[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 19th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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 2839)
---------------------------------------
Vector Time (GMT): 2015/170/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 953746
71 A = 6785333
94 meter
Y = 6554548
35 meter E =
0017193
Z = 1435696
39 I = 52
00900
XDOT = -4965
791205 Wp = 62
71974
YDOT = -562
858240 meter/sec RA = 71
97432 deg
ZDOT = 5822
914119 TA = 312
87261
MA = 313
01687
Ha = 220
511 n
mi
Hp = 211
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3129090
26 X = 873407
27
Y = 21504423
74 feet Y = 6564764
39 meter
Z = 4710289
99 Z = 1440135
18
XDOT = -16291
965897 XDOT = -4987
413460
YDOT = -1846
647769 feet/sec YDOT = -618
510610 meter/sec
ZDOT = 19104
048946 ZDOT = 5798
738840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21265016
76 X = 6481577
11
Y = 4456748
07 feet Y = 1358416
81 meter
Z = 4728079
61 Z = 1441118
66
XDOT = -7031
855553 XDOT = -2143
309572
YDOT = 13236
937926 feet/sec YDOT = 4034
618680 meter/sec
ZDOT = 19000
168924 ZDOT = 5791
251488
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 15170
51548115
00016717 00000-0 10270-3 0 9001
2 25544 51
6436 72
4079 0003357 70
4524 289
6992 15
55202142 28402
Satellite: ISS
Catalog Number: 25544
Epoch time: 15170
51548115 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 72
4079 deg
Eccentricity:
0003357
Arg of perigee: 70
4524 deg
Mean anomaly: 289
6992 deg
Mean motion: 15
55202142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 297
Coasting Arc #2 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2015/171/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 305570
16 A = 6781425
13 meter
Y = -5912930
66 meter E =
0007869
Z = -3313678
18 I = 51
98653
XDOT = 5263
953174 Wp = 85
82947
YDOT = 2922
995762 meter/sec RA = 67
01573 deg
ZDOT = -4739
493118 TA = 132
47777
MA = 132
41124
Ha = 220
426 n
mi
Hp = 211
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1002526
78 X = 387763
74
Y = -19399378
81 feet Y = -5909053
63 meter
Z = -10871647
56 Z = -3311994
81
XDOT = 17270
187578 XDOT = 5253
898806
YDOT = 9589
881110 feet/sec YDOT = 2981
805044 meter/sec
ZDOT = -15549
518105 ZDOT = -4713
946147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17987925
15 X = -5482719
59
Y = -7345652
73 feet Y = -2238954
95 meter
Z = -10863222
99 Z = -3311110
37
XDOT = 14197
078024 XDOT = 4327
269382
YDOT = -11975
862034 feet/sec YDOT = -3650
242748 meter/sec
ZDOT = -15440
208051 ZDOT = -4706
175414
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 15171
47932979
00016717 00000-0 10270-3 0 9013
2 25544 51
6443 67
5948 0003311 73
6994 286
4523 15
55247633 28551
Satellite: ISS
Catalog Number: 25544
Epoch time: 15171
47932979 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 67
5948 deg
Eccentricity:
0003311
Arg of perigee: 73
6994 deg
Mean anomaly: 286
4523 deg
Mean motion: 15
55247633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 338
Coasting Arc #3 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2015/172/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1664520
85 A = 6776845
16 meter
Y = 4629586
00 meter E =
0011009
Z = 4652865
28 I = 51
95775
XDOT = -5179
643079 Wp = 104
73589
YDOT = -4835
451614 meter/sec RA = 62
04155 deg
ZDOT = 2949
754148 TA = 316
01224
MA = 316
09981
Ha = 220
457 n
mi
Hp = 211
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5461026
40 X = -1738767
98
Y = 15188930
44 feet Y = 4610556
65 meter
Z = 15265306
05 Z = 4644599
53
XDOT = -16993
579656 XDOT = -5139
515631
YDOT = -15864
342567 feet/sec YDOT = -4893
