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 40977U 15058P 24262.91021410 .00006202 00000-0 55539-3 0 9990
2 40977 64.7732 91.7106 0184122 277.4375 80.5847 14.84581821 19931
Epoch (UTC): | 18 September 2024 21:50:42 |
Eccentricity: | 0.0184122 |
inclination: | 64.7732° |
perigee height: | 486 km |
apogee height: | 743 km |
right ascension of ascending node: | 91.7106° |
argument of perigee: | 277.4375° |
revolutions per day: | 14.84581821 |
mean anomaly at epoch: | 80.5847° |
orbit number at epoch: | 1993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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