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 56934U 23084C 24358.17182352 .00012213 00000-0 50245-3 0 9993
2 56934 97.5584 116.9355 0008709 95.3928 264.8302 15.24259774 84820
| Epoch (UTC): | 23 December 2024 04:07:25 |
| Eccentricity: | 0.0008709 |
| inclination: | 97.5584° |
| perigee height: | 487 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 116.9355° |
| argument of perigee: | 95.3928° |
| revolutions per day: | 15.24259774 |
| mean anomaly at epoch: | 264.8302° |
| orbit number at epoch: | 8482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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