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 23608U 26040.83822450 +.00000000 +00000-0 +80662-3 0 00001
2 23608 98.2894 241.1100 0007445 128.8018 231.3894 15.44977673 01
| Epoch (UTC): | 09 February 2026 20:07:02 |
| Eccentricity: | 0.0007445 |
| inclination: | 98.2894° |
| perigee height: | 426 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 241.1100° |
| argument of perigee: | 128.8018° |
| revolutions per day: | 15.44977673 |
| mean anomaly at epoch: | 231.3894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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