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 29658U 06060A 12255.88503172 0.00006500 00000-0 24311-3 0 09
2 29658 98.1479 120.2938 0001000 82.9150 277.0848 15.27360175 04
| Epoch (UTC): | 11 September 2012 21:14:26 |
| Eccentricity: | 0.0001000 |
| inclination: | 98.1479° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.2938° |
| argument of perigee: | 82.9150° |
| revolutions per day: | 15.27360175 |
| mean anomaly at epoch: | 277.0848° |
| 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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