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 31834U 99025CHY 24351.90335192 .00001454 00000-0 86317-3 0 9993
2 31834 98.4152 233.9466 0163252 17.9331 342.7505 14.02481155904477
Epoch (UTC): | 16 December 2024 21:40:49 |
Eccentricity: | 0.0163252 |
inclination: | 98.4152° |
perigee height: | 766 km |
apogee height: | 1004 km |
right ascension of ascending node: | 233.9466° |
argument of perigee: | 17.9331° |
revolutions per day: | 14.02481155 |
mean anomaly at epoch: | 342.7505° |
orbit number at epoch: | 90447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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