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 39058U 13001B 24309.28566030 .00000071 00000-0 43849-3 0 9997
2 39058 82.5022 222.5437 0015580 221.1703 138.8203 12.44002993535930
Epoch (UTC): | 04 November 2024 06:51:21 |
Eccentricity: | 0.0015580 |
inclination: | 82.5022° |
perigee height: | 1477 km |
apogee height: | 1502 km |
right ascension of ascending node: | 222.5437° |
argument of perigee: | 221.1703° |
revolutions per day: | 12.44002993 |
mean anomaly at epoch: | 138.8203° |
orbit number at epoch: | 53593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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