[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 3rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17276 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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
062/08:01:38
762 0
8 1
4 1
5
N/A 1
0 -0
1 223
1
000/00:03:17
523 0
7 -0
0 210
7
Coasting Arc #1 (Orbit 1145)
---------------------------------------
Vector Time (GMT): 2015/061/14:54:04
633
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -395710
54 A = 6785753
27 meter
Y = -6574579
76 meter E =
0021373
Z = 1590304
78 I = 51
30558
XDOT = 5011
047794 Wp = 63
96692
YDOT = 1091
961220 meter/sec RA = 255
40441 deg
ZDOT = 5710
631710 TA = 313
53363
MA = 313
71099
Ha = 222
255 n
mi
Hp = 210
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1298262
92 X = -329887
57
Y = -21570143
57 feet Y = -6578636
64 meter
Z = 5217535
35 Z = 1588543
14
XDOT = 16440
445519 XDOT = 4970
725257
YDOT = 3582
549933 feet/sec YDOT = 1147
773203 meter/sec
ZDOT = 18735
668339 ZDOT = 5734
875841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9573986
05 X = -2918150
95
Y = -19374272
73 feet Y = -5905278
33 meter
Z = 5211103
80 Z = 1588344
44
XDOT = 15024
037781 XDOT = 4579
326716
YDOT = -2312
385071 feet/sec YDOT = -704
814970 meter/sec
ZDOT = 18839
199428 ZDOT = 5742
187986
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 15061
68205391
00016717 00000-0 10270-3 0 9004
2 25544 51
6420 255
9881 0007453 65
8245 294
3687 15
54993299 11464
Satellite: ISS
Catalog Number: 25544
Epoch time: 15061
68205391 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 255
9881 deg
Eccentricity:
0007453
Arg of perigee: 65
8245 deg
Mean anomaly: 294
3687 deg
Mean motion: 15
54993299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1146
Checksum: 332
Coasting Arc #2 (Orbit 1156)
---------------------------------------
Vector Time (GMT): 2015/062/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2516742
11 A = 6778384
68 meter
Y = -4243809
02 meter E =
0015210
Z = 4634419
02 I = 51
28738
XDOT = 4287
973878 Wp = 88
09368
YDOT = 5686
460989 meter/sec RA = 251
83139 deg
ZDOT = 2870
905417 TA = 333
23766
MA = 333
31606
Ha = 223
086 n
mi
Hp = 210
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8257027
91 X = 2541498
52
Y = -13923257
95 feet Y = -4215526
18 meter
Z = 15204786
83 Z = 4646705
27
XDOT = 14068
155768 XDOT = 4210
122337
YDOT = 18656
368075 feet/sec YDOT = 5733
976969 meter/sec
ZDOT = 9418
981027 ZDOT = 2891
545349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15201886
52 X = 4633535
01
Y = 5414387
15 feet Y = 1650305
20 meter
Z = 15258054
34 Z = 4650654
96
XDOT = -15315
178776 XDOT = -4668
066491
YDOT = 16140
105168 feet/sec YDOT = 4919
504055 meter/sec
ZDOT = 9506
333960 ZDOT = 2897
530591
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 15062
38899694
00016717 00000-0 10270-3 0 9018
2 25544 51
6449 252
4645 0008835 62
6880 297
5172 15
54725363 11571
Satellite: ISS
Catalog Number: 25544
Epoch time: 15062
38899694 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 252
4645 deg
Eccentricity:
0008835
Arg of perigee: 62
6880 deg
Mean anomaly: 297
5172 deg
Mean motion: 15
54725363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1157
Checksum: 343
Coasting Arc #3 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2015/063/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3505627
64 A = 6775681
81 meter
Y = 2502637
01 meter E =
0022970
Z = -5250471
34 I = 51
28953
XDOT = -3581
218962 Wp = 76
79930
YDOT = -6714
391945 meter/sec RA = 246
80268 deg
ZDOT = -807
158983 TA = 185
41963
MA = 185
44454
Ha = 223
064 n
mi
Hp = 210
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11501403
03 X = -3507847
83
Y = 8210751
36 feet Y = 2463421
67 meter
Z = -17225955
83 Z = -5267506
41
XDOT = -11749
406043 XDOT = -3501
950079
YDOT = -22028
844965 feet/sec YDOT = -6753
996365 meter/sec
ZDOT = -2648
159393 ZDOT = -824
