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 26040.26643833 +.00000000 +00000-0 +20200-3 0 00008
2 21422 82.4963 111.0945 0013303 149.9043 210.2948 14.99996315 08
| Epoch (UTC): | 09 February 2026 06:23:40 |
| Eccentricity: | 0.0013303 |
| inclination: | 82.4963° |
| perigee height: | 558 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 111.0945° |
| argument of perigee: | 149.9043° |
| revolutions per day: | 14.99996315 |
| mean anomaly at epoch: | 210.2948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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