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 14450U 83108A 23083.05254506 .00000096 00000-0 82329-4 0 9990
2 14450 82.9275 70.2115 0044266 64.1642 0.9932 13.76337943795448
Epoch (UTC): | 24 March 2023 01:15:39 |
Eccentricity: | 0.0044266 |
inclination: | 82.9275° |
perigee height: | 944 km |
apogee height: | 1009 km |
right ascension of ascending node: | 70.2115° |
argument of perigee: | 64.1642° |
revolutions per day: | 13.76337943 |
mean anomaly at epoch: | 0.9932° |
orbit number at epoch: | 79544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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