[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 19th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 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 1863)
---------------------------------------
Vector Time (GMT): 2013/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4799612
54 A = 6794956
15 meter
Y = 3120118
60 meter E =
0006169
Z = -3666904
79 I = 51
97186
XDOT = -694
330396 Wp = 100
94536
YDOT = 6228
546729 meter/sec RA = 63
09039 deg
ZDOT = 4396
104263 TA = 215
83888
MA = 215
88029
Ha = 227
324 n
mi
Hp = 220
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15746760
30 X = 4782179
20
Y = 10236609
57 feet Y = 3173693
59 meter
Z = -12030527
51 Z = -3643630
38
XDOT = -2277
986862 XDOT = -785
283355
YDOT = 20434
864597 feet/sec YDOT = 6220
273562 meter/sec
ZDOT = 14422
914250 ZDOT = 4392
510514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17218084
92 X = -5248072
28
Y = 7656373
20 feet Y = 2333662
55 meter
Z = -11933135
74 Z = -3637219
77
XDOT = -15262
422378 XDOT = -4651
986341
YDOT = -11895
190440 feet/sec YDOT = -3625
654046 meter/sec
ZDOT = 14406
784642 ZDOT = 4391
187959
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 13322
50771295
00016717 00000-0 10270-3 0 9004
2 25544 51
6504 63
7720 0000764 119
5977 240
5250 15
50281750 18645
Satellite: ISS
Catalog Number: 25544
Epoch time: 13322
50771295 = yrday
fracday
Element set: 900
Inclination: 51
6504 deg
RA of node: 63
7720 deg
Eccentricity:
0000764
Arg of perigee: 119
5977 deg
Mean anomaly: 240
5250 deg
Mean motion: 15
50281750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1864
Checksum: 293
Coasting Arc #2 (Orbit 1879)
---------------------------------------
Vector Time (GMT): 2013/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5013973
07 A = 6795899
00 meter
Y = -3159224
50 meter E =
0013525
Z = 3313600
65 I = 51
96038
XDOT = 637
662445 Wp = 93
72032
YDOT = -5994
626938 meter/sec RA = 58
15691 deg
ZDOT = -4734
696470 TA = 47
98877
MA = 47
87369
Ha = 227
412 n
mi
Hp = 220
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16450042
90 X = -4994370
17
Y = -10364909
79 feet Y = -3215184
50 meter
Z = 10871393
22 Z = 3289290
19
XDOT = 2092
068390 XDOT = 727
648634
YDOT = -19667
411215 feet/sec YDOT = -5986
992811 meter/sec
ZDOT = -15533
781068 ZDOT = -4731
380425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17562853
10 X = 5353157
62
Y = -8472497
69 feet Y = -2582417
30 meter
Z = 10769653
23 Z = 3282590
30
XDOT = 14872
242729 XDOT = 4533
059584
YDOT = 11036
172300 feet/sec YDOT = 3363
825317 meter/sec
ZDOT = -15518
845427 ZDOT = -4730
144086
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 13323
53908363
00016717 00000-0 10270-3 0 9017
2 25544 51
6503 58
6611 0000951 116
8954 243
2294 15
50311562 18800
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
53908363 = yrday
fracday
Element set: 901
Inclination: 51
6503 deg
RA of node: 58
6611 deg
Eccentricity:
0000951
Arg of perigee: 116
8954 deg
Mean anomaly: 243
2294 deg
Mean motion: 15
50311562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1880
Checksum: 291
Coasting Arc #3 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2013/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5246750
18 A = 6796744
17 meter
Y = 3149365
88 meter E =
0005090
Z = -2959855
05 I = 51
94678
XDOT = -617
758362 Wp = 71
11874
YDOT = 5744
054753 meter/sec RA = 53
22256 deg
ZDOT = 5025
427513 TA = 255
31066
MA = 255
36709
Ha = 227
233 n
mi
Hp = 220
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17213747
32 X = 5225521
74
Y = 10332565
22 feet Y = 3207919
84 meter
Z = -9710810
52 Z = -2934417
76
XDOT = -2026
766280 XDOT = -706
356320
YDOT = 18845
