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 21397U 91039A 23160.92348967 .00002451 00000-0 21857-3 0 9992
2 21397 82.5213 221.9523 0018626 124.3531 235.9456 14.95455166714564
Epoch (UTC): | 09 June 2023 22:09:49 |
Eccentricity: | 0.0018626 |
inclination: | 82.5213° |
perigee height: | 568 km |
apogee height: | 594 km |
right ascension of ascending node: | 221.9523° |
argument of perigee: | 124.3531° |
revolutions per day: | 14.95455166 |
mean anomaly at epoch: | 235.9456° |
orbit number at epoch: | 71456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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