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 24298U 96051B 25197.76216754 -.00000179 00000-0 -70089-4 0 9995
2 24298 70.7672 314.5694 0013791 129.2254 231.0092 14.12407405488335
Epoch (UTC): | 16 July 2025 18:17:31 |
Eccentricity: | 0.0013791 |
inclination: | 70.7672° |
perigee height: | 841 km |
apogee height: | 861 km |
right ascension of ascending node: | 314.5694° |
argument of perigee: | 129.2254° |
revolutions per day: | 14.12407405 |
mean anomaly at epoch: | 231.0092° |
orbit number at epoch: | 48833 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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