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 62617U 25009J 25322.11815923 .00035503 00000-0 11058-2 0 9995
2 62617 97.4087 41.7999 0004896 356.0135 4.1067 15.33177567 46809
| Epoch (UTC): | 18 November 2025 02:50:08 |
| Eccentricity: | 0.0004896 |
| inclination: | 97.4087° |
| perigee height: | 463 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 41.7999° |
| argument of perigee: | 356.0135° |
| revolutions per day: | 15.33177567 |
| mean anomaly at epoch: | 4.1067° |
| orbit number at epoch: | 4680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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