323994 feet/sec YDOT = 5736
650934 meter/sec
ZDOT = 16487
623075 ZDOT = 5022
211555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17778276
34 X = -5418818
63
Y = 9437401
37 feet Y = 2876519
94 meter
Z = -9604331
70 Z = -2927400
30
XDOT = -14338
711591 XDOT = -4370
439293
YDOT = -10276
130248 feet/sec YDOT = -3132
164500 meter/sec
ZDOT = 16473
139751 ZDOT = 5021
012996
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 13324
50597126
00016717 00000-0 10270-3 0 9027
2 25544 51
6506 53
8693 0000699 111
6001 248
5224 15
50340696 18952
Satellite: ISS
Catalog Number: 25544
Epoch time: 13324
50597126 = yrday
fracday
Element set: 902
Inclination: 51
6506 deg
RA of node: 53
8693 deg
Eccentricity:
0000699
Arg of perigee: 111
6001 deg
Mean anomaly: 248
5224 deg
Mean motion: 15
50340696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 303
Coasting Arc #4 (Orbit 1910)
---------------------------------------
Vector Time (GMT): 2013/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5461262
61 A = 6797575
89 meter
Y = -3135686
76 meter E =
0014553
Z = 2541141
92 I = 51
93019
XDOT = 673
393077 Wp = 104
58285
YDOT = -5490
564211 meter/sec RA = 48
28768 deg
ZDOT = -5306
171421 TA = 47
03683
MA = 46
91488
Ha = 227
259 n
mi
Hp = 220
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17917528
24 X = -5438137
12
Y = -10287686
22 feet Y = -3196628
90 meter
Z = 8337079
78 Z = 2514667
23
XDOT = 2209
294871 XDOT = 760
516038
YDOT = -18013
662111 feet/sec YDOT = -5482
546495 meter/sec
ZDOT = -17408
698887 ZDOT = -5302
688755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17923991
57 X = 5463232
63
Y = -10365363
19 feet Y = -3159362
70 meter
Z = 8226237
14 Z = 2507357
08
XDOT = 13654
325972 XDOT = 4161
838556
YDOT = 9750
158989 feet/sec YDOT = 2971
848460 meter/sec
ZDOT = -17393
128032 ZDOT = -5301
425424
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 13325
53729767
00016717 00000-0 10270-3 0 9030
2 25544 51
6500 48
7580 0000887 109
9601 250
1645 15
50387062 19112
Satellite: ISS
Catalog Number: 25544
Epoch time: 13325
53729767 = yrday
fracday
Element set: 903
Inclination: 51
6500 deg
RA of node: 48
7580 deg
Eccentricity:
0000887
Arg of perigee: 109
9601 deg
Mean anomaly: 250
1645 deg
Mean motion: 15
50387062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1911
Checksum: 306
Coasting Arc #5 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2013/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5679338
47 A = 6798348
29 meter
Y = 3067883
37 meter E =
0006834
Z = -2128005
70 I = 51
91171
XDOT = -764
284487 Wp = 45
88404
YDOT = 5241
331789 meter/sec RA = 43
35140 deg
ZDOT = 5532
146129 TA = 290
67517
MA = 290
74842
Ha = 227
159 n
mi
Hp = 220
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18633000
23 X = 5654948
01
Y = 10065234
14 feet Y = 3131257
06 meter
Z = -6981645
99 Z = -2100474
76
XDOT = -2507
495035 XDOT = -849
711402
YDOT = 17195
970436 feet/sec YDOT = 5232
307178 meter/sec
ZDOT = 18150
085726 ZDOT = 5528
225992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17893673
17 X = -5453991
58
Y = 11397837
41 feet Y = 3474060
84 meter
Z = -6866351
24 Z = -2092863
86
XDOT = -12905
604721 XDOT = -3933
628319
YDOT = -9368
555606 feet/sec YDOT = -2855
535749 meter/sec
ZDOT = 18132
710529 ZDOT = 5526
850169
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 13326
50414456
00016717 00000-0 10270-3 0 9045
2 25544 51
6501 43
9657 0000688 100
7101 259
4127 15
50395831 19264
Satellite: ISS
Catalog Number: 25544
Epoch time: 13326
50414456 = yrday
fracday
Element set: 904
Inclination: 51
6501 deg
RA of node: 43
9657 deg
Eccentricity:
0000688
Arg of perigee: 100
7101 deg
Mean anomaly: 259
4127 deg
