[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 11th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24218 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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 3169)
---------------------------------------
Vector Time (GMT): 2014/041/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2286491
34 A = 6789727
57 meter
Y = -3833693
37 meter E =
0016864
Z = -5131351
69 I = 51
67582
XDOT = 7175
294240 Wp = 105
84646
YDOT = 2078
316022 meter/sec RA = 6
13245 deg
ZDOT = 1644
539828 TA = 180
05896
MA = 180
05916
Ha = 228
394 n
mi
Hp = 219
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7501612
01 X = 2354116
56
Y = -12577734
17 feet Y = -3807746
37 meter
Z = -16835143
33 Z = -5120080
12
XDOT = 23540
991602 XDOT = 7143
532285
YDOT = 6818
622120 feet/sec YDOT = 2158
377198 meter/sec
ZDOT = 5395
471876 ZDOT = 1679
318474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1162132
86 X = 354218
10
Y = -14654185
47 feet Y = -4466595
73 meter
Z = -16786897
45 Z = -5116646
34
XDOT = 23001
310558 XDOT = 7010
799458
YDOT = -4524
299075 feet/sec YDOT = -1379
006358 meter/sec
ZDOT = 5541
909715 ZDOT = 1689
174081
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 14041
69870848
00016717 00000-0 10270-3 0 9007
2 25544 51
6506 6
6208 0003624 119
6122 240
5390 15
50212841 31707
Satellite: ISS
Catalog Number: 25544
Epoch time: 14041
69870848 = yrday
fracday
Element set: 900
Inclination: 51
6506 deg
RA of node: 6
6208 deg
Eccentricity:
0003624
Arg of perigee: 119
6122 deg
Mean anomaly: 240
5390 deg
Mean motion: 15
50212841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 278
Coasting Arc #2 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2014/042/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2449121
36 A = 6790101
41 meter
Y = 3895995
57 meter E =
0008307
Z = 4986260
85 I = 51
64683
XDOT = -7150
500497 Wp = 79
50615
YDOT = -1806
027317 meter/sec RA = 1
17577 deg
ZDOT = -2096
555970 TA = 30
92547
MA = 30
87657
Ha = 228
295 n
mi
Hp = 219
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8035175
05 X = -2516726
32
Y = 12782137
70 feet Y = 3868230
10 meter
Z = 16359123
52 Z = 4974199
30
XDOT = -23459
647301 XDOT = -7119
589497
YDOT = -5925
286473 feet/sec YDOT = -1885
816024 meter/sec
ZDOT = -6878
464470 ZDOT = -2131
216152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1285317
85 X = -391764
88
Y = 15099015
36 feet Y = 4602179
88 meter
Z = 16307535
00 Z = 4970536
67
XDOT = -22394
653188 XDOT = -6825
890292
YDOT = 5696
137307 feet/sec YDOT = 1736
182651 meter/sec
ZDOT = -7024
447091 ZDOT = -2141
051473
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 14042
73013581
00016717 00000-0 10270-3 0 9017
2 25544 51
6506 1
5095 0003506 123
5520 236
5966 15
50275799 31862
Satellite: ISS
Catalog Number: 25544
Epoch time: 14042
73013581 = yrday
fracday
Element set: 901
Inclination: 51
6506 deg
RA of node: 1
5095 deg
Eccentricity:
0003506
Arg of perigee: 123
5520 deg
Mean anomaly: 236
5966 deg
Mean motion: 15
50275799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 293
Coasting Arc #3 (Orbit 3200)
---------------------------------------
Vector Time (GMT): 2014/043/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2611226
81 A = 6790805
21 meter
Y = -4009183
76 meter E =
0014773
Z = -4833133
78 I = 51
61847
XDOT = 7052
439248 Wp = 112
29461
YDOT = 1542
880329 meter/sec RA = 356
21686 deg
ZDOT = 2531
154826 TA = 182
66737
MA = 182
67526
Ha = 228
206 n
mi
Hp = 219
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8567017
08 X = 2679341
56
Y = -13153490
02 feet Y = -3979602
73 meter
Z = -15856738
11 Z = -4820283
48
XDOT = 23137
924042 XDOT = 7022
367028
