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 21808U 91076D 21008.77084331 0.00000250 00000-0 43968-4 0 00
2 21808 63.3244 330.8117 0855591 41.1517 318.8483 13.41425099 01
Epoch (UTC): | 08 January 2021 18:30:00 |
Eccentricity: | 0.0855591 |
inclination: | 63.3244° |
perigee height: | 464 km |
apogee height: | 1744 km |
right ascension of ascending node: | 330.8117° |
argument of perigee: | 41.1517° |
revolutions per day: | 13.41425099 |
mean anomaly at epoch: | 318.8483° |
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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