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 47259U 26145.34752736 +.00000000 +00000-0 +10587-2 0 00008
2 47259 87.8961 355.2004 0001620 88.2984 271.8330 13.12441721 05
| Epoch (UTC): | 25 May 2026 08:20:26 |
| Eccentricity: | 0.0001620 |
| inclination: | 87.8961° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2004° |
| argument of perigee: | 88.2984° |
| revolutions per day: | 13.12441721 |
| mean anomaly at epoch: | 271.8330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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