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 52305U 26145.63599100 +.00000000 +00000-0 +46938-3 0 00002
2 52305 53.2130 113.8023 0001245 86.0029 274.1105 15.08805698 06
| Epoch (UTC): | 25 May 2026 15:15:49 |
| Eccentricity: | 0.0001245 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 113.8023° |
| argument of perigee: | 86.0029° |
| revolutions per day: | 15.08805698 |
| mean anomaly at epoch: | 274.1105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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