Mean motion: 15
50395831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 293
Coasting Arc #6 (Orbit 1941)
---------------------------------------
Vector Time (GMT): 2013/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5866090
20 A = 6798910
80 meter
Y = -2999190
49 meter E =
0014721
Z = 1650861
18 I = 51
89068
XDOT = 933
190337 Wp = 115
47737
YDOT = -4999
847638 meter/sec RA = 38
41429 deg
ZDOT = -5733
830801 TA = 46
52923
MA = 46
40691
Ha = 227
113 n
mi
Hp = 220
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19245702
75 X = -5840136
12
Y = -9839863
82 feet Y = -3064643
79 meter
Z = 5416211
22 Z = 1622426
87
XDOT = 3061
648088 XDOT = 1016
884076
YDOT = -16403
699601 feet/sec YDOT = -4988
943954 meter/sec
ZDOT = -18811
780843 ZDOT = -5729
094280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17781360
09 X = 5419758
56
Y = -12341767
27 feet Y = -3761770
66 meter
Z = 5297107
91 Z = 1614558
49
XDOT = 12056
347609 XDOT = 3674
774751
YDOT = 9256
554314 feet/sec YDOT = 2821
397755 meter/sec
ZDOT = -18791
007890 ZDOT = -5727
499205
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 13327
53542753
00016717 00000-0 10270-3 0 9052
2 25544 51
6496 38
8536 0000862 100
8488 259
2760 15
50462098 19428
Satellite: ISS
Catalog Number: 25544
Epoch time: 13327
53542753 = yrday
fracday
Element set: 905
Inclination: 51
6496 deg
RA of node: 38
8536 deg
Eccentricity:
0000862
Arg of perigee: 100
8488 deg
Mean anomaly: 259
2760 deg
Mean motion: 15
50462098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1942
Checksum: 324
Coasting Arc #7 (Orbit 1956)
---------------------------------------
Vector Time (GMT): 2013/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6040838
07 A = 6799484
10 meter
Y = 2877228
83 meter E =
0009807
Z = -1187295
74 I = 51
86761
XDOT = -1130
086084 Wp = 41
32357
YDOT = 4783
229925 meter/sec RA = 33
47545 deg
ZDOT = 5876
499566 TA = 305
84288
MA = 305
93394
Ha = 227
108 n
mi
Hp = 220
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19819022
52 X = 6013982
91
Y = 9439727
13 feet Y = 2944631
20 meter
Z = -3895327
23 Z = -1158014
75
XDOT = -3707
631510 XDOT = -1212
035969
YDOT = 15693
011564 feet/sec YDOT = 4770
134238 meter/sec
ZDOT = 19279
854218 ZDOT = 5870
810709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17468533
61 X = -5324409
04
Y = 13330159
55 feet Y = 4063032
63 meter
Z = -3772645
82 Z = -1149902
44
XDOT = -11235
161099 XDOT = -3424
477103
YDOT = -9307
038641 feet/sec YDOT = -2836
785378 meter/sec
ZDOT = 19255
108860 ZDOT = 5868
957181
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 13328
50223463
00016717 00000-0 10270-3 0 9065
2 25544 51
6494 34
0608 0000771 89
5663 270
5576 15
50448937 19574
Satellite: ISS
Catalog Number: 25544
Epoch time: 13328
50223463 = yrday
fracday
Element set: 906
Inclination: 51
6494 deg
RA of node: 34
0608 deg
Eccentricity:
0000771
Arg of perigee: 89
5663 deg
Mean anomaly: 270
5576 deg
Mean motion: 15
50448937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1957
Checksum: 323
Coasting Arc #8 (Orbit 1972)
---------------------------------------
Vector Time (GMT): 2013/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6170890
53 A = 6799638
55 meter
Y = -2761777
09 meter E =
0013862
Z = 663808
37 I = 51
84281
XDOT = 1400
523204 Wp = 125
65753
YDOT = -4585
460644 meter/sec RA = 28
53541 deg
ZDOT = -5978
593723 TA = 47
20384
MA = 47
08736
Ha = 227
000 n
mi
Hp = 220
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20245703
84 X = -6142773
73
Y = -9060948
46 feet Y = -2830626
72 meter
Z = 2177848
98 Z = 633898
66
XDOT = 4594
892402 XDOT = 1480
737465
YDOT = -15044
162218 feet/sec YDOT = -4569
350525 meter/sec
