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 23339.42066700 .00007014 00000-0 62595-3 0 9999
2 40025 98.0185 289.6624 0013113 86.3741 273.8978 14.96220162513724
| Epoch (UTC): | 05 December 2023 10:05:45 |
| Eccentricity: | 0.0013113 |
| inclination: | 98.0185° |
| perigee height: | 569 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 289.6624° |
| argument of perigee: | 86.3741° |
| revolutions per day: | 14.96220162 |
| mean anomaly at epoch: | 273.8978° |
| orbit number at epoch: | 51372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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