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 66404U 26145.41789863 +.00000000 +00000-0 +40537-3 0 00009
2 66404 53.1597 219.7265 0001434 60.1311 299.9834 15.34385549 09
| Epoch (UTC): | 25 May 2026 10:01:46 |
| Eccentricity: | 0.0001434 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 219.7265° |
| argument of perigee: | 60.1311° |
| revolutions per day: | 15.34385549 |
| mean anomaly at epoch: | 299.9834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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