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 12849U 81094B 22145.25465226 .00001196 00000-0 11168-3 0 9999
2 12849 82.4945 222.0517 0897046 243.4715 107.1797 13.51335049985319
Epoch (UTC): | 25 May 2022 06:06:41 |
Eccentricity: | 0.0897046 |
inclination: | 82.4945° |
perigee height: | 399 km |
apogee height: | 1735 km |
right ascension of ascending node: | 222.0517° |
argument of perigee: | 243.4715° |
revolutions per day: | 13.51335049 |
mean anomaly at epoch: | 107.1797° |
orbit number at epoch: | 98531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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