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 36105U 09066B 13133.89455522 0.00004500 00000-0 32623-3 0 08
2 36105 97.5261 192.5433 0037584 76.8222 283.1776 15.03418677 04
| Epoch (UTC): | 13 May 2013 21:28:09 |
| Eccentricity: | 0.0037584 |
| inclination: | 97.5261° |
| perigee height: | 530 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 192.5433° |
| argument of perigee: | 76.8222° |
| revolutions per day: | 15.03418677 |
| mean anomaly at epoch: | 283.1776° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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