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 25520U 26106.94825251 +.00000000 +00000-0 +20998-3 0 00009
2 25520 28.4326 34.4983 0001764 280.6593 79.3817 15.82920802 05
| Epoch (UTC): | 16 April 2026 22:45:29 |
| Eccentricity: | 0.0001764 |
| inclination: | 28.4326° |
| perigee height: | 321 km |
| apogee height: | 323 km |
| right ascension of ascending node: | 34.4983° |
| argument of perigee: | 280.6593° |
| revolutions per day: | 15.82920802 |
| mean anomaly at epoch: | 79.3817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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