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 47285U 26145.29683956 +.00000000 +00000-0 -10338-2 0 00003
2 47285 87.8957 355.2036 0001725 86.6083 273.5243 13.12443391 09
| Epoch (UTC): | 25 May 2026 07:07:26 |
| Eccentricity: | 0.0001725 |
| inclination: | 87.8957° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2036° |
| argument of perigee: | 86.6083° |
| revolutions per day: | 13.12443391 |
| mean anomaly at epoch: | 273.5243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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