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 25940U 26041.93705446 +.00000000 +00000-0 +97350-4 0 00002
2 25940 98.8511 47.9280 0005273 22.8229 337.3190 14.36945275 08
| Epoch (UTC): | 10 February 2026 22:29:21 |
| Eccentricity: | 0.0005273 |
| inclination: | 98.8511° |
| perigee height: | 765 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 47.9280° |
| argument of perigee: | 22.8229° |
| revolutions per day: | 14.36945275 |
| mean anomaly at epoch: | 337.3190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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