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 25132.17308767 .00009494 00000-0 17728-3 0 9996
2 25544 51.6373 125.4662 0002565 109.5780 353.0059 15.49484849509578
| Epoch (UTC): | 12 May 2025 04:09:14 |
| Eccentricity: | 0.0002565 |
| inclination: | 51.6373° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 125.4662° |
| argument of perigee: | 109.5780° |
| revolutions per day: | 15.49484849 |
| mean anomaly at epoch: | 353.0059° |
| orbit number at epoch: | 50957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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