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 62859U 26145.37941008 +.00000000 +00000-0 +90531-3 0 00004
2 62859 53.1574 133.2446 0001075 77.7227 282.3894 15.30208545 04
| Epoch (UTC): | 25 May 2026 09:06:21 |
| Eccentricity: | 0.0001075 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.2446° |
| argument of perigee: | 77.7227° |
| revolutions per day: | 15.30208545 |
| mean anomaly at epoch: | 282.3894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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