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 39761U 14028A 25134.15801989 .00000047 00000-0 26659-3 0 9999
2 39761 82.4480 358.6617 0018899 228.7338 131.2114 12.42889535498009
Epoch (UTC): | 14 May 2025 03:47:32 |
Eccentricity: | 0.0018899 |
inclination: | 82.4480° |
perigee height: | 1479 km |
apogee height: | 1509 km |
right ascension of ascending node: | 358.6617° |
argument of perigee: | 228.7338° |
revolutions per day: | 12.42889535 |
mean anomaly at epoch: | 131.2114° |
orbit number at epoch: | 49800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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