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 23156.57755963 .00005341 00000-0 33238-3 0 9996
2 33410 97.9157 175.7938 0122210 84.2293 277.2850 15.03965251797187
Epoch (UTC): | 05 June 2023 13:51:41 |
Eccentricity: | 0.0122210 |
inclination: | 97.9157° |
perigee height: | 470 km |
apogee height: | 639 km |
right ascension of ascending node: | 175.7938° |
argument of perigee: | 84.2293° |
revolutions per day: | 15.03965251 |
mean anomaly at epoch: | 277.2850° |
orbit number at epoch: | 79718 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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