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 40021U 14033M 22179.80141837 .00002149 00000-0 21262-3 0 9993
2 40021 98.0128 130.2084 0012794 11.2267 348.9234 14.92933059436390
Epoch (UTC): | 28 June 2022 19:14:02 |
Eccentricity: | 0.0012794 |
inclination: | 98.0128° |
perigee height: | 580 km |
apogee height: | 598 km |
right ascension of ascending node: | 130.2084° |
argument of perigee: | 11.2267° |
revolutions per day: | 14.92933059 |
mean anomaly at epoch: | 348.9234° |
orbit number at epoch: | 43639 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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