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 47911U 26145.40849058 +.00000000 +00000-0 +79092-4 0 00002
2 47911 53.1600 284.1645 0001342 91.1301 268.9854 15.31708419 05
| Epoch (UTC): | 25 May 2026 09:48:13 |
| Eccentricity: | 0.0001342 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 284.1645° |
| argument of perigee: | 91.1301° |
| revolutions per day: | 15.31708419 |
| mean anomaly at epoch: | 268.9854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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