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 64460U 26145.54250314 +.00000000 +00000-0 +39179-3 0 00007
2 64460 53.1564 91.2675 0001268 89.2129 270.9017 15.30205249 01
| Epoch (UTC): | 25 May 2026 13:01:12 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.1564° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.2675° |
| argument of perigee: | 89.2129° |
| revolutions per day: | 15.30205249 |
| mean anomaly at epoch: | 270.9017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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