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 00011U 59001A 24311.85605936 .00002015 00000-0 10460-2 0 9991
2 00011 32.8706 145.8257 1454298 317.7210 31.9769 11.88889868465494
Epoch (UTC): | 06 November 2024 20:32:43 |
Eccentricity: | 0.1454298 |
inclination: | 32.8706° |
perigee height: | 551 km |
apogee height: | 2910 km |
right ascension of ascending node: | 145.8257° |
argument of perigee: | 317.7210° |
revolutions per day: | 11.88889868 |
mean anomaly at epoch: | 31.9769° |
orbit number at epoch: | 46549 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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