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 20682U 90050B 24284.55870293 .00011601 00000-0 88851-3 0 9993
2 20682 63.2980 61.1922 0906089 71.0549 298.6400 13.55199989 20209
| Epoch (UTC): | 10 October 2024 13:24:31 |
| Eccentricity: | 0.0906089 |
| inclination: | 63.2980° |
| perigee height: | 380 km |
| apogee height: | 1726 km |
| right ascension of ascending node: | 61.1922° |
| argument of perigee: | 71.0549° |
| revolutions per day: | 13.55199989 |
| mean anomaly at epoch: | 298.6400° |
| orbit number at epoch: | 2020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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