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 23696U 95057A 23267.68450920 -.00000220 00000-0 00000-0 0 9991
2 23696 10.7129 19.2104 0008745 140.7185 48.7673 0.98765765101937
Epoch (UTC): | 24 September 2023 16:25:41 |
Eccentricity: | 0.0008745 |
inclination: | 10.7129° |
perigee height: | 36176 km |
apogee height: | 36251 km |
right ascension of ascending node: | 19.2104° |
argument of perigee: | 140.7185° |
revolutions per day: | 0.98765765 |
mean anomaly at epoch: | 48.7673° |
orbit number at epoch: | 10193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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