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 64833U 26145.46177507 +.00000000 +00000-0 +45095-3 0 00008
2 64833 51.8996 301.0907 0000611 110.1162 249.9866 14.79939384 05
| Epoch (UTC): | 25 May 2026 11:04:57 |
| Eccentricity: | 0.0000611 |
| inclination: | 51.8996° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 301.0907° |
| argument of perigee: | 110.1162° |
| revolutions per day: | 14.79939384 |
| mean anomaly at epoch: | 249.9866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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