149692 meter/sec
ZDOT = 9677
671089 ZDOT = 2924
689632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12717856
24 X = 3876402
58
Y = 9994760
06 feet Y = 3046402
87 meter
Z = 15228817
75 Z = 4641743
65
XDOT = -19641
451169 XDOT = -5986
714316
YDOT = 10367
174660 feet/sec YDOT = 3159
914836 meter/sec
ZDOT = 9570
823806 ZDOT = 2917
187096
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 15172
50741698
00016717 00000-0 10270-3 0 9025
2 25544 51
6439 62
4608 0003278 78
0172 282
1349 15
55269971 28718
Satellite: ISS
Catalog Number: 25544
Epoch time: 15172
50741698 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 62
4608 deg
Eccentricity:
0003278
Arg of perigee: 78
0172 deg
Mean anomaly: 282
1349 deg
Mean motion: 15
55269971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 327
Coasting Arc #4 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2015/173/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3072553
87 A = 6774053
22 meter
Y = -2903414
38 meter E =
0017886
Z = -5308642
57 I = 51
93371
XDOT = 4584
767860 Wp = 83
80198
YDOT = 6095
050422 meter/sec RA = 57
05307 deg
ZDOT = -680
016209 TA = 179
72172
MA = 179
72072
Ha = 220
308 n
mi
Hp = 211
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10080557
32 X = 3130579
43
Y = -9525637
72 feet Y = -2868730
18 meter
Z = -17416806
32 Z = -5293576
09
XDOT = 15041
889304 XDOT = 4519
574040
YDOT = 19996
884585 feet/sec YDOT = 6145
955835 meter/sec
ZDOT = -2231
024308 ZDOT = -657
902259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6113770
43 X = -1863477
23
Y = -12539976
12 feet Y = -3822184
72 meter
Z = -17351408
07 Z = -5288709
18
XDOT = 22622
351089 XDOT = 6895
292612
YDOT = -8072
623184 feet/sec YDOT = -2460
535546 meter/sec
ZDOT = -2137
130679 ZDOT = -651
397431
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 15173
47123092
00016717 00000-0 10270-3 0 9035
2 25544 51
6446 57
6474 0003228 80
0109 280
1409 15
55312675 28862
Satellite: ISS
Catalog Number: 25544
Epoch time: 15173
47123092 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 57
6474 deg
Eccentricity:
0003228
Arg of perigee: 80
0109 deg
Mean anomaly: 280
1409 deg
Mean motion: 15
55312675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 301
Coasting Arc #5 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2015/174/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4333204
45 A = 6774728
62 meter
Y = 958526
83 meter E =
0008057
Z = 5113349
79 I = 51
91828
XDOT = -3478
018932 Wp = 64
59460
YDOT = -6627
365445 meter/sec RA = 52
06011 deg
ZDOT = -1699
586777 TA = 41
77556
MA = 41
71408
Ha = 220
309 n
mi
Hp = 211
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14216550
05 X = -4368439
52
Y = 3144773
07 feet Y = 909872
69 meter
Z = 16776081
98 Z = 5092214
49
XDOT = -11410
823268 XDOT = -3395
395727
YDOT = -21743
324952 feet/sec YDOT = -6665
796823 meter/sec
ZDOT = -5576
072103 ZDOT = -1716
282092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -947709
48 X = -288861
85
Y = 14633877
52 feet Y = 4460405
87 meter
Z = 16684972
13 Z = 5085579
51
XDOT = -22977
957820 XDOT = -7003
681544
YDOT = 4970
384570 feet/sec YDOT = 1514
973217 meter/sec
ZDOT = -5646
539428 ZDOT = -1721
065218
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 15174
49927979
00016717 00000-0 10270-3 0 9045
2 25544 51
6445 52
5132 0003042 82
0155 278
1343 15
55364666 29023
Satellite: ISS
Catalog Number: 25544
Epoch time: 15174
49927979 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 52
5132 deg
Eccentricity:
0003042
Arg of perigee: 82
0155 deg
Mean anomaly: 278
1343 deg
Mean motion: 15
