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 60123U 26145.45031631 +.00000000 +00000-0 +31559-4 0 00003
2 60123 53.1584 202.5483 0001154 76.0929 284.0217 15.69712700 00
| Epoch (UTC): | 25 May 2026 10:48:27 |
| Eccentricity: | 0.0001154 |
| inclination: | 53.1584° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 202.5483° |
| argument of perigee: | 76.0929° |
| revolutions per day: | 15.69712700 |
| mean anomaly at epoch: | 284.0217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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