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 41275U 00055GB 24262.37005130 .00010486 00000-0 49488-2 0 9998
2 41275 98.7083 312.4711 0022618 206.7682 153.2329 14.19815822450561
Epoch (UTC): | 18 September 2024 08:52:52 |
Eccentricity: | 0.0022618 |
inclination: | 98.7083° |
perigee height: | 809 km |
apogee height: | 842 km |
right ascension of ascending node: | 312.4711° |
argument of perigee: | 206.7682° |
revolutions per day: | 14.19815822 |
mean anomaly at epoch: | 153.2329° |
orbit number at epoch: | 45056 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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