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 64222U 26145.42922365 +.00000000 +00000-0 +36676-3 0 00001
2 64222 53.1610 43.2406 0001163 98.5174 261.5959 15.30206700 09
| Epoch (UTC): | 25 May 2026 10:18:04 |
| Eccentricity: | 0.0001163 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.2406° |
| argument of perigee: | 98.5174° |
| revolutions per day: | 15.30206700 |
| mean anomaly at epoch: | 261.5959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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