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 23405U 26064.95131016 +.00000000 +00000-0 -84264-4 0 00000
2 23405 70.9852 0.3529 0003315 217.4117 142.6775 14.15561521 04
| Epoch (UTC): | 05 March 2026 22:49:53 |
| Eccentricity: | 0.0003315 |
| inclination: | 70.9852° |
| perigee height: | 838 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 0.3529° |
| argument of perigee: | 217.4117° |
| revolutions per day: | 14.15561521 |
| mean anomaly at epoch: | 142.6775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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