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 10011U 77036B 24309.94814737 .00000053 00000-0 38877-3 0 9991
2 10011 65.8629 150.0753 0707033 265.7277 205.9020 12.32251138114347
Epoch (UTC): | 04 November 2024 22:45:19 |
Eccentricity: | 0.0707033 |
inclination: | 65.8629° |
perigee height: | 980 km |
apogee height: | 2099 km |
right ascension of ascending node: | 150.0753° |
argument of perigee: | 265.7277° |
revolutions per day: | 12.32251138 |
mean anomaly at epoch: | 205.9020° |
orbit number at epoch: | 11434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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