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 52090U 26145.25416848 +.00000000 +00000-0 +35469-4 0 00006
2 52090 53.2119 105.4072 0000817 71.8508 288.2573 15.08853636 03
| Epoch (UTC): | 25 May 2026 06:06:00 |
| Eccentricity: | 0.0000817 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 105.4072° |
| argument of perigee: | 71.8508° |
| revolutions per day: | 15.08853636 |
| mean anomaly at epoch: | 288.2573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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