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 47228U 26145.60168080 +.00000000 +00000-0 -23975-3 0 00003
2 47228 82.4958 315.2001 0013884 242.2173 117.7499 12.42885294 01
| Epoch (UTC): | 25 May 2026 14:26:25 |
| Eccentricity: | 0.0013884 |
| inclination: | 82.4958° |
| perigee height: | 1483 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 315.2001° |
| argument of perigee: | 242.2173° |
| revolutions per day: | 12.42885294 |
| mean anomaly at epoch: | 117.7499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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