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 23344U 26100.03836882 +.00000000 +00000-0 +18333-3 0 00007
2 23344 97.9637 111.0383 0115400 290.9768 133.3907 14.59764127 00
| Epoch (UTC): | 10 April 2026 00:55:15 |
| Eccentricity: | 0.0115400 |
| inclination: | 97.9637° |
| perigee height: | 612 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 111.0383° |
| argument of perigee: | 290.9768° |
| revolutions per day: | 14.59764127 |
| mean anomaly at epoch: | 133.3907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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