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 27422U 26038.84957866 +.00000000 +00000-0 +17457-3 0 00009
2 27422 98.5841 337.8184 0010693 276.8822 83.1145 14.31004501 03
| Epoch (UTC): | 07 February 2026 20:23:23 |
| Eccentricity: | 0.0010693 |
| inclination: | 98.5841° |
| perigee height: | 781 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 337.8184° |
| argument of perigee: | 276.8822° |
| revolutions per day: | 14.31004501 |
| mean anomaly at epoch: | 83.1145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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