55364666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 312
Coasting Arc #6 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2015/175/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5294092
89 A = 6778616
53 meter
Y = 926276
57 meter E =
0010285
Z = -4141041
01 I = 51
91140
XDOT = 1858
428010 Wp = 101
81777
YDOT = 6382
023383 meter/sec RA = 47
07386 deg
ZDOT = 3809
375875 TA = 207
33451
MA = 207
38867
Ha = 220
201 n
mi
Hp = 211
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17369071
17 X = 5303457
18
Y = 3038965
13 feet Y = 985531
26 meter
Z = -13586092
56 Z = -4115300
55
XDOT = 6097
204758 XDOT = 1768
420078
YDOT = 20938
396925 feet/sec YDOT = 6402
301986 meter/sec
ZDOT = 12497
952345 ZDOT = 3818
185615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7482534
54 X = 2280676
53
Y = -16059974
26 feet Y = -4895080
15 meter
Z = -13475561
48 Z = -4107351
14
XDOT = 20613
125163 XDOT = 6282
880550
YDOT = -897
077828 feet/sec YDOT = -273
429322 meter/sec
ZDOT = 12534
539947 ZDOT = 3820
527776
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 15175
46306043
00016717 00000-0 10270-3 0 9057
2 25544 51
6450 47
6997 0003026 85
0765 275
0734 15
55353781 29177
Satellite: ISS
Catalog Number: 25544
Epoch time: 15175
46306043 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 47
6997 deg
Eccentricity:
0003026
Arg of perigee: 85
0765 deg
Mean anomaly: 275
0734 deg
Mean motion: 15
55353781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 318
Coasting Arc #7 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2015/176/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5753973
57 A = 6783221
05 meter
Y = -2585777
79 meter E =
0016771
Z = 2473544
56 I = 51
90460
XDOT = 162
674530 Wp = 102
31668
YDOT = -5502
404074 meter/sec RA = 42
10147 deg
ZDOT = -5346
655733 TA = 50
04689
MA = 49
89969
Ha = 220
254 n
mi
Hp = 211
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18877866
05 X = -5736646
70
Y = -8483522
94 feet Y = -2650025
81 meter
Z = 8115303
66 Z = 2445634
71
XDOT = 533
709089 XDOT = 250
163720
YDOT = -18052
506806 feet/sec YDOT = -5500
095336 meter/sec
ZDOT = -17541
521434 ZDOT = -5345
653425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12845314
59 X = -3915251
89
Y = 16287031
55 feet Y = 4964287
22 meter
Z = 7995788
76 Z = 2437116
42
XDOT = -16163
268434 XDOT = -4926
564219
YDOT = -4094
589914 feet/sec YDOT = -1248
031006 meter/sec
ZDOT = -17536
075937 ZDOT = -5344
995945
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 15176
49107491
00016717 00000-0 10270-3 0 9068
2 25544 51
6450 42
5654 0003108 89
9477 270
2033 15
55363953 29334
Satellite: ISS
Catalog Number: 25544
Epoch time: 15176
49107491 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 42
5654 deg
Eccentricity:
0003108
Arg of perigee: 89
9477 deg
Mean anomaly: 270
2033 deg
Mean motion: 15
55363953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 316
Coasting Arc #8 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2015/177/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5597037
96 A = 6785492
14 meter
Y = 3801264
65 meter E =
0013316
Z = -444939
91 I = 51
88897
XDOT = -2345
219430 Wp = 51
31209
YDOT = 4142
025448 meter/sec RA = 37
13956 deg
ZDOT = 6014
492026 TA = 303
90385
MA = 304
03042
Ha = 220
047 n
mi
Hp = 211
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18362985
44 X = 5556276
68
Y = 12471340
71 feet Y = 3863626
52 meter
Z = -1459776
61 Z = -417849
17
XDOT = -7694
289467 XDOT = -2420
578489
YDOT = 13589
322336 feet/sec YDOT = 4115
377784 meter/sec
ZDOT = 19732
585386 ZDOT = 6002
916690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16320646
