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 48132U 26145.36690443 +.00000000 +00000-0 +28026-4 0 00006
2 48132 53.1585 171.1519 0001185 92.5492 267.5646 15.31708513 08
| Epoch (UTC): | 25 May 2026 08:48:20 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 171.1519° |
| argument of perigee: | 92.5492° |
| revolutions per day: | 15.31708513 |
| mean anomaly at epoch: | 267.5646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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