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 32376U 07059A 21060.52410544 -.00000776 00000-0 -90952-4 0 9997
2 32376 97.8852 245.9504 0001619 81.9956 278.1441 14.82150227715659
Epoch (UTC): | 01 March 2021 12:34:42 |
Eccentricity: | 0.0001619 |
inclination: | 97.8852° |
perigee height: | 621 km |
apogee height: | 623 km |
right ascension of ascending node: | 245.9504° |
argument of perigee: | 81.9956° |
revolutions per day: | 14.82150227 |
mean anomaly at epoch: | 278.1441° |
orbit number at epoch: | 71565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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