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 23075.83768936 0.00003000 00000-0 10826-3 0 06
2 32283 98.1894 122.1519 0001130 201.7760 158.2239 15.28536553 01
| Epoch (UTC): | 16 March 2023 20:06:16 |
| Eccentricity: | 0.0001130 |
| inclination: | 98.1894° |
| perigee height: | 479 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 122.1519° |
| argument of perigee: | 201.7760° |
| revolutions per day: | 15.28536553 |
| mean anomaly at epoch: | 158.2239° |
| 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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