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 41465U 16026B 23080.30396515 .00025657 00000-0 41064-3 0 9993
2 41465 97.0126 313.3664 0007182 185.4958 286.0866 15.53082089386308
| Epoch (UTC): | 21 March 2023 07:17:42 |
| Eccentricity: | 0.0007182 |
| inclination: | 97.0126° |
| perigee height: | 403 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 313.3664° |
| argument of perigee: | 185.4958° |
| revolutions per day: | 15.53082089 |
| mean anomaly at epoch: | 286.0866° |
| orbit number at epoch: | 38630 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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