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 is defined by the following mean orbital elements,
1 32797U 08021L 12260.72212042 .00344703 00000-0 53616-2 0 9994
2 32797 097.8859 353.7789 0007409 275.5558 066.5928 15.52667758237511
| Epoch (UTC): | 16 September 2012 17:19:51 |
| Eccentricity: | 0.0007409 |
| inclination: | 97.8859° |
| perigee height: | 404 km |
| apogee height: | 414 km |
| right ascension of ascending node: | 353.7789° |
| argument of perigee: | 275.5558° |
| revolutions per day: | 15.52667758 |
| mean anomaly at epoch: | 66.5928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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