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 26064.93979304 +.00000000 +00000-0 +22289-3 0 00006
2 48274 41.4658 230.9734 0006880 250.1024 109.9073 15.60447182 06
| Epoch (UTC): | 05 March 2026 22:33:18 |
| Eccentricity: | 0.0006880 |
| inclination: | 41.4658° |
| perigee height: | 382 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 230.9734° |
| argument of perigee: | 250.1024° |
| revolutions per day: | 15.60447182 |
| mean anomaly at epoch: | 109.9073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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