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 35693U 09038E 10087.99866888 .23496735 12787-4 17715-3 0 9996
2 35693 051.6099 254.5746 0006270 294.4866 097.5899 16.52338462 38395
| Epoch (UTC): | 28 March 2010 23:58:04 |
| Eccentricity: | 0.0006270 |
| inclination: | 51.6099° |
| perigee height: | 129 km |
| apogee height: | 137 km |
| right ascension of ascending node: | 254.5746° |
| argument of perigee: | 294.4866° |
| revolutions per day: | 16.52338462 |
| mean anomaly at epoch: | 97.5899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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