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 52289U 26145.61757753 +.00000000 +00000-0 +44725-3 0 00003
2 52289 53.2116 113.7718 0001156 61.0756 299.0351 15.08808345 03
| Epoch (UTC): | 25 May 2026 14:49:18 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 113.7718° |
| argument of perigee: | 61.0756° |
| revolutions per day: | 15.08808345 |
| mean anomaly at epoch: | 299.0351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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