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 53226U 26145.40949280 +.00000000 +00000-0 -93980-4 0 00009
2 53226 97.4466 205.3311 0001603 119.2548 240.8839 15.05654207 00
| Epoch (UTC): | 25 May 2026 09:49:40 |
| Eccentricity: | 0.0001603 |
| inclination: | 97.4466° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.3311° |
| argument of perigee: | 119.2548° |
| revolutions per day: | 15.05654207 |
| mean anomaly at epoch: | 240.8839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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