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 24311.77395666 .00007970 00000-0 99637-3 0 9999
2 00107 28.7842 92.6554 0513887 59.6695 305.3690 14.17211551192921
Epoch (UTC): | 06 November 2024 18:34:29 |
Eccentricity: | 0.0513887 |
inclination: | 28.7842° |
perigee height: | 464 km |
apogee height: | 1205 km |
right ascension of ascending node: | 92.6554° |
argument of perigee: | 59.6695° |
revolutions per day: | 14.17211551 |
mean anomaly at epoch: | 305.3690° |
orbit number at epoch: | 19292 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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