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 26068.53479242 +.00000000 +00000-0 +87809-4 0 00002
2 23343 97.7110 99.3588 0005760 211.0399 273.5673 14.79407790 08
| Epoch (UTC): | 09 March 2026 12:50:06 |
| Eccentricity: | 0.0005760 |
| inclination: | 97.7110° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 99.3588° |
| argument of perigee: | 211.0399° |
| revolutions per day: | 14.79407790 |
| mean anomaly at epoch: | 273.5673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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