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 48666U 26145.33918565 +.00000000 +00000-0 -99042-5 0 00001
2 48666 53.1591 117.9318 0001288 83.6718 276.4429 15.29363341 09
| Epoch (UTC): | 25 May 2026 08:08:25 |
| Eccentricity: | 0.0001288 |
| inclination: | 53.1591° |
| perigee height: | 477 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 117.9318° |
| argument of perigee: | 83.6718° |
| revolutions per day: | 15.29363341 |
| mean anomaly at epoch: | 276.4429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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