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 8459U 75112B 25199.14380568 .00000133 00000-0 52396-4 0 9999
2 8459 74.0609 90.3197 0016655 241.4536 118.4941 14.38035875598364
| Epoch (UTC): | 18 July 2025 03:27:04 |
| Eccentricity: | 0.0016655 |
| inclination: | 74.0609° |
| perigee height: | 753 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 90.3197° |
| argument of perigee: | 241.4536° |
| revolutions per day: | 14.38035875 |
| mean anomaly at epoch: | 118.4941° |
| orbit number at epoch: | 59836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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