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 23079.16510883 .00041951 00000-0 11615-2 0 9994
2 40912 97.4264 95.6067 0012090 53.9408 11.5344 15.36792222415900
Epoch (UTC): | 20 March 2023 03:57:45 |
Eccentricity: | 0.0012090 |
inclination: | 97.4264° |
perigee height: | 447 km |
apogee height: | 464 km |
right ascension of ascending node: | 95.6067° |
argument of perigee: | 53.9408° |
revolutions per day: | 15.36792222 |
mean anomaly at epoch: | 11.5344° |
orbit number at epoch: | 41590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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