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 48320U 26145.27139981 +.00000000 +00000-0 -16728-4 0 00007
2 48320 53.1599 105.2609 0001437 89.2588 270.8578 15.31695500 01
| Epoch (UTC): | 25 May 2026 06:30:48 |
| Eccentricity: | 0.0001437 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 105.2609° |
| argument of perigee: | 89.2588° |
| revolutions per day: | 15.31695500 |
| mean anomaly at epoch: | 270.8578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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