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 40907U 15049J 23079.19879839 .00020551 00000-0 81409-3 0 9992
2 40907 97.4965 86.5031 0014191 107.0541 320.3603 15.25351590414900
| Epoch (UTC): | 20 March 2023 04:46:16 |
| Eccentricity: | 0.0014191 |
| inclination: | 97.4965° |
| perigee height: | 480 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 86.5031° |
| argument of perigee: | 107.0541° |
| revolutions per day: | 15.25351590 |
| mean anomaly at epoch: | 320.3603° |
| orbit number at epoch: | 41490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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