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 23151.45101869 .00000289 00000-0 17281-3 0 9991
2 23705 71.0202 147.0694 0014101 229.7695 130.2195 14.15232625424483
| Epoch (UTC): | 31 May 2023 10:49:28 |
| Eccentricity: | 0.0014101 |
| inclination: | 71.0202° |
| perigee height: | 831 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 147.0694° |
| argument of perigee: | 229.7695° |
| revolutions per day: | 14.15232625 |
| mean anomaly at epoch: | 130.2195° |
| orbit number at epoch: | 42448 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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