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 23152.05329052 .00005156 00000-0 32163-3 0 9991
2 33410 97.9170 171.1618 0122037 99.2412 262.2639 15.03916187796725
Epoch (UTC): | 01 June 2023 01:16:44 |
Eccentricity: | 0.0122037 |
inclination: | 97.9170° |
perigee height: | 470 km |
apogee height: | 639 km |
right ascension of ascending node: | 171.1618° |
argument of perigee: | 99.2412° |
revolutions per day: | 15.03916187 |
mean anomaly at epoch: | 262.2639° |
orbit number at epoch: | 79672 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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