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 59U 60013B 25343.76537678 .00000138 00000-0 63670-4 0 9998
2 59 28.2502 16.8426 0188904 165.4488 195.1589 13.53154622217491
| Epoch (UTC): | 09 December 2025 18:22:08 |
| Eccentricity: | 0.0188904 |
| inclination: | 28.2502° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 16.8426° |
| argument of perigee: | 165.4488° |
| revolutions per day: | 13.53154622 |
| mean anomaly at epoch: | 195.1589° |
| orbit number at epoch: | 21749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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