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 26106.12836676 +.00000000 +00000-0 +18121-3 0 00008
2 48274 41.4686 340.0449 0005797 217.8333 142.2100 15.62435361 01
| Epoch (UTC): | 16 April 2026 03:04:50 |
| Eccentricity: | 0.0005797 |
| inclination: | 41.4686° |
| perigee height: | 377 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 340.0449° |
| argument of perigee: | 217.8333° |
| revolutions per day: | 15.62435361 |
| mean anomaly at epoch: | 142.2100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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