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 62505U 26145.50130705 +.00000000 +00000-0 +45316-3 0 00002
2 62505 43.0041 214.7517 0001251 273.2802 86.7906 15.27589402 01
| Epoch (UTC): | 25 May 2026 12:01:52 |
| Eccentricity: | 0.0001251 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 214.7517° |
| argument of perigee: | 273.2802° |
| revolutions per day: | 15.27589402 |
| mean anomaly at epoch: | 86.7906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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