YDOT = 5061
943338 feet/sec YDOT = 1621
577195 meter/sec
ZDOT = 8304
313733 ZDOT = 2565
340627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1311863
83 X = 399856
10
Y = -15697967
83 feet Y = -4784740
60 meter
Z = -15801805
09 Z = -4816390
19
XDOT = 21547
639814 XDOT = 6567
720615
YDOT = -6701
048218 feet/sec YDOT = -2042
479497 meter/sec
ZDOT = 8448
336546 ZDOT = 2575
052979
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 14043
69708278
00016717 00000-0 10270-3 0 9028
2 25544 51
6509 356
7174 0003522 127
6189 232
5282 15
50271631 32018
Satellite: ISS
Catalog Number: 25544
Epoch time: 14043
69708278 = yrday
fracday
Element set: 902
Inclination: 51
6509 deg
RA of node: 356
7174 deg
Eccentricity:
0003522
Arg of perigee: 127
6189 deg
Mean anomaly: 232
5282 deg
Mean motion: 15
50271631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3201
Checksum: 300
Coasting Arc #4 (Orbit 3216)
---------------------------------------
Vector Time (GMT): 2014/044/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2769972
87 A = 6791429
39 meter
Y = 4129843
34 meter E =
0010388
Z = 4617203
78 I = 51
59062
XDOT = -6941
632072 Wp = 82
78802
YDOT = -1320
159757 meter/sec RA = 351
25648 deg
ZDOT = -2976
611332 TA = 36
94589
MA = 36
87439
Ha = 228
104 n
mi
Hp = 219
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9087837
49 X = -2838376
17
Y = 13549354
79 feet Y = 4098485
56 meter
Z = 15148306
37 Z = 4603581
57
XDOT = -22774
383438 XDOT = -6911
894771
YDOT = -4331
232797 feet/sec YDOT = -1397
619450 meter/sec
ZDOT = -9765
785210 ZDOT = -3010
259651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1295301
11 X = -394807
78
Y = 16317354
47 feet Y = 4973529
64 meter
Z = 15090100
37 Z = 4599462
59
XDOT = -20700
715175 XDOT = -6309
577985
YDOT = 7540
560725 feet/sec YDOT = 2298
362909 meter/sec
ZDOT = -9907
573734 ZDOT = -3019
828474
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 14044
72847175
00016717 00000-0 10270-3 0 9034
2 25544 51
6512 351
6061 0003420 131
1753 228
9693 15
50336108 32178
Satellite: ISS
Catalog Number: 25544
Epoch time: 14044
72847175 = yrday
fracday
Element set: 903
Inclination: 51
6512 deg
RA of node: 351
6061 deg
Eccentricity:
0003420
Arg of perigee: 131
1753 deg
Mean anomaly: 228
9693 deg
Mean motion: 15
50336108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3217
Checksum: 286
Coasting Arc #5 (Orbit 3231)
---------------------------------------
Vector Time (GMT): 2014/045/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2911219
25 A = 6792340
56 meter
Y = -4298330
36 meter E =
0011966
Z = -4392565
82 I = 51
56286
XDOT = 6766
990505 Wp = 117
15751
YDOT = 1119
741748 meter/sec RA = 346
29392 deg
ZDOT = 3390
975840 TA = 187
29119
MA = 187
30861
Ha = 228
007 n
mi
Hp = 219
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9551244
27 X = 2980404
95
Y = -14102133
74 feet Y = -4265388
77 meter
Z = -14411305
20 Z = -4378255
47
XDOT = 22201
412419 XDOT = 6737
494488
YDOT = 3673
693398 feet/sec YDOT = 1195
249925 meter/sec
ZDOT = 11125
248820 ZDOT = 3423
776406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1128352
00 X = 343921
69
Y = -17046451
53 feet Y = -5195758
43 meter
Z = -14350173
26 Z = -4373932
81
XDOT = 19681
224691 XDOT = 5998
837286
YDOT = -8174
164702 feet/sec YDOT = -2491
485401 meter/sec
ZDOT = 11263
488408 ZDOT = 3433
111267
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 14045
69538249
00016717 00000-0 10270-3 0 9041
2 25544 51
6509 346
8138 0003432 136
0979 224
0444 15
50329740 32324
Satellite: ISS
Catalog Number: 25544
Epoch time: 14045
69538249 = yrday
fracday
Element set: 904
Inclination: 51
6509 deg
RA of node: 346
8138 deg
Eccentricity:
0003432
Arg of perigee: 136
