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 48305U 26145.27978582 +.00000000 +00000-0 +23917-4 0 00005
2 48305 53.1614 103.2646 0001317 89.1917 270.9236 15.31703679 02
| Epoch (UTC): | 25 May 2026 06:42:53 |
| Eccentricity: | 0.0001317 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 103.2646° |
| argument of perigee: | 89.1917° |
| revolutions per day: | 15.31703679 |
| mean anomaly at epoch: | 270.9236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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