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 64507U 26145.53191360 +.00000000 +00000-0 +44401-3 0 00007
2 64507 51.8983 235.7627 0000215 59.6925 300.4059 14.79970651 04
| Epoch (UTC): | 25 May 2026 12:45:57 |
| Eccentricity: | 0.0000215 |
| inclination: | 51.8983° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 235.7627° |
| argument of perigee: | 59.6925° |
| revolutions per day: | 14.79970651 |
| mean anomaly at epoch: | 300.4059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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