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 3266U 68042A 24358.13038940 .00000187 00000-0 11513-3 0 9997
2 3266 98.5812 198.6359 0053517 57.6520 302.9819 14.15709655836988
Epoch (UTC): | 23 December 2024 03:07:45 |
Eccentricity: | 0.0053517 |
inclination: | 98.5812° |
perigee height: | 801 km |
apogee height: | 878 km |
right ascension of ascending node: | 198.6359° |
argument of perigee: | 57.6520° |
revolutions per day: | 14.15709655 |
mean anomaly at epoch: | 302.9819° |
orbit number at epoch: | 83698 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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