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 14699U 84013A 22138.20292769 .00002735 00000-0 18300-3 0 9990
2 14699 82.5284 29.4205 0013459 52.3170 307.9276 15.06497780 83329
Epoch (UTC): | 18 May 2022 04:52:12 |
Eccentricity: | 0.0013459 |
inclination: | 82.5284° |
perigee height: | 537 km |
apogee height: | 556 km |
right ascension of ascending node: | 29.4205° |
argument of perigee: | 52.3170° |
revolutions per day: | 15.06497780 |
mean anomaly at epoch: | 307.9276° |
orbit number at epoch: | 8332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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