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 26039.41596981 +.00000000 +00000-0 +18509-3 0 00000
2 22626 82.5190 294.7156 0017671 47.3808 312.8900 14.96427122 02
| Epoch (UTC): | 08 February 2026 09:58:59 |
| Eccentricity: | 0.0017671 |
| inclination: | 82.5190° |
| perigee height: | 566 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 294.7156° |
| argument of perigee: | 47.3808° |
| revolutions per day: | 14.96427122 |
| mean anomaly at epoch: | 312.8900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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