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 52092U 26145.25786273 +.00000000 +00000-0 -15867-3 0 00000
2 52092 53.2128 105.3898 0001236 70.1817 289.9309 15.08835122 06
| Epoch (UTC): | 25 May 2026 06:11:19 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.3898° |
| argument of perigee: | 70.1817° |
| revolutions per day: | 15.08835122 |
| mean anomaly at epoch: | 289.9309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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