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 26039.75030736 +.00000000 +00000-0 +17070-3 0 00000
2 22626 82.5191 294.3959 0017653 46.3532 313.9151 14.96428066 01
| Epoch (UTC): | 08 February 2026 18:00:26 |
| Eccentricity: | 0.0017653 |
| inclination: | 82.5191° |
| perigee height: | 566 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 294.3959° |
| argument of perigee: | 46.3532° |
| revolutions per day: | 14.96428066 |
| mean anomaly at epoch: | 313.9151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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