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 21059.13676120 0.00000000 00000-0 00000-0 0 04
2 28646 57.0106 121.8333 0006643 157.6108 202.3892 14.51847205 08
Epoch (UTC): | 28 February 2021 03:16:56 |
Eccentricity: | 0.0006643 |
inclination: | 57.0106° |
perigee height: | 715 km |
apogee height: | 724 km |
right ascension of ascending node: | 121.8333° |
argument of perigee: | 157.6108° |
revolutions per day: | 14.51847205 |
mean anomaly at epoch: | 202.3892° |
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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