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 64711U 26145.34645340 +.00000000 +00000-0 +27028-3 0 00001
2 64711 69.9999 121.1540 0003968 261.7696 98.3013 14.98336433 07
| Epoch (UTC): | 25 May 2026 08:18:53 |
| Eccentricity: | 0.0003968 |
| inclination: | 69.9999° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1540° |
| argument of perigee: | 261.7696° |
| revolutions per day: | 14.98336433 |
| mean anomaly at epoch: | 98.3013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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