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 26105.37290066 +.00000000 +00000-0 +58456-4 0 00000
2 25407 71.0091 104.4298 0008908 316.2646 43.7771 14.16198820 08
| Epoch (UTC): | 15 April 2026 08:56:58 |
| Eccentricity: | 0.0008908 |
| inclination: | 71.0091° |
| perigee height: | 832 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 104.4298° |
| argument of perigee: | 316.2646° |
| revolutions per day: | 14.16198820 |
| mean anomaly at epoch: | 43.7771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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