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 52454U 26145.54674429 +.00000000 +00000-0 +61454-3 0 00005
2 52454 53.2128 84.0958 0001371 102.5036 257.6110 15.08784886 03
| Epoch (UTC): | 25 May 2026 13:07:18 |
| Eccentricity: | 0.0001371 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.0958° |
| argument of perigee: | 102.5036° |
| revolutions per day: | 15.08784886 |
| mean anomaly at epoch: | 257.6110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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