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 54147U 26145.41008395 +.00000000 +00000-0 +22565-3 0 00005
2 54147 87.9159 309.4976 0002087 99.9422 260.1946 13.19726240 05
| Epoch (UTC): | 25 May 2026 09:50:31 |
| Eccentricity: | 0.0002087 |
| inclination: | 87.9159° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4976° |
| argument of perigee: | 99.9422° |
| revolutions per day: | 13.19726240 |
| mean anomaly at epoch: | 260.1946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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