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 21397U 91039A 24286.52588324 .00007719 00000-0 62081-3 0 9997
2 21397 82.5152 112.3505 0014294 275.8846 84.0748 14.99790698809059
Epoch (UTC): | 12 October 2024 12:37:16 |
Eccentricity: | 0.0014294 |
inclination: | 82.5152° |
perigee height: | 557 km |
apogee height: | 577 km |
right ascension of ascending node: | 112.3505° |
argument of perigee: | 275.8846° |
revolutions per day: | 14.99790698 |
mean anomaly at epoch: | 84.0748° |
orbit number at epoch: | 80905 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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