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 10967U 78064A 25198.35560489 .00000220 00000-0 10040-3 0 9995
2 10967 108.0112 351.8086 0001107 298.3047 61.7987 14.45867252472499
Epoch (UTC): | 17 July 2025 08:32:04 |
Eccentricity: | 0.0001107 |
inclination: | 108.0112° |
perigee height: | 738 km |
apogee height: | 740 km |
right ascension of ascending node: | 351.8086° |
argument of perigee: | 298.3047° |
revolutions per day: | 14.45867252 |
mean anomaly at epoch: | 61.7987° |
orbit number at epoch: | 47249 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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