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 18961U 88021B 21020.11318265 -.00000245 00000-0 -13195-3 0 9991
2 18961 99.2203 68.8424 0053617 225.4389 187.9689 14.00774045679214
Epoch (UTC): | 20 January 2021 02:42:58 |
Eccentricity: | 0.0053617 |
inclination: | 99.2203° |
perigee height: | 852 km |
apogee height: | 930 km |
right ascension of ascending node: | 68.8424° |
argument of perigee: | 225.4389° |
revolutions per day: | 14.00774045 |
mean anomaly at epoch: | 187.9689° |
orbit number at epoch: | 67921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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