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 13553U 82092B 25189.56226756 .00000340 00000-0 35690-4 0 9996
2 13553 82.5676 9.7034 0021375 34.6959 24.2926 14.86337310313749
| Epoch (UTC): | 08 July 2025 13:29:39 |
| Eccentricity: | 0.0021375 |
| inclination: | 82.5676° |
| perigee height: | 594 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 9.7034° |
| argument of perigee: | 34.6959° |
| revolutions per day: | 14.86337310 |
| mean anomaly at epoch: | 24.2926° |
| orbit number at epoch: | 31374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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