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 40746U 15036A 23080.79316157 .00000000 00000-0 00000-0 0 9998
2 40746 0.0065 175.5022 0000815 230.6906 233.3587 1.00269881 28002
| Epoch (UTC): | 21 March 2023 19:02:09 |
| Eccentricity: | 0.0000815 |
| inclination: | 0.0065° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 175.5022° |
| argument of perigee: | 230.6906° |
| revolutions per day: | 1.00269881 |
| mean anomaly at epoch: | 233.3587° |
| orbit number at epoch: | 2800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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