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 33410U 08053C 23159.03922277 .00005897 00000-0 36637-3 0 9996
2 33410 97.9157 178.3144 0122052 76.0797 285.3968 15.03994820797552
Epoch (UTC): | 08 June 2023 00:56:28 |
Eccentricity: | 0.0122052 |
inclination: | 97.9157° |
perigee height: | 470 km |
apogee height: | 639 km |
right ascension of ascending node: | 178.3144° |
argument of perigee: | 76.0797° |
revolutions per day: | 15.03994820 |
mean anomaly at epoch: | 285.3968° |
orbit number at epoch: | 79755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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