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 47283U 26145.27806251 +.00000000 +00000-0 +68375-3 0 00008
2 47283 87.8962 355.2144 0001876 88.6373 271.4971 13.12441904 07
| Epoch (UTC): | 25 May 2026 06:40:24 |
| Eccentricity: | 0.0001876 |
| inclination: | 87.8962° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2144° |
| argument of perigee: | 88.6373° |
| revolutions per day: | 13.12441904 |
| mean anomaly at epoch: | 271.4971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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