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 24282.56635170 .00021969 00000-0 16696-2 0 9990
2 20682 63.2984 66.5020 0906155 71.0207 298.6725 13.55158200 19935
| Epoch (UTC): | 08 October 2024 13:35:32 |
| Eccentricity: | 0.0906155 |
| inclination: | 63.2984° |
| perigee height: | 380 km |
| apogee height: | 1727 km |
| right ascension of ascending node: | 66.5020° |
| argument of perigee: | 71.0207° |
| revolutions per day: | 13.55158200 |
| mean anomaly at epoch: | 298.6725° |
| orbit number at epoch: | 1993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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