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 25940U 99057A 24308.57387272 .00001307 00000-0 46113-3 0 9997
2 25940 98.8214 291.2659 0004127 309.9896 50.0927 14.36507179312705
Epoch (UTC): | 03 November 2024 13:46:22 |
Eccentricity: | 0.0004127 |
inclination: | 98.8214° |
perigee height: | 767 km |
apogee height: | 773 km |
right ascension of ascending node: | 291.2659° |
argument of perigee: | 309.9896° |
revolutions per day: | 14.36507179 |
mean anomaly at epoch: | 50.0927° |
orbit number at epoch: | 31270 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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