ZDOT = -19614
808802 ZDOT = -5971
595248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17080825
39 X = 5206235
58
Y = -14169154
84 feet Y = -4318758
39 meter
Z = 2052508
81 Z = 625604
69
XDOT = 10379
135502 XDOT = 3163
560501
YDOT = 9634
816671 feet/sec YDOT = 2936
692121 meter/sec
ZDOT = -19584
586086 ZDOT = -5969
381839
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 13329
53347516
00016717 00000-0 10270-3 0 9076
2 25544 51
6495 28
9483 0000924 93
0887 267
0369 15
50532592 19736
Satellite: ISS
Catalog Number: 25544
Epoch time: 13329
53347516 = yrday
fracday
Element set: 907
Inclination: 51
6495 deg
RA of node: 28
9483 deg
Eccentricity:
0000924
Arg of perigee: 93
0887 deg
Mean anomaly: 267
0369 deg
Mean motion: 15
50532592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1973
Checksum: 336
Coasting Arc #9 (Orbit 1987)
---------------------------------------
Vector Time (GMT): 2013/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6274877
32 A = 6799873
58 meter
Y = 2600070
10 meter E =
0012593
Z = -163708
88 I = 51
81556
XDOT = -1686
494993 Wp = 46
86745
YDOT = 4430
258892 meter/sec RA = 23
59342 deg
ZDOT = 6020
394453 TA = 311
37589
MA = 311
48411
Ha = 227
073 n
mi
Hp = 220
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20586867
84 X = 6246131
66
Y = 8530413
72 feet Y = 2670079
05 meter
Z = -537102
64 Z = -133295
51
XDOT = -5533
120055 XDOT = -1765
155613
YDOT = 14534
970118 feet/sec YDOT = 4410
959595 meter/sec
ZDOT = 19751
950306 ZDOT = 6012
010454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16495933
37 X = -5027960
49
Y = 14986392
36 feet Y = 4567852
39 meter
Z = -409623
21 Z = -124853
15
XDOT = -9644
002498 XDOT = -2939
491961
YDOT = -10111
829863 feet/sec YDOT = -3082
085742 meter/sec
ZDOT = 19715
924601 ZDOT = 6009
413818
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 13330
50024331
00016717 00000-0 10270-3 0 9083
2 25544 51
6493 24
1553 0000957 83
5993 276
5266 15
50505326 19880
Satellite: ISS
Catalog Number: 25544
Epoch time: 13330
50024331 = yrday
fracday
Element set: 908
Inclination: 51
6493 deg
RA of node: 24
1553 deg
Eccentricity:
0000957
Arg of perigee: 83
5993 deg
Mean anomaly: 276
5266 deg
Mean motion: 15
50505326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1988
Checksum: 307
Coasting Arc #10 (Orbit 2003)
---------------------------------------
Vector Time (GMT): 2013/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6322661
66 A = 6799542
10 meter
Y = -2456899
37 meter E =
0011918
Z = -388717
36 I = 51
78742
XDOT = 2033
740487 Wp = 133
75507
YDOT = -4303
085488 meter/sec RA = 18
64964 deg
ZDOT = -6004
851306 TA = 50
42057
MA = 50
31537
Ha = 226
926 n
mi
Hp = 219
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20743640
61 X = -6292829
83
Y = -8060693
46 feet Y = -2527436
60 meter
Z = -1275319
41 Z = -419360
30
XDOT = 6672
376925 XDOT = 2110
877791
YDOT = -14117
734540 feet/sec YDOT = -4279
911612 meter/sec
ZDOT = -19700
955729 ZDOT = -5994
784052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15867353
40 X = 4836369
32
Y = -15593471
06 feet Y = -4752889
98 meter
Z = -1403780
91 Z = -427872
42
XDOT = 8944
494908 XDOT = 2726
282048
YDOT = 10838
282995 feet/sec YDOT = 3303
508657 meter/sec
ZDOT = -19657
870612 ZDOT = -5991
718962
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 13331
53144229
00016717 00000-0 10270-3 0 9097
2 25544 51
6500 19
0424 0001050 90
9437 269
1834 15
50594742 20048
Satellite: ISS
Catalog Number: 25544
Epoch time: 13331
53144229 = yrday
fracday
Element set: 909
Inclination: 51
6500 deg
RA of node: 19
0424 deg
Eccentricity:
0001050
Arg of perigee: 90
9437 deg
Mean anomaly: 269
1834 deg
Mean motion: 15
