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 39843U 92093KV 23329.21540952 .00087965 00000-0 78539-2 0 9996
2 39843 70.8991 167.7673 0027737 65.5831 294.8222 14.95140245504894
Epoch (UTC): | 25 November 2023 05:10:11 |
Eccentricity: | 0.0027737 |
inclination: | 70.8991° |
perigee height: | 562 km |
apogee height: | 601 km |
right ascension of ascending node: | 167.7673° |
argument of perigee: | 65.5831° |
revolutions per day: | 14.95140245 |
mean anomaly at epoch: | 294.8222° |
orbit number at epoch: | 50489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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