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 41334U 16010A 25121.10454475 0.00000000 00000-0 00000-0 0 07
2 41334 123.0031 7.3212 0003229 58.0456 301.8756 13.41424232 02
Epoch (UTC): | 01 May 2025 02:30:32 |
Eccentricity: | 0.0003229 |
inclination: | 123.0031° |
perigee height: | 1101 km |
apogee height: | 1106 km |
right ascension of ascending node: | 7.3212° |
argument of perigee: | 58.0456° |
revolutions per day: | 13.41424232 |
mean anomaly at epoch: | 301.8756° |
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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