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 26039.48716295 +.00000000 +00000-0 +40154-3 0 00000
2 25876 51.7650 57.8962 0502305 262.1571 92.2080 14.11719355 08
| Epoch (UTC): | 08 February 2026 11:41:30 |
| Eccentricity: | 0.0502305 |
| inclination: | 51.7650° |
| perigee height: | 490 km |
| apogee height: | 1217 km |
| right ascension of ascending node: | 57.8962° |
| argument of perigee: | 262.1571° |
| revolutions per day: | 14.11719355 |
| mean anomaly at epoch: | 92.2080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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