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 26108.57000534 +.00000000 +00000-0 +18147-3 0 00008
2 39440 97.8868 57.3342 0056806 224.0248 135.6441 14.93349273 08
| Epoch (UTC): | 18 April 2026 13:40:48 |
| Eccentricity: | 0.0056806 |
| inclination: | 97.8868° |
| perigee height: | 548 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 57.3342° |
| argument of perigee: | 224.0248° |
| revolutions per day: | 14.93349273 |
| mean anomaly at epoch: | 135.6441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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