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 52135U 26145.49896832 +.00000000 +00000-0 +40094-2 0 00005
2 52135 53.2177 71.6239 0001029 184.5035 175.5982 15.87574508 06
| Epoch (UTC): | 25 May 2026 11:58:30 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.2177° |
| perigee height: | 308 km |
| apogee height: | 310 km |
| right ascension of ascending node: | 71.6239° |
| argument of perigee: | 184.5035° |
| revolutions per day: | 15.87574508 |
| mean anomaly at epoch: | 175.5982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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