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 31663U 99025CBV 24357.47183381 .00005429 00000-0 61677-3 0 9990
2 31663 98.8743 225.9446 0197337 272.4306 85.4321 14.73697625940428
| Epoch (UTC): | 22 December 2024 11:19:26 |
| Eccentricity: | 0.0197337 |
| inclination: | 98.8743° |
| perigee height: | 510 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 225.9446° |
| argument of perigee: | 272.4306° |
| revolutions per day: | 14.73697625 |
| mean anomaly at epoch: | 85.4321° |
| orbit number at epoch: | 94042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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