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 65346U 26145.58082074 +.00000000 +00000-0 +80468-3 0 00008
2 65346 53.1588 209.2736 0001181 79.0265 281.0868 15.30200500 04
| Epoch (UTC): | 25 May 2026 13:56:22 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.2736° |
| argument of perigee: | 79.0265° |
| revolutions per day: | 15.30200500 |
| mean anomaly at epoch: | 281.0868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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