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 44354U 19036R 22137.11830330 .00078865 -49329-5 76455-3 0 9990
2 44354 28.5278 34.9281 0245984 338.5469 20.4971 15.35214441159841
Epoch (UTC): | 17 May 2022 02:50:21 |
Eccentricity: | 0.0245984 |
inclination: | 28.5278° |
perigee height: | 292 km |
apogee height: | 628 km |
right ascension of ascending node: | 34.9281° |
argument of perigee: | 338.5469° |
revolutions per day: | 15.35214441 |
mean anomaly at epoch: | 20.4971° |
orbit number at epoch: | 15984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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