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 25198.51597351 .00000347 00000-0 36501-4 0 9992
2 13553 82.5684 1.3299 0020605 5.7131 53.3010 14.86343258293994
| Epoch (UTC): | 17 July 2025 12:23:00 |
| Eccentricity: | 0.0020605 |
| inclination: | 82.5684° |
| perigee height: | 595 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 1.3299° |
| argument of perigee: | 5.7131° |
| revolutions per day: | 14.86343258 |
| mean anomaly at epoch: | 53.3010° |
| orbit number at epoch: | 29399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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