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 66408U 26145.41368698 +.00000000 +00000-0 +38029-3 0 00005
2 66408 53.1589 219.6889 0001069 116.0765 244.0348 15.34398122 05
| Epoch (UTC): | 25 May 2026 09:55:42 |
| Eccentricity: | 0.0001069 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.6889° |
| argument of perigee: | 116.0765° |
| revolutions per day: | 15.34398122 |
| mean anomaly at epoch: | 244.0348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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