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 53732U 26145.33747758 +.00000000 +00000-0 +26991-4 0 00006
2 53732 53.2147 270.1161 0001204 84.1896 275.9233 15.08836349 03
| Epoch (UTC): | 25 May 2026 08:05:58 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 270.1161° |
| argument of perigee: | 84.1896° |
| revolutions per day: | 15.08836349 |
| mean anomaly at epoch: | 275.9233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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