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 62856U 26145.58335647 +.00000000 +00000-0 -63822-3 0 00004
2 62856 53.1584 132.6834 0001161 78.4617 135.6236 15.33561034 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001161 |
| inclination: | 53.1584° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 132.6834° |
| argument of perigee: | 78.4617° |
| revolutions per day: | 15.33561034 |
| mean anomaly at epoch: | 135.6236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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