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 is defined by the following mean orbital elements,
1 28505U 04052A 06105.74206257 .17719394 -16078-5 22993-3 0 9993
2 28505 082.5155 147.1105 0006107 020.6594 339.4942 16.49441267 74545
| Epoch (UTC): | 15 April 2006 17:48:34 |
| Eccentricity: | 0.0006107 |
| inclination: | 82.5155° |
| perigee height: | 137 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 147.1105° |
| argument of perigee: | 20.6594° |
| revolutions per day: | 16.49441267 |
| mean anomaly at epoch: | 339.4942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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