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 41879U 16075A 23080.47050671 -.00000220 00000-0 00000+0 0 9995
2 41879 0.0082 154.9314 0000443 279.0391 63.9147 1.00269808 23054
Epoch (UTC): | 21 March 2023 11:17:31 |
Eccentricity: | 0.0000443 |
inclination: | 0.0082° |
perigee height: | 35785 km |
apogee height: | 35788 km |
right ascension of ascending node: | 154.9314° |
argument of perigee: | 279.0391° |
revolutions per day: | 1.00269808 |
mean anomaly at epoch: | 63.9147° |
orbit number at epoch: | 2305 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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