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 26133.47815922 +.00000000 +00000-0 +13972-3 0 00006
2 48274 41.4670 173.0841 0004122 296.9881 63.0537 15.62173368 01
| Epoch (UTC): | 13 May 2026 11:28:32 |
| Eccentricity: | 0.0004122 |
| inclination: | 41.4670° |
| perigee height: | 379 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 173.0841° |
| argument of perigee: | 296.9881° |
| revolutions per day: | 15.62173368 |
| mean anomaly at epoch: | 63.0537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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