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 28384U 04034A 20355.63302333 0.00000000 00000-0 00000-0 0 07
2 28384 63.7068 144.2383 7105305 268.5198 16.6007 2.00616600 03
Epoch (UTC): | 20 December 2020 15:11:33 |
Eccentricity: | 0.7105305 |
inclination: | 63.7068° |
perigee height: | 1309 km |
apogee height: | 39046 km |
right ascension of ascending node: | 144.2383° |
argument of perigee: | 268.5198° |
revolutions per day: | 2.00616600 |
mean anomaly at epoch: | 16.6007° |
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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