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 23855U 96026A 22277.80536195 0.00000000 00000-0 00000-0 0 06
2 23855 8.5591 353.3250 0359634 283.9458 76.0545 1.00270000 00
Epoch (UTC): | 04 October 2022 19:19:43 |
Eccentricity: | 0.0359634 |
inclination: | 8.5591° |
perigee height: | 34270 km |
apogee height: | 37303 km |
right ascension of ascending node: | 353.3250° |
argument of perigee: | 283.9458° |
revolutions per day: | 1.00270000 |
mean anomaly at epoch: | 76.0545° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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