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 20691U 90050C 23070.09848100 0.00004900 00000-0 50839-3 0 08
2 20691 63.3561 149.9560 0912865 62.1952 297.8048 13.45378296 00
| Epoch (UTC): | 11 March 2023 02:21:48 |
| Eccentricity: | 0.0912865 |
| inclination: | 63.3561° |
| perigee height: | 407 km |
| apogee height: | 1771 km |
| right ascension of ascending node: | 149.9560° |
| argument of perigee: | 62.1952° |
| revolutions per day: | 13.45378296 |
| mean anomaly at epoch: | 297.8048° |
| 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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