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 23318U 26042.16734573 +.00000000 +00000-0 +52589-4 0 00003
2 23318 82.5408 114.9688 0021797 322.8619 37.1085 14.80872863 01
| Epoch (UTC): | 11 February 2026 04:00:58 |
| Eccentricity: | 0.0021797 |
| inclination: | 82.5408° |
| perigee height: | 611 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 114.9688° |
| argument of perigee: | 322.8619° |
| revolutions per day: | 14.80872863 |
| mean anomaly at epoch: | 37.1085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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