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 44909U 19096E 22178.82340676 .00000034 00000-0 10014-3 0 9993
2 44909 82.5207 223.3863 0216272 295.6372 62.2527 12.79713621116835
Epoch (UTC): | 27 June 2022 19:45:42 |
Eccentricity: | 0.0216272 |
inclination: | 82.5207° |
perigee height: | 1175 km |
apogee height: | 1509 km |
right ascension of ascending node: | 223.3863° |
argument of perigee: | 295.6372° |
revolutions per day: | 12.79713621 |
mean anomaly at epoch: | 62.2527° |
orbit number at epoch: | 11683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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