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 66765U 26144.94538852 +.00000000 +00000-0 +39650-3 0 00000
2 66765 97.4218 219.5472 0001557 101.7372 258.4040 15.23064751 09
| Epoch (UTC): | 24 May 2026 22:41:21 |
| Eccentricity: | 0.0001557 |
| inclination: | 97.4218° |
| perigee height: | 496 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 219.5472° |
| argument of perigee: | 101.7372° |
| revolutions per day: | 15.23064751 |
| mean anomaly at epoch: | 258.4040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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