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 40012U 14033C 25193.82716316 .00002256 00000-0 26266-3 0 9992
2 40012 97.7460 349.0997 0049073 105.3654 255.2991 14.85390494595739
Epoch (UTC): | 12 July 2025 19:51:06 |
Eccentricity: | 0.0049073 |
inclination: | 97.7460° |
perigee height: | 578 km |
apogee height: | 646 km |
right ascension of ascending node: | 349.0997° |
argument of perigee: | 105.3654° |
revolutions per day: | 14.85390494 |
mean anomaly at epoch: | 255.2991° |
orbit number at epoch: | 59573 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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