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 26066.09178101 +.00000000 +00000-0 +30186-3 0 00006
2 48274 41.4664 223.9664 0006989 257.1897 102.8161 15.60509219 02
| Epoch (UTC): | 07 March 2026 02:12:09 |
| Eccentricity: | 0.0006989 |
| inclination: | 41.4664° |
| perigee height: | 381 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 223.9664° |
| argument of perigee: | 257.1897° |
| revolutions per day: | 15.60509219 |
| mean anomaly at epoch: | 102.8161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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