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 25407U 26022.16717142 +.00000000 +00000-0 +19814-3 0 00008
2 25407 71.0112 279.4105 0005196 99.7364 260.4347 14.16184912 02
| Epoch (UTC): | 22 January 2026 04:00:43 |
| Eccentricity: | 0.0005196 |
| inclination: | 71.0112° |
| perigee height: | 835 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 279.4105° |
| argument of perigee: | 99.7364° |
| revolutions per day: | 14.16184912 |
| mean anomaly at epoch: | 260.4347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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