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 66092U 26145.61349749 +.00000000 +00000-0 +62287-3 0 00005
2 66092 53.1613 106.4538 0001302 98.9961 261.1189 15.34399586 00
| Epoch (UTC): | 25 May 2026 14:43:26 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 106.4538° |
| argument of perigee: | 98.9961° |
| revolutions per day: | 15.34399586 |
| mean anomaly at epoch: | 261.1189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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