362067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10358511
74 X = -3157274
38
Y = -9479955
00 feet Y = -2889490
28 meter
Z = -17299247
14 Z = -5272810
53
XDOT = 18484
586167 XDOT = 5634
101864
YDOT = -15220
099458 feet/sec YDOT = -4639
086315 meter/sec
ZDOT = -2720
656378 ZDOT = -829
256064
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 15063
35314240
00016717 00000-0 10270-3 0 9026
2 25544 51
6448 247
6532 0008734 65
0700 295
1360 15
54784566 11727
Satellite: ISS
Catalog Number: 25544
Epoch time: 15063
35314240 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 247
6532 deg
Eccentricity:
0008734
Arg of perigee: 65
0700 deg
Mean anomaly: 295
1360 deg
Mean motion: 15
54784566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 297
Coasting Arc #4 (Orbit 1187)
---------------------------------------
Vector Time (GMT): 2015/064/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4364845
19 A = 6775893
06 meter
Y = -576881
42 meter E =
0012936
Z = 5141615
11 I = 51
30431
XDOT = 2565
919908 Wp = 63
92949
YDOT = 7104
608302 meter/sec RA = 241
77112 deg
ZDOT = -1372
862686 TA = 39
36222
MA = 39
26828
Ha = 222
833 n
mi
Hp = 210
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14320358
22 X = 4345995
97
Y = -1892655
58 feet Y = -528175
50 meter
Z = 16868815
97 Z = 5162772
64
XDOT = 8418
372402 XDOT = 2492
952541
YDOT = 23309
082357 feet/sec YDOT = 7132
893905 meter/sec
ZDOT = -4504
142672 ZDOT = -1360
576432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4979976
55 X = 1517896
85
Y = 13445791
20 feet Y = 4098277
16 meter
Z = 16959430
70 Z = 5169234
48
XDOT = -19890
644878 XDOT = -6062
668559
YDOT = 13017
394874 feet/sec YDOT = 3967
701958 meter/sec
ZDOT = -4452
728396 ZDOT = -1357
191615
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 15064
38154119
00016717 00000-0 10270-3 0 9038
2 25544 51
6449 242
5211 0008635 68
2310 291
9761 15
54836083 11886
Satellite: ISS
Catalog Number: 25544
Epoch time: 15064
38154119 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 242
5211 deg
Eccentricity:
0008635
Arg of perigee: 68
2310 deg
Mean anomaly: 291
9761 deg
Mean motion: 15
54836083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1188
Checksum: 308
Coasting Arc #5 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2015/065/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5025715
37 A = 6778995
22 meter
Y = -1265139
00 meter E =
0016650
Z = -4384678
23 I = 51
33019
XDOT = -1220
719832 Wp = 91
63747
YDOT = -6770
024474 meter/sec RA = 236
74592 deg
ZDOT = 3363
219771 TA = 212
54344
MA = 212
64618
Ha = 222
939 n
mi
Hp = 210
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16488567
49 X = -4989895
91
Y = -4150718
49 feet Y = -1321140
23 meter
Z = -14385427
28 Z = -4409004
67
XDOT = -4004
986326 XDOT = -1161
262148
YDOT = -22211
366385 feet/sec YDOT = -6783
342389 meter/sec
ZDOT = 11034
185602 ZDOT = 3357
435298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 141614
28 X = 43164
03
Y = -16913950
96 feet Y = -5155372
25 meter
Z = -14489308
06 Z = -4416341
10
XDOT = 19375
226749 XDOT = 5905
569113
YDOT = -9240
251834 feet/sec YDOT = -2816
428759 meter/sec
ZDOT = 11010
521172 ZDOT = 3356
006853
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 15065
34564476
00016717 00000-0 10270-3 0 9047
2 25544 51
6445 237
7093 0008610 71
1532 289
0554 15
54843375 12036
Satellite: ISS
Catalog Number: 25544
Epoch time: 15065
34564476 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 237
7093 deg
Eccentricity:
0008610
Arg of perigee: 71
1532 deg
Mean anomaly: 289
0554 deg
Mean motion: 15
54843375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 307
Coasting Arc #6 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2015/066/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5338095
12 A = 6783231
65 meter
Y = 2919338
39 meter E =
0021398
Z = 2981504
66 I = 51
36338
XDOT = -419
993928 Wp = 87
87593
YDOT = 5852
336868 meter/sec RA = 231
73438 deg