0979 deg
Mean anomaly: 224
0444 deg
Mean motion: 15
50329740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3232
Checksum: 309
Coasting Arc #6 (Orbit 3247)
---------------------------------------
Vector Time (GMT): 2014/046/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3043492
02 A = 6793157
50 meter
Y = 4468248
39 meter E =
0012507
Z = 4102345
91 I = 51
53663
XDOT = -6580
975833 Wp = 90
41477
YDOT = -973
139461 meter/sec RA = 341
33036 deg
ZDOT = -3812
441671 TA = 39
05132
MA = 38
96109
Ha = 227
890 n
mi
Hp = 219
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9985210
05 X = -3113158
23
Y = 14659607
57 feet Y = 4433824
99 meter
Z = 13459140
13 Z = 4087391
73
XDOT = -21591
128061 XDOT = -6551
085643
YDOT = -3192
714766 feet/sec YDOT = -1046
565395 meter/sec
ZDOT = -12508
010733 ZDOT = -3844
337731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -907987
55 X = -276754
60
Y = 17762298
75 feet Y = 5413948
66 meter
Z = 13395270
39 Z = 4082878
41
XDOT = -18707
688343 XDOT = -5702
103407
YDOT = 8602
695282 feet/sec YDOT = 2622
101522 meter/sec
ZDOT = -12642
451590 ZDOT = -3853
419245
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 14046
72673284
00016717 00000-0 10270-3 0 9056
2 25544 51
6512 341
7024 0003325 139
4248 220
7151 15
50394829 32488
Satellite: ISS
Catalog Number: 25544
Epoch time: 14046
72673284 = yrday
fracday
Element set: 905
Inclination: 51
6512 deg
RA of node: 341
7024 deg
Eccentricity:
0003325
Arg of perigee: 139
4248 deg
Mean anomaly: 220
7151 deg
Mean motion: 15
50394829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3248
Checksum: 298
Coasting Arc #7 (Orbit 3262)
---------------------------------------
Vector Time (GMT): 2014/047/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3143050
98 A = 6794193
45 meter
Y = -4677943
30 meter E =
0008784
Z = -3804833
79 I = 51
50994
XDOT = 6346
426727 Wp = 117
47015
YDOT = 859
166747 meter/sec RA = 336
36442 deg
ZDOT = 4189
751081 TA = 196
89709
MA = 196
92637
Ha = 227
809 n
mi
Hp = 219
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10311847
06 X = 3213609
51
Y = -15347583
00 feet Y = -4642401
59 meter
Z = -12483050
50 Z = -3789393
69
XDOT = 20821
609998 XDOT = 6315
995568
YDOT = 2818
788541 feet/sec YDOT = 929
966864 meter/sec
ZDOT = 13745
902497 ZDOT = 4220
506538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 502507
88 X = 153164
40
Y = -18527602
91 feet Y = -5647213
37 meter
Z = -12417103
52 Z = -3784733
15
XDOT = 17645
780783 XDOT = 5378
433983
YDOT = -8813
000354 feet/sec YDOT = -2686
202508 meter/sec
ZDOT = 13875
542142 ZDOT = 4229
265245
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 14047
69360733
00016717 00000-0 10270-3 0 9066
2 25544 51
6501 336
9096 0003386 144
9001 215
2374 15
50386242 32639
Satellite: ISS
Catalog Number: 25544
Epoch time: 14047
69360733 = yrday
fracday
Element set: 906
Inclination: 51
6501 deg
RA of node: 336
9096 deg
Eccentricity:
0003386
Arg of perigee: 144
9001 deg
Mean anomaly: 215
2374 deg
Mean motion: 15
50386242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3263
Checksum: 299
Coasting Arc #8 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2014/048/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3229347
13 A = 6795097
92 meter
Y = 4879228
62 meter E =
0014357
Z = 3440169
42 I = 51
48574
XDOT = -6105
256949 Wp = 100
61376
YDOT = -811
007735 meter/sec RA = 331
39795 deg
ZDOT = -4567
192960 TA = 39
01368
MA = 38
91020
Ha = 227
659 n
mi
Hp = 219
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10594970
91 X = -3300378
74
Y = 16007967
92 feet Y = 4842719
23 meter
Z = 11286645
07 Z = 3424308
86
XDOT = -20030
370567 XDOT = -6073
548704
YDOT = -2660
786531 feet/sec YDOT = -879
