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 23465U 95002C 23272.44375042 .00000036 00000-0 22917-4 0 9995
2 23465 82.9298 35.7165 0038332 41.1654 23.0664 13.71940854435866
| Epoch (UTC): | 29 September 2023 10:39:00 |
| Eccentricity: | 0.0038332 |
| inclination: | 82.9298° |
| perigee height: | 964 km |
| apogee height: | 1021 km |
| right ascension of ascending node: | 35.7165° |
| argument of perigee: | 41.1654° |
| revolutions per day: | 13.71940854 |
| mean anomaly at epoch: | 23.0664° |
| orbit number at epoch: | 43586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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