ZDOT = -4946
798421 TA = 57
83643
MA = 57
62903
Ha = 222
857 n
mi
Hp = 210
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17513435
42 X = 5290570
74
Y = 9577881
86 feet Y = 2978767
20 meter
Z = 9781839
42 Z = 3007319
95
XDOT = -1377
932834 XDOT = -461
375447
YDOT = 19200
580277 feet/sec YDOT = 5847
408065 meter/sec
ZDOT = -16229
653611 ZDOT = -4948
940084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4831665
47 X = -1472691
64
Y = 19311841
87 feet Y = 5886249
40 meter
Z = 9891834
81 Z = 3015031
25
XDOT = -17485
047028 XDOT = -5329
442334
YDOT = 3996
080623 feet/sec YDOT = 1218
005374 meter/sec
ZDOT = -16239
746406 ZDOT = -4949
874704
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 15066
37399719
00016717 00000-0 10270-3 0 9058
2 25544 51
6449 232
5770 0008684 73
9849 286
2260 15
54899910 12193
Satellite: ISS
Catalog Number: 25544
Epoch time: 15066
37399719 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 232
5770 deg
Eccentricity:
0008684
Arg of perigee: 73
9849 deg
Mean anomaly: 286
2260 deg
Mean motion: 15
54899910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 355
Coasting Arc #7 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2015/067/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5233222
90 A = 6786410
23 meter
Y = -4138683
50 meter E =
0016564
Z = -1220270
64 I = 51
39364
XDOT = 2189
895302 Wp = 57
25310
YDOT = -4469
391832 meter/sec RA = 226
73593 deg
ZDOT = 5833
445656 TA = 289
43652
MA = 289
61543
Ha = 222
849 n
mi
Hp = 210
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17169366
48 X = -5180626
63
Y = -13578357
95 feet Y = -4196910
92 meter
Z = -4003512
60 Z = -1245564
09
XDOT = 7184
695873 XDOT = 2211
373800
YDOT = -14663
359029 feet/sec YDOT = -4444
782003 meter/sec
ZDOT = 19138
601232 ZDOT = 5844
136536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8432674
71 X = 2570279
25
Y = -20178602
05 feet Y = -6150437
91 meter
Z = -4111092
25 Z = -1253060
92
XDOT = 14554
589763 XDOT = 4436
238960
YDOT = 2217
030353 feet/sec YDOT = 675
750852 meter/sec
ZDOT = 19185
051841 ZDOT = 5847
603801
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 15067
33805547
00016717 00000-0 10270-3 0 9067
2 25544 51
6442 227
7649 0008558 77
1540 283
0568 15
54901843 12343
Satellite: ISS
Catalog Number: 25544
Epoch time: 15067
33805547 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 227
7649 deg
Eccentricity:
0008558
Arg of perigee: 77
1540 deg
Mean anomaly: 283
0568 deg
Mean motion: 15
54901843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 324
Coasting Arc #8 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2015/068/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4586445
15 A = 6786779
91 meter
Y = 4935788
01 meter E =
0016513
Z = -788189
12 I = 51
41719
XDOT = -3990
374275 Wp = 114
35375
YDOT = 2777
999157 meter/sec RA = 221
74603 deg
ZDOT = -5928
297461 TA = 74
19404
MA = 74
01203
Ha = 222
873 n
mi
Hp = 210
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15047392
23 X = 4534739
85
Y = 16193530
22 feet Y = 4986787
42 meter
Z = -2585922
33 Z = -766035
43
XDOT = -13091
779117 XDOT = -3992
344572
YDOT = 9114
170462 feet/sec YDOT = 2733
364312 meter/sec
ZDOT = -19449
794821 ZDOT = -5947
687056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11186109
98 X = -3409526
32
Y = 19078858
51 feet Y = 5815236
07 meter
Z = -2491892
83 Z = -759528
93
XDOT = -11061
131553 XDOT = -3371
432897
YDOT = -8989
875673 feet/sec YDOT = -2740
114105 meter/sec
ZDOT = -19533
203647 ZDOT = -5953
720472
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 15068
36636050
00016717 00000-0 10270-3 0 9073
2 25544 51
6441 222
6325 0008516 81
6060 278
6058 15
54920086 12500
Satellite: ISS
Catalog Number: 25544
Epoch time: 15068
36636050 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 222
6325 deg
Eccentricity:
0008516
Arg of perigee: 81
6060 deg
Mean anomaly: 278
6058 deg
Mean motion: 15
