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 23081.84511780 .00039977 00000-0 11003-2 0 9995
2 40912 97.4263 98.3127 0011489 46.1597 77.6381 15.36995446416313
Epoch (UTC): | 22 March 2023 20:16:58 |
Eccentricity: | 0.0011489 |
inclination: | 97.4263° |
perigee height: | 447 km |
apogee height: | 463 km |
right ascension of ascending node: | 98.3127° |
argument of perigee: | 46.1597° |
revolutions per day: | 15.36995446 |
mean anomaly at epoch: | 77.6381° |
orbit number at epoch: | 41631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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