99 X = 4974533
20
Y = -15056378
90 feet Y = -4589184
29 meter
Z = -1344045
05 Z = -409664
93
XDOT = 10360
112943 XDOT = 3157
762425
YDOT = 9514
143996 feet/sec YDOT = 2899
911090 meter/sec
ZDOT = 19681
938648 ZDOT = 5999
054900
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 15177
45481945
00016717 00000-0 10270-3 0 9075
2 25544 51
6453 37
7515 0002891 91
6349 268
5136 15
55424013 29480
Satellite: ISS
Catalog Number: 25544
Epoch time: 15177
45481945 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 37
7515 deg
Eccentricity:
0002891
Arg of perigee: 91
6349 deg
Mean anomaly: 268
5136 deg
Mean motion: 15
55424013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 329
Coasting Arc #9 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2015/178/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4723738
20 A = 6784338
86 meter
Y = -4556791
29 meter E =
0009711
Z = -1707829
40 I = 51
85894
XDOT = 4462
378792 Wp = 129
96109
YDOT = -2494
311545 meter/sec RA = 32
17923 deg
ZDOT = -5714
908432 TA = 68
71280
MA = 68
60914
Ha = 219
972 n
mi
Hp = 211
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15497828
74 X = -4664135
96
Y = -14950102
67 feet Y = -4609281
80 meter
Z = -5603114
84 Z = -1730632
20
XDOT = 14640
350368 XDOT = 4517
700128
YDOT = -8183
436828 feet/sec YDOT = -2444
100402 meter/sec
ZDOT = -18749
699580 ZDOT = -5693
096849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17870508
06 X = -5446930
86
Y = 11968099
38 feet Y = 3647876
69 meter
Z = -5700236
90 Z = -1737432
21
XDOT = -4022
029332 XDOT = -1225
914540
YDOT = -14848
591650 feet/sec YDOT = -4525
850735 meter/sec
ZDOT = -18655
366916 ZDOT = -5686
155836
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 15178
48279722
00016717 00000-0 10270-3 0 9088
2 25544 51
6451 32
6171 0002748 97
3961 262
7505 15
55403642 29643
Satellite: ISS
Catalog Number: 25544
Epoch time: 15178
48279722 = yrday
fracday
Element set: 908
Inclination: 51
6451 deg
RA of node: 32
6171 deg
Eccentricity:
0002748
Arg of perigee: 97
3961 deg
Mean anomaly: 262
7505 deg
Mean motion: 15
55403642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 325
Coasting Arc #10 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2015/179/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3218953
24 A = 6780108
92 meter
Y = 4790389
76 meter E =
0014849
Z = 3546052
98 I = 51
81732
XDOT = -6167
963180 Wp = 92
81610
YDOT = 804
395879 meter/sec RA = 27
20614 deg
ZDOT = 4495
429475 TA = 308
94225
MA = 309
07450
Ha = 219
908 n
mi
Hp = 211
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10560870
20 X = 3147921
25
Y = 15716501
83 feet Y = 4825988
61 meter
Z = 11634032
10 Z = 3561518
14
XDOT = -20236
099672 XDOT = -6198
336907
YDOT = 2639
094092 feet/sec YDOT = 735
251311 meter/sec
ZDOT = 14748
784368 ZDOT = 4465
392904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17450914
61 X = 5319038
77
Y = -7244135
68 feet Y = -2208012
55 meter
Z = 11699538
01 Z = 3566019
19
XDOT = -1874
876549 XDOT = -571
462372
YDOT = 19183
509873 feet/sec YDOT = 5847
133809 meter/sec
ZDOT = 14619
431526 ZDOT = 4456
002729
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 15179
51075638
00016717 00000-0 10270-3 0 9094
2 25544 51
6446 27
4818 0002775 95
0634 265
0836 15
55442348 29806
Satellite: ISS
Catalog Number: 25544
Epoch time: 15179
51075638 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 27
4818 deg
Eccentricity:
0002775
Arg of perigee: 95
0634 deg
Mean anomaly: 265
0836 deg
Mean motion: 15
55442348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 334
