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 21063.72897367 .00000084 00000-0 72707-5 0 9991
2 18959 82.5347 83.1351 0016451 348.4040 11.6794 14.83468404760603
Epoch (UTC): | 04 March 2021 17:29:43 |
Eccentricity: | 0.0016451 |
inclination: | 82.5347° |
perigee height: | 607 km |
apogee height: | 630 km |
right ascension of ascending node: | 83.1351° |
argument of perigee: | 348.4040° |
revolutions per day: | 14.83468404 |
mean anomaly at epoch: | 11.6794° |
orbit number at epoch: | 76060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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