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 37386U 11014A 22229.10525436 0.00000000 00000-0 00000-0 0 00
2 37386 63.4333 252.5387 0235152 357.7901 2.2099 13.40839280 03
Epoch (UTC): | 17 August 2022 02:31:33 |
Eccentricity: | 0.0235152 |
inclination: | 63.4333° |
perigee height: | 930 km |
apogee height: | 1282 km |
right ascension of ascending node: | 252.5387° |
argument of perigee: | 357.7901° |
revolutions per day: | 13.40839280 |
mean anomaly at epoch: | 2.2099° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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