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 52578U 26145.43954671 +.00000000 +00000-0 -11692-3 0 00000
2 52578 53.2107 149.5768 0001147 63.6245 296.4864 15.08846825 02
| Epoch (UTC): | 25 May 2026 10:32:56 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.2107° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 149.5768° |
| argument of perigee: | 63.6245° |
| revolutions per day: | 15.08846825 |
| mean anomaly at epoch: | 296.4864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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