54920086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1250
Checksum: 297
Coasting Arc #9 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2015/069/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3454378
70 A = 6783901
90 meter
Y = -5199182
01 meter E =
0021977
Z = 2632102
16 I = 51
43182
XDOT = 5547
825964 Wp = 80
18851
YDOT = -1035
015438 meter/sec RA = 216
75231 deg
ZDOT = 5203
117516 TA = 309
60899
MA = 309
80281
Ha = 222
720 n
mi
Hp = 210
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11333263
45 X = -3408769
23
Y = -17057683
75 feet Y = -5237555
76 meter
Z = 8635505
78 Z = 2615432
95
XDOT = 18201
528753 XDOT = 5533
712651
YDOT = -3395
719941 feet/sec YDOT = -973
054249 meter/sec
ZDOT = 17070
595526 ZDOT = 5230
033603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12794976
97 X = 3899908
98
Y = -16028384
41 feet Y = -4885451
57 meter
Z = 8564978
29 Z = 2610605
38
XDOT = 7557
732749 XDOT = 2303
596942
YDOT = 15275
691853 feet/sec YDOT = 4656
030877 meter/sec
ZDOT = 17185
947527 ZDOT = 5238
276806
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 15069
39463811
00016717 00000-0 10270-3 0 9081
2 25544 51
6434 217
4991 0008405 84
5388 275
6724 15
55002247 12660
Satellite: ISS
Catalog Number: 25544
Epoch time: 15069
39463811 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 217
4991 deg
Eccentricity:
0008405
Arg of perigee: 84
5388 deg
Mean anomaly: 275
6724 deg
Mean motion: 15
55002247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1266
Checksum: 325
Coasting Arc #10 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2015/070/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1817546
83 A = 6779402
06 meter
Y = 5036752
89 meter E =
0016045
Z = -4173517
00 I = 51
44179
XDOT = -6669
350482 Wp = 79
79037
YDOT = -654
819640 meter/sec RA = 211
74865 deg
ZDOT = -3704
115225 TA = 152
03639
MA = 151
95008
Ha = 222
716 n
mi
Hp = 210
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5963080
14 X = 1781362
95
Y = 16524779
81 feet Y = 5056875
07 meter
Z = -13692641
06 Z = -4164776
20
XDOT = -21881
071135 XDOT = -6643
539259
YDOT = -2148
358400 feet/sec YDOT = -729
256793 meter/sec
ZDOT = -12152
609006 ZDOT = -3736
450838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13719770
24 X = -4181785
97
Y = 11017999
29 feet Y = 3358286
18 meter
Z = -13656012
88 Z = -4162352
73
XDOT = -4135
406606 XDOT = -1260
471934
YDOT = -20344
890428 feet/sec YDOT = -6201
122602 meter/sec
ZDOT = -12290
903948 ZDOT = -3746
267523
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 15070
35862721
00016717 00000-0 10270-3 0 9093
2 25544 51
6423 212
6867 0008515 87
5418 272
6710 15
55020593 12819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15070
35862721 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 212
6867 deg
Eccentricity:
0008515
Arg of perigee: 87
5418 deg
Mean anomaly: 272
6710 deg
Mean motion: 15
55020593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1281
Checksum: 306
Coasting Arc #11 (Orbit 1296)
---------------------------------------
Vector Time (GMT): 2015/071/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 106015
82 A = 6775755
62 meter
Y = -4474835
34 meter E =
0013259
Z = 5076462
40 I = 51
45697
XDOT = 7186
654161 Wp = 103
92444
YDOT = 2104
727715 meter/sec RA = 206
73277 deg
ZDOT = 1698
346527 TA = 329
61075
MA = 329
68755
Ha = 222
726 n
mi
Hp = 210
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 347820
92 X = 131387
09
Y = -14681218
31 feet Y = -4473507
40 meter
Z = 16655060
35 Z = 5077039
50
XDOT = 23578
261684 XDOT = 7154
334553
YDOT = 6905
274656 feet/sec YDOT = 2184
913044 meter/sec
ZDOT = 5572
003042 ZDOT = 1733
179105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13906851
49 X = 4238808
33
Y = -4706723
36 feet Y = -1434609
28 meter
Z = 16658223
88 Z = 5077426
64
XDOT = 1067
090266 XDOT = 325
249113
YDOT = 23479
736494 feet/sec YDOT = 7156
623683 meter/sec
ZDOT = 5720
776358 ZDOT = 1743
692634
