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 40025U 14033R 23334.87296506 .00009719 00000-0 86694-3 0 9992
2 40025 98.0177 285.0059 0012663 99.0812 261.1842 14.96132185513554
| Epoch (UTC): | 30 November 2023 20:57:04 |
| Eccentricity: | 0.0012663 |
| inclination: | 98.0177° |
| perigee height: | 570 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 285.0059° |
| argument of perigee: | 99.0812° |
| revolutions per day: | 14.96132185 |
| mean anomaly at epoch: | 261.1842° |
| orbit number at epoch: | 51355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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