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 20465U 90010A 21019.86415055 .00000276 00000-0 21000-4 0 9996
2 20465 82.4880 65.0960 0015270 185.6366 174.4687 14.98124196660728
Epoch (UTC): | 19 January 2021 20:44:22 |
Eccentricity: | 0.0015270 |
inclination: | 82.4880° |
perigee height: | 562 km |
apogee height: | 583 km |
right ascension of ascending node: | 65.0960° |
argument of perigee: | 185.6366° |
revolutions per day: | 14.98124196 |
mean anomaly at epoch: | 174.4687° |
orbit number at epoch: | 66072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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