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 22178.52797321 .00002410 00000-0 23770-3 0 9993
2 40021 98.0125 128.9117 0012921 14.9445 345.2153 14.92927613436207
Epoch (UTC): | 27 June 2022 12:40:16 |
Eccentricity: | 0.0012921 |
inclination: | 98.0125° |
perigee height: | 580 km |
apogee height: | 598 km |
right ascension of ascending node: | 128.9117° |
argument of perigee: | 14.9445° |
revolutions per day: | 14.92927613 |
mean anomaly at epoch: | 345.2153° |
orbit number at epoch: | 43620 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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