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 20862U 90081AA 24357.61757618 .00000189 00000-0 24723-3 0 9997
2 20862 98.9735 223.7605 0234965 168.3025 210.0607 13.61527898699471
| Epoch (UTC): | 22 December 2024 14:49:18 |
| Eccentricity: | 0.0234965 |
| inclination: | 98.9735° |
| perigee height: | 856 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 223.7605° |
| argument of perigee: | 168.3025° |
| revolutions per day: | 13.61527898 |
| mean anomaly at epoch: | 210.0607° |
| orbit number at epoch: | 69947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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