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 48892U 26145.50893698 +.00000000 +00000-0 +20317-3 0 00006
2 48892 96.0086 227.5033 0011060 104.7061 255.5384 14.81799973 01
| Epoch (UTC): | 25 May 2026 12:12:52 |
| Eccentricity: | 0.0011060 |
| inclination: | 96.0086° |
| perigee height: | 616 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 227.5033° |
| argument of perigee: | 104.7061° |
| revolutions per day: | 14.81799973 |
| mean anomaly at epoch: | 255.5384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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