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 47279U 26145.28470267 +.00000000 +00000-0 -17644-3 0 00002
2 47279 87.8964 355.2018 0001739 80.4293 279.7032 13.12441630 08
| Epoch (UTC): | 25 May 2026 06:49:58 |
| Eccentricity: | 0.0001739 |
| inclination: | 87.8964° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2018° |
| argument of perigee: | 80.4293° |
| revolutions per day: | 13.12441630 |
| mean anomaly at epoch: | 279.7032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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