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 23343U 26067.02906405 +.00000000 +00000-0 +10109-3 0 00009
2 23343 97.7111 97.9140 0005659 216.7769 173.4297 14.79406173 01
| Epoch (UTC): | 08 March 2026 00:41:51 |
| Eccentricity: | 0.0005659 |
| inclination: | 97.7111° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 97.9140° |
| argument of perigee: | 216.7769° |
| revolutions per day: | 14.79406173 |
| mean anomaly at epoch: | 173.4297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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