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 48686U 26145.51622486 +.00000000 +00000-0 +30097-4 0 00000
2 48686 53.1610 78.0447 0001142 100.3084 259.8046 15.31706546 06
| Epoch (UTC): | 25 May 2026 12:23:21 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 78.0447° |
| argument of perigee: | 100.3084° |
| revolutions per day: | 15.31706546 |
| mean anomaly at epoch: | 259.8046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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