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 00016U 58002A 24309.39526406 .00000687 00000-0 94879-3 0 9996
2 00016 34.2603 210.7225 2023361 149.8864 223.5337 10.49473708626948
Epoch (UTC): | 04 November 2024 09:29:10 |
Eccentricity: | 0.2023361 |
inclination: | 34.2603° |
perigee height: | 651 km |
apogee height: | 4217 km |
right ascension of ascending node: | 210.7225° |
argument of perigee: | 149.8864° |
revolutions per day: | 10.49473708 |
mean anomaly at epoch: | 223.5337° |
orbit number at epoch: | 62694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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