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 59023U 26145.16475911 +.00000000 +00000-0 +61993-4 0 00006
2 59023 43.0003 315.1641 0001303 271.0062 89.0640 15.27578091 09
| Epoch (UTC): | 25 May 2026 03:57:15 |
| Eccentricity: | 0.0001303 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 315.1641° |
| argument of perigee: | 271.0062° |
| revolutions per day: | 15.27578091 |
| mean anomaly at epoch: | 89.0640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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