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 66311U 26145.38448394 +.00000000 +00000-0 +00000-0 0 00001
2 66311 0.0292 91.6303 0002423 309.8544 53.8691 1.00271954 09
| Epoch (UTC): | 25 May 2026 09:13:39 |
| Eccentricity: | 0.0002423 |
| inclination: | 0.0292° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 91.6303° |
| argument of perigee: | 309.8544° |
| revolutions per day: | 1.00271954 |
| mean anomaly at epoch: | 53.8691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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