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 64506U 26145.06327727 +.00000000 +00000-0 +14522-3 0 00003
2 64506 51.8980 265.3166 0000510 97.7971 262.3050 14.79932722 03
| Epoch (UTC): | 25 May 2026 01:31:07 |
| Eccentricity: | 0.0000510 |
| inclination: | 51.8980° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 265.3166° |
| argument of perigee: | 97.7971° |
| revolutions per day: | 14.79932722 |
| mean anomaly at epoch: | 262.3050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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