Coasting Arc #11 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2015/180/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1179060
36 A = 6775410
12 meter
Y = -4602612
73 meter E =
0014070
Z = -4843412
78 I = 51
77233
XDOT = 7191
381259 Wp = 76
77805
YDOT = 798
896771 meter/sec RA = 22
21512 deg
ZDOT = -2512
818207 TA = 168
55360
MA = 168
52157
Ha = 219
795 n
mi
Hp = 211
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3868308
28 X = -1103977
68
Y = -15100435
47 feet Y = -4615377
29 meter
Z = -15890461
89 Z = -4848958
70
XDOT = 23593
770536 XDOT = 7194
119678
YDOT = 2621
052397 feet/sec YDOT = 879
331155 meter/sec
ZDOT = -8244
154224 ZDOT = -2477
877032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15530009
05 X = -4733546
76
Y = 1038348
62 feet Y = 316488
66 meter
Z = -15913340
01 Z = -4850386
04
XDOT = 6834
368156 XDOT = 2083
115414
YDOT = -21677
817307 feet/sec YDOT = -6607
398715 meter/sec
ZDOT = -8094
048059 ZDOT = -2467
065848
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 15180
47444962
00016717 00000-0 10270-3 0 9103
2 25544 51
6435 22
6674 0002586 99
9208 260
2237 15
55489343 29955
Satellite: ISS
Catalog Number: 25544
Epoch time: 15180
47444962 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 22
6674 deg
Eccentricity:
0002586
Arg of perigee: 99
9208 deg
Mean anomaly: 260
2237 deg
Mean motion: 15
55489343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 332
Coasting Arc #12 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2015/181/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1103501
02 A = 6773333
64 meter
Y = 4046301
26 meter E =
0005022
Z = 5314355
64 I = 51
73582
XDOT = -7359
416622 Wp = 98
55206
YDOT = -2174
784930 meter/sec RA = 17
21017 deg
ZDOT = 126
880511 TA = 350
23662
MA = 350
24638
Ha = 219
822 n
mi
Hp = 211
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3620410
16 X = -1174480
83
Y = 13275266
60 feet Y = 4033563
54 meter
Z = 17435550
01 Z = 5308823
24
XDOT = -24145
067656 XDOT = -7335
167024
YDOT = -7135
121160 feet/sec YDOT = -2256
947174 meter/sec
ZDOT = 416
274641 ZDOT = 91
188508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12510008
55 X = 3813050
61
Y = 5805069
97 feet Y = 1769385
33 meter
Z = 17410896
76 Z = 5306841
33
XDOT = -10478
892290 XDOT = -3193
966370
YDOT = 21784
455353 feet/sec YDOT = 6639
901992 meter/sec
ZDOT = 263
233681 ZDOT = 80
233626
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 15181
50237298
00016717 00000-0 10270-3 0 9111
2 25544 51
6436 17
5324 0002630 103
8636 256
2811 15
55506810 30113
Satellite: ISS
Catalog Number: 25544
Epoch time: 15181
50237298 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 17
5324 deg
Eccentricity:
0002630
Arg of perigee: 103
8636 deg
Mean anomaly: 256
2811 deg
Mean motion: 15
55506810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 278
Coasting Arc #13 (Orbit 3025)
---------------------------------------
Vector Time (GMT): 2015/182/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3346738
66 A = 6775017
06 meter
Y = -3253693
75 meter E =
0014595
Z = -4924128
78 I = 51
70971
XDOT = 6539
753086 Wp = 106
47809
YDOT = 3263
625557 meter/sec RA = 12
20060 deg
ZDOT = 2289
911528 TA = 185
90385
MA = 185
92107
Ha = 219
666 n
mi
Hp = 211
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10980113
71 X = 3406792
95
Y = -10674848
25 feet Y = -3215931
81 meter
Z = -16155278
15 Z = -4907725
67
XDOT = 21455
882828 XDOT = 6491
648923
YDOT = 10707
432931 feet/sec YDOT = 3336
488051 meter/sec
ZDOT = 7512
833097 ZDOT = 2321
563860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8984344
82 X = -2738428
30
Y = -12493739
01 feet Y = -3808091
65 meter
Z = -16084039