103860 meter/sec
ZDOT = -14984
228872 ZDOT = -4596
773873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -48824
79 X = -14881
80
Y = 19236182
77 feet Y = 5863188
51 meter
Z = 11218898
83 Z = 3419520
36
XDOT = -16687
080865 XDOT = -5086
222248
YDOT = 8795
734649 feet/sec YDOT = 2680
939921 meter/sec
ZDOT = -15108
913082 ZDOT = -4605
196707
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 14048
72491896
00016717 00000-0 10270-3 0 9077
2 25544 51
6503 331
7980 0003252 148
4022 211
7325 15
50451936 32797
Satellite: ISS
Catalog Number: 25544
Epoch time: 14048
72491896 = yrday
fracday
Element set: 907
Inclination: 51
6503 deg
RA of node: 331
7980 deg
Eccentricity:
0003252
Arg of perigee: 148
4022 deg
Mean anomaly: 211
7325 deg
Mean motion: 15
50451936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 308
Coasting Arc #9 (Orbit 3293)
---------------------------------------
Vector Time (GMT): 2014/049/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3271438
16 A = 6796141
74 meter
Y = -5107981
60 meter E =
0006020
Z = -3071929
03 I = 51
46079
XDOT = 5835
491069 Wp = 105
35207
YDOT = 801
066172 meter/sec RA = 326
42887 deg
ZDOT = 4888
947202 TA = 219
36491
MA = 219
40868
Ha = 227
615 n
mi
Hp = 219
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10733064
83 X = 3343235
89
Y = -16758469
83 feet Y = -5070997
19 meter
Z = -10078507
32 Z = -3055862
07
XDOT = 19145
311907 XDOT = 5802
351004
YDOT = 2628
169855 feet/sec YDOT = 866
137623 meter/sec
ZDOT = 16039
853026 ZDOT = 4917
214274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -599669
00 X = -182779
11
Y = -19926474
80 feet Y = -6073589
52 meter
Z = -10009860
16 Z = -3051005
38
XDOT = 15729
682445 XDOT = 4794
407209
YDOT = -8579
932595 feet/sec YDOT = -2615
163455 meter/sec
ZDOT = 16158
988497 ZDOT = 4925
259694
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 14049
69175737
00016717 00000-0 10270-3 0 9088
2 25544 51
6487 327
0045 0003396 153
7088 206
4236 15
50440934 32943
Satellite: ISS
Catalog Number: 25544
Epoch time: 14049
69175737 = yrday
fracday
Element set: 908
Inclination: 51
6487 deg
RA of node: 327
0045 deg
Eccentricity:
0003396
Arg of perigee: 153
7088 deg
Mean anomaly: 206
4236 deg
Mean motion: 15
50440934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3294
Checksum: 325
Coasting Arc #10 (Orbit 3309)
---------------------------------------
Vector Time (GMT): 2014/050/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3298697
20 A = 6796983
63 meter
Y = 5315121
97 meter E =
0015661
Z = 2636852
76 I = 51
43910
XDOT = -5567
153171 Wp = 112
23135
YDOT = -865
646870 meter/sec RA = 321
45971 deg
ZDOT = -5200
603888 TA = 37
98405
MA = 37
87370
Ha = 227
417 n
mi
Hp = 219
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10822497
36 X = -3370695
79
Y = 17438064
21 feet Y = 5277831
54 meter
Z = 8651091
73 Z = 2620652
86
XDOT = -18264
938226 XDOT = -5531
796909
YDOT = -2840
048787 feet/sec YDOT = -927
705197 meter/sec
ZDOT = -17062
348714 ZDOT = -5227
562124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1271350
23 X = 387507
55
Y = 20513150
14 feet Y = 6252408
16 meter
Z = 8581856
47 Z = 2615749
85
XDOT = -14937
165991 XDOT = -4552
848194
YDOT = 8137
766148 feet/sec YDOT = 2480
391122 meter/sec
ZDOT = -17175
945684 ZDOT = -5235
228245
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 14050
72303032
00016717 00000-0 10270-3 0 9096
2 25544 51
6488 321
8924 0003219 157
7113 202
4178 15
50509173 33100
Satellite: ISS
Catalog Number: 25544
Epoch time: 14050
72303032 = yrday
fracday
Element set: 909
Inclination: 51
6488 deg
RA of node: 321
8924 deg
Eccentricity:
0003219
Arg of perigee: 157
7113 deg
Mean anomaly: 202
4178 deg
