[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 19th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
176/10:51:32
563 1
4 3
3 3
3
N/A 3
0 -0
0 227
2
000/00:01:05
126 0
5 -0
0 220
8
Coasting Arc #1 (Orbit 1152)
---------------------------------------
Vector Time (GMT): 2014/169/11:48:51
734
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4093710
37 A = 6787463
93 meter
Y = 1205250
81 meter E =
0018240
Z = -5294032
30 I = 51
98714
XDOT = -1019
948161 Wp = 99
48402
YDOT = 7524
483303 meter/sec RA = 92
26063 deg
ZDOT = 924
138431 TA = 179
33778
MA = 179
33536
Ha = 227
686 n
mi
Hp = 218
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13430808
29 X = 4105645
30
Y = 3954234
95 feet Y = 1251096
49 meter
Z = -17368872
37 Z = -5274116
63
XDOT = -3346
286619 XDOT = -1108
501988
YDOT = 24686
625010 feet/sec YDOT = 7512
582376 meter/sec
ZDOT = 3031
950234 ZDOT = 918
969237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5566076
58 X = 1696540
14
Y = -12960033
40 feet Y = -3950218
18 meter
Z = -17284578
05 Z = -5268339
39
XDOT = 23151
233854 XDOT = 7056
496079
YDOT = 5929
420177 feet/sec YDOT = 1807
287270 meter/sec
ZDOT = 3008
707079 ZDOT = 917
053918
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 14169
50682858
00016717 00000-0 10270-3 0 9000
2 25544 51
6469 93
0372 0003888 108
3879 251
7695 15
50759850 11530
Satellite: ISS
Catalog Number: 25544
Epoch time: 14169
50682858 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 93
0372 deg
Eccentricity:
0003888
Arg of perigee: 108
3879 deg
Mean anomaly: 251
7695 deg
Mean motion: 15
50759850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1153
Checksum: 344
Coasting Arc #2 (Orbit 1168)
---------------------------------------
Vector Time (GMT): 2014/170/11:48:51
734
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4108580
43 A = 6787890
87 meter
Y = -1597897
29 meter E =
0007683
Z = 5155385
84 I = 51
98923
XDOT = 896
190151 Wp = 79
52944
YDOT = -7447
799289 meter/sec RA = 87
32054 deg
ZDOT = -1590
840428 TA = 25
75583
MA = 25
71760
Ha = 227
734 n
mi
Hp = 218
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13479594
58 X = -4115450
18
Y = -5242445
17 feet Y = -1643880
89 meter
Z = 16913995
54 Z = 5135410
15
XDOT = 2940
256402 XDOT = 987
134312
YDOT = -24435
037039 feet/sec YDOT = -7437
268893 meter/sec
ZDOT = -5219
292742 ZDOT = -1586
266552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6628345
47 X = -2020319
70
Y = 12965276
69 feet Y = 3951816
34 meter
Z = 16829515
23 Z = 5129636
24
XDOT = -23047
122473 XDOT = -7024
762930
YDOT = -5020
175823 feet/sec YDOT = -1530
149591 meter/sec
ZDOT = -5198
577424 ZDOT = -1584
526399
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 14170
53788968
00016717 00000-0 10270-3 0 9015
2 25544 51
6468 87
9238 0003821 111
9305 248
2253 15
50797113 11695
Satellite: ISS
Catalog Number: 25544
Epoch time: 14170
53788968 = yrday
fracday
Element set: 901
Inclination: 51
6468 deg
RA of node: 87
9238 deg
Eccentricity:
0003821
Arg of perigee: 111
9305 deg
Mean anomaly: 248
2253 deg
Mean motion: 15
50797113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 324
Coasting Arc #3 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2014/171/11:48:51
734
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4189224
04 A = 6788726
44 meter
Y = 1978363
76 meter E =
0016075
Z = -4977078
46 I = 51
99026
