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 54383U 26145.54598381 +.00000000 +00000-0 +50367-4 0 00002
2 54383 67.1405 157.2363 0001917 121.3332 238.7941 13.97707852 01
| Epoch (UTC): | 25 May 2026 13:06:13 |
| Eccentricity: | 0.0001917 |
| inclination: | 67.1405° |
| perigee height: | 900 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 157.2363° |
| argument of perigee: | 121.3332° |
| revolutions per day: | 13.97707852 |
| mean anomaly at epoch: | 238.7941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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