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 64505U 26145.36446279 +.00000000 +00000-0 +23752-3 0 00004
2 64505 51.8983 266.5018 0000743 108.3370 251.7673 14.79936630 09
| Epoch (UTC): | 25 May 2026 08:44:49 |
| Eccentricity: | 0.0000743 |
| inclination: | 51.8983° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 266.5018° |
| argument of perigee: | 108.3370° |
| revolutions per day: | 14.79936630 |
| mean anomaly at epoch: | 251.7673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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