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 43145U 18005A 25118.07742531 0.00000000 00000-0 00000-0 0 00
2 43145 106.0151 44.9635 0001704 118.5577 241.4422 13.48014130 04
| Epoch (UTC): | 28 April 2025 01:51:29 |
| Eccentricity: | 0.0001704 |
| inclination: | 106.0151° |
| perigee height: | 1078 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 44.9635° |
| argument of perigee: | 118.5577° |
| revolutions per day: | 13.48014130 |
| mean anomaly at epoch: | 241.4422° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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