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 24276.76998888 .00045353 00000-0 11183-2 0 9997
2 18421 82.4902 147.7836 0009092 350.1552 9.9514 15.40312899 23195
Epoch (UTC): | 02 October 2024 18:28:47 |
Eccentricity: | 0.0009092 |
inclination: | 82.4902° |
perigee height: | 439 km |
apogee height: | 451 km |
right ascension of ascending node: | 147.7836° |
argument of perigee: | 350.1552° |
revolutions per day: | 15.40312899 |
mean anomaly at epoch: | 9.9514° |
orbit number at epoch: | 2319 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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