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 48466U 26145.41432860 +.00000000 +00000-0 +44186-4 0 00004
2 48466 53.1592 194.2584 0001130 83.6746 276.4385 15.31704714 05
| Epoch (UTC): | 25 May 2026 09:56:37 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.2584° |
| argument of perigee: | 83.6746° |
| revolutions per day: | 15.31704714 |
| mean anomaly at epoch: | 276.4385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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