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 25544U 98067A 25133.84454933 .00008976 00000-0 16787-3 0 9996
2 25544 51.6365 117.1903 0002541 106.6326 325.8583 15.49515413509833
| Epoch (UTC): | 13 May 2025 20:16:09 |
| Eccentricity: | 0.0002541 |
| inclination: | 51.6365° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 117.1903° |
| argument of perigee: | 106.6326° |
| revolutions per day: | 15.49515413 |
| mean anomaly at epoch: | 325.8583° |
| orbit number at epoch: | 50983 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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