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 66405U 26145.57131522 +.00000000 +00000-0 +37322-3 0 00008
2 66405 53.1585 219.2581 0001376 90.8926 269.2235 15.34394365 01
| Epoch (UTC): | 25 May 2026 13:42:41 |
| Eccentricity: | 0.0001376 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 219.2581° |
| argument of perigee: | 90.8926° |
| revolutions per day: | 15.34394365 |
| mean anomaly at epoch: | 269.2235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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