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 26042.15752801 +.00000000 +00000-0 +20179-3 0 00006
2 22626 82.5190 292.0941 0017487 38.8168 321.4306 14.96438446 01
| Epoch (UTC): | 11 February 2026 03:46:50 |
| Eccentricity: | 0.0017487 |
| inclination: | 82.5190° |
| perigee height: | 566 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 292.0941° |
| argument of perigee: | 38.8168° |
| revolutions per day: | 14.96438446 |
| mean anomaly at epoch: | 321.4306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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