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 25163.57147990 .00008388 00000-0 15402-3 0 9991
2 25544 51.6380 329.9459 0001375 214.4784 224.8613 15.50142004514448
| Epoch (UTC): | 12 June 2025 13:42:55 |
| Eccentricity: | 0.0001375 |
| inclination: | 51.6380° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 329.9459° |
| argument of perigee: | 214.4784° |
| revolutions per day: | 15.50142004 |
| mean anomaly at epoch: | 224.8613° |
| orbit number at epoch: | 51444 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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