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 25168.40319660 .00000106 00000-0 23555-4 0 9996
2 59 28.2457 197.8986 0189027 133.1882 228.4622 13.53139488194594
| Epoch (UTC): | 17 June 2025 09:40:36 |
| Eccentricity: | 0.0189027 |
| inclination: | 28.2457° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 197.8986° |
| argument of perigee: | 133.1882° |
| revolutions per day: | 13.53139488 |
| mean anomaly at epoch: | 228.4622° |
| orbit number at epoch: | 19459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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