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 51143U 26145.52465161 +.00000000 +00000-0 +66621-5 0 00001
2 51143 53.2132 324.1949 0001150 86.6888 273.4236 15.08834362 02
| Epoch (UTC): | 25 May 2026 12:35:29 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 324.1949° |
| argument of perigee: | 86.6888° |
| revolutions per day: | 15.08834362 |
| mean anomaly at epoch: | 273.4236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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