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 48656U 26145.63759947 +.00000000 +00000-0 +36751-4 0 00006
2 48656 53.1609 115.9455 0001373 99.8232 260.2925 15.31701711 05
| Epoch (UTC): | 25 May 2026 15:18:08 |
| Eccentricity: | 0.0001373 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 115.9455° |
| argument of perigee: | 99.8232° |
| revolutions per day: | 15.31701711 |
| mean anomaly at epoch: | 260.2925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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