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 26041.88977662 +.00000000 +00000-0 +88338-4 0 00005
2 25861 98.0026 101.0181 0014457 349.7627 10.3289 14.81693200 07
| Epoch (UTC): | 10 February 2026 21:21:16 |
| Eccentricity: | 0.0014457 |
| inclination: | 98.0026° |
| perigee height: | 614 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 101.0181° |
| argument of perigee: | 349.7627° |
| revolutions per day: | 14.81693200 |
| mean anomaly at epoch: | 10.3289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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