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 25261U 26041.50747104 +.00000000 +00000-0 +16150-3 0 00006
2 25261 98.8294 69.4371 0004248 129.5879 230.5682 14.36242617 09
| Epoch (UTC): | 10 February 2026 12:10:45 |
| Eccentricity: | 0.0004248 |
| inclination: | 98.8294° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 69.4371° |
| argument of perigee: | 129.5879° |
| revolutions per day: | 14.36242617 |
| mean anomaly at epoch: | 230.5682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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