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 24357.87820652 .00000057 00000-0 34092-3 0 9999
2 32953 82.5037 332.1188 0020545 55.0119 305.2886 12.43155596752436
| Epoch (UTC): | 22 December 2024 21:04:37 |
| Eccentricity: | 0.0020545 |
| inclination: | 82.5037° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 332.1188° |
| argument of perigee: | 55.0119° |
| revolutions per day: | 12.43155596 |
| mean anomaly at epoch: | 305.2886° |
| orbit number at epoch: | 75243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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