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 47271U 26145.30347530 +.00000000 +00000-0 -12601-2 0 00000
2 47271 87.8961 355.2049 0002103 85.8133 274.3235 13.12442841 00
| Epoch (UTC): | 25 May 2026 07:17:00 |
| Eccentricity: | 0.0002103 |
| inclination: | 87.8961° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2049° |
| argument of perigee: | 85.8133° |
| revolutions per day: | 13.12442841 |
| mean anomaly at epoch: | 274.3235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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