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 66461U 26145.61838411 +.00000000 +00000-0 +63857-3 0 00008
2 66461 42.9983 221.5487 0001862 263.3825 96.6814 15.27585855 00
| Epoch (UTC): | 25 May 2026 14:50:28 |
| Eccentricity: | 0.0001862 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.5487° |
| argument of perigee: | 263.3825° |
| revolutions per day: | 15.27585855 |
| mean anomaly at epoch: | 96.6814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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