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 21015.49005931 .00000283 00000-0 37568-4 0 9993
2 25510 31.4328 194.3730 0326889 166.5978 224.0629 14.37551020166209
| Epoch (UTC): | 15 January 2021 11:45:41 |
| Eccentricity: | 0.0326889 |
| inclination: | 31.4328° |
| perigee height: | 533 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 194.3730° |
| argument of perigee: | 166.5978° |
| revolutions per day: | 14.37551020 |
| mean anomaly at epoch: | 224.0629° |
| orbit number at epoch: | 16620 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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