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 24281.26829032 .00001805 00000-0 57923-3 0 9996
2 08344 74.0547 245.8220 0022156 201.6332 158.3889 14.40048262569399
| Epoch (UTC): | 07 October 2024 06:26:20 |
| Eccentricity: | 0.0022156 |
| inclination: | 74.0547° |
| perigee height: | 742 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 245.8220° |
| argument of perigee: | 201.6332° |
| revolutions per day: | 14.40048262 |
| mean anomaly at epoch: | 158.3889° |
| orbit number at epoch: | 56939 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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