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 26040.04448752 +.00000000 +00000-0 +15554-3 0 00008
2 25261 98.8295 67.9385 0004197 133.0535 227.1002 14.36241015 09
| Epoch (UTC): | 09 February 2026 01:04:03 |
| Eccentricity: | 0.0004197 |
| inclination: | 98.8295° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 67.9385° |
| argument of perigee: | 133.0535° |
| revolutions per day: | 14.36241015 |
| mean anomaly at epoch: | 227.1002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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