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 23083.33391463 .00000150 00000-0 14791-3 0 9995
2 23465 82.9311 175.3944 0037025 202.1482 219.6175 13.71929145409933
| Epoch (UTC): | 24 March 2023 08:00:50 |
| Eccentricity: | 0.0037025 |
| inclination: | 82.9311° |
| perigee height: | 965 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 175.3944° |
| argument of perigee: | 202.1482° |
| revolutions per day: | 13.71929145 |
| mean anomaly at epoch: | 219.6175° |
| orbit number at epoch: | 40993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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