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 38274U 79095BU 24350.63207588 .00014591 00000-0 49438-2 0 9997
2 38274 81.1936 314.1185 0017763 128.8736 231.4037 14.36590153533374
Epoch (UTC): | 15 December 2024 15:10:11 |
Eccentricity: | 0.0017763 |
inclination: | 81.1936° |
perigee height: | 757 km |
apogee height: | 782 km |
right ascension of ascending node: | 314.1185° |
argument of perigee: | 128.8736° |
revolutions per day: | 14.36590153 |
mean anomaly at epoch: | 231.4037° |
orbit number at epoch: | 53337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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