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 65696U 26145.26108551 +.00000000 +00000-0 +50195-3 0 00004
2 65696 53.1586 349.5290 0001058 61.7062 298.4046 15.31714230 00
| Epoch (UTC): | 25 May 2026 06:15:57 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 349.5290° |
| argument of perigee: | 61.7062° |
| revolutions per day: | 15.31714230 |
| mean anomaly at epoch: | 298.4046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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