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 31442U 99025BUE 23340.46920327 .00001167 00000-0 44624-3 0 9992
2 31442 98.5617 66.0371 0083262 30.7702 329.8324 14.30611482868974
| Epoch (UTC): | 06 December 2023 11:15:39 |
| Eccentricity: | 0.0083262 |
| inclination: | 98.5617° |
| perigee height: | 730 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 66.0371° |
| argument of perigee: | 30.7702° |
| revolutions per day: | 14.30611482 |
| mean anomaly at epoch: | 329.8324° |
| orbit number at epoch: | 86897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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