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 45293U 91056AF 24280.23495059 .00091695 00000-0 55470-1 0 9999
2 45293 82.5416 104.9876 0191657 161.9153 198.8960 13.97188544231233
Epoch (UTC): | 06 October 2024 05:38:19 |
Eccentricity: | 0.0191657 |
inclination: | 82.5416° |
perigee height: | 764 km |
apogee height: | 1043 km |
right ascension of ascending node: | 104.9876° |
argument of perigee: | 161.9153° |
revolutions per day: | 13.97188544 |
mean anomaly at epoch: | 198.8960° |
orbit number at epoch: | 23123 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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