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 66943U 26145.58335647 +.00000000 +00000-0 +11234-2 0 00003
2 66943 53.1598 0.7645 0001394 98.7578 17.7421 15.34373756 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001394 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 0.7645° |
| argument of perigee: | 98.7578° |
| revolutions per day: | 15.34373756 |
| mean anomaly at epoch: | 17.7421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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