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 62857U 26145.35103299 +.00000000 +00000-0 +42804-3 0 00002
2 62857 53.1585 133.7936 0001243 94.9889 265.1253 15.30212146 05
| Epoch (UTC): | 25 May 2026 08:25:29 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.7936° |
| argument of perigee: | 94.9889° |
| revolutions per day: | 15.30212146 |
| mean anomaly at epoch: | 265.1253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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