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 62322U 26145.58335647 +.00000000 +00000-0 +18800-2 0 00006
2 62322 53.1608 196.5666 0001556 80.3152 124.4391 15.33519233 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001556 |
| inclination: | 53.1608° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 196.5666° |
| argument of perigee: | 80.3152° |
| revolutions per day: | 15.33519233 |
| mean anomaly at epoch: | 124.4391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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