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 41334U 16010A 22199.02170228 0.00000000 00000-0 00000-0 0 01
2 41334 122.9994 87.7592 0002633 95.0677 264.9322 13.41436467 06
Epoch (UTC): | 18 July 2022 00:31:15 |
Eccentricity: | 0.0002633 |
inclination: | 122.9994° |
perigee height: | 1102 km |
apogee height: | 1106 km |
right ascension of ascending node: | 87.7592° |
argument of perigee: | 95.0677° |
revolutions per day: | 13.41436467 |
mean anomaly at epoch: | 264.9322° |
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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