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 52713U 22054A 25131.94431013 .00004637 00000-0 19149-3 0 9995
2 52713 97.5883 70.3907 0001471 67.8014 292.3379 15.24531221165592
| Epoch (UTC): | 11 May 2025 22:39:48 |
| Eccentricity: | 0.0001471 |
| inclination: | 97.5883° |
| perigee height: | 491 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 70.3907° |
| argument of perigee: | 67.8014° |
| revolutions per day: | 15.24531221 |
| mean anomaly at epoch: | 292.3379° |
| orbit number at epoch: | 16559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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