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 26907U 01040C 25169.94169614 0.00000227 00000-0 11863-3 0 08
2 26907 63.3837 92.1250 0636214 10.7135 349.1969 13.42111920 09
Epoch (UTC): | 18 June 2025 22:36:02 |
Eccentricity: | 0.0636214 |
inclination: | 63.3837° |
perigee height: | 625 km |
apogee height: | 1577 km |
right ascension of ascending node: | 92.1250° |
argument of perigee: | 10.7135° |
revolutions per day: | 13.42111920 |
mean anomaly at epoch: | 349.1969° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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