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 12785U 81082A 25198.51075274 .00028146 00000-0 36529-3 0 9997
2 12785 82.4864 5.2103 0000698 162.8941 197.2338 15.58678506400976
| Epoch (UTC): | 17 July 2025 12:15:29 |
| Eccentricity: | 0.0000698 |
| inclination: | 82.4864° |
| perigee height: | 391 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 5.2103° |
| argument of perigee: | 162.8941° |
| revolutions per day: | 15.58678506 |
| mean anomaly at epoch: | 197.2338° |
| orbit number at epoch: | 40097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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