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 00016U 58002A 21059.64169005 .00000170 00000-0 20932-3 0 9997
2 00016 34.2726 135.0477 2023735 237.8861 100.9388 10.48696041485732
Epoch (UTC): | 28 February 2021 15:24:02 |
Eccentricity: | 0.2023735 |
inclination: | 34.2726° |
perigee height: | 654 km |
apogee height: | 4223 km |
right ascension of ascending node: | 135.0477° |
argument of perigee: | 237.8861° |
revolutions per day: | 10.48696041 |
mean anomaly at epoch: | 100.9388° |
orbit number at epoch: | 48573 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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