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 32283U 07053A 23254.86018360 0.00010000 00000-0 36732-3 0 09
2 32283 98.1823 318.6229 0001345 104.2544 255.7455 15.27955044 00
| Epoch (UTC): | 11 September 2023 20:38:39 |
| Eccentricity: | 0.0001345 |
| inclination: | 98.1823° |
| perigee height: | 481 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 318.6229° |
| argument of perigee: | 104.2544° |
| revolutions per day: | 15.27955044 |
| mean anomaly at epoch: | 255.7455° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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