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 66252U 26145.50003470 +.00000000 +00000-0 -24061-3 0 00008
2 66252 53.1596 286.8465 0001191 88.1884 150.5155 15.30197073 08
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.8465° |
| argument of perigee: | 88.1884° |
| revolutions per day: | 15.30197073 |
| mean anomaly at epoch: | 150.5155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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