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 23031U 94017B 14153.94708263 0.00350000 00000-0 55981-3 0 05
2 23031 105.0538 267.7474 0002000 296.5480 63.4519 16.03503507 04
| Epoch (UTC): | 02 June 2014 22:43:47 |
| Eccentricity: | 0.0002000 |
| inclination: | 105.0538° |
| perigee height: | 263 km |
| apogee height: | 266 km |
| right ascension of ascending node: | 267.7474° |
| argument of perigee: | 296.5480° |
| revolutions per day: | 16.03503507 |
| mean anomaly at epoch: | 63.4519° |
| 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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