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 08344U 75094B 24284.25550444 .00001762 00000-0 56556-3 0 9999
2 08344 74.0551 240.3083 0022045 195.3600 164.6889 14.40058381569826
| Epoch (UTC): | 10 October 2024 06:07:55 |
| Eccentricity: | 0.0022045 |
| inclination: | 74.0551° |
| perigee height: | 742 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 240.3083° |
| argument of perigee: | 195.3600° |
| revolutions per day: | 14.40058381 |
| mean anomaly at epoch: | 164.6889° |
| orbit number at epoch: | 56982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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