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 64664U 26145.36366698 +.00000000 +00000-0 +95234-3 0 00000
2 64664 53.1588 130.1678 0001222 86.3622 273.7521 15.34400930 04
| Epoch (UTC): | 25 May 2026 08:43:40 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 130.1678° |
| argument of perigee: | 86.3622° |
| revolutions per day: | 15.34400930 |
| mean anomaly at epoch: | 273.7521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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