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 32089U 99025CQF 23033.29514497 .00001071 00000-0 59319-3 0 9998
2 32089 98.7069 61.8063 0118236 216.7935 142.5078 14.09880325484778
| Epoch (UTC): | 02 February 2023 07:05:00 |
| Eccentricity: | 0.0118236 |
| inclination: | 98.7069° |
| perigee height: | 774 km |
| apogee height: | 945 km |
| right ascension of ascending node: | 61.8063° |
| argument of perigee: | 216.7935° |
| revolutions per day: | 14.09880325 |
| mean anomaly at epoch: | 142.5078° |
| orbit number at epoch: | 48477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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