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 62482U 26145.43871800 +.00000000 +00000-0 +69169-3 0 00008
2 62482 43.0015 306.1462 0001754 273.0006 87.0645 15.27591552 06
| Epoch (UTC): | 25 May 2026 10:31:45 |
| Eccentricity: | 0.0001754 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.1462° |
| argument of perigee: | 273.0006° |
| revolutions per day: | 15.27591552 |
| mean anomaly at epoch: | 87.0645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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