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 18421U 87088A 24281.70654889 .00047792 00000-0 11612-2 0 9993
2 18421 82.4891 142.7142 0008408 330.4329 29.6440 15.40758720 24173
Epoch (UTC): | 07 October 2024 16:57:25 |
Eccentricity: | 0.0008408 |
inclination: | 82.4891° |
perigee height: | 438 km |
apogee height: | 449 km |
right ascension of ascending node: | 142.7142° |
argument of perigee: | 330.4329° |
revolutions per day: | 15.40758720 |
mean anomaly at epoch: | 29.6440° |
orbit number at epoch: | 2417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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