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 32956U 08025D 23083.75685427 .00000013 00000-0 19790-4 0 9994
2 32956 82.5124 11.5043 0021557 13.7646 346.4018 12.43030016673147
Epoch (UTC): | 24 March 2023 18:09:52 |
Eccentricity: | 0.0021557 |
inclination: | 82.5124° |
perigee height: | 1477 km |
apogee height: | 1511 km |
right ascension of ascending node: | 11.5043° |
argument of perigee: | 13.7646° |
revolutions per day: | 12.43030016 |
mean anomaly at epoch: | 346.4018° |
orbit number at epoch: | 67314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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