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 48406U 26145.56637557 +.00000000 +00000-0 +83428-4 0 00006
2 48406 53.1612 338.2868 0001466 98.5556 261.5611 15.31700814 07
| Epoch (UTC): | 25 May 2026 13:35:34 |
| Eccentricity: | 0.0001466 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 338.2868° |
| argument of perigee: | 98.5556° |
| revolutions per day: | 15.31700814 |
| mean anomaly at epoch: | 261.5611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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