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 38861U 12056B 24358.08131918 .00005324 00000-0 58941-3 0 9997
2 38861 97.5601 353.7242 0015273 208.1438 151.8955 14.87649519659183
Epoch (UTC): | 23 December 2024 01:57:05 |
Eccentricity: | 0.0015273 |
inclination: | 97.5601° |
perigee height: | 594 km |
apogee height: | 616 km |
right ascension of ascending node: | 353.7242° |
argument of perigee: | 208.1438° |
revolutions per day: | 14.87649519 |
mean anomaly at epoch: | 151.8955° |
orbit number at epoch: | 65918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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