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 64220U 26145.41972638 +.00000000 +00000-0 +44516-3 0 00008
2 64220 53.1598 43.1778 0001125 82.6444 277.4685 15.30205894 00
| Epoch (UTC): | 25 May 2026 10:04:24 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.1778° |
| argument of perigee: | 82.6444° |
| revolutions per day: | 15.30205894 |
| mean anomaly at epoch: | 277.4685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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