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 41874U 16062F 23083.30294079 .00647798 00000-0 40145-2 0 9996
2 41874 51.6334 63.3580 0010534 101.1120 259.1064 15.74585813353131
Epoch (UTC): | 24 March 2023 07:16:14 |
Eccentricity: | 0.0010534 |
inclination: | 51.6334° |
perigee height: | 339 km |
apogee height: | 353 km |
right ascension of ascending node: | 63.3580° |
argument of perigee: | 101.1120° |
revolutions per day: | 15.74585813 |
mean anomaly at epoch: | 259.1064° |
orbit number at epoch: | 35313 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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