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 66225U 26145.53928828 +.00000000 +00000-0 +57972-3 0 00000
2 66225 53.1577 233.0855 0000498 308.5399 51.5557 15.30193561 07
| Epoch (UTC): | 25 May 2026 12:56:34 |
| Eccentricity: | 0.0000498 |
| inclination: | 53.1577° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.0855° |
| argument of perigee: | 308.5399° |
| revolutions per day: | 15.30193561 |
| mean anomaly at epoch: | 51.5557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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