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 26038.74828611 +.00000000 +00000-0 +34977-3 0 00006
2 25520 28.4309 175.7037 0002383 111.5342 248.5519 15.75013970 07
| Epoch (UTC): | 07 February 2026 17:57:31 |
| Eccentricity: | 0.0002383 |
| inclination: | 28.4309° |
| perigee height: | 343 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 175.7037° |
| argument of perigee: | 111.5342° |
| revolutions per day: | 15.75013970 |
| mean anomaly at epoch: | 248.5519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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