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 25860U 26128.13235161 +.00000000 +00000-0 +70543-4 0 00008
2 25860 97.9340 187.3852 0001835 105.8987 254.2428 14.80418982 06
| Epoch (UTC): | 08 May 2026 03:10:35 |
| Eccentricity: | 0.0001835 |
| inclination: | 97.9340° |
| perigee height: | 627 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 187.3852° |
| argument of perigee: | 105.8987° |
| revolutions per day: | 14.80418982 |
| mean anomaly at epoch: | 254.2428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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