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 47981U 26145.50499118 +.00000000 +00000-0 -52992-4 0 00009
2 47981 53.1596 335.1771 0001118 89.6763 270.4367 15.31696110 09
| Epoch (UTC): | 25 May 2026 12:07:11 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 335.1771° |
| argument of perigee: | 89.6763° |
| revolutions per day: | 15.31696110 |
| mean anomaly at epoch: | 270.4367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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