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 48125U 26145.32432605 +.00000000 +00000-0 +43928-4 0 00006
2 48125 53.1605 169.1582 0001070 84.2294 275.8830 15.31703396 02
| Epoch (UTC): | 25 May 2026 07:47:01 |
| Eccentricity: | 0.0001070 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 169.1582° |
| argument of perigee: | 84.2294° |
| revolutions per day: | 15.31703396 |
| mean anomaly at epoch: | 275.8830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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