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 25134.15405506 .00008594 00000-0 16106-3 0 9994
2 25544 51.6345 115.6637 0002291 108.2504 251.8734 15.49518201509885
| Epoch (UTC): | 14 May 2025 03:41:50 |
| Eccentricity: | 0.0002291 |
| inclination: | 51.6345° |
| perigee height: | 416 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 115.6637° |
| argument of perigee: | 108.2504° |
| revolutions per day: | 15.49518201 |
| mean anomaly at epoch: | 251.8734° |
| orbit number at epoch: | 50988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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