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 64524U 26145.34148253 +.00000000 +00000-0 +49252-3 0 00007
2 64524 51.9020 256.5873 0000502 107.0169 253.0848 14.79938939 09
| Epoch (UTC): | 25 May 2026 08:11:44 |
| Eccentricity: | 0.0000502 |
| inclination: | 51.9020° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 256.5873° |
| argument of perigee: | 107.0169° |
| revolutions per day: | 14.79938939 |
| mean anomaly at epoch: | 253.0848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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