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 26075.80175059 +.00000000 +00000-0 +49751-3 0 00007
2 39440 97.8820 24.4857 0057727 335.4987 24.3491 14.93047088 00
| Epoch (UTC): | 16 March 2026 19:14:31 |
| Eccentricity: | 0.0057727 |
| inclination: | 97.8820° |
| perigee height: | 548 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 24.4857° |
| argument of perigee: | 335.4987° |
| revolutions per day: | 14.93047088 |
| mean anomaly at epoch: | 24.3491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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