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 48278U 26145.37784275 +.00000000 +00000-0 +86046-4 0 00001
2 48278 53.1634 27.7073 0001280 90.0334 270.0815 15.31696220 07
| Epoch (UTC): | 25 May 2026 09:04:05 |
| Eccentricity: | 0.0001280 |
| inclination: | 53.1634° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 27.7073° |
| argument of perigee: | 90.0334° |
| revolutions per day: | 15.31696220 |
| mean anomaly at epoch: | 270.0815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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