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 65269U 26145.63470279 +.00000000 +00000-0 +18289-3 0 00008
2 65269 96.5866 77.2138 0003422 180.8169 179.3105 15.96389071 07
| Epoch (UTC): | 25 May 2026 15:13:58 |
| Eccentricity: | 0.0003422 |
| inclination: | 96.5866° |
| perigee height: | 282 km |
| apogee height: | 287 km |
| right ascension of ascending node: | 77.2138° |
| argument of perigee: | 180.8169° |
| revolutions per day: | 15.96389071 |
| mean anomaly at epoch: | 179.3105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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