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 22889U 26044.67136346 +.00000000 +00000-0 +39517-4 0 00003
2 22889 82.9465 123.4672 0049506 1.5879 358.5427 13.78272483 03
| Epoch (UTC): | 13 February 2026 16:06:45 |
| Eccentricity: | 0.0049506 |
| inclination: | 82.9465° |
| perigee height: | 934 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 123.4672° |
| argument of perigee: | 1.5879° |
| revolutions per day: | 13.78272483 |
| mean anomaly at epoch: | 358.5427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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