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 52342U 26145.36550450 +.00000000 +00000-0 +48685-4 0 00000
2 52342 53.2130 215.0267 0001253 83.1018 277.0116 15.08835685 00
| Epoch (UTC): | 25 May 2026 08:46:19 |
| Eccentricity: | 0.0001253 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 215.0267° |
| argument of perigee: | 83.1018° |
| revolutions per day: | 15.08835685 |
| mean anomaly at epoch: | 277.0116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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