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 23340.49068103 .00006781 00000-0 60509-3 0 9990
2 40025 98.0185 290.7588 0013109 83.1203 277.1508 14.96235759513880
| Epoch (UTC): | 06 December 2023 11:46:34 |
| Eccentricity: | 0.0013109 |
| inclination: | 98.0185° |
| perigee height: | 569 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 290.7588° |
| argument of perigee: | 83.1203° |
| revolutions per day: | 14.96235759 |
| mean anomaly at epoch: | 277.1508° |
| orbit number at epoch: | 51388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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