Mean motion: 15
50509173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3310
Checksum: 280
Coasting Arc #11 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2014/051/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3275571
83 A = 6797896
33 meter
Y = -5534631
26 meter E =
0005403
Z = -2204296
39 I = 51
41673
XDOT = 5292
752163 Wp = 75
95631
YDOT = 967
853414 meter/sec RA = 316
48785 deg
ZDOT = 5447
425436 TA = 259
53861
MA = 259
59951
Ha = 227
428 n
mi
Hp = 219
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10746626
73 X = 3347925
56
Y = -18158239
03 feet Y = -5497597
36 meter
Z = -7231943
55 Z = -2188207
99
XDOT = 17364
672452 XDOT = 5255
074384
YDOT = 3175
372093 feet/sec YDOT = 1026
830190 meter/sec
ZDOT = 17872
130695 ZDOT = 5473
045090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2120288
30 X = -646263
87
Y = -21016810
41 feet Y = -6405923
81 meter
Z = -7163148
44 Z = -2183327
65
XDOT = 14227
955148 XDOT = 4336
680729
YDOT = -7549
359120 feet/sec YDOT = -2301
044660 meter/sec
ZDOT = 17980
059502 ZDOT = 5480
322136
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 14051
68983299
00016717 00000-0 10270-3 0 9103
2 25544 51
6471 317
0983 0003454 161
9965 198
1309 15
50494670 33255
Satellite: ISS
Catalog Number: 25544
Epoch time: 14051
68983299 = yrday
fracday
Element set: 910
Inclination: 51
6471 deg
RA of node: 317
0983 deg
Eccentricity:
0003454
Arg of perigee: 161
9965 deg
Mean anomaly: 198
1309 deg
Mean motion: 15
50494670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 332
Coasting Arc #12 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2014/052/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3240129
48 A = 6798501
40 meter
Y = 5717096
66 meter E =
0016160
Z = 1707751
52 I = 51
39790
XDOT = -5030
277950 Wp = 124
39060
YDOT = -1148
070185 meter/sec RA = 311
51634 deg
ZDOT = -5671
056041 TA = 36
83488
MA = 36
72397
Ha = 227
176 n
mi
Hp = 219
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10630346
06 X = -3312114
17
Y = 18756878
81 feet Y = 5680461
10 meter
Z = 5602859
33 Z = 1691836
26
XDOT = -16503
536581 XDOT = -4989
518135
YDOT = -3766
634464 feet/sec YDOT = -1204
094511 meter/sec
ZDOT = -18605
826907 ZDOT = -5695
393157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2945952
29 X = 897926
26
Y = 21375324
13 feet Y = 6515198
79 meter
Z = 5534769
77 Z = 1686997
83
XDOT = -13739
585675 XDOT = -4187
825714
YDOT = 6763
150769 feet/sec YDOT = 2061
408354 meter/sec
ZDOT = -18708
313462 ZDOT = -5702
293943
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 14052
72106757
00016717 00000-0 10270-3 0 9116
2 25544 51
6474 311
9856 0003232 166
3715 193
7523 15
50568051 33418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14052
72106757 = yrday
fracday
Element set: 911
Inclination: 51
6474 deg
RA of node: 311
9856 deg
Eccentricity:
0003232
Arg of perigee: 166
3715 deg
Mean anomaly: 193
7523 deg
Mean motion: 15
50568051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 298
Coasting Arc #13 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2014/053/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3154400
37 A = 6799136
56 meter
Y = -5896090
38 meter E =
0007324
Z = -1222104
60 I = 51
37894
XDOT = 4784
192639 Wp = 59
02761
YDOT = 1358
567853 meter/sec RA = 306
54232 deg
ZDOT = 5823
839447 TA = 287
66875
MA = 287
74870
Ha = 227
243 n
mi
Hp = 219
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10349082
57 X = 3226033
87
Y = -19344128
53 feet Y = -5860415
40 meter
Z = -4009529
54 Z = -1206606
74
XDOT = 15696
170074 XDOT = 4740
355164
YDOT = 4457
243612 feet/sec YDOT = 1411
823020 meter/sec
ZDOT = 19107
084799 ZDOT = 5846
973610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3906379
