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 40912U 15049P 23333.46641209 .00215169 00000-0 16902-2 0 9995
2 40912 97.3933 356.8046 0005269 154.6288 205.5234 15.70852497455272
Epoch (UTC): | 29 November 2023 11:11:38 |
Eccentricity: | 0.0005269 |
inclination: | 97.3933° |
perigee height: | 353 km |
apogee height: | 360 km |
right ascension of ascending node: | 356.8046° |
argument of perigee: | 154.6288° |
revolutions per day: | 15.70852497 |
mean anomaly at epoch: | 205.5234° |
orbit number at epoch: | 45527 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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