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 data is extracted from the following two-line orbital elements,
1 21891U 92009B 25117.71044265 .00005462 00000-0 48201-3 0 9991
2 21891 19.9941 133.2851 0039576 334.2999 25.5457 14.91548075772624
| Epoch (UTC): | 27 April 2025 17:03:02 |
| Eccentricity: | 0.0039576 |
| inclination: | 19.9941° |
| perigee height: | 565 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 133.2851° |
| argument of perigee: | 334.2999° |
| revolutions per day: | 14.91548075 |
| mean anomaly at epoch: | 25.5457° |
| orbit number at epoch: | 77262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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