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 23271.90301338 .00010569 00000-0 85921-3 0 9999
2 40021 98.0662 239.3742 0010072 282.9851 77.0246 14.99736255504720
Epoch (UTC): | 28 September 2023 21:40:20 |
Eccentricity: | 0.0010072 |
inclination: | 98.0662° |
perigee height: | 561 km |
apogee height: | 575 km |
right ascension of ascending node: | 239.3742° |
argument of perigee: | 282.9851° |
revolutions per day: | 14.99736255 |
mean anomaly at epoch: | 77.0246° |
orbit number at epoch: | 50472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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