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 22626U 26040.75331775 +.00000000 +00000-0 +18018-3 0 00002
2 22626 82.5190 293.4368 0017567 43.2087 317.0510 14.96432385 02
| Epoch (UTC): | 09 February 2026 18:04:46 |
| Eccentricity: | 0.0017567 |
| inclination: | 82.5190° |
| perigee height: | 566 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 293.4368° |
| argument of perigee: | 43.2087° |
| revolutions per day: | 14.96432385 |
| mean anomaly at epoch: | 317.0510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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