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 18959U 88020B 21061.30073324 .00000065 00000-0 50095-5 0 9997
2 18959 82.5348 85.4057 0016662 356.5169 3.5927 14.83468074781321
Epoch (UTC): | 02 March 2021 07:13:03 |
Eccentricity: | 0.0016662 |
inclination: | 82.5348° |
perigee height: | 607 km |
apogee height: | 630 km |
right ascension of ascending node: | 85.4057° |
argument of perigee: | 356.5169° |
revolutions per day: | 14.83468074 |
mean anomaly at epoch: | 3.5927° |
orbit number at epoch: | 78132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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