XDOT = -786
061353 Wp = 108
30282
YDOT = 7275
331385 meter/sec RA = 82
37974 deg
ZDOT = 2231
280489 TA = 183
41781
MA = 183
42881
Ha = 227
581 n
mi
Hp = 218
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13744173
35 X = 4190967
26
Y = 6490694
74 feet Y = 2025220
50 meter
Z = -16328997
56 Z = -4956723
36
XDOT = -2578
941448 XDOT = -878
196208
YDOT = 23869
197458 feet/sec YDOT = 7266
025805 meter/sec
ZDOT = 7320
474045 ZDOT = 2227
238707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7670626
02 X = 2338006
81
Y = -13228559
90 feet Y = -4032065
06 meter
Z = -16242976
34 Z = -4950859
19
XDOT = 22585
859122 XDOT = 6884
169860
YDOT = 4134
589721 feet/sec YDOT = 1260
222947 meter/sec
ZDOT = 7302
033521 ZDOT = 2225
659817
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 14171
50450084
00016717 00000-0 10270-3 0 9029
2 25544 51
6475 83
1288 0003835 115
1285 245
0265 15
50793240 11846
Satellite: ISS
Catalog Number: 25544
Epoch time: 14171
50450084 = yrday
fracday
Element set: 902
Inclination: 51
6475 deg
RA of node: 83
1288 deg
Eccentricity:
0003835
Arg of perigee: 115
1285 deg
Mean anomaly: 245
0265 deg
Mean motion: 15
50793240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1184
Checksum: 289
Coasting Arc #4 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2014/172/11:48:51
734
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4289189
21 A = 6789702
66 meter
Y = -2344279
73 meter E =
0010728
Z = 4704153
60 I = 51
98874
XDOT = 717
650774 Wp = 80
58763
YDOT = -7076
896298 meter/sec RA = 77
44044 deg
ZDOT = -2865
114570 TA = 37
75745
MA = 37
68222
Ha = 227
637 n
mi
Hp = 218
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14072143
08 X = -4285507
53
Y = -7691206
47 feet Y = -2392224
05 meter
Z = 15433574
79 Z = 4683325
95
XDOT = 2354
497291 XDOT = 810
650772
YDOT = -23218
163707 feet/sec YDOT = -7068
350808 meter/sec
ZDOT = -9399
982185 ZDOT = -2861
403070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8662139
02 X = -2640219
97
Y = 13596120
43 feet Y = 4144097
51 meter
Z = 15345616
81 Z = 4677344
00
XDOT = -22001
846045 XDOT = -6706
162675
YDOT = -3400
098068 feet/sec YDOT = -1036
349891 meter/sec
ZDOT = -9382
963748 ZDOT = -2859
927350
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 14172
53554214
00016717 00000-0 10270-3 0 9034
2 25544 51
6474 78
0152 0003790 118
5291 241
6242 15
50820743 12007
Satellite: ISS
Catalog Number: 25544
Epoch time: 14172
53554214 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 78
0152 deg
Eccentricity:
0003790
Arg of perigee: 118
5291 deg
Mean anomaly: 241
6242 deg
Mean motion: 15
50820743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 275
Coasting Arc #5 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2014/173/11:48:51
734
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4445657
95 A = 6790902
51 meter
Y = 2671011
84 meter E =
0012448
Z = -4396697
35 I = 51
98617
XDOT = -680
237138 Wp = 113
83850
YDOT = 6798
602941 meter/sec RA = 72
50112 deg
ZDOT = 3445
181524 TA = 191
00011
MA = 191
02735
Ha = 227
453 n
mi
Hp = 218
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14585491
95 X = 4436817
53
Y = 8763162
19 feet Y = 2720677
09 meter
Z = -14424860
06 Z = -4375122
02
XDOT = -2231
749139 XDOT = -772
945786
YDOT = 22305
127759 feet/sec YDOT = 6790
477356 meter/sec
ZDOT = 11303
088988 ZDOT = 3441
