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 54225U 26144.80164373 +.00000000 +00000-0 +00000-0 0 00000
2 54225 0.0407 234.4848 0001975 307.8333 1.6674 1.00272308 00
| Epoch (UTC): | 24 May 2026 19:14:22 |
| Eccentricity: | 0.0001975 |
| inclination: | 0.0407° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 234.4848° |
| argument of perigee: | 307.8333° |
| revolutions per day: | 1.00272308 |
| mean anomaly at epoch: | 1.6674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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