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 26039.06916427 +.00000000 +00000-0 +17412-3 0 00002
2 25261 98.8295 66.9392 0004177 135.2580 224.8943 14.36240293 03
| Epoch (UTC): | 08 February 2026 01:39:35 |
| Eccentricity: | 0.0004177 |
| inclination: | 98.8295° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 66.9392° |
| argument of perigee: | 135.2580° |
| revolutions per day: | 14.36240293 |
| mean anomaly at epoch: | 224.8943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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