652558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9524295
59 X = 2903005
30
Y = -14192828
01 feet Y = -4325973
98 meter
Z = -14333792
28 Z = -4368939
89
XDOT = 21118
537856 XDOT = 6436
930338
YDOT = 2782
291600 feet/sec YDOT = 848
042480 meter/sec
ZDOT = 11286
880079 ZDOT = 3440
241048
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 14173
50213413
00016717 00000-0 10270-3 0 9046
2 25544 51
6485 73
2205 0003746 122
1678 237
9837 15
50827235 12153
Satellite: ISS
Catalog Number: 25544
Epoch time: 14173
50213413 = yrday
fracday
Element set: 904
Inclination: 51
6485 deg
RA of node: 73
2205 deg
Eccentricity:
0003746
Arg of perigee: 122
1678 deg
Mean anomaly: 237
9837 deg
Mean motion: 15
50827235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 293
Coasting Arc #6 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2014/174/11:48:51
734
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4607741
61 A = 6792236
83 meter
Y = -2972896
98 meter E =
0013840
Z = 3996095
57 I = 51
98053
XDOT = 706
798362 Wp = 90
54905
YDOT = -6499
305746 meter/sec RA = 67
56304 deg
ZDOT = -4008
352657 TA = 41
06942
MA = 40
96531
Ha = 227
510 n
mi
Hp = 218
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15117262
51 X = -4593567
39
Y = -9753599
00 feet Y = -3024344
95 meter
Z = 13110549
76 Z = 3973745
75
XDOT = 2318
892263 XDOT = 798
893935
YDOT = -21323
181582 feet/sec YDOT = -6490
886439 meter/sec
ZDOT = -13150
763311 ZDOT = -4004
696223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10287309
85 X = -3135572
04
Y = 14842479
80 feet Y = 4523987
84 meter
Z = 13016254
60 Z = 3967354
40
XDOT = -20143
019689 XDOT = -6139
592401
YDOT = -2408
800872 feet/sec YDOT = -734
202506 meter/sec
ZDOT = -13134
053465 ZDOT = -4003
259496
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 14174
53315604
00016717 00000-0 10270-3 0 9056
2 25544 51
6484 68
1068 0003732 125
3804 234
7696 15
50843971 12314
Satellite: ISS
Catalog Number: 25544
Epoch time: 14174
53315604 = yrday
fracday
Element set: 905
Inclination: 51
6484 deg
RA of node: 68
1068 deg
Eccentricity:
0003732
Arg of perigee: 125
3804 deg
Mean anomaly: 234
7696 deg
Mean motion: 15
50843971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 304
Coasting Arc #7 (Orbit 1245)
---------------------------------------
Vector Time (GMT): 2014/175/11:48:51
734
Vector Time (MET): N/A
Weight (LBS) : 888319
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4809600
09 A = 6793561
54 meter
Y = 3214627
83 meter E =
0008384
Z = -3571269
49 I = 51
97317
XDOT = -775
435957 Wp = 108
99324
YDOT = 6146
879127 meter/sec RA = 62
62499 deg
ZDOT = 4494
670270 TA = 209
18164
MA = 209
22850
Ha = 227
299 n
mi
Hp = 218
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15779527
85 X = 4790644
06
Y = 10546679
24 feet Y = 3268306
37 meter
Z = -11716763
43 Z = -3547950
66
XDOT = -2544
081224 XDOT = -865
947857
YDOT = 20166
926269 feet/sec YDOT = 6137
701006 meter/sec
ZDOT = 14746
293537 ZDOT = 4490
684295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10835570
95 X = 3302682
03
Y = -15656039
30 feet Y = -4771960
78 meter
Z = -11618404
51 Z = -3541289
69
XDOT = 18974
648186 XDOT = 5783
472767
YDOT = 2217
141919 feet/sec YDOT = 675
784857 meter/sec
ZDOT = 14728
237109 ZDOT = 4489
166671
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 14175
49972914
00016717 00000-0 10270-3 0 9066
2 25544 51
6492 63
3123 0003601 129
