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 28647U 05016B 21059.62229189 .00000110 00000-0 24684-4 0 9995
2 28647 56.9970 278.5050 0119579 244.6817 114.1796 15.06270749 98553
Epoch (UTC): | 28 February 2021 14:56:06 |
Eccentricity: | 0.0119579 |
inclination: | 56.9970° |
perigee height: | 465 km |
apogee height: | 630 km |
right ascension of ascending node: | 278.5050° |
argument of perigee: | 244.6817° |
revolutions per day: | 15.06270749 |
mean anomaly at epoch: | 114.1796° |
orbit number at epoch: | 9855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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