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 65349U 26145.58125250 +.00000000 +00000-0 +60320-3 0 00000
2 65349 53.1594 209.2756 0001148 80.6265 279.4866 15.31717822 07
| Epoch (UTC): | 25 May 2026 13:57:00 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.2756° |
| argument of perigee: | 80.6265° |
| revolutions per day: | 15.31717822 |
| mean anomaly at epoch: | 279.4866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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