50594742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2004
Checksum: 279
Coasting Arc #11 (Orbit 2019)
---------------------------------------
Vector Time (GMT): 2013/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6333997
70 A = 6799314
91 meter
Y = 2279951
16 meter E =
0014509
Z = 906572
17 I = 51
75635
XDOT = -2380
490780 Wp = 57
04397
YDOT = 4230
798539 meter/sec RA = 13
70369 deg
ZDOT = 5930
679090 TA = 312
74007
MA = 312
86209
Ha = 227
027 n
mi
Hp = 219
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20780832
35 X = 6303628
05
Y = 7480154
72 feet Y = 2350612
14 meter
Z = 2974318
14 Z = 937268
98
XDOT = -7810
009121 XDOT = -2456
433756
YDOT = 13880
572634 feet/sec YDOT = 4203
753735 meter/sec
ZDOT = 19457
608564 ZDOT = 5918
930211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15074104
42 X = -4594587
03
Y = 16117843
18 feet Y = 4912718
60 meter
Z = 3103028
06 Z = 945802
95
XDOT = -8444
388840 XDOT = -2573
849719
YDOT = -11670
918799 feet/sec YDOT = -3557
296050 meter/sec
ZDOT = 19407
461848 ZDOT = 5915
394371
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 13332
56262187
00016717 00000-0 10270-3 0 9107
2 25544 51
6494 13
9298 0001176 84
3771 275
7514 15
50571333 20206
Satellite: ISS
Catalog Number: 25544
Epoch time: 13332
56262187 = yrday
fracday
Element set: 910
Inclination: 51
6494 deg
RA of node: 13
9298 deg
Eccentricity:
0001176
Arg of perigee: 84
3771 deg
Mean anomaly: 275
7514 deg
Mean motion: 15
50571333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2020
Checksum: 297
Coasting Arc #12 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2013/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6281875
39 A = 6798499
85 meter
Y = -2137297
59 meter E =
0009070
Z = -1465345
55 I = 51
72515
XDOT = 2768
656859 Wp = 136
25636
YDOT = -4191
133072 meter/sec RA = 8
75514 deg
ZDOT = -5783
890930 TA = 59
68668
MA = 59
59699
Ha = 226
868 n
mi
Hp = 219
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20609827
38 X = -6250390
36
Y = -7012131
19 feet Y = -2207369
45 meter
Z = -4807564
15 Z = -1495786
55
XDOT = 9083
519879 XDOT = 2843
414442
YDOT = -13750
436587 feet/sec YDOT = -4159
754095 meter/sec
ZDOT = -18976
020111 ZDOT = -5770
259240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14292524
96 X = 4356361
61
Y = -16383376
61 feet Y = -4993653
19 meter
Z = -4935214
60 Z = -1504253
41
XDOT = 8041
046889 XDOT = 2450
911092
YDOT = 12686
794575 feet/sec YDOT = 3866
934987 meter/sec
ZDOT = -18917
960058 ZDOT = -5766
194226
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 13333
52933005
00016717 00000-0 10270-3 0 9119
2 25544 51
6503 9
1363 0001166 93
3177 266
8108 15
50650239 20355
Satellite: ISS
Catalog Number: 25544
Epoch time: 13333
52933005 = yrday
fracday
Element set: 911
Inclination: 51
6503 deg
RA of node: 9
1363 deg
Eccentricity:
0001166
Arg of perigee: 93
3177 deg
Mean anomaly: 266
8108 deg
Mean motion: 15
50650239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 278
Coasting Arc #13 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2013/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6188293
59 A = 6797762
11 meter
Y = 1977267
61 meter E =
0015164
Z = 1977660
30 I = 51
69095
XDOT = -3139
188050 Wp = 69
77365
YDOT = 4211
373710 meter/sec RA = 3
80390 deg
ZDOT = 5582
665913 TA = 312
01218
MA = 312
14119
Ha = 226
935 n
mi
Hp = 219
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20302800
50 X = 6156116
26
Y = 6487098
44 feet Y = 2046289
05 meter
Z = 6488386
82 Z = 2007645
09
XDOT = -10299
173393 XDOT = -3213
166953
YDOT = 13816
842879 feet/sec YDOT = 4175
855449 meter/sec
ZDOT = 18315
833049 ZDOT = 5567
