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 54083U 26145.53155917 +.00000000 +00000-0 +36384-4 0 00005
2 54083 53.2112 349.2297 0002049 91.9847 268.1379 15.08837450 02
| Epoch (UTC): | 25 May 2026 12:45:26 |
| Eccentricity: | 0.0002049 |
| inclination: | 53.2112° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 349.2297° |
| argument of perigee: | 91.9847° |
| revolutions per day: | 15.08837450 |
| mean anomaly at epoch: | 268.1379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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