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 40967U 15058D 25343.72037323 .00007097 00000-0 63785-3 0 9994
2 40967 64.7748 147.2121 0135277 131.1675 230.1201 14.89614349 85338
| Epoch (UTC): | 09 December 2025 17:17:20 |
| Eccentricity: | 0.0135277 |
| inclination: | 64.7748° |
| perigee height: | 505 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 147.2121° |
| argument of perigee: | 131.1675° |
| revolutions per day: | 14.89614349 |
| mean anomaly at epoch: | 230.1201° |
| orbit number at epoch: | 8533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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