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 45515U 81043AA 24353.87078595 .00012010 00000-0 41590-2 0 9997
2 45515 81.2489 206.5407 0007312 33.2180 338.3130 14.35583548573853
Epoch (UTC): | 18 December 2024 20:53:55 |
Eccentricity: | 0.0007312 |
inclination: | 81.2489° |
perigee height: | 768 km |
apogee height: | 778 km |
right ascension of ascending node: | 206.5407° |
argument of perigee: | 33.2180° |
revolutions per day: | 14.35583548 |
mean anomaly at epoch: | 338.3130° |
orbit number at epoch: | 57385 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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