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 14207U 83075A 13028.01864212 .17144267 28817-5 11508-3 0 9996
2 14207 097.5736 255.6458 0007149 229.5798 131.1414 16.53734211 67024
| Epoch (UTC): | 28 January 2013 00:26:50 |
| Eccentricity: | 0.0007149 |
| inclination: | 97.5736° |
| perigee height: | 125 km |
| apogee height: | 134 km |
| right ascension of ascending node: | 255.6458° |
| argument of perigee: | 229.5798° |
| revolutions per day: | 16.53734211 |
| mean anomaly at epoch: | 131.1414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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