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 47831U 26145.25917076 +.00000000 +00000-0 +45603-4 0 00003
2 47831 53.1588 246.5662 0001279 88.8424 271.2724 15.31699135 07
| Epoch (UTC): | 25 May 2026 06:13:12 |
| Eccentricity: | 0.0001279 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 246.5662° |
| argument of perigee: | 88.8424° |
| revolutions per day: | 15.31699135 |
| mean anomaly at epoch: | 271.2724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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