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 25194.50080108 .00002479 00000-0 28795-3 0 9997
2 40012 97.7461 349.7550 0049073 103.2128 257.4569 14.85393962595834
Epoch (UTC): | 13 July 2025 12:01:09 |
Eccentricity: | 0.0049073 |
inclination: | 97.7461° |
perigee height: | 578 km |
apogee height: | 646 km |
right ascension of ascending node: | 349.7550° |
argument of perigee: | 103.2128° |
revolutions per day: | 14.85393962 |
mean anomaly at epoch: | 257.4569° |
orbit number at epoch: | 59583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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