6298 230
5172 15
50858467 12466
Satellite: ISS
Catalog Number: 25544
Epoch time: 14175
49972914 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 63
3123 deg
Eccentricity:
0003601
Arg of perigee: 129
6298 deg
Mean anomaly: 230
5172 deg
Mean motion: 15
50858467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1246
Checksum: 316
Coasting Arc #8 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2014/176/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4352386
79 A = 6789438
85 meter
Y = -690921
37 meter E =
0014149
Z = -5177452
38 I = 51
93897
XDOT = 2918
121845 Wp = 108
94950
YDOT = 6905
471299 meter/sec RA = 57
89340 deg
ZDOT = 1530
526090 TA = 175
77420
MA = 175
76224
Ha = 227
229 n
mi
Hp = 220
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14279484
22 X = 4384939
76
Y = -2266802
40 feet Y = -642067
42 meter
Z = -16986392
32 Z = -5156230
12
XDOT = 9573
890568 XDOT = 2833
251604
YDOT = 22655
745730 feet/sec YDOT = 6937
628853 meter/sec
ZDOT = 5021
411057 ZDOT = 1544
496783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1355727
02 X = 413225
60
Y = -14500343
67 feet Y = -4419704
75 meter
Z = -16896201
48 Z = -5149962
21
XDOT = 23253
854412 XDOT = 7087
774825
YDOT = -3748
547417 feet/sec YDOT = -1142
557253 meter/sec
ZDOT = 5079
404536 ZDOT = 1548
202503
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 14176
46629451
00016717 00000-0 10270-3 0 9070
2 25544 51
6491 58
5178 0001885 178
6244 181
4912 15
50259504 12618
Satellite: ISS
Catalog Number: 25544
Epoch time: 14176
46629451 = yrday
fracday
Element set: 907
Inclination: 51
6491 deg
RA of node: 58
5178 deg
Eccentricity:
0001885
Arg of perigee: 178
6244 deg
Mean anomaly: 181
4912 deg
Mean motion: 15
50259504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 322
Coasting Arc #9 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2014/177/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4506140
58 A = 6789842
46 meter
Y = 586106
69 meter E =
0004966
Z = 5041486
99 I = 51
92330
XDOT = -3109
816315 Wp = 72
27768
YDOT = -6715
496498 meter/sec RA = 52
95481 deg
ZDOT = -1995
782113 TA = 37
05491
MA = 37
02062
Ha = 227
202 n
mi
Hp = 220
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14783925
78 X = -4536849
50
Y = 1922922
20 feet Y = 535543
67 meter
Z = 16540311
65 Z = 5019522
35
XDOT = -10202
809433 XDOT = -3024
796135
YDOT = -22032
468824 feet/sec YDOT = -6749
796791 meter/sec
ZDOT = -6547
841579 ZDOT = -2010
683611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1556313
68 X = -474364
41
Y = 14930456
17 feet Y = 4550803
04 meter
Z = 16446986
56 Z = 5013041
50
XDOT = -22692
372200 XDOT = -6916
635046
YDOT = 4927
013575 feet/sec YDOT = 1501
753738 meter/sec
ZDOT = -6609
812402 ZDOT = -2014
670820
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 14177
49769634
00016717 00000-0 10270-3 0 9083
2 25544 51
6489 53
4066 0001801 186
7580 173
3547 15
50305539 12777
Satellite: ISS
Catalog Number: 25544
Epoch time: 14177
49769634 = yrday
fracday
Element set: 908
Inclination: 51
6489 deg
RA of node: 53
4066 deg
Eccentricity:
0001801
Arg of perigee: 186
7580 deg
Mean anomaly: 173
3547 deg
Mean motion: 15
50305539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 334
Coasting Arc #10 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2014/178/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4695322
52 A = 6790569
