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 62806U 26145.46104492 +.00000000 +00000-0 +18629-2 0 00001
2 62806 53.1611 312.9228 0001196 82.1723 277.9414 15.30274300 07
| Epoch (UTC): | 25 May 2026 11:03:54 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 312.9228° |
| argument of perigee: | 82.1723° |
| revolutions per day: | 15.30274300 |
| mean anomaly at epoch: | 277.9414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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