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 40344U 14081A 22179.92576680 0.00000000 00000-0 00000-0 0 06
2 40344 63.2115 233.1918 6837574 271.4435 17.7233 2.00615000 05
Epoch (UTC): | 28 June 2022 22:13:06 |
Eccentricity: | 0.6837574 |
inclination: | 63.2115° |
perigee height: | 2020 km |
apogee height: | 38335 km |
right ascension of ascending node: | 233.1918° |
argument of perigee: | 271.4435° |
revolutions per day: | 2.00615000 |
mean anomaly at epoch: | 17.7233° |
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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