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 48667U 26145.34735647 +.00000000 +00000-0 +49983-3 0 00007
2 48667 53.1595 117.7848 0001731 14.3767 345.7282 15.29964239 08
| Epoch (UTC): | 25 May 2026 08:20:11 |
| Eccentricity: | 0.0001731 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 117.7848° |
| argument of perigee: | 14.3767° |
| revolutions per day: | 15.29964239 |
| mean anomaly at epoch: | 345.7282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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