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 23126.12428437 0.00008053 00000-0 75562-3 0 04
2 20691 63.3072 2.9404 0921700 63.7505 296.2495 13.46274083 00
| Epoch (UTC): | 06 May 2023 02:58:58 |
| Eccentricity: | 0.0921700 |
| inclination: | 63.3072° |
| perigee height: | 398 km |
| apogee height: | 1774 km |
| right ascension of ascending node: | 2.9404° |
| argument of perigee: | 63.7505° |
| revolutions per day: | 13.46274083 |
| mean anomaly at epoch: | 296.2495° |
| 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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