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 26323U 26088.17627426 +.00000000 +00000-0 +56874-3 0 00001
2 26323 98.4391 154.3815 0065530 300.4834 123.0662 14.58462778 02
| Epoch (UTC): | 29 March 2026 04:13:50 |
| Eccentricity: | 0.0065530 |
| inclination: | 98.4391° |
| perigee height: | 652 km |
| apogee height: | 745 km |
| right ascension of ascending node: | 154.3815° |
| argument of perigee: | 300.4834° |
| revolutions per day: | 14.58462778 |
| mean anomaly at epoch: | 123.0662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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