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 54867U 26145.42739947 +.00000000 +00000-0 -63107-4 0 00008
2 54867 43.0013 48.4575 0000777 257.3329 102.7436 15.27560024 03
| Epoch (UTC): | 25 May 2026 10:15:27 |
| Eccentricity: | 0.0000777 |
| inclination: | 43.0013° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.4575° |
| argument of perigee: | 257.3329° |
| revolutions per day: | 15.27560024 |
| mean anomaly at epoch: | 102.7436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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