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 28636U 05011A 11067.75881337 0.00009400 00000-0 30001-3 0 02
2 28636 98.5490 258.3711 0226829 47.1785 312.8214 15.11053919 06
| Epoch (UTC): | 08 March 2011 18:12:41 |
| Eccentricity: | 0.0226829 |
| inclination: | 98.5490° |
| perigee height: | 376 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 258.3711° |
| argument of perigee: | 47.1785° |
| revolutions per day: | 15.11053919 |
| mean anomaly at epoch: | 312.8214° |
| 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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