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 25133.18664600 .00008383 00000-0 15740-3 0 9997
2 25544 51.6343 120.4533 0002335 105.7353 254.3893 15.49501655509738
| Epoch (UTC): | 13 May 2025 04:28:46 |
| Eccentricity: | 0.0002335 |
| inclination: | 51.6343° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 120.4533° |
| argument of perigee: | 105.7353° |
| revolutions per day: | 15.49501655 |
| mean anomaly at epoch: | 254.3893° |
| orbit number at epoch: | 50973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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