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 25560U 26071.25284912 +.00000000 +00000-0 +25784-3 0 00009
2 25560 69.8952 117.3643 0004263 9.0208 351.1031 15.08912024 04
| Epoch (UTC): | 12 March 2026 06:04:06 |
| Eccentricity: | 0.0004263 |
| inclination: | 69.8952° |
| perigee height: | 537 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 117.3643° |
| argument of perigee: | 9.0208° |
| revolutions per day: | 15.08912024 |
| mean anomaly at epoch: | 351.1031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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