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 42279U 95015GV 24356.55657967 .00033821 00000-0 76586-2 0 9995
2 42279 98.7406 32.0703 0009557 278.0213 81.9899 14.55979842502616
Epoch (UTC): | 21 December 2024 13:21:28 |
Eccentricity: | 0.0009557 |
inclination: | 98.7406° |
perigee height: | 699 km |
apogee height: | 713 km |
right ascension of ascending node: | 32.0703° |
argument of perigee: | 278.0213° |
revolutions per day: | 14.55979842 |
mean anomaly at epoch: | 81.9899° |
orbit number at epoch: | 50261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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