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 41465U 16026B 22137.48244507 .00015089 00000-0 37102-3 0 9993
2 41465 97.0598 14.8735 0008366 235.0301 246.3927 15.40685587338764
Epoch (UTC): | 17 May 2022 11:34:43 |
Eccentricity: | 0.0008366 |
inclination: | 97.0598° |
perigee height: | 438 km |
apogee height: | 450 km |
right ascension of ascending node: | 14.8735° |
argument of perigee: | 235.0301° |
revolutions per day: | 15.40685587 |
mean anomaly at epoch: | 246.3927° |
orbit number at epoch: | 33876 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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