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 64225U 26145.42289185 +.00000000 +00000-0 +52642-3 0 00001
2 64225 53.1596 43.1995 0001235 95.4459 264.6683 15.30203675 05
| Epoch (UTC): | 25 May 2026 10:08:57 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.1995° |
| argument of perigee: | 95.4459° |
| revolutions per day: | 15.30203675 |
| mean anomaly at epoch: | 264.6683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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