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 39440U 26101.33338259 +.00000000 +00000-0 +32241-3 0 00004
2 39440 97.8850 50.0766 0056434 248.4783 111.0415 14.93318254 04
| Epoch (UTC): | 11 April 2026 08:00:04 |
| Eccentricity: | 0.0056434 |
| inclination: | 97.8850° |
| perigee height: | 548 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 50.0766° |
| argument of perigee: | 248.4783° |
| revolutions per day: | 14.93318254 |
| mean anomaly at epoch: | 111.0415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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