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 24263.79709092 .00000029 00000-0 13765-3 0 9993
2 32953 82.5062 30.6253 0018698 257.1714 102.7277 12.43148324740880
| Epoch (UTC): | 19 September 2024 19:07:48 |
| Eccentricity: | 0.0018698 |
| inclination: | 82.5062° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 30.6253° |
| argument of perigee: | 257.1714° |
| revolutions per day: | 12.43148324 |
| mean anomaly at epoch: | 102.7277° |
| orbit number at epoch: | 74088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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