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 00107U 61013A 23338.93424094 .00002868 00000-0 35408-3 0 9990
2 00107 28.7865 219.6609 0527339 178.5535 181.6678 14.13758178145026
Epoch (UTC): | 04 December 2023 22:25:18 |
Eccentricity: | 0.0527339 |
inclination: | 28.7865° |
perigee height: | 465 km |
apogee height: | 1227 km |
right ascension of ascending node: | 219.6609° |
argument of perigee: | 178.5535° |
revolutions per day: | 14.13758178 |
mean anomaly at epoch: | 181.6678° |
orbit number at epoch: | 14502 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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