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 31736U 99025CEK 24357.98380094 .00000554 00000-0 31449-3 0 9995
2 31736 98.6774 4.1411 0012095 171.2751 188.8635 14.13858597907089
| Epoch (UTC): | 22 December 2024 23:36:40 |
| Eccentricity: | 0.0012095 |
| inclination: | 98.6774° |
| perigee height: | 837 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 4.1411° |
| argument of perigee: | 171.2751° |
| revolutions per day: | 14.13858597 |
| mean anomaly at epoch: | 188.8635° |
| orbit number at epoch: | 90708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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