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 40374U 15002A 23081.75894969 -.00000142 00000-0 00000+0 0 9994
2 40374 2.7128 22.8737 0052006 179.8526 235.0395 1.00271393 29969
| Epoch (UTC): | 22 March 2023 18:12:53 |
| Eccentricity: | 0.0052006 |
| inclination: | 2.7128° |
| perigee height: | 35567 km |
| apogee height: | 36005 km |
| right ascension of ascending node: | 22.8737° |
| argument of perigee: | 179.8526° |
| revolutions per day: | 1.00271393 |
| mean anomaly at epoch: | 235.0395° |
| orbit number at epoch: | 2996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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