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 31217U 99025BKX 24356.82998846 .00002038 00000-0 10004-2 0 9993
2 31217 98.6509 8.5646 0102286 102.6400 258.6235 14.16087657913081
Epoch (UTC): | 21 December 2024 19:55:11 |
Eccentricity: | 0.0102286 |
inclination: | 98.6509° |
perigee height: | 765 km |
apogee height: | 912 km |
right ascension of ascending node: | 8.5646° |
argument of perigee: | 102.6400° |
revolutions per day: | 14.16087657 |
mean anomaly at epoch: | 258.6235° |
orbit number at epoch: | 91308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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