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 62818U 26145.58335647 +.00000000 +00000-0 -71717-3 0 00004
2 62818 53.1596 312.1627 0001153 91.0641 316.1565 15.30207815 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 312.1627° |
| argument of perigee: | 91.0641° |
| revolutions per day: | 15.30207815 |
| mean anomaly at epoch: | 316.1565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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