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 26069.56340331 +.00000000 +00000-0 +97162-4 0 00009
2 10521 74.0256 121.8831 0018982 76.4473 283.8797 14.42394552 01
| Epoch (UTC): | 10 March 2026 13:31:18 |
| Eccentricity: | 0.0018982 |
| inclination: | 74.0256° |
| perigee height: | 737 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 121.8831° |
| argument of perigee: | 76.4473° |
| revolutions per day: | 14.42394552 |
| mean anomaly at epoch: | 283.8797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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