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 23490U 26065.31191404 +.00000000 +00000-0 -18576-3 0 00004
2 23490 64.8296 28.5062 0128333 20.6854 50.8982 11.20508134 00
| Epoch (UTC): | 06 March 2026 07:29:09 |
| Eccentricity: | 0.0128333 |
| inclination: | 64.8296° |
| perigee height: | 1949 km |
| apogee height: | 2166 km |
| right ascension of ascending node: | 28.5062° |
| argument of perigee: | 20.6854° |
| revolutions per day: | 11.20508134 |
| mean anomaly at epoch: | 50.8982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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