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 26040.67148064 +.00000000 +00000-0 +16634-3 0 00000
2 25261 98.8295 68.5807 0004218 131.4693 228.6855 14.36241831 04
| Epoch (UTC): | 09 February 2026 16:06:55 |
| Eccentricity: | 0.0004218 |
| inclination: | 98.8295° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 68.5807° |
| argument of perigee: | 131.4693° |
| revolutions per day: | 14.36241831 |
| mean anomaly at epoch: | 228.6855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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