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 61361U 24140WA 24357.93229032 .00004099 00000-0 95514-3 0 9998
2 61361 89.0502 335.6148 0110416 326.4442 32.9803 14.50972828 16010
Epoch (UTC): | 22 December 2024 22:22:29 |
Eccentricity: | 0.0110416 |
inclination: | 89.0502° |
perigee height: | 644 km |
apogee height: | 801 km |
right ascension of ascending node: | 335.6148° |
argument of perigee: | 326.4442° |
revolutions per day: | 14.50972828 |
mean anomaly at epoch: | 32.9803° |
orbit number at epoch: | 1601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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