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 is defined by the following mean orbital elements,
1 48569U 26145.36568756 +.00000000 +00000-0 +99978-4 0 00005
2 48569 53.1579 130.0924 0001228 81.5428 278.5713 15.31701481 08
| Epoch (UTC): | 25 May 2026 08:46:35 |
| Eccentricity: | 0.0001228 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 130.0924° |
| argument of perigee: | 81.5428° |
| revolutions per day: | 15.31701481 |
| mean anomaly at epoch: | 278.5713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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