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 22176.06982122 .00010109 00000-0 39225-3 0 9998
2 40912 97.4360 187.4344 0010589 275.6205 160.6719 15.26252355374918
Epoch (UTC): | 25 June 2022 01:40:32 |
Eccentricity: | 0.0010589 |
inclination: | 97.4360° |
perigee height: | 480 km |
apogee height: | 494 km |
right ascension of ascending node: | 187.4344° |
argument of perigee: | 275.6205° |
revolutions per day: | 15.26252355 |
mean anomaly at epoch: | 160.6719° |
orbit number at epoch: | 37491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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