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 21809U 91076E 21009.71621468 0.00000300 00000-0 53465-4 0 03
2 21809 63.3257 325.5500 0852385 39.0773 320.9227 13.41640958 04
| Epoch (UTC): | 09 January 2021 17:11:20 |
| Eccentricity: | 0.0852385 |
| inclination: | 63.3257° |
| perigee height: | 465 km |
| apogee height: | 1741 km |
| right ascension of ascending node: | 325.5500° |
| argument of perigee: | 39.0773° |
| revolutions per day: | 13.41640958 |
| mean anomaly at epoch: | 320.9227° |
| 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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