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 15071
38685753
00016717 00000-0 10270-3 0 9107
2 25544 51
6423 207
5532 0008562 90
7474 269
4660 15
55019660 12979
Satellite: ISS
Catalog Number: 25544
Epoch time: 15071
38685753 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 207
5532 deg
Eccentricity:
0008562
Arg of perigee: 90
7474 deg
Mean anomaly: 269
4660 deg
Mean motion: 15
55019660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1297
Checksum: 320
Coasting Arc #12 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2015/072/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2173196
94 A = 6774642
19 meter
Y = 3664658
65 meter E =
0023293
Z = -5287466
83 I = 51
48168
XDOT = -6903
528159 Wp = 94
78257
YDOT = -3250
005894 meter/sec RA = 201
70994 deg
ZDOT = 585
215939 TA = 180
82450
MA = 180
82834
Ha = 222
606 n
mi
Hp = 209
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7129911
22 X = -2188330
07
Y = 12023158
31 feet Y = 3640271
42 meter
Z = -17347332
11 Z = -5298060
87
XDOT = -22649
370599 XDOT = -6869
515487
YDOT = -10662
748997 feet/sec YDOT = -3327
015418 meter/sec
ZDOT = 1919
999801 ZDOT = 551
763011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13723994
01 X = -4183073
37
Y = -2334247
58 feet Y = -711478
66 meter
Z = -17393250
92 Z = -5301462
88
XDOT = 1824
807332 XDOT = 556
201275
YDOT = -23963
920062 feet/sec YDOT = -7304
202835 meter/sec
ZDOT = 1777
291066 ZDOT = 541
718317
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 15072
35079715
00016717 00000-0 10270-3 0 9111
2 25544 51
6412 202
7399 0008564 94
6732 265
5400 15
55097110 13120
Satellite: ISS
Catalog Number: 25544
Epoch time: 15072
35079715 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 202
7399 deg
Eccentricity:
0008564
Arg of perigee: 94
6732 deg
Mean anomaly: 265
5400 deg
Mean motion: 15
55097110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 295
Coasting Arc #13 (Orbit 1327)
---------------------------------------
Vector Time (GMT): 2015/073/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4098838
54 A = 6776986
91 meter
Y = -2658332
23 meter E =
0015545
Z = 4684566
39 I = 51
51971
XDOT = 5865
976080 Wp = 81
62309
YDOT = 4085
770885 meter/sec RA = 196
69251 deg
ZDOT = -2803
815110 TA = 36
23259
MA = 36
12740
Ha = 222
419 n
mi
Hp = 210
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13447633
00 X = 4105504
29
Y = -8721562
42 feet Y = -2612458
63 meter
Z = 15369312
30 Z = 4704494
05
XDOT = 19245
328347 XDOT = 5833
471841
YDOT = 13404
760123 feet/sec YDOT = 4151
186055 meter/sec
ZDOT = -9198
868472 ZDOT = -2775
398870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13024629
51 X = 3969907
08
Y = 9198964
46 feet Y = 2803844
37 meter
Z = 15455042
02 Z = 4710696
81
XDOT = -4680
000506 XDOT = -1426
464154
YDOT = 21933
658159 feet/sec YDOT = 6685
379007 meter/sec
ZDOT = -9077
833049 ZDOT = -2766
923513
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 15073
37897504
00016717 00000-0 10270-3 0 9129
2 25544 51
6413 197
6064 0008466 98
2252 261
9861 15
55123212 13281
Satellite: ISS
Catalog Number: 25544
Epoch time: 15073
37897504 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 197
6064 deg
Eccentricity:
0008466
Arg of perigee: 98
2252 deg
Mean anomaly: 261
9861 deg
Mean motion: 15
55123212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1328
Checksum: 314
Coasting Arc #14 (Orbit 1342)
---------------------------------------
Vector Time (GMT): 2015/074/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5637236
07 A = 6781220
49 meter
Y = 1607635
99 meter E =
0013535
Z = -3422791
67 I = 51
56479
XDOT = -4084
259707 Wp = 98
61751
YDOT = -4568
321051 meter/sec RA = 191
68791 deg
ZDOT = 4594
565965 TA = 221
31271
MA = 221
41518
Ha = 222
464 n
mi
Hp = 209
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18494868
99 X = -5638167
59
Y = 5274396
28 feet Y = 1544591
20 meter
Z = -11229631
45 Z = -3450178
40
XDOT = -13399
