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 64224U 26145.41233889 +.00000000 +00000-0 +69579-3 0 00006
2 64224 53.1583 43.1353 0001105 84.2930 275.8196 15.30203962 06
| Epoch (UTC): | 25 May 2026 09:53:46 |
| Eccentricity: | 0.0001105 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.1353° |
| argument of perigee: | 84.2930° |
| revolutions per day: | 15.30203962 |
| mean anomaly at epoch: | 275.8196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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