14 X = -1190664
36
Y = -21600155
26 feet Y = -6583727
32 meter
Z = -3943176
47 Z = -1201880
19
XDOT = 13395
715191 XDOT = 4083
013990
YDOT = -5910
345124 feet/sec YDOT = -1801
473194 meter/sec
ZDOT = 19204
462365 ZDOT = 5853
520129
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 14053
68783489
00016717 00000-0 10270-3 0 9126
2 25544 51
6463 307
1912 0003538 169
3303 190
7923 15
50549661 33564
Satellite: ISS
Catalog Number: 25544
Epoch time: 14053
68783489 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 307
1912 deg
Eccentricity:
0003538
Arg of perigee: 169
3303 deg
Mean anomaly: 190
7923 deg
Mean motion: 15
50549661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3356
Checksum: 324
Coasting Arc #14 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2014/054/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3063904
32 A = 6799349
71 meter
Y = 6022217
28 meter E =
0015617
Z = 678402
38 I = 51
36298
XDOT = -4561
305809 Wp = 136
30824
YDOT = -1643
696850 meter/sec RA = 301
56880 deg
ZDOT = -5938
339050 TA = 36
34384
MA = 36
23788
Ha = 226
958 n
mi
Hp = 219
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10052179
53 X = -3134313
81
Y = 19757930
71 feet Y = 5987561
10 meter
Z = 2225729
58 Z = 663347
20
XDOT = -14964
914071 XDOT = -4513
740419
YDOT = -5392
706202 feet/sec YDOT = -1694
438663 meter/sec
ZDOT = -19482
739665 ZDOT = -5960
381342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4778038
28 X = 1456346
07
Y = 21653532
06 feet Y = 6599996
57 meter
Z = 2161229
07 Z = 658742
62
XDOT = -13310
789366 XDOT = -4057
128599
YDOT = 4914
879784 feet/sec YDOT = 1498
055358 meter/sec
ZDOT = -19575
467071 ZDOT = -5966
602363
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 14054
71903161
00016717 00000-0 10270-3 0 9133
2 25544 51
6466 302
0782 0003284 173
6237 186
4956 15
50626201 33720
Satellite: ISS
Catalog Number: 25544
Epoch time: 14054
71903161 = yrday
fracday
Element set: 913
Inclination: 51
6466 deg
RA of node: 302
0782 deg
Eccentricity:
0003284
Arg of perigee: 173
6237 deg
Mean anomaly: 186
4956 deg
Mean motion: 15
50626201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 297
Coasting Arc #15 (Orbit 3386)
---------------------------------------
Vector Time (GMT): 2014/055/16:27:06
921
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2929674
70 A = 6799566
07 meter
Y = -6130599
37 meter E =
0009793
Z = -155848
79 I = 51
34774
XDOT = 4374
205924 Wp = 60
32037
YDOT = 1945
662092 meter/sec RA = 296
59321 deg
ZDOT = 5979
649930 TA = 297
99702
MA = 298
09607
Ha = 227
049 n
mi
Hp = 219
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9611793
63 X = 2998767
75
Y = -20113514
98 feet Y = -6097451
56 meter
Z = -511314
91 Z = -141448
92
XDOT = 14351
069305 XDOT = 4323
077242
YDOT = 6383
405814 feet/sec YDOT = 1994
291706 meter/sec
ZDOT = 19618
274050 ZDOT = 6000
774574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5723687
12 X = -1744579
83
Y = -21546201
48 feet Y = -6567282
21 meter
Z = -449568
76 Z = -137028
56
XDOT = 13400
388736 XDOT = 4084
438487
YDOT = -3948
491556 feet/sec YDOT = -1203
500226 meter/sec
ZDOT = 19707
085922 ZDOT = 6006
719789
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 14055
68576365
00016717 00000-0 10270-3 0 9143
2 25544 51
6461 297
2841 0003626 175
9319 184
1862 15
50609233 33875
Satellite: ISS
Catalog Number: 25544
Epoch time: 14055
68576365 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 297
2841 deg
Eccentricity:
0003626
Arg of perigee: 175
9319 deg
Mean anomaly: 184
1862 deg
Mean motion: 15
50609233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3387
Checksum: 332
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