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 01807U 65098C 25198.72725173 .00000249 00000-0 81161-4 0 9999
2 01807 79.8383 324.8160 1332864 349.1599 8.3145 12.27565920632255
Epoch (UTC): | 17 July 2025 17:27:14 |
Eccentricity: | 0.1332864 |
inclination: | 79.8383° |
perigee height: | 502 km |
apogee height: | 2618 km |
right ascension of ascending node: | 324.8160° |
argument of perigee: | 349.1599° |
revolutions per day: | 12.27565920 |
mean anomaly at epoch: | 8.3145° |
orbit number at epoch: | 63225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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