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 48658U 26145.41264737 +.00000000 +00000-0 +59197-2 0 00009
2 48658 53.1568 117.4654 0001880 328.4031 31.6857 15.30926928 02
| Epoch (UTC): | 25 May 2026 09:54:12 |
| Eccentricity: | 0.0001880 |
| inclination: | 53.1568° |
| perigee height: | 472 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 117.4654° |
| argument of perigee: | 328.4031° |
| revolutions per day: | 15.30926928 |
| mean anomaly at epoch: | 31.6857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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