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 54146U 26145.65751617 +.00000000 +00000-0 +36267-7 0 00000
2 54146 87.9174 278.9272 0002323 120.5815 239.5548 13.20772231 01
| Epoch (UTC): | 25 May 2026 15:46:49 |
| Eccentricity: | 0.0002323 |
| inclination: | 87.9174° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9272° |
| argument of perigee: | 120.5815° |
| revolutions per day: | 13.20772231 |
| mean anomaly at epoch: | 239.5548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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