53 meter
Y = -513322
67 meter E =
0012050
Z = -4890134
36 I = 51
90625
XDOT = 3254
329829 Wp = 115
86964
YDOT = 6480
283873 meter/sec RA = 48
01473 deg
ZDOT = 2444
011242 TA = 178
07526
MA = 178
07061
Ha = 227
038 n
mi
Hp = 220
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15404601
45 X = 4724468
20
Y = -1684129
51 feet Y = -460652
89 meter
Z = -16043747
89 Z = -4867254
56
XDOT = 10676
935135 XDOT = 3169
751801
YDOT = 21260
773862 feet/sec YDOT = 6516
202624 meter/sec
ZDOT = 8018
409588 ZDOT = 2459
615734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1664467
23 X = 507329
61
Y = -15507320
06 feet Y = -4726631
16 meter
Z = -15946550
02 Z = -4860508
45
XDOT = 21909
499910 XDOT = 6678
015573
YDOT = -5962
179296 feet/sec YDOT = -1817
272249 meter/sec
ZDOT = 8083
402064 ZDOT = 2463
820949
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 14178
46462863
00016717 00000-0 10270-3 0 9096
2 25544 51
6490 48
6143 0001804 190
5958 169
5155 15
50288485 12925
Satellite: ISS
Catalog Number: 25544
Epoch time: 14178
46462863 = yrday
fracday
Element set: 909
Inclination: 51
6490 deg
RA of node: 48
6143 deg
Eccentricity:
0001804
Arg of perigee: 190
5958 deg
Mean anomaly: 169
5155 deg
Mean motion: 15
50288485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 335
Coasting Arc #11 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2014/179/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4890205
53 A = 6791222
16 meter
Y = 459173
94 meter E =
0007139
Z = 4684941
46 I = 51
88732
XDOT = -3363
415156 Wp = 74
30309
YDOT = -6250
909909 meter/sec RA = 43
07392 deg
ZDOT = -2892
579965 TA = 44
38666
MA = 44
32946
Ha = 227
018 n
mi
Hp = 220
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16043981
39 X = -4917734
40
Y = 1506476
18 feet Y = 404333
96 meter
Z = 15370542
85 Z = 4661118
93
XDOT = -11034
826626 XDOT = -3279
214980
YDOT = -20508
234610 feet/sec YDOT = -6288
050594 meter/sec
ZDOT = -9490
091749 ZDOT = -2908
715162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1696660
15 X = -517142
01
Y = 16121433
22 feet Y = 4913812
85 meter
Z = 15269352
71 Z = 4654098
71
XDOT = -21091
715512 XDOT = -6428
754888
YDOT = 6849
824559 feet/sec YDOT = 2087
826525 meter/sec
ZDOT = -9557
375545 ZDOT = -2913
088066
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 14179
49601196
00016717 00000-0 10270-3 0 9106
2 25544 51
6489 43
5027 0001710 198
1680 161
9410 15
50335947 13084
Satellite: ISS
Catalog Number: 25544
Epoch time: 14179
49601196 = yrday
fracday
Element set: 910
Inclination: 51
6489 deg
RA of node: 43
5027 deg
Eccentricity:
0001710
Arg of perigee: 198
1680 deg
Mean anomaly: 161
9410 deg
Mean motion: 15
50335947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 304
Coasting Arc #12 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2014/180/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5106537
35 A = 6792155
93 meter
Y = -448134
70 meter E =
0009204
Z = -4465505
01 I = 51
86651
XDOT = 3421
763313 Wp = 121
17716
YDOT = 5991
591574 meter/sec RA = 38
13141 deg
ZDOT = 3312
091629 TA = 182
19949
MA = 182
20354
Ha = 226
851 n
mi
Hp = 221
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16753731
45 X = 5132860
72
Y = -1470258
21 feet Y = -390882
38 meter
Z = -14650607
00 Z = -4440634
55
XDOT = 11226
257587 XDOT = 3338
420752
YDOT = 19657
452671 feet/sec YDOT = 6029
389525 meter/sec
ZDOT = 10866
