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 26088.07523639 +.00000000 +00000-0 +48133-5 0 00004
2 10539 75.8340 226.9670 0301958 12.9658 347.9022 13.89156260 04
| Epoch (UTC): | 29 March 2026 01:48:20 |
| Eccentricity: | 0.0301958 |
| inclination: | 75.8340° |
| perigee height: | 711 km |
| apogee height: | 1152 km |
| right ascension of ascending node: | 226.9670° |
| argument of perigee: | 12.9658° |
| revolutions per day: | 13.89156260 |
| mean anomaly at epoch: | 347.9022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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