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 25198.83174649 .00030082 00000-0 39008-3 0 9995
2 12785 82.4862 4.8711 0000654 162.8835 197.2443 15.58698610401020
| Epoch (UTC): | 17 July 2025 19:57:42 |
| Eccentricity: | 0.0000654 |
| inclination: | 82.4862° |
| perigee height: | 391 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 4.8711° |
| argument of perigee: | 162.8835° |
| revolutions per day: | 15.58698610 |
| mean anomaly at epoch: | 197.2443° |
| orbit number at epoch: | 40102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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