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 25991U 99067A 25109.20192777 .00000288 00000-0 16500-3 0 9992
2 25991 99.0439 136.3228 0010828 124.9935 300.2035 14.17351731310605
Epoch (UTC): | 19 April 2025 04:50:46 |
Eccentricity: | 0.0010828 |
inclination: | 99.0439° |
perigee height: | 826 km |
apogee height: | 842 km |
right ascension of ascending node: | 136.3228° |
argument of perigee: | 124.9935° |
revolutions per day: | 14.17351731 |
mean anomaly at epoch: | 300.2035° |
orbit number at epoch: | 31060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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