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 27386U 02009A 24316.87932979 .00000658 00000-0 22801-3 0 9992
2 27386 98.3040 272.9900 0001346 82.6202 300.9983 14.38756298189817
Epoch (UTC): | 11 November 2024 21:06:14 |
Eccentricity: | 0.0001346 |
inclination: | 98.3040° |
perigee height: | 761 km |
apogee height: | 763 km |
right ascension of ascending node: | 272.9900° |
argument of perigee: | 82.6202° |
revolutions per day: | 14.38756298 |
mean anomaly at epoch: | 300.9983° |
orbit number at epoch: | 18981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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