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 47311U 21002C 22179.80837428 .00004160 00000-0 17342-3 0 9993
2 47311 60.6859 319.4958 0018262 345.9533 14.1045 15.25454428 80195
Epoch (UTC): | 28 June 2022 19:24:03 |
Eccentricity: | 0.0018262 |
inclination: | 60.6859° |
perigee height: | 477 km |
apogee height: | 502 km |
right ascension of ascending node: | 319.4958° |
argument of perigee: | 345.9533° |
revolutions per day: | 15.25454428 |
mean anomaly at epoch: | 14.1045° |
orbit number at epoch: | 8019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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