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 48274U 26039.39486024 +.00000000 +00000-0 +26814-3 0 00008
2 48274 41.4686 26.2335 0005047 28.7158 331.3958 15.59352670 09
| Epoch (UTC): | 08 February 2026 09:28:35 |
| Eccentricity: | 0.0005047 |
| inclination: | 41.4686° |
| perigee height: | 386 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 26.2335° |
| argument of perigee: | 28.7158° |
| revolutions per day: | 15.59352670 |
| mean anomaly at epoch: | 331.3958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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