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 59303U 26145.39196610 +.00000000 +00000-0 +14270-4 0 00004
2 59303 43.0001 157.6476 0001182 276.0909 83.9808 15.27577058 04
| Epoch (UTC): | 25 May 2026 09:24:25 |
| Eccentricity: | 0.0001182 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 157.6476° |
| argument of perigee: | 276.0909° |
| revolutions per day: | 15.27577058 |
| mean anomaly at epoch: | 83.9808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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