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 23466U 95002D 24357.66058476 .00000157 00000-0 14863-3 0 9998
2 23466 82.9250 28.6618 0035998 110.1974 8.2529 13.74639839500179
| Epoch (UTC): | 22 December 2024 15:51:14 |
| Eccentricity: | 0.0035998 |
| inclination: | 82.9250° |
| perigee height: | 956 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 28.6618° |
| argument of perigee: | 110.1974° |
| revolutions per day: | 13.74639839 |
| mean anomaly at epoch: | 8.2529° |
| orbit number at epoch: | 50017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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