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 20663U 90055A 24317.31791368 .00006584 00000-0 48164-3 0 9990
2 20663 62.7901 175.8484 0093457 134.0956 226.7883 15.01069624863790
Epoch (UTC): | 12 November 2024 07:37:47 |
Eccentricity: | 0.0093457 |
inclination: | 62.7901° |
perigee height: | 499 km |
apogee height: | 628 km |
right ascension of ascending node: | 175.8484° |
argument of perigee: | 134.0956° |
revolutions per day: | 15.01069624 |
mean anomaly at epoch: | 226.7883° |
orbit number at epoch: | 86379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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