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 54259U 26145.58572177 +.00000000 +00000-0 +00000-0 0 00008
2 54259 0.0619 102.1677 0001309 8.1648 353.6669 1.00267318 03
| Epoch (UTC): | 25 May 2026 14:03:26 |
| Eccentricity: | 0.0001309 |
| inclination: | 0.0619° |
| perigee height: | 35782 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 102.1677° |
| argument of perigee: | 8.1648° |
| revolutions per day: | 1.00267318 |
| mean anomaly at epoch: | 353.6669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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