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 22136.60581282 .00000005 00000-0 -25696-4 0 9995
2 44909 82.5219 251.4289 0217855 34.4720 327.0292 12.79713092111430
Epoch (UTC): | 16 May 2022 14:32:22 |
Eccentricity: | 0.0217855 |
inclination: | 82.5219° |
perigee height: | 1174 km |
apogee height: | 1511 km |
right ascension of ascending node: | 251.4289° |
argument of perigee: | 34.4720° |
revolutions per day: | 12.79713092 |
mean anomaly at epoch: | 327.0292° |
orbit number at epoch: | 11143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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