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 48123U 26145.45174339 +.00000000 +00000-0 +35448-4 0 00003
2 48123 53.1580 155.5937 0001242 88.2571 271.8573 15.31706498 04
| Epoch (UTC): | 25 May 2026 10:50:30 |
| Eccentricity: | 0.0001242 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.5937° |
| argument of perigee: | 88.2571° |
| revolutions per day: | 15.31706498 |
| mean anomaly at epoch: | 271.8573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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