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 64690U 26145.36787245 +.00000000 +00000-0 +54377-3 0 00007
2 64690 53.1587 130.1833 0001177 74.9538 285.1594 15.34395910 01
| Epoch (UTC): | 25 May 2026 08:49:44 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 130.1833° |
| argument of perigee: | 74.9538° |
| revolutions per day: | 15.34395910 |
| mean anomaly at epoch: | 285.1594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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