487
Ha = 226
590 n
mi
Hp = 222
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14558454
07 X = -4377513
49
Y = -12592546
38 feet Y = -3887495
07 meter
Z = -11247825
41 Z = -3449748
27
XDOT = 5289
205898 XDOT = 1656
248644
YDOT = -19477
517805 feet/sec YDOT = -5918
472964 meter/sec
ZDOT = 14971
728610 ZDOT = 4571
321364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2422056
52 X = -738242
83
Y = -19042933
85 feet Y = -5804286
24 meter
Z = -11337314
42 Z = -3455613
44
XDOT = 15457
210916 XDOT = 4711
357887
YDOT = -10893
071858 feet/sec YDOT = -3320
208302 meter/sec
ZDOT = 15006
050498 ZDOT = 4573
844192
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
63709882
00016717 00000-0 10270-3 0 9122
2 25544 51
6478 249
6624 0005221 304
6731 55
3927 15
49949736 24093
Satellite: ISS
Catalog Number: 25544
Epoch time: 13357
63709882 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 249
6624 deg
Eccentricity:
0005221
Arg of perigee: 304
6731 deg
Mean anomaly: 55
3927 deg
Mean motion: 15
49949736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 339
Coasting Arc #14 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2013/358/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4680332
56 A = 6797030
58 meter
Y = 3778276
71 meter E =
0008940
Z = 3160675
16 I = 51
33109
XDOT = -1427
785498 Wp = 73
84535
YDOT = 5796
135856 meter/sec RA = 243
77929 deg
ZDOT = -4800
650977 TA = 69
58761
MA = 69
49163
Ha = 226
735 n
mi
Hp = 222
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15355421
78 X = 4622381
54
Y = 12395920
95 feet Y = 3830291
03 meter
Z = 10369669
16 Z = 3183271
06
XDOT = -4684
335625 XDOT = -1469
172908
YDOT = 19016
193753 feet/sec YDOT = 5779
938210 meter/sec
ZDOT = -15750
167249 ZDOT = -4807
687319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3485433
18 X = 1062360
03
Y = 19373458
77 feet Y = 5905030
23 meter
Z = 10464163
78 Z = 3189477
12
XDOT = -14477
143349 XDOT = -4412
633293
YDOT = 11152
362428 feet/sec YDOT = 3399
240068 meter/sec
ZDOT = -15780
664340 ZDOT = -4809
946491
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
66870169
00016717 00000-0 10270-3 0 9134
2 25544 51
6481 244
5523 0005409 308
9394 51
1274 15
50012894 24254
Satellite: ISS
Catalog Number: 25544
Epoch time: 13358
66870169 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 244
5523 deg
Eccentricity:
0005409
Arg of perigee: 308
9394 deg
Mean anomaly: 51
1274 deg
Mean motion: 15
50012894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 312
Coasting Arc #15 (Orbit 2439)
---------------------------------------
Vector Time (GMT): 2013/359/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4929646
49 A = 6797752
46 meter
Y = -3674421
00 meter E =
0005338
Z = -2892564
92 I = 51
34637
XDOT = 1270
159340 Wp = 3
34138
YDOT = -5648
721990 meter/sec RA = 238
80348 deg
ZDOT = 5016
591978 TA = 323
62602
MA = 323
66229
Ha = 226
758 n
mi
Hp = 222
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16173380
89 X = -4874140
65
Y = -12055187
00 feet Y = -3729237
00 meter
Z = -9490042
39 Z = -2916377
96
XDOT = 4167
189435 XDOT = 1308
861006
YDOT = -18532
552459 feet/sec YDOT = -5634
302038 meter/sec
ZDOT = 16458
635100 ZDOT = 5022
856095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4669028
43 X = -1423119
87
Y = -19575617
55 feet Y = -5966648
23 meter
Z = -9589685
02 Z = -2922935
99
XDOT = 13553
530505 XDOT = 4131
116098
YDOT = -11299
703399 feet/sec YDOT = -3444
149596 meter/sec
ZDOT = 16485
854735 ZDOT = 5024
888523
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
63581565
00016717 00000-0 10270-3 0 9142
2 25544 51
6467 239
7601 0005183 311
5339 48
5366 15
49999076 24402
Satellite: ISS
Catalog Number: 25544
Epoch time: 13359
63581565 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 239
7601 deg
Eccentricity:
0005183
Arg of perigee: 311
5339 deg
Mean anomaly: 48
5366 deg
Mean motion: 15
49999076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2440
Checksum: 338
Coasting Arc #16 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2013/360/15:06:59
551
Vector Time (MET): N/A
Weight (LBS) : 901551
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5170768
06 A = 6798288
42 meter
Y = 3572580
13 meter E =
0009460
Z = 2584616
57 I = 51
36596
XDOT = -1166
139463 Wp = 85
35619
YDOT = 5479
756117 meter/sec RA = 233
83059 deg
ZDOT = -5224
077366 TA = 65
50728
MA = 65
40867
Ha = 226
907 n
mi
Hp = 222
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16964462
13 X = 5117878
99
Y = 11721063
42 feet Y = 3630107
13 meter
Z = 8479713
15 Z = 2609607
39
XDOT = -3825
916874 XDOT = -1201
951479
YDOT = 17978
202483 feet/sec YDOT = 5466
515577 meter/sec
ZDOT = -17139
361438 ZDOT = -5229
829133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5835910
56 X = 1778785
54
Y = 19731526
22 feet Y = 6014169
19 meter
Z = 8584338
03 Z = 2616506
23
XDOT = -12723
065644 XDOT = -3877
990408
YDOT = 11254
973770 feet/sec YDOT = 3430
516005 meter/sec
ZDOT = -17164
395841 ZDOT = -5231
707852
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
66738367
00016717 00000-0 10270-3 0 9152
2 25544 51
6471 234
6498 0005416 315
5241 44
5475 15
50062522 24563
Satellite: ISS
Catalog Number: 25544
Epoch time: 13360
66738367 = yrday
fracday
Element set: 915
Inclination: 51
6471 deg
RA of node: 234
6498 deg
Eccentricity:
0005416
Arg of perigee: 315
5241 deg
Mean anomaly: 44
5475 deg
Mean motion: 15
50062522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 309
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