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 23705U 95058B 23149.75467543 .00000280 00000-0 16805-3 0 9997
2 23705 71.0199 150.6290 0014172 231.8948 128.0897 14.15231534424249
| Epoch (UTC): | 29 May 2023 18:06:43 |
| Eccentricity: | 0.0014172 |
| inclination: | 71.0199° |
| perigee height: | 831 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 150.6290° |
| argument of perigee: | 231.8948° |
| revolutions per day: | 14.15231534 |
| mean anomaly at epoch: | 128.0897° |
| orbit number at epoch: | 42424 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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