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 26137.59486794 +.00000000 +00000-0 +53313-4 0 00004
2 25860 97.9334 196.7413 0001983 98.0545 262.0892 14.80426804 07
| Epoch (UTC): | 17 May 2026 14:16:36 |
| Eccentricity: | 0.0001983 |
| inclination: | 97.9334° |
| perigee height: | 627 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 196.7413° |
| argument of perigee: | 98.0545° |
| revolutions per day: | 14.80426804 |
| mean anomaly at epoch: | 262.0892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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