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 48274U 26110.92198984 +.00000000 +00000-0 +33518-3 0 00001
2 48274 41.4677 310.7964 0006515 246.3399 113.6757 15.62720710 00
| Epoch (UTC): | 20 April 2026 22:07:39 |
| Eccentricity: | 0.0006515 |
| inclination: | 41.4677° |
| perigee height: | 375 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 310.7964° |
| argument of perigee: | 246.3399° |
| revolutions per day: | 15.62720710 |
| mean anomaly at epoch: | 113.6757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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