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 00107U 61013A 24310.50600951 .00007555 00000-0 94408-3 0 9995
2 00107 28.7842 99.9100 0513881 47.9241 316.3893 14.17191683192749
Epoch (UTC): | 05 November 2024 12:08:39 |
Eccentricity: | 0.0513881 |
inclination: | 28.7842° |
perigee height: | 464 km |
apogee height: | 1205 km |
right ascension of ascending node: | 99.9100° |
argument of perigee: | 47.9241° |
revolutions per day: | 14.17191683 |
mean anomaly at epoch: | 316.3893° |
orbit number at epoch: | 19274 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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