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 64847U 26145.55167955 +.00000000 +00000-0 +20269-3 0 00005
2 64847 97.4485 0.8921 0002007 76.2768 283.8683 15.05655019 08
| Epoch (UTC): | 25 May 2026 13:14:25 |
| Eccentricity: | 0.0002007 |
| inclination: | 97.4485° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.8921° |
| argument of perigee: | 76.2768° |
| revolutions per day: | 15.05655019 |
| mean anomaly at epoch: | 283.8683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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