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 64556U 26145.29489829 +.00000000 +00000-0 +32626-3 0 00000
2 64556 97.4716 261.9365 0002916 123.1931 236.9586 15.25389950 08
| Epoch (UTC): | 25 May 2026 07:04:39 |
| Eccentricity: | 0.0002916 |
| inclination: | 97.4716° |
| perigee height: | 488 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 261.9365° |
| argument of perigee: | 123.1931° |
| revolutions per day: | 15.25389950 |
| mean anomaly at epoch: | 236.9586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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