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 31702U 07027B 14058.07535121 0.00000700 00000-0 31302-3 0 03
2 31702 63.3790 133.4519 0130000 347.1296 12.8704 14.18057467 00
| Epoch (UTC): | 27 February 2014 01:48:30 |
| Eccentricity: | 0.0130000 |
| inclination: | 63.3790° |
| perigee height: | 738 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 133.4519° |
| argument of perigee: | 347.1296° |
| revolutions per day: | 14.18057467 |
| mean anomaly at epoch: | 12.8704° |
| 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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