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 52131U 26145.52334191 +.00000000 +00000-0 +10471-2 0 00006
2 52131 53.2134 78.7219 0003905 82.3359 277.8081 15.17417924 07
| Epoch (UTC): | 25 May 2026 12:33:36 |
| Eccentricity: | 0.0003905 |
| inclination: | 53.2134° |
| perigee height: | 511 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 78.7219° |
| argument of perigee: | 82.3359° |
| revolutions per day: | 15.17417924 |
| mean anomaly at epoch: | 277.8081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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