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 30750U 99025ATL 24251.69793260 .00013203 00000-0 59097-2 0 9997
2 30750 98.9499 311.4170 0042816 351.1911 131.6772 14.22179900902119
Epoch (UTC): | 07 September 2024 16:45:01 |
Eccentricity: | 0.0042816 |
inclination: | 98.9499° |
perigee height: | 787 km |
apogee height: | 849 km |
right ascension of ascending node: | 311.4170° |
argument of perigee: | 351.1911° |
revolutions per day: | 14.22179900 |
mean anomaly at epoch: | 131.6772° |
orbit number at epoch: | 90211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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