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 26039.48715999 +.00000000 +00000-0 +17412-3 0 00009
2 25261 98.8295 67.3674 0004194 134.2662 225.8868 14.36240755 00
| Epoch (UTC): | 08 February 2026 11:41:30 |
| Eccentricity: | 0.0004194 |
| inclination: | 98.8295° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 67.3674° |
| argument of perigee: | 134.2662° |
| revolutions per day: | 14.36240755 |
| mean anomaly at epoch: | 225.8868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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