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 00020U 59007A 21101.93577681 -.00000031 00000-0 -52447-5 0 9997
2 00020 33.3409 198.6205 1666223 50.2186 323.3693 11.55804494265143
Epoch (UTC): | 11 April 2021 22:27:31 |
Eccentricity: | 0.1666223 |
inclination: | 33.3409° |
perigee height: | 508 km |
apogee height: | 3262 km |
right ascension of ascending node: | 198.6205° |
argument of perigee: | 50.2186° |
revolutions per day: | 11.55804494 |
mean anomaly at epoch: | 323.3693° |
orbit number at epoch: | 26514 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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