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 30979U 99025BBV 24356.69400948 .00018761 00000-0 21975-2 0 9992
2 30979 97.8578 260.2123 0218713 309.4525 79.5514 14.69361656939111
Epoch (UTC): | 21 December 2024 16:39:22 |
Eccentricity: | 0.0218713 |
inclination: | 97.8578° |
perigee height: | 509 km |
apogee height: | 817 km |
right ascension of ascending node: | 260.2123° |
argument of perigee: | 309.4525° |
revolutions per day: | 14.69361656 |
mean anomaly at epoch: | 79.5514° |
orbit number at epoch: | 93911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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