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 26137.73897221 +.00000000 +00000-0 +43421-4 0 00008
2 22889 82.9471 54.1494 0051091 98.3822 262.3132 13.78275686 09
| Epoch (UTC): | 17 May 2026 17:44:07 |
| Eccentricity: | 0.0051091 |
| inclination: | 82.9471° |
| perigee height: | 932 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 54.1494° |
| argument of perigee: | 98.3822° |
| revolutions per day: | 13.78275686 |
| mean anomaly at epoch: | 262.3132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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