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 26040.41958422 +.00000000 +00000-0 +22932-3 0 00006
2 48274 41.4684 20.0103 0004697 39.0740 321.0437 15.59384169 00
| Epoch (UTC): | 09 February 2026 10:04:12 |
| Eccentricity: | 0.0004697 |
| inclination: | 41.4684° |
| perigee height: | 386 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 20.0103° |
| argument of perigee: | 39.0740° |
| revolutions per day: | 15.59384169 |
| mean anomaly at epoch: | 321.0437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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