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 11416U 79057A 25194.79101325 .00000215 00000-0 90510-4 0 9997
2 11416 98.5978 221.1057 0009969 174.6507 185.4786 14.35200741402622
Epoch (UTC): | 13 July 2025 18:59:03 |
Eccentricity: | 0.0009969 |
inclination: | 98.5978° |
perigee height: | 767 km |
apogee height: | 781 km |
right ascension of ascending node: | 221.1057° |
argument of perigee: | 174.6507° |
revolutions per day: | 14.35200741 |
mean anomaly at epoch: | 185.4786° |
orbit number at epoch: | 40262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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