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 25510U 98061C 21019.81899902 .00000303 00000-0 40034-4 0 9997
2 25510 31.4340 169.5296 0327063 205.0143 307.1402 14.37552984166822
| Epoch (UTC): | 19 January 2021 19:39:21 |
| Eccentricity: | 0.0327063 |
| inclination: | 31.4340° |
| perigee height: | 533 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 169.5296° |
| argument of perigee: | 205.0143° |
| revolutions per day: | 14.37552984 |
| mean anomaly at epoch: | 307.1402° |
| orbit number at epoch: | 16682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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