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 31810U 99025CGY 24355.77709439 .00003820 00000-0 86035-3 0 9991
2 31810 98.2923 14.1032 0223479 144.6286 216.9965 14.42662097592619
| Epoch (UTC): | 20 December 2024 18:39:00 |
| Eccentricity: | 0.0223479 |
| inclination: | 98.2923° |
| perigee height: | 590 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 14.1032° |
| argument of perigee: | 144.6286° |
| revolutions per day: | 14.42662097 |
| mean anomaly at epoch: | 216.9965° |
| orbit number at epoch: | 59261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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