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 26039.37190992 +.00000000 +00000-0 +60727-4 0 00008
2 22889 82.9472 127.4122 0049884 16.3782 343.8973 13.78272030 02
| Epoch (UTC): | 08 February 2026 08:55:33 |
| Eccentricity: | 0.0049884 |
| inclination: | 82.9472° |
| perigee height: | 933 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 127.4122° |
| argument of perigee: | 16.3782° |
| revolutions per day: | 13.78272030 |
| mean anomaly at epoch: | 343.8973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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