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 25876U 26040.19510455 +.00000000 +00000-0 +40613-3 0 00000
2 25876 51.7652 55.0694 0502293 264.2488 90.0990 14.11722843 00
| Epoch (UTC): | 09 February 2026 04:40:57 |
| Eccentricity: | 0.0502293 |
| inclination: | 51.7652° |
| perigee height: | 490 km |
| apogee height: | 1217 km |
| right ascension of ascending node: | 55.0694° |
| argument of perigee: | 264.2488° |
| revolutions per day: | 14.11722843 |
| mean anomaly at epoch: | 90.0990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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