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 00082U 61004B 21059.87818319 -.00000060 00000-0 -23745-4 0 9996
2 00082 38.8653 328.8768 1176430 241.2099 106.5511 12.26044419839288
Epoch (UTC): | 28 February 2021 21:04:35 |
Eccentricity: | 0.1176430 |
inclination: | 38.8653° |
perigee height: | 632 km |
apogee height: | 2501 km |
right ascension of ascending node: | 328.8768° |
argument of perigee: | 241.2099° |
revolutions per day: | 12.26044419 |
mean anomaly at epoch: | 106.5511° |
orbit number at epoch: | 83928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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