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 24298U 96051B 25194.64601566 -.00000179 00000-0 -70078-4 0 9996
2 24298 70.7674 321.1627 0013936 134.4197 225.8066 14.12408254487897
Epoch (UTC): | 13 July 2025 15:30:15 |
Eccentricity: | 0.0013936 |
inclination: | 70.7674° |
perigee height: | 841 km |
apogee height: | 861 km |
right ascension of ascending node: | 321.1627° |
argument of perigee: | 134.4197° |
revolutions per day: | 14.12408254 |
mean anomaly at epoch: | 225.8066° |
orbit number at epoch: | 48789 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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