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 54066U 26145.31857977 +.00000000 +00000-0 -10825-2 0 00008
2 54066 53.2190 0.0325 0001130 96.0251 264.0870 15.08107743 04
| Epoch (UTC): | 25 May 2026 07:38:45 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.2190° |
| perigee height: | 541 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 0.0325° |
| argument of perigee: | 96.0251° |
| revolutions per day: | 15.08107743 |
| mean anomaly at epoch: | 264.0870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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