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 26157.12980580 +.00000000 +00000-0 +55538-4 0 00001
2 15945 82.5263 301.7658 0017250 258.4771 101.4509 14.86506965 01
| Epoch (UTC): | 06 June 2026 03:06:55 |
| Eccentricity: | 0.0017250 |
| inclination: | 82.5263° |
| perigee height: | 597 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 301.7658° |
| argument of perigee: | 258.4771° |
| revolutions per day: | 14.86506965 |
| mean anomaly at epoch: | 101.4509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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