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 47832U 26145.58616760 +.00000000 +00000-0 +11708-3 0 00004
2 47832 53.1598 248.0596 0001182 80.9130 279.2006 15.31698854 00
| Epoch (UTC): | 25 May 2026 14:04:04 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 248.0596° |
| argument of perigee: | 80.9130° |
| revolutions per day: | 15.31698854 |
| mean anomaly at epoch: | 279.2006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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