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 33277U 08038D 24357.88902094 .00003254 00000-0 39325-2 0 9990
2 33277 2.4888 306.9574 5595441 117.8137 309.1967 4.51276311219444
Epoch (UTC): | 22 December 2024 21:20:11 |
Eccentricity: | 0.5595441 |
inclination: | 2.4888° |
perigee height: | 435 km |
apogee height: | 17745 km |
right ascension of ascending node: | 306.9574° |
argument of perigee: | 117.8137° |
revolutions per day: | 4.51276311 |
mean anomaly at epoch: | 309.1967° |
orbit number at epoch: | 21944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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