442352 ZDOT = 3328
512212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1581605
59 X = 482073
38
Y = -16835432
83 feet Y = -5131439
93 meter
Z = -14544971
21 Z = -4433307
22
XDOT = 20116
731021 XDOT = 6131
579615
YDOT = -7556
234580 feet/sec YDOT = -2303
140300 meter/sec
ZDOT = 10934
983261 ZDOT = 3332
982898
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 14180
46292680
00016717 00000-0 10270-3 0 9110
2 25544 51
6486 38
7099 0001759 203
2715 156
8356 15
50315954 13231
Satellite: ISS
Catalog Number: 25544
Epoch time: 14180
46292680 = yrday
fracday
Element set: 911
Inclination: 51
6486 deg
RA of node: 38
7099 deg
Eccentricity:
0001759
Arg of perigee: 203
2715 deg
Mean anomaly: 156
8356 deg
Mean motion: 15
50315954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1323
Checksum: 315
Coasting Arc #13 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2014/181/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5320327
93 A = 6792987
38 meter
Y = 455327
39 meter E =
0009243
Z = 4191869
05 I = 51
84487
XDOT = -3436
306479 Wp = 82
64944
YDOT = -5748
230445 meter/sec RA = 33
18835 deg
ZDOT = -3728
791586 TA = 45
60522
MA = 45
52958
Ha = 226
826 n
mi
Hp = 220
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17455144
14 X = -5345386
61
Y = 1493856
25 feet Y = 395691
49 meter
Z = 13752851
20 Z = 4165963
12
XDOT = -11273
971389 XDOT = -3353
659999
YDOT = -18859
023769 feet/sec YDOT = -5786
194922 meter/sec
ZDOT = -12233
568196 ZDOT = -3745
284382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1381899
94 X = -421203
10
Y = 17550452
26 feet Y = 5349377
85 meter
Z = 13642820
73 Z = 4158331
76
XDOT = -19152
162590 XDOT = -5837
579157
YDOT = 8076
347518 feet/sec YDOT = 2461
670724 meter/sec
ZDOT = -12302
458947 ZDOT = -3749
789487
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 14181
49429181
00016717 00000-0 10270-3 0 9123
2 25544 51
6487 33
5980 0001660 210
8074 149
2980 15
50364533 13390
Satellite: ISS
Catalog Number: 25544
Epoch time: 14181
49429181 = yrday
fracday
Element set: 912
Inclination: 51
6487 deg
RA of node: 33
5980 deg
Eccentricity:
0001660
Arg of perigee: 210
8074 deg
Mean anomaly: 149
2980 deg
Mean motion: 15
50364533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 307
Coasting Arc #14 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2014/182/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5539480
90 A = 6794039
64 meter
Y = -511792
72 meter E =
0005951
Z = -3907031
49 I = 51
82082
XDOT = 3402
194400 Wp = 120
77352
YDOT = 5492
494508 meter/sec RA = 28
24325 deg
ZDOT = 4105
916195 TA = 192
24469
MA = 192
25915
Ha = 226
684 n
mi
Hp = 221
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18174149
94 X = 5563771
07
Y = -1679109
97 feet Y = -449710
49 meter
Z = -12818344
78 Z = -3880062
82
XDOT = 11162
055118 XDOT = 3320
578216
YDOT = 18019
995105 feet/sec YDOT = 5530
083301 meter/sec
ZDOT = 13470
853657 ZDOT = 4122
245681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1000646
25 X = 304996
98
Y = -18304135
35 feet Y = -5579100
45 meter
Z = -12703796
11 Z = -3872117
05
XDOT = 18109
583155 XDOT = 5519
800946
YDOT = -8402
795436 feet/sec YDOT = -2561
172049 meter/sec
ZDOT = 13539
097033 ZDOT = 4126
716776
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 14182
46118955
00016717 00000-0 10270-3 0 9136
2 25544 51
6479 28
8048 0001759 215
2168 144
8867 15
