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 21422U 26040.80010720 +.00000000 +00000-0 +18248-3 0 00000
2 21422 82.4964 110.5799 0013348 148.2755 211.9276 14.99998073 06
| Epoch (UTC): | 09 February 2026 19:12:09 |
| Eccentricity: | 0.0013348 |
| inclination: | 82.4964° |
| perigee height: | 558 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 110.5799° |
| argument of perigee: | 148.2755° |
| revolutions per day: | 14.99998073 |
| mean anomaly at epoch: | 211.9276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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