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 62232U 26145.51081626 +.00000000 +00000-0 +36592-3 0 00003
2 62232 53.1575 222.5451 0001327 43.1447 316.9657 15.30207927 03
| Epoch (UTC): | 25 May 2026 12:15:34 |
| Eccentricity: | 0.0001327 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.5451° |
| argument of perigee: | 43.1447° |
| revolutions per day: | 15.30207927 |
| mean anomaly at epoch: | 316.9657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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