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 54182U 26145.59038433 +.00000000 +00000-0 -85455-4 0 00008
2 54182 53.2113 348.5324 0001382 94.8703 265.2447 15.08845319 05
| Epoch (UTC): | 25 May 2026 14:10:09 |
| Eccentricity: | 0.0001382 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.5324° |
| argument of perigee: | 94.8703° |
| revolutions per day: | 15.08845319 |
| mean anomaly at epoch: | 265.2447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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