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 47291U 26145.31363762 +.00000000 +00000-0 -69693-3 0 00002
2 47291 87.8952 355.2196 0001719 88.2516 271.8810 13.12443194 02
| Epoch (UTC): | 25 May 2026 07:31:38 |
| Eccentricity: | 0.0001719 |
| inclination: | 87.8952° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2196° |
| argument of perigee: | 88.2516° |
| revolutions per day: | 13.12443194 |
| mean anomaly at epoch: | 271.8810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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