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 53265U 26145.36410852 +.00000000 +00000-0 +69258-4 0 00005
2 53265 53.2129 209.9170 0001078 84.0184 276.0931 15.08837771 09
| Epoch (UTC): | 25 May 2026 08:44:18 |
| Eccentricity: | 0.0001078 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 209.9170° |
| argument of perigee: | 84.0184° |
| revolutions per day: | 15.08837771 |
| mean anomaly at epoch: | 276.0931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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