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 52283U 26145.23761722 +.00000000 +00000-0 +57881-3 0 00003
2 52283 53.2139 125.4813 0001586 71.3061 288.8103 15.08794388 00
| Epoch (UTC): | 25 May 2026 05:42:10 |
| Eccentricity: | 0.0001586 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.4813° |
| argument of perigee: | 71.3061° |
| revolutions per day: | 15.08794388 |
| mean anomaly at epoch: | 288.8103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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