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 11964U 80074A 23088.86073295 -.00000165 00000-0 00000-0 0 9994
2 11964 10.5358 312.6562 0033802 81.1004 104.7345 0.99233316115771
Epoch (UTC): | 29 March 2023 20:39:27 |
Eccentricity: | 0.0033802 |
inclination: | 10.5358° |
perigee height: | 35936 km |
apogee height: | 36223 km |
right ascension of ascending node: | 312.6562° |
argument of perigee: | 81.1004° |
revolutions per day: | 0.99233316 |
mean anomaly at epoch: | 104.7345° |
orbit number at epoch: | 11577 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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