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 26088.14780372 +.00000000 +00000-0 +87488-4 0 00000
2 25861 97.9924 147.2114 0014580 189.1889 170.9059 14.81757578 00
| Epoch (UTC): | 29 March 2026 03:32:50 |
| Eccentricity: | 0.0014580 |
| inclination: | 97.9924° |
| perigee height: | 614 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 147.2114° |
| argument of perigee: | 189.1889° |
| revolutions per day: | 14.81757578 |
| mean anomaly at epoch: | 170.9059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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