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 48405U 26145.53334479 +.00000000 +00000-0 +67037-4 0 00007
2 48405 53.1590 335.4404 0000832 101.9954 258.1140 15.31701826 06
| Epoch (UTC): | 25 May 2026 12:48:00 |
| Eccentricity: | 0.0000832 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 335.4404° |
| argument of perigee: | 101.9954° |
| revolutions per day: | 15.31701826 |
| mean anomaly at epoch: | 258.1140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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