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 23561U 26041.65477968 +.00000000 +00000-0 +11616-3 0 00003
2 23561 98.4555 113.4961 0006186 214.8448 262.9768 14.39752325 03
| Epoch (UTC): | 10 February 2026 15:42:52 |
| Eccentricity: | 0.0006186 |
| inclination: | 98.4555° |
| perigee height: | 755 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 113.4961° |
| argument of perigee: | 214.8448° |
| revolutions per day: | 14.39752325 |
| mean anomaly at epoch: | 262.9768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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