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 63866U 26145.41646877 +.00000000 +00000-0 +17640-3 0 00004
2 63866 70.0023 41.0978 0002192 272.5849 87.5060 14.98336182 04
| Epoch (UTC): | 25 May 2026 09:59:42 |
| Eccentricity: | 0.0002192 |
| inclination: | 70.0023° |
| perigee height: | 571 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.0978° |
| argument of perigee: | 272.5849° |
| revolutions per day: | 14.98336182 |
| mean anomaly at epoch: | 87.5060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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