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 40012U 14033C 23091.55051702 .00003930 00000-0 56019-3 0 9997
2 40012 97.6684 269.4179 0054942 305.7158 53.8947 14.76285206472460
Epoch (UTC): | 01 April 2023 13:12:44 |
Eccentricity: | 0.0054942 |
inclination: | 97.6684° |
perigee height: | 602 km |
apogee height: | 679 km |
right ascension of ascending node: | 269.4179° |
argument of perigee: | 305.7158° |
revolutions per day: | 14.76285206 |
mean anomaly at epoch: | 53.8947° |
orbit number at epoch: | 47246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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