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 54762U 26145.49936694 +.00000000 +00000-0 +52123-3 0 00001
2 54762 53.2140 59.3801 0001237 102.8577 257.2553 15.08802021 06
| Epoch (UTC): | 25 May 2026 11:59:05 |
| Eccentricity: | 0.0001237 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.3801° |
| argument of perigee: | 102.8577° |
| revolutions per day: | 15.08802021 |
| mean anomaly at epoch: | 257.2553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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