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 28537U 05004A 21060.80728292 0.00000000 00000-0 00000-0 0 04
2 28537 63.4259 334.8626 0387813 358.4792 1.5720 13.40817300 08
Epoch (UTC): | 01 March 2021 19:22:29 |
Eccentricity: | 0.0387813 |
inclination: | 63.4259° |
perigee height: | 816 km |
apogee height: | 1396 km |
right ascension of ascending node: | 334.8626° |
argument of perigee: | 358.4792° |
revolutions per day: | 13.40817300 |
mean anomaly at epoch: | 1.5720° |
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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