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 47641U 26145.36646944 +.00000000 +00000-0 +75293-3 0 00004
2 47641 53.0402 285.5578 0003543 280.9967 79.0653 15.74517027 03
| Epoch (UTC): | 25 May 2026 08:47:42 |
| Eccentricity: | 0.0003543 |
| inclination: | 53.0402° |
| perigee height: | 344 km |
| apogee height: | 348 km |
| right ascension of ascending node: | 285.5578° |
| argument of perigee: | 280.9967° |
| revolutions per day: | 15.74517027 |
| mean anomaly at epoch: | 79.0653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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