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 66797U 26145.41799736 +.00000000 +00000-0 +65685-3 0 00005
2 66797 43.0033 41.0519 0000990 280.1163 79.9577 15.27598169 06
| Epoch (UTC): | 25 May 2026 10:01:54 |
| Eccentricity: | 0.0000990 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.0519° |
| argument of perigee: | 280.1163° |
| revolutions per day: | 15.27598169 |
| mean anomaly at epoch: | 79.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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