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 64532U 26145.57303576 +.00000000 +00000-0 +41372-3 0 00007
2 64532 97.4704 261.8175 0003439 230.2973 129.7962 15.25659099 05
| Epoch (UTC): | 25 May 2026 13:45:10 |
| Eccentricity: | 0.0003439 |
| inclination: | 97.4704° |
| perigee height: | 486 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 261.8175° |
| argument of perigee: | 230.2973° |
| revolutions per day: | 15.25659099 |
| mean anomaly at epoch: | 129.7962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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