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 23696U 95057A 23341.53932803 -.00000044 00000-0 00000-0 0 9997
2 23696 10.7704 18.9301 0006331 159.5606 9.9662 0.98764065102666
| Epoch (UTC): | 07 December 2023 12:56:37 |
| Eccentricity: | 0.0006331 |
| inclination: | 10.7704° |
| perigee height: | 36187 km |
| apogee height: | 36241 km |
| right ascension of ascending node: | 18.9301° |
| argument of perigee: | 159.5606° |
| revolutions per day: | 0.98764065 |
| mean anomaly at epoch: | 9.9662° |
| orbit number at epoch: | 10266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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