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 32953U 08025A 25143.82333140 .00000011 00000-0 44665-5 0 9998
2 32953 82.5037 237.5959 0020478 84.1553 276.1861 12.43164472771455
| Epoch (UTC): | 23 May 2025 19:45:35 |
| Eccentricity: | 0.0020478 |
| inclination: | 82.5037° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 237.5959° |
| argument of perigee: | 84.1553° |
| revolutions per day: | 12.43164472 |
| mean anomaly at epoch: | 276.1861° |
| orbit number at epoch: | 77145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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