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 28646U 05016A 21057.20879102 0.00000000 00000-0 00000-0 0 05
2 28646 57.0106 129.0273 0006643 154.4421 205.5579 14.51847205 01
Epoch (UTC): | 26 February 2021 05:00:39 |
Eccentricity: | 0.0006643 |
inclination: | 57.0106° |
perigee height: | 715 km |
apogee height: | 724 km |
right ascension of ascending node: | 129.0273° |
argument of perigee: | 154.4421° |
revolutions per day: | 14.51847205 |
mean anomaly at epoch: | 205.5579° |
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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