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 66235U 26145.39776189 +.00000000 +00000-0 +61672-3 0 00008
2 66235 53.1592 287.3947 0001233 121.9458 238.1662 15.30212843 05
| Epoch (UTC): | 25 May 2026 09:32:46 |
| Eccentricity: | 0.0001233 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.3947° |
| argument of perigee: | 121.9458° |
| revolutions per day: | 15.30212843 |
| mean anomaly at epoch: | 238.1662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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