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 59682U 26145.60769154 +.00000000 +00000-0 -24703-5 0 00001
2 59682 43.0053 349.1109 0000800 271.5623 88.5137 15.27577966 05
| Epoch (UTC): | 25 May 2026 14:35:04 |
| Eccentricity: | 0.0000800 |
| inclination: | 43.0053° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.1109° |
| argument of perigee: | 271.5623° |
| revolutions per day: | 15.27577966 |
| mean anomaly at epoch: | 88.5137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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