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 64886U 26145.58745479 +.00000000 +00000-0 +76935-3 0 00005
2 64886 97.4453 116.0611 0004312 220.2578 139.8349 15.40135014 09
| Epoch (UTC): | 25 May 2026 14:05:56 |
| Eccentricity: | 0.0004312 |
| inclination: | 97.4453° |
| perigee height: | 443 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 116.0611° |
| argument of perigee: | 220.2578° |
| revolutions per day: | 15.40135014 |
| mean anomaly at epoch: | 139.8349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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