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 64867U 26145.35432174 +.00000000 +00000-0 +00000-0 0 00001
2 64867 0.0555 8.4600 0002029 261.1190 90.3973 5.00114863 08
| Epoch (UTC): | 25 May 2026 08:30:13 |
| Eccentricity: | 0.0002029 |
| inclination: | 0.0555° |
| perigee height: | 8063 km |
| apogee height: | 8069 km |
| right ascension of ascending node: | 8.4600° |
| argument of perigee: | 261.1190° |
| revolutions per day: | 5.00114863 |
| mean anomaly at epoch: | 90.3973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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