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 00020U 59007A 25341.92000231 .00002134 00000-0 86020-3 0 9994
2 00020 33.3396 235.4903 1639236 108.3176 270.2152 11.61584491462363
| Epoch (UTC): | 07 December 2025 22:04:48 |
| Eccentricity: | 0.1639236 |
| inclination: | 33.3396° |
| perigee height: | 507 km |
| apogee height: | 3207 km |
| right ascension of ascending node: | 235.4903° |
| argument of perigee: | 108.3176° |
| revolutions per day: | 11.61584491 |
| mean anomaly at epoch: | 270.2152° |
| orbit number at epoch: | 46236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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