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 27700U 03009C 12154.98816624 .16982402 24126-5 14754-3 0 9991
2 27700 096.9637 159.8595 0011978 208.9979 151.8555 16.51542568515127
| Epoch (UTC): | 02 June 2012 23:42:57 |
| Eccentricity: | 0.0011978 |
| inclination: | 96.9637° |
| perigee height: | 127 km |
| apogee height: | 143 km |
| right ascension of ascending node: | 159.8595° |
| argument of perigee: | 208.9979° |
| revolutions per day: | 16.51542568 |
| mean anomaly at epoch: | 151.8555° |
| orbit number at epoch: | 51512 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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