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 10539U 26099.59772355 +.00000000 +00000-0 +25011-4 0 00003
2 10539 75.8358 209.5177 0302176 347.9572 11.4445 13.89157258 01
| Epoch (UTC): | 09 April 2026 14:20:43 |
| Eccentricity: | 0.0302176 |
| inclination: | 75.8358° |
| perigee height: | 711 km |
| apogee height: | 1152 km |
| right ascension of ascending node: | 209.5177° |
| argument of perigee: | 347.9572° |
| revolutions per day: | 13.89157258 |
| mean anomaly at epoch: | 11.4445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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