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 54863U 26145.01707775 +.00000000 +00000-0 -33143-5 0 00001
2 54863 43.0027 50.5411 0001351 231.6251 128.4479 15.27577495 07
| Epoch (UTC): | 25 May 2026 00:24:35 |
| Eccentricity: | 0.0001351 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 50.5411° |
| argument of perigee: | 231.6251° |
| revolutions per day: | 15.27577495 |
| mean anomaly at epoch: | 128.4479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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