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 is defined by the following mean orbital elements,
1 65023U 26145.40515728 +.00000000 +00000-0 +82109-3 0 00002
2 65023 53.1611 297.9906 0001588 82.8149 277.3032 15.30219583 02
| Epoch (UTC): | 25 May 2026 09:43:25 |
| Eccentricity: | 0.0001588 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.9906° |
| argument of perigee: | 82.8149° |
| revolutions per day: | 15.30219583 |
| mean anomaly at epoch: | 277.3032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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