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 00059U 60013B 25347.30630855 .00000135 00000-0 58399-4 0 9992
2 00059 28.2506 358.6495 0188887 195.1795 164.3022 13.53154942217977
| Epoch (UTC): | 13 December 2025 07:21:05 |
| Eccentricity: | 0.0188887 |
| inclination: | 28.2506° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 358.6495° |
| argument of perigee: | 195.1795° |
| revolutions per day: | 13.53154942 |
| mean anomaly at epoch: | 164.3022° |
| orbit number at epoch: | 21797 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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