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 8344U 75094B 24284.18603453 .00001784 00000-0 57238-3 0 9992
2 8344 74.0551 240.4365 0022044 195.4919 164.5564 14.40058265570106
| Epoch (UTC): | 10 October 2024 04:27:53 |
| Eccentricity: | 0.0022044 |
| inclination: | 74.0551° |
| perigee height: | 742 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 240.4365° |
| argument of perigee: | 195.4919° |
| revolutions per day: | 14.40058265 |
| mean anomaly at epoch: | 164.5564° |
| orbit number at epoch: | 57010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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