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 62810U 26145.46317383 +.00000000 +00000-0 +80752-3 0 00008
2 62810 53.1598 312.9287 0001958 104.6896 255.4322 15.30206982 08
| Epoch (UTC): | 25 May 2026 11:06:58 |
| Eccentricity: | 0.0001958 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 312.9287° |
| argument of perigee: | 104.6896° |
| revolutions per day: | 15.30206982 |
| mean anomaly at epoch: | 255.4322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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