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 22221.86176201 0.00003000 00000-0 39129-3 0 02
2 31702 63.3218 132.7856 0496934 23.7866 336.2134 14.20007747 01
| Epoch (UTC): | 09 August 2022 20:40:56 |
| Eccentricity: | 0.0496934 |
| inclination: | 63.3218° |
| perigee height: | 467 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 132.7856° |
| argument of perigee: | 23.7866° |
| revolutions per day: | 14.20007747 |
| mean anomaly at epoch: | 336.2134° |
| 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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