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 48319U 26145.30830362 +.00000000 +00000-0 +32780-4 0 00005
2 48319 53.1596 104.7836 0001431 99.3590 260.7573 15.31702635 02
| Epoch (UTC): | 25 May 2026 07:23:57 |
| Eccentricity: | 0.0001431 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.7836° |
| argument of perigee: | 99.3590° |
| revolutions per day: | 15.31702635 |
| mean anomaly at epoch: | 260.7573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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