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 54093U 26145.56831935 +.00000000 +00000-0 -23789-4 0 00006
2 54093 53.2150 348.7486 0001324 87.6372 272.4772 15.08836978 08
| Epoch (UTC): | 25 May 2026 13:38:22 |
| Eccentricity: | 0.0001324 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.7486° |
| argument of perigee: | 87.6372° |
| revolutions per day: | 15.08836978 |
| mean anomaly at epoch: | 272.4772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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