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 64531U 26145.57217912 +.00000000 +00000-0 +40762-3 0 00006
2 64531 97.4689 261.7833 0003479 231.2670 128.8258 15.25654888 04
| Epoch (UTC): | 25 May 2026 13:43:56 |
| Eccentricity: | 0.0003479 |
| inclination: | 97.4689° |
| perigee height: | 486 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 261.7833° |
| argument of perigee: | 231.2670° |
| revolutions per day: | 15.25654888 |
| mean anomaly at epoch: | 128.8258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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