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 26038.21038541 +.00000000 +00000-0 +78986-4 0 00007
2 22889 82.9473 128.2768 0049953 19.6148 340.6916 13.78271952 01
| Epoch (UTC): | 07 February 2026 05:02:57 |
| Eccentricity: | 0.0049953 |
| inclination: | 82.9473° |
| perigee height: | 933 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 128.2768° |
| argument of perigee: | 19.6148° |
| revolutions per day: | 13.78271952 |
| mean anomaly at epoch: | 340.6916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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