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 64775U 26145.26155880 +.00000000 +00000-0 +50780-3 0 00008
2 64775 53.1569 246.4845 0001662 66.8859 293.2318 15.34413588 00
| Epoch (UTC): | 25 May 2026 06:16:38 |
| Eccentricity: | 0.0001662 |
| inclination: | 53.1569° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 246.4845° |
| argument of perigee: | 66.8859° |
| revolutions per day: | 15.34413588 |
| mean anomaly at epoch: | 293.2318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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