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 31708U 07027C 23087.92977934 0.00000000 00000-0 00000-0 0 08
2 31708 63.3855 96.0768 0372658 20.1891 339.8109 13.40867537 06
| Epoch (UTC): | 28 March 2023 22:18:52 |
| Eccentricity: | 0.0372658 |
| inclination: | 63.3855° |
| perigee height: | 827 km |
| apogee height: | 1385 km |
| right ascension of ascending node: | 96.0768° |
| argument of perigee: | 20.1891° |
| revolutions per day: | 13.40867537 |
| mean anomaly at epoch: | 339.8109° |
| 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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