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Location: Cran-Gévrier
(45.9039°N, 6.1012°E)
Time: 13:36:50
(UTC+00:00)
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Dodecapole I - Orbit

View from above orbital plane
View from above orbital plane
View from above satellite
View from above satellite

Ground track
Ground track

The orbit data is extracted from the following two-line orbital elements,

1 01272U 65016H   24169.93189423  .00000030  00000-0  61272-4 0  9996
2 01272  70.0804 358.7332 0022458 352.6971   7.3804 13.94383034 14711
Epoch (UTC): 17 June 2024 22:21:55
Eccentricity: 0.0022458
inclination: 70.0804°
perigee height: 897 km
apogee height: 929 km
right ascension of ascending node: 358.7332°
argument of perigee: 352.6971°
revolutions per day: 13.94383034
mean anomaly at epoch: 7.3804°
orbit number at epoch: 1471

The dashed part of the orbit path shows where the satellite is in the earth's shadow,  

DLR