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 27424U 02022A 25322.53238390 .00001624 00000-0 33565-3 0 9990
2 27424 98.4001 283.0242 0000655 63.7646 29.4341 14.61727967252497
| Epoch (UTC): | 18 November 2025 12:46:37 |
| Eccentricity: | 0.0000655 |
| inclination: | 98.4001° |
| perigee height: | 687 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 283.0242° |
| argument of perigee: | 63.7646° |
| revolutions per day: | 14.61727967 |
| mean anomaly at epoch: | 29.4341° |
| orbit number at epoch: | 25249 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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