50341538 13547
Satellite: ISS
Catalog Number: 25544
Epoch time: 14182
46118955 = yrday
fracday
Element set: 913
Inclination: 51
6479 deg
RA of node: 28
8048 deg
Eccentricity:
0001759
Arg of perigee: 215
2168 deg
Mean anomaly: 144
8867 deg
Mean motion: 15
50341538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1354
Checksum: 327
Coasting Arc #15 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2014/183/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5746806
03 A = 6794945
85 meter
Y = 582925
60 meter E =
0011009
Z = 3568347
50 I = 51
79688
XDOT = -3319
535378 Wp = 93
57807
YDOT = -5263
962451 meter/sec RA = 23
29794 deg
ZDOT = -4474
938957 TA = 44
44720
MA = 44
35891
Ha = 226
631 n
mi
Hp = 220
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18854350
48 X = -5770231
03
Y = 1912485
58 feet Y = 518529
85 meter
Z = 11707176
82 Z = 3540373
74
XDOT = -10890
864102 XDOT = -3238
688230
YDOT = -17270
218015 feet/sec YDOT = -5300
631219 meter/sec
ZDOT = -14681
558258 ZDOT = -4490
868703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -541047
70 X = -164911
34
Y = 19016294
41 feet Y = 5796166
54 meter
Z = 11588353
49 Z = 3532130
14
XDOT = -17132
147594 XDOT = -5221
878587
YDOT = 8522
635157 feet/sec YDOT = 2597
699196 meter/sec
ZDOT = -14748
145290 ZDOT = -4495
234684
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 14183
49253639
00016717 00000-0 10270-3 0 9140
2 25544 51
6483 23
6929 0001667 223
6596 136
4423 15
50391459 13709
Satellite: ISS
Catalog Number: 25544
Epoch time: 14183
49253639 = yrday
fracday
Element set: 914
Inclination: 51
6483 deg
RA of node: 23
6929 deg
Eccentricity:
0001667
Arg of perigee: 223
6596 deg
Mean anomaly: 136
4423 deg
Mean motion: 15
50391459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1370
Checksum: 323
Coasting Arc #16 (Orbit 1384)
---------------------------------------
Vector Time (GMT): 2014/184/10:52:05
126
Vector Time (MET): N/A
Weight (LBS) : 887995
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5943159
28 A = 6796006
96 meter
Y = -703921
54 meter E =
0003211
Z = -3223252
43 I = 51
77008
XDOT = 3196
118245 Wp = 96
05478
YDOT = 5040
728818 meter/sec RA = 18
35019 deg
ZDOT = 4796
071425 TA = 226
81396
MA = 226
84079
Ha = 226
543 n
mi
Hp = 221
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19498554
05 X = 5966246
39
Y = -2309453
87 feet Y = -637331
98 meter
Z = -10574975
18 Z = -3194325
59
XDOT = 10485
952248 XDOT = 3116
216524
YDOT = 16537
824207 feet/sec YDOT = 5076
022761 meter/sec
ZDOT = 15735
142469 ZDOT = 4811
403898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -109316
65 X = -33319
72
Y = -19700232
46 feet Y = -6004630
85 meter
Z = -10452089
66 Z = -3185796
93
XDOT = 16159
904964 XDOT = 4925
539033
YDOT = -8465
401371 feet/sec YDOT = -2580
254338 meter/sec
ZDOT = 15799
233452 ZDOT = 4815
606356
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 14184
45941731
00016717 00000-0 10270-3 0 9155
2 25544 51
6471 18
8993 0001785 225
4320 134
6685 15
50365597 13859
Satellite: ISS
Catalog Number: 25544
Epoch time: 14184
45941731 = yrday
fracday
Element set: 915
Inclination: 51
6471 deg
RA of node: 18
8993 deg
Eccentricity:
0001785
Arg of perigee: 225
4320 deg
Mean anomaly: 134
6685 deg
Mean motion: 15
50365597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1385
Checksum: 328
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