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 00020U 59007A 13142.01463878 .00000376 00000-0 13867-3 0 2257
2 00020 033.3585 013.6272 1681941 260.2189 080.5235 11.52672258931881
| Epoch (UTC): | 22 May 2013 00:21:04 |
| Eccentricity: | 0.1681941 |
| inclination: | 33.3585° |
| perigee height: | 507 km |
| apogee height: | 3292 km |
| right ascension of ascending node: | 13.6272° |
| argument of perigee: | 260.2189° |
| revolutions per day: | 11.52672258 |
| mean anomaly at epoch: | 80.5235° |
| orbit number at epoch: | 93188 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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