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 25867U 26108.55302551 +.00000000 +00000-0 +00000-0 0 00004
2 25867 55.2416 118.3602 7940395 310.5754 0.2310 0.37809990 07
| Epoch (UTC): | 18 April 2026 13:16:21 |
| Eccentricity: | 0.7940395 |
| inclination: | 55.2416° |
| perigee height: | 10260 km |
| apogee height: | 138553 km |
| right ascension of ascending node: | 118.3602° |
| argument of perigee: | 310.5754° |
| revolutions per day: | 0.37809990 |
| mean anomaly at epoch: | 0.2310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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