802188 XDOT = -4055
190570
YDOT = -14987
929957 feet/sec YDOT = -4613
830933 meter/sec
ZDOT = 15074
035319 ZDOT = 4574
796668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11948524
11 X = -3641910
15
Y = -14981956
47 feet Y = -4566500
33 meter
Z = -11347149
85 Z = -3458611
27
XDOT = 7557
071737 XDOT = 2303
395465
YDOT = -17346
866828 feet/sec YDOT = -5287
325009 meter/sec
ZDOT = 14990
082016 ZDOT = 4568
976999
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 15074
34286817
00016717 00000-0 10270-3 0 9137
2 25544 51
6411 192
7928 0008612 101
7569 258
4551 15
55173336 13434
Satellite: ISS
Catalog Number: 25544
Epoch time: 15074
34286817 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 192
7928 deg
Eccentricity:
0008612
Arg of perigee: 101
7569 deg
Mean anomaly: 258
4551 deg
Mean motion: 15
55173336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1343
Checksum: 315
Coasting Arc #15 (Orbit 1358)
---------------------------------------
Vector Time (GMT): 2015/075/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6569674
73 A = 6784975
45 meter
Y = -490537
07 meter E =
0022210
Z = 1582340
03 I = 51
60921
XDOT = 1753
233880 Wp = 112
38001
YDOT = 4785
014232 meter/sec RA = 186
70051 deg
ZDOT = -5739
745381 TA = 50
28446
MA = 50
08890
Ha = 222
256 n
mi
Hp = 209
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21554050
97 X = 6566985
44
Y = -1609373
58 feet Y = -417085
55 meter
Z = 5191404
30 Z = 1614247
36
XDOT = 5752
079658 XDOT = 1727
477608
YDOT = 15698
865590 feet/sec YDOT = 4804
475414 meter/sec
ZDOT = -18831
185632 ZDOT = -5731
291685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10085450
72 X = 3074045
38
Y = 19079115
07 feet Y = 5815314
27 meter
Z = 5328126
03 Z = 1624012
82
XDOT = -10645
328030 XDOT = -3244
695984
YDOT = 10926
284060 feet/sec YDOT = 3330
331382 meter/sec
ZDOT = -18795
711367 ZDOT = -5728
932825
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 15075
37099346
00016717 00000-0 10270-3 0 9141
2 25544 51
6412 187
6586 0008398 104
2289 255
9798 15
55243990 13592
Satellite: ISS
Catalog Number: 25544
Epoch time: 15075
37099346 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 187
6586 deg
Eccentricity:
0008398
Arg of perigee: 104
2289 deg
Mean anomaly: 255
9798 deg
Mean motion: 15
55243990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1359
Checksum: 357
Coasting Arc #16 (Orbit 1374)
---------------------------------------
Vector Time (GMT): 2015/076/08:03:17
523
Vector Time (MET): N/A
Weight (LBS) : 905272
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6743319
43 A = 6785976
95 meter
Y = -558301
13 meter E =
0018785
Z = 448914
38 I = 51
64470
XDOT = 803
089137 Wp = 73
25809
YDOT = -4719
455338 meter/sec RA = 181
72350 deg
ZDOT = 5991
849312 TA = 291
58450
MA = 291
78455
Ha = 222
330 n
mi
Hp = 209
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22123751
39 X = -6738755
82
Y = -1831696
61 feet Y = -633683
76 meter
Z = 1472816
20 Z = 416168
23
XDOT = 2634
806881 XDOT = 826
697740
YDOT = -15483
777355 feet/sec YDOT = -4710
341923 meter/sec
ZDOT = 19658
298268 ZDOT = 5995
808439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7537688
36 X = -2297487
41
Y = -20889997
29 feet Y = -6367271
18 meter
Z = 1332645
12 Z = 406190
23
XDOT = 13600
481530 XDOT = 4145
426770
YDOT = -3605
454468 feet/sec YDOT = -1098
942522 meter/sec
ZDOT = 19675
971528 ZDOT = 5997
236122
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 15076
39909528
00016717 00000-0 10270-3 0 9157
2 25544 51
6418 182
5245 0008658 108
9983 251
2109 15
55258819 13754
Satellite: ISS
Catalog Number: 25544
Epoch time: 15076
39909528 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 182
5245 deg
Eccentricity:
0008658
Arg of perigee: 108
9983 deg
Mean anomaly: 251
2109 deg
Mean motion: 15
55258819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1375
Checksum: 345
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