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 40912U 15049P 22179.55241145 .00008515 00000-0 33039-3 0 9993
2 40912 97.4359 190.9011 0010645 261.9411 217.4750 15.26306057375440
Epoch (UTC): | 28 June 2022 13:15:28 |
Eccentricity: | 0.0010645 |
inclination: | 97.4359° |
perigee height: | 479 km |
apogee height: | 494 km |
right ascension of ascending node: | 190.9011° |
argument of perigee: | 261.9411° |
revolutions per day: | 15.26306057 |
mean anomaly at epoch: | 217.4750° |
orbit number at epoch: | 37544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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