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 40967U 15058D 24315.63677840 .00013261 00000-0 11489-2 0 9999
2 40967 64.7765 285.7057 0186973 260.1135 97.8823 14.84824017 26711
Epoch (UTC): | 10 November 2024 15:16:57 |
Eccentricity: | 0.0186973 |
inclination: | 64.7765° |
perigee height: | 483 km |
apogee height: | 745 km |
right ascension of ascending node: | 285.7057° |
argument of perigee: | 260.1135° |
revolutions per day: | 14.84824017 |
mean anomaly at epoch: | 97.8823° |
orbit number at epoch: | 2671 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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