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 37224U 10062C 24340.53405306 .00006709 00000-0 70719-3 0 9995
2 37224 71.9725 262.2125 0013534 43.3410 316.8820 14.89568884 33322
Epoch (UTC): | 05 December 2024 12:49:02 |
Eccentricity: | 0.0013534 |
inclination: | 71.9725° |
perigee height: | 590 km |
apogee height: | 609 km |
right ascension of ascending node: | 262.2125° |
argument of perigee: | 43.3410° |
revolutions per day: | 14.89568884 |
mean anomaly at epoch: | 316.8820° |
orbit number at epoch: | 3332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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