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 65686U 26145.56022228 +.00000000 +00000-0 +57700-3 0 00001
2 65686 53.1584 338.5677 0001374 102.6228 257.4927 15.30216628 04
| Epoch (UTC): | 25 May 2026 13:26:43 |
| Eccentricity: | 0.0001374 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.5677° |
| argument of perigee: | 102.6228° |
| revolutions per day: | 15.30216628 |
| mean anomaly at epoch: | 257.4927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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