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 52492U 26145.19528262 +.00000000 +00000-0 -79115-4 0 00006
2 52492 53.2143 65.6702 0001891 81.3152 278.8054 15.08851919 08
| Epoch (UTC): | 25 May 2026 04:41:12 |
| Eccentricity: | 0.0001891 |
| inclination: | 53.2143° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 65.6702° |
| argument of perigee: | 81.3152° |
| revolutions per day: | 15.08851919 |
| mean anomaly at epoch: | 278.8054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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