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 4382U 70034A 22229.21470001 .00001511 00000-0 23581-3 0 9993
2 4382 68.4264 24.8151 1046409 156.3717 208.9254 13.08660779462115
Epoch (UTC): | 17 August 2022 05:09:10 |
Eccentricity: | 0.1046409 |
inclination: | 68.4264° |
perigee height: | 432 km |
apogee height: | 2024 km |
right ascension of ascending node: | 24.8151° |
argument of perigee: | 156.3717° |
revolutions per day: | 13.08660779 |
mean anomaly at epoch: | 208.9254° |
orbit number at epoch: | 46211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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