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 53636U 26145.63366060 +.00000000 +00000-0 +15830-2 0 00003
2 53636 53.2137 238.5321 0001483 82.0056 278.1104 15.08904548 04
| Epoch (UTC): | 25 May 2026 15:12:28 |
| Eccentricity: | 0.0001483 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 238.5321° |
| argument of perigee: | 82.0056° |
| revolutions per day: | 15.08904548 |
| mean anomaly at epoch: | 278.1104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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