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 23657U 95046A 25189.57983737 .00001215 00000-0 11373-3 0 9998
2 23657 82.5239 9.0406 0020165 39.2754 320.9924 14.93106127614685
| Epoch (UTC): | 08 July 2025 13:54:57 |
| Eccentricity: | 0.0020165 |
| inclination: | 82.5239° |
| perigee height: | 574 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 9.0406° |
| argument of perigee: | 39.2754° |
| revolutions per day: | 14.93106127 |
| mean anomaly at epoch: | 320.9924° |
| orbit number at epoch: | 61468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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