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 64269U 26145.32998476 +.00000000 +00000-0 +10447-2 0 00004
2 64269 53.1594 118.3295 0001549 84.3922 275.7258 15.34411088 03
| Epoch (UTC): | 25 May 2026 07:55:10 |
| Eccentricity: | 0.0001549 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 118.3295° |
| argument of perigee: | 84.3922° |
| revolutions per day: | 15.34411088 |
| mean anomaly at epoch: | 275.7258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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