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 10121U 77059B 24277.72412522 .00001739 00000-0 59621-3 0 9996
2 10121 74.0443 281.0599 0019378 331.2271 28.7812 14.36825365472217
Epoch (UTC): | 03 October 2024 17:22:44 |
Eccentricity: | 0.0019378 |
inclination: | 74.0443° |
perigee height: | 755 km |
apogee height: | 783 km |
right ascension of ascending node: | 281.0599° |
argument of perigee: | 331.2271° |
revolutions per day: | 14.36825365 |
mean anomaly at epoch: | 28.7812° |
orbit number at epoch: | 47221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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