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 64769U 26145.57251063 +.00000000 +00000-0 +77750-3 0 00001
2 64769 53.1581 244.8757 0000462 343.0809 17.0179 15.34394133 04
| Epoch (UTC): | 25 May 2026 13:44:24 |
| Eccentricity: | 0.0000462 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 244.8757° |
| argument of perigee: | 343.0809° |
| revolutions per day: | 15.34394133 |
| mean anomaly at epoch: | 17.0179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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