236140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13404231
83 X = -4085609
86
Y = 16521653
82 feet Y = 5035800
08 meter
Z = 6614139
58 Z = 2015989
74
XDOT = -7887
521619 XDOT = -2404
116589
YDOT = -13743
551865 feet/sec YDOT = -4189
034609 meter/sec
ZDOT = 18250
205256 ZDOT = 5562
662562
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 13334
56046847
00016717 00000-0 10270-3 0 9124
2 25544 51
6492 4
0234 0001328 88
8021 271
3282 15
50645125 20510
Satellite: ISS
Catalog Number: 25544
Epoch time: 13334
56046847 = yrday
fracday
Element set: 912
Inclination: 51
6492 deg
RA of node: 4
0234 deg
Eccentricity:
0001328
Arg of perigee: 88
8021 deg
Mean anomaly: 271
3282 deg
Mean motion: 15
50645125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 278
Coasting Arc #14 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2013/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6030503
08 A = 6796544
98 meter
Y = -1869025
10 meter E =
0006275
Z = -2515601
46 I = 51
65726
XDOT = 3525
262951 Wp = 122
62639
YDOT = -4261
763596 meter/sec RA = 358
84933 deg
ZDOT = -5297
472018 TA = 85
53380
MA = 85
46211
Ha = 226
802 n
mi
Hp = 219
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19785115
10 X = -5996934
64
Y = -6131972
10 feet Y = -1936274
16 meter
Z = -8253285
62 Z = -2544816
35
XDOT = 11565
823330 XDOT = 3598
391192
YDOT = -13982
164028 feet/sec YDOT = -4221
932628 meter/sec
ZDOT = -17380
157538 ZDOT = -5280
168871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12601627
26 X = 3840975
99
Y = -16377218
92 feet Y = -4991776
33 meter
Z = -8375814
92 Z = -2552948
39
XDOT = 7867
218009 XDOT = 2397
928049
YDOT = 14883
263256 feet/sec YDOT = 4536
418640 meter/sec
ZDOT = -17306
639574 ZDOT = -5275
063742
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 13335
52713896
00016717 00000-0 10270-3 0 9137
2 25544 51
6498 359
2296 0001234 96
9420 263
1872 15
50704867 20667
Satellite: ISS
Catalog Number: 25544
Epoch time: 13335
52713896 = yrday
fracday
Element set: 913
Inclination: 51
6498 deg
RA of node: 359
2296 deg
Eccentricity:
0001234
Arg of perigee: 96
9420 deg
Mean anomaly: 263
1872 deg
Mean motion: 15
50704867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 328
Coasting Arc #15 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2013/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5832454
30 A = 6795375
99 meter
Y = 1761457
33 meter E =
0014414
Z = 2995154
01 I = 51
62141
XDOT = -3878
312308 Wp = 84
08490
YDOT = 4368
766664 meter/sec RA = 353
89139 deg
ZDOT = 4963
820102 TA = 310
16307
MA = 310
28921
Ha = 226
792 n
mi
Hp = 219
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19135348
75 X = 5797773
88
Y = 5779059
48 feet Y = 1826485
37 meter
Z = 9826620
77 Z = 3023404
03
XDOT = -12724
121747 XDOT = -3950
989944
YDOT = 14333
223962 feet/sec YDOT = 4324
990100 meter/sec
ZDOT = 16285
499023 ZDOT = 4944
803093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11766866
55 X = -3586540
92
Y = 16085932
53 feet Y = 4902992
24 meter
Z = 9945109
46 Z = 3031269
36
XDOT = -8109
037688 XDOT = -2471
634687
YDOT = -15988
660902 feet/sec YDOT = -4873
343843 meter/sec
ZDOT = 16204
751334 ZDOT = 4939
208206
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 13336
55823627
00016717 00000-0 10270-3 0 9146
2 25544 51
6486 354
1160 0001357 94
4354 265
6952 15
50720377 20821
Satellite: ISS
Catalog Number: 25544
Epoch time: 13336
55823627 = yrday
fracday
Element set: 914
Inclination: 51
6486 deg
RA of node: 354
1160 deg
Eccentricity:
0001357
Arg of perigee: 94
4354 deg
Mean anomaly: 265
6952 deg
Mean motion: 15
50720377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 311
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