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 24337.43636309 .00000045 00000-0 24768-3 0 9999
2 32953 82.5032 344.8372 0020677 97.8403 262.5025 12.43154433750035
| Epoch (UTC): | 02 December 2024 10:28:21 |
| Eccentricity: | 0.0020677 |
| inclination: | 82.5032° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 344.8372° |
| argument of perigee: | 97.8403° |
| revolutions per day: | 12.43154433 |
| mean anomaly at epoch: | 262.5025° |
| orbit number at epoch: | 75003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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