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 48582U 26145.66668980 +.00000000 +00000-0 +27818-2 0 00005
2 48582 53.0518 106.9923 0001595 105.1215 344.4961 15.27243695 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001595 |
| inclination: | 53.0518° |
| perigee height: | 483 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 106.9923° |
| argument of perigee: | 105.1215° |
| revolutions per day: | 15.27243695 |
| mean anomaly at epoch: | 344.4961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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