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 16262U 85108A 25197.46341074 .00009553 00000-0 24211-3 0 9997
2 16262 82.4627 206.5753 0008864 124.9875 235.2204 15.39513381165568
Epoch (UTC): | 16 July 2025 11:07:18 |
Eccentricity: | 0.0008864 |
inclination: | 82.4627° |
perigee height: | 441 km |
apogee height: | 453 km |
right ascension of ascending node: | 206.5753° |
argument of perigee: | 124.9875° |
revolutions per day: | 15.39513381 |
mean anomaly at epoch: | 235.2204° |
orbit number at epoch: | 16556 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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