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 42761U 17034D 23339.14766728 .00011449 00000-0 50751-3 0 9996
2 42761 43.0136 241.2099 0010952 145.0369 215.1201 15.21563496357640
Epoch (UTC): | 05 December 2023 03:32:38 |
Eccentricity: | 0.0010952 |
inclination: | 43.0136° |
perigee height: | 493 km |
apogee height: | 508 km |
right ascension of ascending node: | 241.2099° |
argument of perigee: | 145.0369° |
revolutions per day: | 15.21563496 |
mean anomaly at epoch: | 215.1201° |
orbit number at epoch: | 35764 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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