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 26106.42583080 +.00000000 +00000-0 +13513-3 0 00004
2 39440 97.8866 55.1835 0056662 231.2901 128.3245 14.93340613 05
| Epoch (UTC): | 16 April 2026 10:13:11 |
| Eccentricity: | 0.0056662 |
| inclination: | 97.8866° |
| perigee height: | 548 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 55.1835° |
| argument of perigee: | 231.2901° |
| revolutions per day: | 14.93340613 |
| mean anomaly at epoch: | 128.3245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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