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 66510U 26145.37961492 +.00000000 +00000-0 +82743-3 0 00007
2 66510 43.0000 277.9383 0001846 281.6475 78.4169 15.27591406 03
| Epoch (UTC): | 25 May 2026 09:06:38 |
| Eccentricity: | 0.0001846 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.9383° |
| argument of perigee: | 281.6475° |
| revolutions per day: | 15.27591406 |
| mean anomaly at epoch: | 78.4169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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