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 64822U 26145.34310566 +.00000000 +00000-0 +59102-3 0 00001
2 64822 51.8662 208.0571 0003006 196.1458 163.9436 15.43888464 01
| Epoch (UTC): | 25 May 2026 08:14:04 |
| Eccentricity: | 0.0003006 |
| inclination: | 51.8662° |
| perigee height: | 433 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 208.0571° |
| argument of perigee: | 196.1458° |
| revolutions per day: | 15.43888464 |
| mean anomaly at epoch: | 163.9436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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