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 39554U 93036BUL 24356.19359622 .00023906 00000-0 28618-2 0 9991
2 39554 74.0248 265.3598 0012366 150.5201 0.1690 14.83991661590539
Epoch (UTC): | 21 December 2024 04:38:46 |
Eccentricity: | 0.0012366 |
inclination: | 74.0248° |
perigee height: | 608 km |
apogee height: | 625 km |
right ascension of ascending node: | 265.3598° |
argument of perigee: | 150.5201° |
revolutions per day: | 14.83991661 |
mean anomaly at epoch: | 0.1690° |
orbit number at epoch: | 59053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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