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 64805U 26145.39428291 +.00000000 +00000-0 +30147-3 0 00000
2 64805 70.0005 301.1663 0002404 271.3608 88.7275 14.98338461 08
| Epoch (UTC): | 25 May 2026 09:27:46 |
| Eccentricity: | 0.0002404 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.1663° |
| argument of perigee: | 271.3608° |
| revolutions per day: | 14.98338461 |
| mean anomaly at epoch: | 88.7275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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