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 36514U 10015A 10333.18495302 0.00024000 00000-0 53063-4 0 08
2 36514 39.9979 75.6969 0006000 32.7289 327.2703 15.96897868 07
| Epoch (UTC): | 29 November 2010 04:26:19 |
| Eccentricity: | 0.0006000 |
| inclination: | 39.9979° |
| perigee height: | 279 km |
| apogee height: | 287 km |
| right ascension of ascending node: | 75.6969° |
| argument of perigee: | 32.7289° |
| revolutions per day: | 15.96897868 |
| mean anomaly at epoch: | 327.2703° |
| 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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