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 48643U 26145.61895802 +.00000000 +00000-0 +61795-4 0 00007
2 48643 53.1586 116.0704 0001769 86.3443 273.7761 15.31710814 09
| Epoch (UTC): | 25 May 2026 14:51:17 |
| Eccentricity: | 0.0001769 |
| inclination: | 53.1586° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 116.0704° |
| argument of perigee: | 86.3443° |
| revolutions per day: | 15.31710814 |
| mean anomaly at epoch: | 273.7761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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