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 45274U 91056L 24357.52205764 .00000528 00000-0 13305-2 0 9994
2 45274 82.5374 159.0563 0027089 64.2607 296.1307 13.17416621233393
Epoch (UTC): | 22 December 2024 12:31:45 |
Eccentricity: | 0.0027089 |
inclination: | 82.5374° |
perigee height: | 1174 km |
apogee height: | 1215 km |
right ascension of ascending node: | 159.0563° |
argument of perigee: | 64.2607° |
revolutions per day: | 13.17416621 |
mean anomaly at epoch: | 296.1307° |
orbit number at epoch: | 23339 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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