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 64748U 26145.38802311 +.00000000 +00000-0 +29926-3 0 00007
2 64748 53.1585 184.8574 0000983 77.1560 282.9551 15.30205929 09
| Epoch (UTC): | 25 May 2026 09:18:45 |
| Eccentricity: | 0.0000983 |
| inclination: | 53.1585° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.8574° |
| argument of perigee: | 77.1560° |
| revolutions per day: | 15.30205929 |
| mean anomaly at epoch: | 282.9551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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