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 59305U 26145.45349825 +.00000000 +00000-0 +22247-4 0 00004
2 59305 43.0005 157.2477 0001181 273.5377 86.5339 15.27577260 00
| Epoch (UTC): | 25 May 2026 10:53:02 |
| Eccentricity: | 0.0001181 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 157.2477° |
| argument of perigee: | 273.5377° |
| revolutions per day: | 15.27577260 |
| mean anomaly at epoch: | 86.5339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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