55 Z = -4902415
25
XDOT = 12744
346850 XDOT = 3884
476920
YDOT = -19003
961707 feet/sec YDOT = -5792
407528 meter/sec
ZDOT = 7648
266943 ZDOT = 2331
191764
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 15182
46603319
00016717 00000-0 10270-3 0 9129
2 25544 51
6423 12
7165 0002534 107
1535 252
9896 15
55550990 30267
Satellite: ISS
Catalog Number: 25544
Epoch time: 15182
46603319 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 12
7165 deg
Eccentricity:
0002534
Arg of perigee: 107
1535 deg
Mean anomaly: 252
9896 deg
Mean motion: 15
55550990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3026
Checksum: 300
Coasting Arc #14 (Orbit 3041)
---------------------------------------
Vector Time (GMT): 2015/183/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5216434
36 A = 6779394
33 meter
Y = 2268109
59 meter E =
0014039
Z = 3676545
89 I = 51
69409
XDOT = -4842
844493 Wp = 89
00347
YDOT = -4071
416322 meter/sec RA = 7
20186 deg
ZDOT = -4344
959535 TA = 47
22722
MA = 47
10922
Ha = 219
586 n
mi
Hp = 211
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17114285
97 X = -5259268
32
Y = 7441304
43 feet Y = 2209535
99 meter
Z = 12062158
43 Z = 3651101
99
XDOT = -15888
597418 XDOT = -4775
851031
YDOT = -13357
665098 feet/sec YDOT = -4125
196981 meter/sec
ZDOT = -14255
116584 ZDOT = -4368
322769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5221563
45 X = 1591532
54
Y = 17990178
16 feet Y = 5483406
30 meter
Z = 11952247
77 Z = 3643045
12
XDOT = -13927
689961 XDOT = -4245
159900
YDOT = 13611
408352 feet/sec YDOT = 4148
757266 meter/sec
ZDOT = -14354
728501 ZDOT = -4375
321247
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 15183
49391874
00016717 00000-0 10270-3 0 9134
2 25544 51
6428 7
5811 0002311 109
2234 250
9170 15
55606104 30424
Satellite: ISS
Catalog Number: 25544
Epoch time: 15183
49391874 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 7
5811 deg
Eccentricity:
0002311
Arg of perigee: 109
2234 deg
Mean anomaly: 250
9170 deg
Mean motion: 15
55606104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3042
Checksum: 282
Coasting Arc #15 (Orbit 3056)
---------------------------------------
Vector Time (GMT): 2015/184/10:53:47
998
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6418334
32 A = 6783702
50 meter
Y = -1201538
70 meter E =
0008307
Z = -1832914
88 I = 51
67550
XDOT = 2460
837360 Wp = 54
47096
YDOT = 4563
346050 meter/sec RA = 2
21604 deg
ZDOT = 5648
423587 TA = 285
37858
MA = 285
47035
Ha = 219
560 n
mi
Hp = 211
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21057527
29 X = 6440196
68
Y = -3942056
12 feet Y = -1129642
21 meter
Z = -6013500
25 Z = -1801683
32
XDOT = 8073
613385 XDOT = 2382
188477
YDOT = 14971
607776 feet/sec YDOT = 4590
424268 meter/sec
ZDOT = 18531
573447 ZDOT = 5660
187258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1626833
03 X = -495858
71
Y = -21398903
58 feet Y = -6522385
81 meter
Z = -5878927
38 Z = -1791897
07
XDOT = 14188
767472 XDOT = 4324
736325
YDOT = -6162
560943 feet/sec YDOT = -1878
348576 meter/sec
ZDOT = 18581
195192 ZDOT = 5663
548295
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 15184
45754691
00016717 00000-0 10270-3 0 9142
2 25544 51
6414 2
7654 0002424 114
7297 245
4109 15
55594213 30570
Satellite: ISS
Catalog Number: 25544
Epoch time: 15184
45754691 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 2
7654 deg
Eccentricity:
0002424
Arg of perigee: 114
7297 deg
Mean anomaly: 245
4109 deg
Mean motion: 15
55594213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3057
Checksum: 306
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