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 26019.03903265 +.00000000 +00000-0 +25083-3 0 00005
2 48274 41.4662 149.9978 0010928 313.3598 46.6329 15.60669378 00
| Epoch (UTC): | 19 January 2026 00:56:12 |
| Eccentricity: | 0.0010928 |
| inclination: | 41.4662° |
| perigee height: | 378 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 149.9978° |
| argument of perigee: | 313.3598° |
| revolutions per day: | 15.60669378 |
| mean anomaly at epoch: | 46.6329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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