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 47457U 21006AW 22183.72988553 .00006785 00000-0 33808-3 0 9990
2 47457 97.4437 243.2045 0009425 215.1251 144.9363 15.17844475 79619
Epoch (UTC): | 02 July 2022 17:31:02 |
Eccentricity: | 0.0009425 |
inclination: | 97.4437° |
perigee height: | 506 km |
apogee height: | 519 km |
right ascension of ascending node: | 243.2045° |
argument of perigee: | 215.1251° |
revolutions per day: | 15.17844475 |
mean anomaly at epoch: | 144.9363° |
orbit number at epoch: | 7961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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