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 54131U 26145.42662933 +.00000000 +00000-0 +12930-3 0 00008
2 54131 87.9157 309.4573 0002105 66.7693 293.3661 13.20267222 06
| Epoch (UTC): | 25 May 2026 10:14:20 |
| Eccentricity: | 0.0002105 |
| inclination: | 87.9157° |
| perigee height: | 1182 km |
| apogee height: | 1185 km |
| right ascension of ascending node: | 309.4573° |
| argument of perigee: | 66.7693° |
| revolutions per day: | 13.20267222 |
| mean anomaly at epoch: | 293.3661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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