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 65055U 26145.58866964 +.00000000 +00000-0 +31184-3 0 00004
2 65055 41.1310 55.0629 0006723 214.1075 145.9307 15.06211062 01
| Epoch (UTC): | 25 May 2026 14:07:41 |
| Eccentricity: | 0.0006723 |
| inclination: | 41.1310° |
| perigee height: | 543 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 55.0629° |
| argument of perigee: | 214.1075° |
| revolutions per day: | 15.06211062 |
| mean anomaly at epoch: | 145.9307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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