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 47231U 26145.64612250 +.00000000 +00000-0 +35298-3 0 00004
2 47231 97.4728 215.8982 0004693 215.0564 145.0366 15.25483773 06
| Epoch (UTC): | 25 May 2026 15:30:24 |
| Eccentricity: | 0.0004693 |
| inclination: | 97.4728° |
| perigee height: | 486 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 215.8982° |
| argument of perigee: | 215.0564° |
| revolutions per day: | 15.25483773 |
| mean anomaly at epoch: | 145.0366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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