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 25861U 26162.15691161 +.00000000 +00000-0 +55785-4 0 00006
2 25861 97.9839 221.0369 0013806 318.1920 41.8237 14.81839095 07
| Epoch (UTC): | 11 June 2026 03:45:57 |
| Eccentricity: | 0.0013806 |
| inclination: | 97.9839° |
| perigee height: | 614 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 221.0369° |
| argument of perigee: | 318.1920° |
| revolutions per day: | 14.81839095 |
| mean anomaly at epoch: | 41.8237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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