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 15945U 26159.88965817 +.00000000 +00000-0 +47385-4 0 00003
2 15945 82.5265 299.1700 0017341 248.6030 111.3337 14.86509191 04
| Epoch (UTC): | 08 June 2026 21:21:06 |
| Eccentricity: | 0.0017341 |
| inclination: | 82.5265° |
| perigee height: | 597 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 299.1700° |
| argument of perigee: | 248.6030° |
| revolutions per day: | 14.86509191 |
| mean anomaly at epoch: | 111.3337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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