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 48386U 26145.55469948 +.00000000 +00000-0 +88059-4 0 00004
2 48386 53.1613 348.0403 0001285 76.0044 284.1100 15.31691795 02
| Epoch (UTC): | 25 May 2026 13:18:46 |
| Eccentricity: | 0.0001285 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 348.0403° |
| argument of perigee: | 76.0044° |
| revolutions per day: | 15.31691795 |
| mean anomaly at epoch: | 284.1100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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