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 24827U 97028A 25197.94087017 .00000003 00000-0 53847-3 0 9992
2 24827 63.2976 48.2889 1084476 65.3309 23.8287 11.07923742137415
Epoch (UTC): | 16 July 2025 22:34:51 |
Eccentricity: | 0.1084476 |
inclination: | 63.2976° |
perigee height: | 1199 km |
apogee height: | 3043 km |
right ascension of ascending node: | 48.2889° |
argument of perigee: | 65.3309° |
revolutions per day: | 11.07923742 |
mean anomaly at epoch: | 23.8287° |
orbit number at epoch: | 13741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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