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 24311.39312965 .00000613 00000-0 84296-3 0 9993
2 00016 34.2603 204.9436 2023333 158.3278 211.6896 10.49476080627158
Epoch (UTC): | 06 November 2024 09:26:06 |
Eccentricity: | 0.2023333 |
inclination: | 34.2603° |
perigee height: | 651 km |
apogee height: | 4217 km |
right ascension of ascending node: | 204.9436° |
argument of perigee: | 158.3278° |
revolutions per day: | 10.49476080 |
mean anomaly at epoch: | 211.6896° |
orbit number at epoch: | 62715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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