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 47861U 26145.57986676 +.00000000 +00000-0 +10687-3 0 00006
2 47861 53.1601 260.6979 0001284 82.4810 277.6337 15.31710493 00
| Epoch (UTC): | 25 May 2026 13:55:00 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 260.6979° |
| argument of perigee: | 82.4810° |
| revolutions per day: | 15.31710493 |
| mean anomaly at epoch: | 277.6337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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