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 10521U 26064.63903850 +.00000000 +00000-0 +12224-3 0 00008
2 10521 74.0263 131.0225 0018971 87.4569 272.8759 14.42391139 09
| Epoch (UTC): | 05 March 2026 15:20:12 |
| Eccentricity: | 0.0018971 |
| inclination: | 74.0263° |
| perigee height: | 737 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 131.0225° |
| argument of perigee: | 87.4569° |
| revolutions per day: | 14.42391139 |
| mean anomaly at epoch: | 272.8759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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