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 23463U 95002A 25131.52466738 .00000083 00000-0 72936-4 0 9999
2 23463 82.9250 312.9591 0039068 173.3067 241.3937 13.72696953517204
| Epoch (UTC): | 11 May 2025 12:35:31 |
| Eccentricity: | 0.0039068 |
| inclination: | 82.9250° |
| perigee height: | 961 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 312.9591° |
| argument of perigee: | 173.3067° |
| revolutions per day: | 13.72696953 |
| mean anomaly at epoch: | 241.3937° |
| orbit number at epoch: | 51720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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