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 47840U 26145.54733149 +.00000000 +00000-0 +27427-4 0 00006
2 47840 53.1601 241.7406 0001290 85.2522 274.8627 15.31705180 08
| Epoch (UTC): | 25 May 2026 13:08:09 |
| Eccentricity: | 0.0001290 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 241.7406° |
| argument of perigee: | 85.2522° |
| revolutions per day: | 15.31705180 |
| mean anomaly at epoch: | 274.8627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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