View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 28931U 06002A 13143.40620771 .00001012 00000-0 21826-3 0 1606
2 28931 098.0330 209.1077 0000964 043.7613 316.3665 14.60401929390421
| Epoch (UTC): | 23 May 2013 09:44:56 |
| Eccentricity: | 0.0000964 |
| inclination: | 98.0330° |
| perigee height: | 691 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 209.1077° |
| argument of perigee: | 43.7613° |
| revolutions per day: | 14.60401929 |
| mean anomaly at epoch: | 316.3665° |
| orbit number at epoch: | 39042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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