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 23150.46148530 .00000288 00000-0 17235-3 0 9995
2 23705 71.0200 149.1458 0014149 231.0005 128.9859 14.15231979424342
| Epoch (UTC): | 30 May 2023 11:04:32 |
| Eccentricity: | 0.0014149 |
| inclination: | 71.0200° |
| perigee height: | 831 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 149.1458° |
| argument of perigee: | 231.0005° |
| revolutions per day: | 14.15231979 |
| mean anomaly at epoch: | 128.9859° |
| orbit number at epoch: | 42434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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