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 54080U 26145.66668980 +.00000000 +00000-0 +53379-2 0 00006
2 54080 53.2165 340.8420 0002114 92.6819 299.9893 15.79960149 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0002114 |
| inclination: | 53.2165° |
| perigee height: | 329 km |
| apogee height: | 332 km |
| right ascension of ascending node: | 340.8420° |
| argument of perigee: | 92.6819° |
| revolutions per day: | 15.79960149 |
| mean anomaly at epoch: | 299.9893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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